Rapid electrostatographic belt treatment system and process

Abstract: A process for treating a seamed flexible electrostatographic imaging belt including providing an imaging belt including at least one imaging layer including a thermoplastic polymer matrix and a seam extending from one edge of the belt to the other, the seam having a region on the belt adjacent each side of the seam and also having an exposed surface on each side of the belt, supporting the belt with at least one vacuum holding device spaced from the seam while maintaining the seam and region of the belt adjacent each side of the seam in an arcuate shape having at least a substantially semicircular cross section having a radius of curvature of between about 9.5 millimeters and about 50 millimeters, heating the thermoplastic polymer matrix of the imaging layer in the seam and the region of the belt adjacent each side of the seam to at least the glass transition temperature (Tg) of the thermoplastic polymer matrix without significantly heating the support member, and contacting the exposed surface of the seam and regions on each side of the belt with a gas to rapidly cool the seam and regions on each side of the belt to a temperature below the glass transition temperature of the polymer matrix while maintaining the arcuate shape of the region of the belt adjacent each side of the seam. Apparatus for carrying out this process is also disclosed.

Description: BACKGROUND OF THE INVENTION This invention relates in general to a heat treatment process and more specifically, to a process for effective seam stress release in a flexible electrostatographic imaging member belt for improved mechanical service life, and an apparatus for treating electrostatographic imaging belt. Flexible electrostatographic belt imaging members are well known in the art. Typical electrostatographic flexible belt imaging members include, for example, photoreceptors for electrophotographic imaging systems, electroreceptors such as ionographic imaging members for electrographic imaging systems, and intermediate transfer belts for transferring toner images in electrophotographic and electrographic imaging systems. These belts are usually formed by cutting a rectangular sheet from a web containing at least one layer of thermoplastic polymeric material, overlapping opposite ends of the sheet, and welding the overlapped ends together to form a welded seam. The seam extends from one edge of the belt to the opposite edge. Generally, these belts comprise at least a supporting substrate layer and at least one imaging layer comprising thermoplastic polymeric matrix material. The "imaging layer" as employed herein is defined as the dielectric imaging layer of an electroreceptor belt, the transfer layer of an intimidate transfer belt and the charge transport layer of an electrophotographic belt. Thus, the thermoplastic polymeric matrix material in the imaging layer is located in the upper portion of a cross section of an electrostatographic imaging member belt, the substrate layer being in the lower portion of the cross section of the electrostatographic imaging member belt. Flexible electrophotographic imaging member belts are usually multilayered photoreceptors that comprise a substrate, an electrically conductive layer, an optional hole blocking layer, an adhesive layer, a charge generating layer, and a charge transport layer and, in some embodiments, an anti-curl backing layer. One type of multilayered photoreceptor comprises a layer of finely divided particles of a photoconductive inorganic compound dispersed in an electrically insulating organic resin binder. A typical layered photoreceptor having separate charge generating (photogenerating) and charge transport layers is described in US-A 4,265,990. The charge generating layer is capable of photogenerating holes and injecting the photogenerated holes into the charge transport layer. Although excellent toner images may be obtained with multilayered belt photoreceptors, it has been found that as more advanced, higher speed electrophotographic copiers, duplicators and printers were developed, cracking of the charge transport layer at the welded seam area was frequently encountered during photoreceptor belt cycling. Seam cracking has also been found to rapidly lead to seam delamination due to fatigue thereby shortening belt service life. Dynamic fatigue seam cracking and delamination also occurs in ionographic imaging member belts as well. The flexible electrostatographic imaging member belt is fabricated from a sheet cut from a web. The sheets are generally rectangular in shape. All edges may be of the same length or one pair of parallel edges may be longer than the other pair of parallel edges. The sheets are formed into a belt by joining overlapping opposite marginal end regions of the sheet. A seam is typically produced in the overlapping marginal end regions at the point of joining. Joining may be effected by any suitable means. Typical joining techniques include welding (including ultrasonic), gluing, taping, pressure heat fusing, and the like. Ultrasonic welding is generally the preferred method of joining because is rapid, clean (no solvents) and produces a thin and narrow seam. In addition, ultrasonic welding is preferred because it causes generation of heat at the contiguous overlapping end marginal regions of the sheet to maximize melting of one or more layers therein. When ultrasonically welded into a belt, the seam of multilayered imaging flexible members can crack and delaminate during extended bending and flexing over small diameter belt support rollers of an imaging machine or when subjected to lateral forces caused by rubbing contact with stationary web edge guides of a belt support module during cycling. Seam cracking and delamination is further aggravated when the belt is employed in electrostatographic imaging systems utilizing blade cleaning devices. Alteration of materials in the various photoreceptor belt layers such as the conductive layer, hole blocking layer, adhesive layer, charge generating layer, and/or charge transport layer to suppress cracking and delamination problems is not easily accomplished. The alteration of the materials may adversely affect the overall electrical, mechanical and other properties of the belt such as well as residual voltage, background, dark decay, flexibility, and the like. For example, when a flexible imaging member in an electrophotographic machine is a photoreceptor belt fabricated by ultrasonic welding of overlapped opposite ends of a sheet, the ultrasonic energy transmitted to the overlapped ends melts the thermoplastic sheet components in the overlap region to form a seam. The ultrasonic welded seam of a multilayered photoreceptor belt is relatively brittle and low in strength and toughness. The joining techniques, particularly the welding process, can result in the formation of a splashing that projects out from either side of the seam in the overlap region of the belt. Because of the splashing, a typical flexible imaging. member belt is about 1.6 times thicker in the seam region than that of the remainder of the belt (e.g., in a typical example, 188 micrometers versus 1.6 micrometers). The photoreceptor belt in an electrophotographic imaging apparatus undergoes bending strain as the belt is cycled over a plurality of support and drive rollers. The excessive thickness of the photoreceptor belt in the seam region due to the presence of the splashing results in a large induced bending strain as the seam travels over each roller. Generally, small diameter support rollers are highly desirable for simple, reliable copy paper stripping systems in electrophotographic imaging apparatus utilizing a photoreceptor belt system operating in a very confined space. Unfortunately, small diameter rollers, e.g., less than about 0.75 inch (19 millimeters) in diameter, raise the threshold of mechanical performance criteria to such a high level that photoreceptor belt seam failure can become unacceptable for multilayered belt photoreceptors. For example, when bending over a 19 millimeter diameter roller, a typical photoreceptor belt seam splashing may develop a 0.96 percent tensile strain due to bending. This is 1.63 times greater than a 0.59 percent induced bending strain that develops within the rest of the photoreceptor belt. Therefore, the 0.96 percent tensile strain in the seam splashing region of the belt represents a 63 percent increase in stress placed upon the seam splashing region of the belt. Under dynamic fatiguing conditions, the seam provides a focal point for stress concentration and becomes the initial point of failure in the mechanical integrity of the belt. Thus, the splashing tends to shorten the mechanical life of the seam and service life of the flexible member belt in copiers, duplicators, and printers. Although a solution to suppress the seam cracking/delamination problems has been successfully demonstrated, as described in a prior art, by a specific heat treatment process of a flexible electrophotographic imaging member belt with its seam parked directly on top of a 19 mm diameter back support rod for stress-releasing treatment at a temperature slightly above the glass transition temperature (Tg) of the charge transport layer of the imaging member, nevertheless this seam stress release process was also found to produce various undesirable effects such as causing seam area imaging member set and development of belt ripples in the active electrophotographic imaging zones of the belt (e.g., the region beyond about 25.2 millimeters from either side from the midpoint of the seam). Moreover, the heat treatment can induce undesirable circumferential shrinkage of the imaging belt. The set in the seam area of an imaging member mechanically adversely interacts with the cleaning blade and impacts cleaning efficiency. The ripples in the imaging member belt manifest themselves as copy printout defects. Further, the heat induced imaging belt dimensional shrinkage alters the precise dimensional specifications required for the belt. Another key shortcoming associated with the prior art seam stress release heat treatment process is the extensive heat exposure of a large seam area. This extensive heat exposure heats both the seam area of the belt as well as the rod supporting the seam. Since the belt must be cooled to below the glass transition temperature of the thermoplastic material in the belt prior to removal from the support rod in order to produce the desired degree of seam stress release in each belt, the heat treatment and cooling cycle time is unduly long and leads to very high belt production costs. Therefore, there is an urgent need for improving the mechanical characteristics of seamed flexible imaging belts which can withstand greater dynamic fatiguing conditions and extend belt service life free from any associated shortfalls. US-A 5,240,532 discloses a process for treating a flexible electrostatographic imaging web is disclosed including providing a flexible base layer and a layer including a thermoplastic polymer matrix comprising forming at least a segment of the web into an arc having a radius of curvature between about 10 millimeters and about 25 millimeters measured along the inwardly facing exposed surface of the base layer, the arc having an imaginary axis which traversed the width of the web, heating at least the polymer matrix in the segment to at least the glass transition temperature of the polymer matrix, and cooling the imaging member to a temperature below the glass transition temperature of the polymer matrix while maintaining the segment of the web in the shape of the arc. SUMMARY OF THE INVENTION It is, therefore, an object of the present invention to provide an improved electrostatographic imaging belt which overcomes the above-noted deficiencies. It is yet another object of the present invention to provide a mechanically improved seamed electrostatographic imaging belt. It is still another object of the present invention to provide an improved electrostatographic imaging belt having an ultrasonically welded seam which exhibits greater resistance to cracking and delamination. It is another object of the present invention to provide an improved electrostatographic imaging belt having a welded seam which exhibits greater resistance to cracking and delamination and no seam area set. It is yet another object of the present invention to provide an improved electrostatographic imaging belt having a welded seam which exhibits good dimensional tolerance. It is also another object of the present invention to provide an improved electrostatographic imaging belt having a welded seam which is free of belt ripple induced copy printout defects. It is still another object of the present invention to provide an improved electrostatographic imaging belt with a stress free state in the Imaging layer around the welded seam area when the electrostatographic imaging belt flexes over small diameter support rollers. The foregoing objects and others are accomplished in accordance with this invention by a process having the features set fourth in claim 1. The invention also provides an apparatus for treating an electrostatographic imaging belt having the features as set out in claim 7. BRIEF DESCRIPTION OF THE DRAWINGS In the detailed description of the preferred embodiment of the present invention, reference is made to the accompanying drawings, in which: Figure 1 is a cross-sectional view of a multiple layered flexible sheet of electrophotographic imaging material with opposite ends overlapped. Figure 2 is a cross-sectional view of a multiple layered seamed flexible electrophotographic imaging belt derived from the sheet of Figure 1 after ultrasonic seaming welding. Figure 3 is a schematic, elevational view of an ultrasonic welding apparatus. Figure 4 is a cross-sectional view of a multiple layered seamed flexible electrophotographic imaging belt which has failed due to seam cracking and delamination. Figure 5 is an isometric schematic view of a seamed flexible electrophotographic imaging belt in which the belt seam is positioned over a cylindrical tube, the belt being tensioned by the weight of a second cylindrical tube for seam heat treatment in accordance with prior art processing. Figure 6 is an isometric schematic view of a seamed flexible electrophotographic imaging member belt in which the a belt is transported to a heat treating station and supported at the station by a vacuum holding device which is below and spaced from the seam of the belt. Figure 7 is a schematic, partial cross-sectional view of a belt supported under a heating source by a pair of cantilevered hollow cylindrical members which are below and spaced from the seam of the belt. Figure 8 is a schematic, cross-sectional view of a belt alignment system and a belt supported by a pair of cantilevered hollow cylindrical members which are below and spaced from the seam of the belt. Figure 9 is a schematic, partial cross-sectional view of a belt supported under a heating source by a cantilevered hollow cylindrical member having a rectangular cross section. In the drawings and the following description, it is to be understood that like numeric designations refer to components of like function. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to Figure 1, there is illustrated a flexible member 10 in the form of a sheet having a first end marginal region 12 overlapping a second end marginal region 14 to form an overlap region ready for a seam forming operation. The flexible member 10 can be utilized within an electrophotographic imaging device and may be a single film substrate member or a member having a film substrate layer combined with one or more additional coating layers. At least one of the coating layers comprises a film forming binder. The flexible member 10 may be a single layer or comprise multiple layers. If the flexible member 10 is to be a negatively charged photoreceptor device, the flexible member 10 may comprise a charge generator layer sandwiched between a conductive surface and a charge transport layer. Alternatively, if the flexible member 10 is to be a positively charged photoreceptor device, the flexible member 10 may comprise a charge transport layer sandwiched between a conductive surface and a charge generator layer. The layers of the flexible member 10 can comprise numerous suitable materials having suitable mechanical properties. Examples of typical layers are described in US-A 4,786,570, US-A 4,937,117 and US-A 5,021,309. The flexible member 10 shown in Figure 1, including each end marginal region 12 and 14, comprises from top to bottom a charge transport layer 16 (e.g., 24 micrometers thick), a generator layer 18 (e.g., 1 micrometer thick), an interface layer 20 (e.g., 0.05 micrometer thick), a blocking layer 22 (e.g., 0.04 micrometer thick), a conductive ground plane layer 24 (e.g., 0.02 micrometer thick, a supporting layer 26 (e.g., 76.2 micrometer thick), and an anti-curl back coating layer 28 (e.g., 14 micrometer thick). It should be understood that the thickness of the layers are for purposes of illustration only and that a wide range of thicknesses can be used for each of the layers. The end marginal regions 12 and 14 can be joined by any suitable means including gluing, taping, stapling, pressure and heat fusing to form a continuous member such as a belt, sleeve, or cylinder. Preferably, both heat and pressure are used to bond the end marginal regions 12 and 14 into a seam 30 in the overlap region as illustrated in Figure 2. The flexible member 10 is thus transformed from a sheet of electrophotographic imaging material as illustrated in Figure 1 into a continuous electrophotographic imaging belt as illustrated in Figure 2. The flexible member 10 has a first exterior major surface or side 32 and a second exterior major surface or side 34 on the opposite side. The seam 30 joins the flexible member 10 so that the bottom surface 34 (generally including at least one layer immediately above) at and/or near the first end marginal region 12 is integral with the top surface 32 (generally including at east one layer immediately below) at and/or near the second end marginal region 14. A preferred heat and pressure joining means includes ultrasonic welding to transform the sheet of photoconductive imaging material into a photoreceptor belt. The belt can be fabricated by ultrasonic welding of the overlapped opposite end regions of a sheet. In the ultrasonic seam welding process, ultrasonic energy applied to the overlap region is used to melt suitable layers such as the charge transport layer 16, generator layer 18, interface layer 20, blocking layer 22, part of the support layer 26 and/or anti-curl back coating layer 28. Direct fusing of the support layer achieves optimum seam strength. A conventional ultrasonic welding apparatus 36 is shown in Figure 3. The apparatus 36 comprises an ultrasonic horn 38 which is caused to oscillate along its longitudinal axis by a transducer assembly 40 affixed to the top thereof. A solenoid 42 is mounted above the transducer assembly 40 to extend or retract the ultrasonic horn 38 and the transducer assembly 40 in the vertical direction. The seam 30, (not shown in Figure 3) formed by the overlapping segment end marginal regions 12 and 14 of the flexible member 10, is supported by the upper surface of anvil 44 and held in place below the path of the ultrasonic horn 38 by suction from parallel rows of grooves 46, 48, 50 and 52. The anvil 44 preferably includes or is connected to a vacuum source for holding down overlapping ends of member 10. The ultrasonic hom 38 and the transducer assembly 40 are supported by the lower end of a vertically reciprocating shaft (not shown) extending from the lower end of the solenoid 42 mounted to the upper hinged half of a substantially horizontally reciprocating carriage 54. One side of the lower hinged half of the carriage 54 is suspended from a pair of pillow blocks 56 which, in turn, slides on a horizontal bar 58. The other side of carriage 54 is suspended from a pair of cam followers 60 that rolls on the outer surface of a horizontal bar 62. A rotatable lead screw 64 drives the horizontally reciprocating carriage 54 through a ball screw 66 secured to the carriage 54. The horizontal bars 58 and 62, as well as the lead screw 64, are secured at each end by a frame assembly (not shown). The lead screw 64 is rotated by a belt driven by an electric motor (not shown) which is also supported by the frame assembly. When the overlap region formed by the end marginal regions 12 and 14 of the flexible member 10, is positioned on the anvil 44 below the ultrasonic hom 38 at a belt welding station, the solenoid 42 is inactivated to extend the transducer 40 toward the anvil 44 from a retracted position (in which the solenoid 42 is activated). The transducer 40 is activated by the electric motor to drive the lead screw 64 which, in tum, moves the horizontally reciprocating carriage 54 over the seam 30 supported by the anvil 44. Lowering of the transducer 40 by inactivation of solenoid 42 brings the ultrasonic horn 38 into compressive engagement with an appropriate overlap region, e.g., 1.02 mm (0.040 inch) of the flexible member 10. The high vibration frequency of the ultrasonic horn 38 along its vertical axis causes the temperature of at least the contiguous overlapping surfaces of the flexible member 10 to increase until at least one layer (e.g., charge transport layer 16) of the flexible member 10 flows, resulting in the formation of a welded seam 30. Welding of the contiguous overlapping surfaces of the flexible member 10 can best be accomplished if the flexible member 10 comprises layers which flow as a result of the applied energy of ultrasonic oscillations (e.g., charge transport layer 16 and anti-curl back coating layer 28). For optimum seam strength, it is preferable that the layers of the flexible member 10 at the overlap region be brought to the melting stage by the applied ultrasonic energy. In this manner, fusing of support layer 26 can be achieved to form the welded seam 30 as illustrated in Figure 2. Welding of opposite ends of a sheet to form an electrophotographic belt is well known and described, for example, in US-A 4,838,964, US-A 4,878,985, US-A 5,085,719 and US-A 5,603,790. The flexible member 10 may be of any suitable thickness which will allow adequate heating of the contiguous overlapping surfaces of the end marginal regions 12 and 14 to cause joining when sufficient heat energy to be applied to the contiguous overlapping surfaces. Any suitable heating technique may be used to provide the heat necessary at the contiguous overlapping surfaces to melt the thermoplastic material and cause it to weld the overlap region of the flexible member 10. Thus, a suitable technique permanently transforms the form of the flexible member 10 from a sheet of electrophotographic imaging material into an electrophotographic imaging belt. When ultrasonic welding is utilized at the contiguous overlapping region, the flexible member 10 is positioned between the anvil 44 and ultrasonic horn 38. The rapid impact of the first end marginal region 12 against the second end marginal region 14 of the flexible member 10 causes generation of heat. A horn vibration frequency from a range of about 16 KHz or higher may be utilized to cause the flexible member 10 to soften and melt. Since heat is generated very rapidly at the interface of the device, sufficient heat to cause the layers of the flexible member 10 to melt can occur typically in about 1.2 seconds as the horn 38 traverses along the overlap region. As the hom 38 is lowered to the overlap region of the flexible member 10, electrical power is supplied to the transducer 40 and the electric motor (not shown) is activated to drive the lead screw 64 which, in turn, moves the horizontally reciprocating carriage 54 and ultrasonic horn 38 along the overlap region of the flexible member 10. After the carriage 54 completes its traversal of the overlap region, the solenoid 42 is activated to retract the transducer 40 away from anvil 44, the transducer 40 is inactivated, and the electric motor (not shown) is reversed to return the horizontally reciprocating carriage 54 to its starting position. A typical ultrasonic horn traverse speed for the seaming operation can be selected in a range from 2,54 to 12,7 cm (1 to 5 inches per second). Upon completion of the welding of the overlap region into a seam 30, the overlap region is transformed into an overlapping and abutting region as illustrated in Figures 2 and 4. Within the overlapping and abutting region, the portions of the flexible member 10, which once formed the end marginal regions 12 and 14, are joined by the seam 30 such that the once end marginal regions 12 and 14 are overlapping and abutting one another. The welded seam 30 contains upper and lower splashings 68 and 70 at each end thereof as illustrated in Figures 2 and 4. The splashings 68 and 70 are formed in the process of joining the end marginal regions 12 and 14 together. Molten material is necessarily ejected from either side of the overlap region to facilitate direct support layer 26 to support layer fusing and results in the formation of the splashings 68 and 70. The upper splashing 68 is formed and positioned above the overlapping end marginal region 14 abutting the top surface 32 and adjacent to and abutting the overlapping end marginal region 12. The lower splashing 70 is formed and positioned below the overlapping end marginal region 12 abutting bottom surface 34 and adjacent to and abutting the overlapping end marginal region 14. The splashings 68 and 70 extend beyond the sides and the edges of the seam 30 in the overlap region of the welded flexible member 10. The extension of the splashings 68 and 70 beyond the sides and the edges of the seam 30 is undesirable for many machines such as electrophotographic copiers, duplicators and copiers that require precise edge positioning of a flexible member 10 during machine operation. Generally, the extension of the splashings 68 and 70 at the belt edges of the flexible member 10 are removed by a notching operation. A typical splashing has a thickness of about 68 micrometers. Each of the splashings 68 and 70 has an uneven but generally rectangular shape including one side (free side) 72 (which forms a free end) extending inwardly from an outwardly facing side 74 (extending generally parallel to either the top surface 32 or the bottom surface 34). The free side 72 of the splashing 68 forms an approximately perpendicular angle  1 with the bottom surface 34 of the flexible member 10. Likewise, the free side 72 of the splashing 70 forms an approximately perpendicular angle  2 meeting or junction point 76 which exists at the junction of the free side 72 of the upper splashing 68 and the top surface 32 of the flexible member 10. Likewise, a meeting or junction point 78 exists at the junction of the free side 72 of the lower splashing 70 and the bottom surface 34 of the flexible member 10. Both junction points 76 and 78 provide focal points for the stress concentration and become the initial points of failure affecting the mechanical integrity of the flexible member 10. During machine operation, the seamed belt flexible member 10 cycles or bends over rollers, particularly small diameter rollers, of a belt support module within an electrophotographic imaging apparatus. In this case, as a result of dynamic bending of the flexible member 10 during dynamic cycling, the rollers exert a force on the flexible member 10 which causes large stress to develop generally adjacent to the seam 30 due to the excessive thickness thereof. The stress concentrations that are induced by bending near the junction points 76 and 78 may reach values much larger than the average value of the stress over the entire length of the flexible member 10. The induced bending stress is inversely related to the diameters of a roller that the flexible member 10 bends over and directly related to the thickness of the seam 30 of the flexible member 10. When a structural member, such as the flexible member 10, contains a sudden increase in cross-sectional thickness at the overlap region, high localized stress occurs near the discontinuity, e.g., junction points 76 and 78. When the flexible member 10 bends over the rollers of a belt module within an electrophotographic imaging apparatus, the bottom surface 34 of the flexible member 10, which is adapted to contact the exterior surface of the roller, is compressed. In contrast, the top surface 32 is stretched under tension. This is attributable to the fact that the top surface 32 and bottom surface 34 move in a circular path about the circular roller. Since the top surface 32 is at greater radial distance from the center of the circular roller than the bottom surface 34, the top surface 32 must travel a greater distance than the bottom surface 34 in the same time period. Therefore, the top surface 32 must be stretched under tension relative to a generally central portion of the flexible member 10 (the portion of the flexible member 10 generally extending along the center of gravity of the flexible member 10). Likewise, the bottom surface 34 must be compressed relative to the generally central portion of the flexible member 10 (the portion of the flexible member 10 generally extending along the center of gravity of the flexible member 10). Consequently, the bending stress at the junction point 76 will be tension stress, and the bending stress at the junction point 78 will be compression stress. Compression stresses, such as at the junction point 78, rarely cause seam 30 failure. Tension stresses, such as at junction point 76, however, are much more of a problem. The tension stress concentration at the junction point 76 in great likelihood will eventually result in' crack initiation through the electrically active layers of the flexible member 10 as illustrated in Figure 4. The illustrated crack 80 is adjacent to the top splashing 68 of the second end marginal region 14 of the flexible member 10. The generally vertically extending crack 80 initiated in the charge transport layer 16 continues to propagate through the generator layer 18. Inevitably, the crack 80 extends generally horizontally to develop seam delamination 81 which is propagated through the relatively weak adhesion bond between the adjoining surfaces of the generator layer 18 and the interface layer 20. The formation of the local seam delamination 81 is typically referred to as seam puffing. The effect of the excess thickness of the splashing 68 and stress concentration at the junction point 76 is to cause the flexible member 10 to perform, during extended machine operation, as if a material defect existed therein. Thus, the splashing 68 tends to promote the development of dynamic fatigue seam 30 failure and can lead to separation of the joined end marginal regions 12 and 14 severing the flexible member 10. Consequently, the service life of the flexible member 10 is shortened. In addition to seam failure, the crack 80 acts as a depository site and collects toner, paper fibers, dirt, debris and other unwanted materials during electrophotographic imaging and cleaning of the flexible member 10. For example, during the cleaning process, a cleaning instrument, such as a cleaning blade, will repeatedly pass over the crack 80. As the site of the crack 80 becomes filled with debris, the cleaning instrument dislodges at least some portion of this highly concentrated level of debris from the crack 80. The amount of the debris, however, is beyond the removal capacity of the cleaning instrument. As a consequence, the cleaning instrument dislodges the highly concentrated level of debris but cannot remove the entire amount during the cleaning process. Instead, portions of the highly concentrated debris is deposited onto the surface of the flexible member 10. In effect, the cleaning instrument spreads the debris across the surface of the flexible member 10 instead of removing the debris therefrom. In addition to seam failure and debris spreading, the portion of the flexible member 10 above the seam delamination 81, in effect, becomes a flap which moves upwardly. The upward movement of the flap presents an additional problem during the cleaning operation. The flap becomes an obstacle in the path of the cleaning instrument as the instrument travels across the surface of the flexible member 10. The cleaning instrument eventually strikes the flap when the flap extends upwardly. As the cleaning instrument strikes the flap, great force is exerted on the cleaning instrument which can lead to damage thereof, e.g., excessive wear and tearing of the cleaning blade. In addition to damaging the cleaning blade, the striking of the flap by the cleaning instrument causes unwanted vibration in the flexible member 10. This unwanted vibration adversely affects the copy/print quality produced by the flexible member 10. The copy/print is affected because imaging occurs on one part of the flexible member 10 simultaneously with the cleaning of another part of the flexible member 10. Vibration problems encountered with the flexible member 10 is not exclusively limited to a flexible member 10 undergoing seam delamination 81. The discontinuity in cross-sectional thickness of the flexible member 10 at junction points 76 and 78 also can also create unwanted vibration, particularly when the flexible member 10 bends over small diameter rollers of a belt module or between two closely adjacent rollers. Illustrated in Figure 5 is a belt 10 mounted directly on a supporting cylindrical tube 90 having an outer radius of curvature between about 9.5 millimeters and about 50 millimeters (i.e. diameter of curvature of between about 19 millimeters and about 100 millimeters). When the diameter of curvature chosen for seam heat treatment is less than about 9.5 millimeters (i.e. diameter of curvature of about 19 millimeters), the beam rigidity of the electrophotographic imaging belt will render extremely difficult any effort to bending of the belt 10 to achieve a very small curvature prior to heat treatment. When the radius of curvature Is greater than about 50 millimeters (i.e. diameter of curvature of about 100 micrometers), the benefits of the present invention are not fully realized because no significant seam stress release in the imaging layer is achieved. As shown in Figure 5, the electrophotographic imaging belt 10 may be positioned with belt seam 30 parked directly over supporting cylindrical tube 90, the arcuate surface of tube 90 being in intimate contact with the back surface of belt 10 and the imaging surface of belt 10 facing outwardly away from tube 90. To ensure intimate contact and conformance of the belt with about half of the tube 90, a slight tension is applied to the belt 10 by inserting a light weight cylindrical tube 92 inside the lower loop of belt 10 while the belt 10 is hanging from tube 90. Tube 90 may be cantilevered by securing one end to a supporting wall or frame. The radius of curvature of tube 90 can vary from about 9.5 millimeters to any larger dimension of about 50 millimeters. A desirable wrapped angle for the seam segment parking over the back supporting cylindrical tube 90 should provide an arcuate area at the seam region at least about as wide as the diameter of the heated substantially circular spot. It is preferred that the wrap angle encompassing the seam and region of the belt adjacent each side of the seam conforming to the arcuate supporting surface of the support member be between about 10 degrees and about 180 degrees. The material used for tube 90 and tube 92 may be of any suitable material, including for example, metal, plastic, composites, and the like. With the schematic arrangement described in Figure 5, a heating element or source (not shown) is positioned directly above the cylindrical tube 90 to provide heat energy for the seam stress release heat treatment process. Since the heating means employed in prior art seam heat treatment processes are usually a hot air impingement source, a toaster oven type heater comprising hot wire filaments or a quartz tube, the entire seam length area directly under heat exposure is large and requires a lengthy time for the seam area to reach the seam stress release temperature and a long time for cooling of the seam area and belt support member. Moreover, the typical heat source used for the prior art seam heat treatment process emits a broad band of infrared radiant heat which requires several minutes of elapsed time to complete a heating/cooling processing cycle. These prior approaches caused heating of the supporting cylindrical member which retarded cooling rates for belt after heating. In sharp contrast, the process of the present invention, as illustrated in Figure 6, utilizes at least one vacuum holding device 100 spaced from the seam 30 to provide an air gap and to maintain the seam 30 and region of the belt adjacent each side of the seam in an arcuate shape having at least a substantially semicircular cross section with a radius of curvature of between about 9.5 millimeters and about 50 millimeters. The vacuum holding device 100 comprises a cantilevered hollow tube vacuum holding device sealed and supported by a frame (not shown) at one end and a flexible hose 102 leading to the opposite end to supply vacuum to the interior of vacuum holding device 100. If desired, hollow tube vacuum holding device 100 may have any other suitable cross sectional shape such as oval, square, rectangular and the like. The flexible hose 102 may be connected through any suitable manually or automatically controlled valve (not shown) to a suitable vacuum source such as a pump or tank containing a gas under reduced pressure. Vacuum holding device 100 contains a plurality of tiny openings 103 at about the 3 o'clock and 9 o'clock positions. Although a plurality of tiny openings are shown (e.g. a porous region fabricated by drilling or sintering), any other suitable openings may be employed. The number and size of the openings should be sufficient to support belt 10. The size and number of openings will vary depending upon the weight of the belt and the amount of vacuum employed. For a typical flexible electrostatographic imaging member belt, a low vacuum of about 630 millimeters of Hg is sufficient to effectively hold the imaging belt in position for heat treatment. The size of the openings should be selected so that, with the vacuum used, permanent distortion of the belt is avoided. The openings may be of any suitable shape. Typical shapes include, for example, round, oval, square, rectangular, slits, channels, slots and the like. A reciprocatable vacuum conveyor 104 is used to convey welded belt 10 into position over the vacuum holding device 100. The vacuum conveyor 104 comprises a hollow housing 106 and resilient fingers 108. Fingers 108 each contain a passageway connecting the hollow interior of housing 106 with openings (not shown) at the lower tips of the fingers 108. Fingers 108 may comprise any suitable material. Resilient material is preferred for fingers 108 to ensure that a sufficient seal is achieved between the lower tips of fingers 108 and the seam area of belt 10 when vacuum is supplied to the hollow housing 106. a flexible hose 110 supplies a vacuum to the interior of hollow housing 106. The flexible hose 110 may be connected through any suitable manually or automatically controlled valve (not shown) to a suitable vacuum source such as a pump or tank containing a gas under reduced pressure. A translating mechanism 112 moves vacuum conveyor 104 with imaging belt 10 into position over vacuum holding device 100. Translating mechanism 112 may be any suitable device which can move vacuum conveyor 104 and belt 10 to position seam 30 of belt 10 parallel to and spaced a predetermined distance from vacuum holding device 100. Typical translating mechanisms include, for example, robot arms, slides, rails, reciprocating two way acting pistons, and the like. In operation, the lower tips of resilient fingers 108 are brought into contact with or in close proximity to seam 30 of a belt 10 to be treated. A supply valve is activated to supply a vacuum to the hollow housing 106 through flexible hose 110 so that vacuum conveyor 104 can support and carry belt 10. Translating mechanism 112 is then activated to transport vacuum conveyor and belt 10 from an area remote from vacuum holding device 100 and position seam 30 of belt 10 parallel to and spaced a predetermined distance over the upper surface of vacuum holding device 100. The predetermined distance should be sufficient to form an air space of at least about 0,64 cm (0.25 inch) between the bottom of seam 30 and the upper surface of vacuum holding device 100 and sufficient to maintain the seam 30 and region of the belt 10 adjacent each side of the seam 30 in an arcuate shape having at least a substantially semicircular cross section having a radius of curvature of between about 9.5 millimeters and about 50 millimeters. After belt 10 is in position around vacuum holding device 100, a valve is activated to supply a vacuum through flexible hose 102 to the interior of vacuum holding device 100 to draw the adjacent inside surfaces of belt 10 against the openings 103 at about the 3 o'clock and 9 o'clock positions of vacuum holding device 100. The vacuum supplied to the interior of hollow housing 106 is then terminated and vacuum conveyor 104 is retracted by translating mechanism 112 to a home position away from belt 10. The thermoplastic polymer matrix in at least the upper portion of seam 30 and the region of the belt 10 adjacent each side of the seam is then heated by any suitable device (not shown) to at least the glass transition temperature (Tg) of the polymer matrix in at least the upper portion of the seam without significantly heating the vacuum holding device 100. Any suitable heat treatment device may be employed. Typical heat treatment devices include, for example, resistance heaters, tungsten halogen lamps, hot impinging air blowers, hot wires, toaster oven type heating filaments, carbon dioxide lasers, and the like. The heat treatment devices may be elongated and extend over the entire length of seam 30 or may be translated from one end of the seam to the other by moving the belt, moving the heat treatment device or moving both the belt and the heat treatment device. Typical heat treatment devices are described in US-A 5,240,532, the entire disclosure thereof being incorporated herein by reference. The maintenance of an open air space below the seam 30 such as an air gap between the upper surface of vacuum holding device 100 located within the belt loop effectively insulates vacuum holding device 100 from the heat energy applied to seam 30 during the heat exposure treatment step and also facilitates substantially instantaneous cooling of the arcuate seam 30 and regions of the belt immediately adjacent the seam to a temperature below the Tg of the thermoplastic polymer matrix in the seam 30 and regions of the belt immediately adjacent the seam immediately following heat treatment. Heating of the seam areas of the belt while it is maintained in an arcuate shape with only a gas contacting the top and bottom of the seam, rapidly elevates the temperature of the imaging layer in the seam area above the glass transition temperature (Tg). Typically, the Tg of a film forming polymer used for electrostatographic imaging layer coating applications is at least about 45°C to satisfy most imaging belt machine operating conditions. Preferably, the heat treatment is carried out between about the Tg and about 25°C above the Tg of the thermoplastic imaging layer to achieve sufficient seam stress release. Referring to Figure 7, belt 10 is shown supported by a pair of cantilevered hollow cylindrical holding members 114 and 116 containing slits 118 and 120, respectively. Slits 118 and 120 of cantilevered hollow cylindrical members 114 and 116 grip the interior surface of belt 10. Seam 30 of belt 10 is heated by a heating source 122 comprising a heating element 124 backed by a reflector 126. Heating source 122 may be an elongated device which extends along the entire length of seam 30 or it may be a traversing device that only heats a small section of the seam at any given moment in time during traverse. If heating source is of the latter type, it is moved along the length of the seam to incrementally heat the thermoplastic material in the seam to a temperature at least as high as the Tg of the thermoplastic material. The heating source 122 may be moved substantially continuously or incrementally along the seam 30 manually or automatically, such as by any suitable horizontally reciprocateable carriage system (not shown). Alternatively, where the heating source 122 only heats a small section of the seam at any given moment in time, heating source 122 may be held stationary and the belt with the cylindrical holding members 114 and 116 may be moved substantially continuously or incrementally either manually or automatically such as by any suitable horizontally reciprocateable carriage system (not shown). The horizontally reciprocateable carriage system may be driven by any suitable device such as a lead screw and motor combination, belt or chain drive slide system, and the like. A suitable horizontally reciprocateable carriage, lead screw and motor combination is described with reference to the welding system illustrated in Figure 3. Thus, for example, the heating source 122 shown in Figure 7 may be mounted on the horizontally reciprocating carriage 54 illustrated in Figure 3 instead of the ultrasonic welding apparatus 36 shown in Figure 3. Conversely, the cylindrical holding members 114 and 116 and belt 10 may be mounted on the horizontally reciprocating carriage 54 illustrated in Figure 3 instead of the ultrasonic welding apparatus 36 shown in Figure 3. Similar suitable horizontally reciprocateable carriage, lead screw and motor combinations are described in US-A 4,838,964, US-A 4,878,985, US-A 5,085,719 and US-A 5,603,790. If desired, both the heating source and belt with the cylindrical holding members 114 and 116 may simultaneously be moved to achieve relative movement between each other. The heating source 122 may, for example, be transported across the width of the belt 30 directly over the entire length of the seam 30 at a speed between about 2.54 centimeters (1 inch) and 12.7 centimeters (5 inches) per second. Preferably, a heating source 122 which is stationary and extends along the entire length of the seam 30 is preferred because the entire seam can be heated more rapidly and the construction of the heat treating system is simpler. Illustrated in Figure 8 is belt 10 supported by a pair of cantilevered hollow holding cylindrical members 128 and 130 containing slits 132 and 134, respectively. If desired, cylindrical members 128 and 130 may have any other suitable cross sectional shape such as oval, square, rectangular and the like. Slits 132 and 134 of cantilevered hollow holding cylindrical members 128 and 130 grip the exterior surface if belt 10. Resilient material is preferred for the outer surface of cantilevered hollow holding cylindrical holding members 128 and 130 adjacent slits 132 and 134 to avoid scratching of the outer surface of belt 10 when vacuum is supplied to members 128 and 130. Located at the bottom of the loop formed by belt 10 is a belt alignment system 136 comprising a retractable cylinder 138 which is movable in a vertical direction by a pair of two way acting air cylinders 140 (only one is visible in Figure 8) connecting each end of retractable cylinder 138 to a frame 142 by connecting rods 144 and 146. When inactivated, two way acting air cylinders 140 retract retractable cylinder 138 upwardly. This facilitates mounting the lower portion of belt 10 around belt alignment system 136 and inserting the upper portion of belt 10 between cantilevered hollow holding cylindrical members 128 and 130. Activation of two way acting air cylinders 140 extends retractable cylinder 138 downwardly to move the lower portion of belt 10 to a predetermined position which automatically moves the upper portion of belt 10 to a predetermined position. Cantilevered hollow holding cylindrical members 128 and 130 are connected by hoses through a conventional valve to a suitable source of vacuum (not shown). After the belt 10 Is mounted around belt alignment system 136 and between hollow cylindrical holding members 128 and 130, the valve to the vacuum source is opened to retain the upper outer portions of belt 10 against slits 132 and 134. Activation of the two way acting air cylinders 140 may be accomplished prior to or subsequent to opening the valve to the vacuum source. Preferably, the two way acting air cylinders 140 are activated prior to opening the valve to the vacuum source to minimize frictional rubbing of the upper outer portions of belt 10 against hollow holding cylindrical members 128 and 130. Altematively, cylinder 138 may be stationary in the downwardly extended position or modified so that it is cantilevered to a frame or other stationary support member (not shown). In this alternative embodiment, the lower portion of belt 10 can be mounted by hand around cylinder 138 and the upper end can be urged upwardly by a hand or robot arm within the upper portion of the loop of belt 10. This alternative embodiment will also position the seam 30 of belt 10 at a predetermined position from a heat treatment source (not shown). Shown in Figure 9 is an alternative embodiment of a cantilevered support member. Instead of having a substantially round cross section, this alternative support member 150 has a rectangular cross section and slits 152 and 154. Any other suitable support member cross section may be utilized. Typical cross sectional shapes include, for example, square, octagonal, oval, and the like. For heat treatment of a flexible imaging member belt having a slanted seam, the heating source may be set to precisely track the seam when traversing the entire belt width. However, it is preferred that the belt is cocked and adjusted such that the seam is positioned without skewing along the upper bend of belt 10 during belt holding. Thus, upon completion of belt holding for heat treatment, the seam is straight and every incremental portion of the seam is at top of the upper bend of belt 10. Since the heat energy applied to on the upper surface of seam 30 substantially instantaneously elevates the temperature of the polymeric matrix in the imaging layer of the electrostatographic imaging member belt in the seam area and regions adjacent the seam above its glass transition temperature (Tg), termination of application of heat energy facilitates rapid cooling of the heated seam because only air is present above and below seam 30. If desired, a cooling gas may be circulated above and below the seam air after heating to accelerate quench cooling of seam 30. With this extremely rapid seam heating/cooling combination, the seam stress release heat treatment operation cycle time can be accomplished in a matter of seconds, depending on the belt width of an electrostatographic imaging belt product. This extremely brief treatment cycle time is of crucial importance because it can be integrated into a high volume production process and function synchronously with high speed ultrasonic seam welding operations without adversely impacting belt fabrication/finishing throughput. Furthermore, the process of this invention effectively suppresses heat induced belt circumferential shrinkage and localized seam area set as well as the formation of ripples in the leading and trailing edges of the imaging zones near the seam, typically associated with prior art welded seam belts. If desired, localized application of heat can be further controlled by the use of masking devices with slots or other suitably shaped openings which limit where the heat energy from the heat supply devices strike the seam and adjacent regions. For belts having a seam extending perpendicular to the parallel edges of the belt, the entire length of the seam is preferably located at the top (12 o'clock position) of the upper belt loop of belt 10. However, for skewed seam belts where the seam is not perpendicular to the parallel edges of the belt, only the mid point of the entire seam length would normally be located at the top (12 o'clock position) of the upper belt loop of belt 10 when the parallel edges of the belt are positioned vertically. To facilitate and simplify heat treatment, it is preferred to cock the edges of the belt to so that the length of entire seam 30 is positioned at the top (12 o'clock position) of the upper belt loop of belt 10. If desired, separate multiple vacuum holding devices aligned in one or more rows or staggered across the width of the belt may be employed to hold the belt. However, the vacuum devices should be spaced from the seam so that a free air space is maintained below the seam during the heat treatment and cooling steps. Preferably, the belt seam is held in a substantially horizontal position by the vacuum holding devices. However, the seam may be inclined at any suitable angle to horizontal so long as an air space is maintained above and below the seam during the heating and cooling treatments. The seam stress release heat treatment process of this invention is designed for high speed processing. The treating of the flexible electrostatographic imaging belt 10 described above and in the working Examples below comprises bending the short segment of the electrostatographic imaging belt into an arc having an a substantially semicircular cross section and an imaginary axis which transverses the width of the belt with the seam situated at the middle of the arc. The desired arc may be conveniently formed by supporting the upper portion of the belt containing the seam with vacuum holding devices spaced from the seam, the arc having at least a substantially semicircular cross section having a radius of curvature of between about 9.5 millimeters and about 50 millimeters. The vacuum support member may be any suitable vacuum holding device. If desired, temperature sensors may be employed below the seam and/or adjacent to the heating source to initially ensure that sufficient heat energy is applied to raise the temperature of the seam area above the glass transition temperature Tg of the thermoplastic polymer in upper coatings, such as in the charge transport layer of photoreceptors, while avoiding undue heating of the support member. Thus, the process and apparatus of this invention provides a photoreceptor belt in which seam bending stress during dynamic flexing over the rollers of a belt support module is eliminated during image cycling. This stress release in the seam prevents premature seam cracking and delamination in the welded seam area as a belt is cycled over belt module support rollers. It is important to note that after the heat treatment of this invention, cracking has never been seen to be a problem when the seam area is under compression as it cycles through any straight, flat runs between roller supports in an imaging system. A number of examples are set forth hereinbelow and are illustrative of different compositions and conditions that can be utilized in practicing the invention. All proportions are by weight unless otherwise indicated. It will be apparent, however, that the invention can be practiced with many types of compositions and can have many different uses in accordance with the disclosure above and as pointed out hereinafter. EXAMPLE I An electrophotographic imaging member web was prepared by providing a roll of titanium coated biaxially oriented thermoplastic polyester (Melinex, available from ICI Americas Inc.) substrate having a thickness of 76.2 micrometers and applying thereto, using a gravure applicator, a solution containing 50 parts by weight 3-aminopropyltriethoxysilane, 50.2 parts by weight distilled water, 15 parts by weight acetic, 684.8 parts by weight of 200 proof denatured alcohol, and 200 parts by weight heptane. This layer was then dried to a maximum temperature of 143.3°C in a forced air oven. The resulting blocking layer had a dry thickness of 0.05 micrometer. An adhesive interface layer was then prepared by applying to the blocking layer a wet coating containing 5 percent by weight, based on the total weight of the solution, of polyester adhesive (Mor-Ester 49,000, available from Morton International, Inc.) in a 70:30 volume ratio mixture of tetrahydrofuran/cyclohexanone. The adhesive interface layer was dried to a maximum temperature of 135°C in a forced air oven. The resulting adhesive interface layer had a dry thickness of 0.07 micrometer. The adhesive interface layer was thereafter coated with a photogenerating layer containing 7.5 percent by volume trigonal selenium, 25 percent by volume N,N'-dipheny-N,N'-bis(3-methylphenyl)-1,1'-biphenyl-4,4'-diamine, and 67.5 percent by volume polyvinylcarbazole. This photogenerating layer was prepared by introducing 160 gms polyvinylcarbazole and 2,800 mls of a 1:1 volume ratio of a mixture of tetrahydrofuran and toluene into a 400 oz. amber bottle. To this solution was added 160 gms of trigonal selenium and 20,000 gms of 3.2 millimeters diameter stainless steel shot. This mixture was then placed on a ball mill for 72 to 96 hours. Subsequently, 500 gms of the resulting slurry were added to a solution of 36; gms of polyvinylcarbazole and 20 gms of N,N'-diphenyl-N,N'-bis(3-methylphenyl)-1,1'-biphenyl-4,4'-diamine dissolved in 750 mls of 1:1 volume ratio of tetrahydrofuran/toluene. This slurry was then placed on a shaker for 10 minutes. The resulting slurry was thereafter applied to the adhesive interface by extrusion coating to form a layer having a wet thickness of 12.7 micrometers. However, a strip about 3 mm wide along one edge of the coating web, having the blocking layer and adhesive layer, was deliberately left uncoated by any of the photogenerating layer material to facilitate adequate electrical contact by the ground strip layer that is applied later. This photogenerating layer was dried to a maximum temperature of 138°C in a forced air oven to form a dry thickness photogenerating layer having a thickness of 2.0 micrometers. This coated imaging member web was simultaneously overcoated with a charge transport layer and a ground strip layer by co-extrusion of the coating materials. The charge transport layer was prepared by introducing into an amber glass bottle in a weight ration of 1:1 N.N'-diphenyl-N,N'-bis(3-methylphenyl)-1,1'-biphenyl-4,4'-diamine and Makrolon 5705, a polycarbonate resin having a molecular weight of about 120,000 commercially available from Farbenfabriken Bayer A.G. The resulting mixture was dissolved to give 15 percent by weight solid in methylene chloride. This solution was applied on the photogenerator layer by extrusion to form a coating which upon drying gave a thickness of 24 micrometers. The strip, about 3 mm wide, of the adhesive layer left uncoated by the photogenerator layer, was coated with a ground strip layer during the co-extrusion process. The ground strip layer coating mixture was prepared by combining 23.81 gms. of polycarbonate resin (Makrolon 5705, 7.87 percent by total weight solids, available from Bayer A.G.), and 332 gms of methylene chloride in a carboy container. The container was covered tightly and placed on a roll mill for about 24 hours until the polycarbonate was dissolved in the methylene chloride. The resulting solution was mixed for 15-30 minutes with about 93,89 gms of graphite dispersion (12.3 percent by weight solids) of 9.41 parts by weight graphite, 2.87 parts by weight ethyl cellulose and 87.7 parts by weight solvent (Acheson Graphite dispersion RW22790, available from Acheson Colloids Company) with the aid of a high shear blade dispersed in a water cooled, jacketed container to prevent the dispersion from overheating and losing solvent. The resulting dispersion was then filtered and the viscosity was adjusted with the aid of methylene chloride. This ground strip layer coating mixture was then applied, by co-extrusion with the charge transport layer, to the electrophotographic imaging member web to form an electrically conductive ground strip layer having a dried thickness of about 14 micrometers. The resulting imaging member web containing all of the above layers was then passed through a maximum temperature zone of 116°C in a forced air oven to simultaneously dry both the charge transport layer and the ground strip. An anti-curl coating was prepared by combining 88.2 gms of polycarbonate resin (Makrolon 5705, available from Goodyear Tire and Rubber Company) and 900.7 gms of methylene chloride in a carboy container to form a coating solution containing 8.9 percent solids. The container was covered tightly and placed on a roll mill for about 24 hours until the polycarbonate and polyester were dissolved in the methylene chloride. 4.5 gms of silane treated microcrystalline silica was dispersed in the resulting solution with a high shear dispersion to form the anti-curl coating solution. The anti-curl coating solution was then applied to the rear surface (side opposite the photogenerator layer and charge transport layer) of the electrophotographic imaging member web by extrusion coating and dried to a maximum temperature of 104°C in a forced air oven to produce a dried coating layer having a thickness of 13.5 micrometers. EXAMPLE II The electrophotographic imaging member web of Example I having a width of 353 millimeters, was cut into 3 separate rectangular sheets of precise 559.5 millimeters in length. The opposite ends of each imaging member were overlapped 1 mm and joined by ultrasonic energy seam welding process using a 40 Khz horn frequency to form 3 seamed electrophotographic imaging member belts. Two of these seamed belts are to be subjected to a seam stress release heat treatment process while the remaining untreated one is used to serve as a control. Comparative Example III One of the welded electrophotographic imaging member belts described in Example II was suspended over a horizontally positioned cylindrical back supporting aluminum tube, having a 5.08 centimeters diameter, a wall thickness of about 6.35 millimeters, and an anodized outer surface, with the welded seam parked directly along the top (i.e. 12 o'clock position) of the back support cylindrical tube. Another cylindrical aluminum tube identical to the back supporting cylindrical tube was inserted inside the hanging belt loop so that the tube hangs at the bottom of the loop to ensure conformance of the welded seam to the outer arcuate upper surface of the back supporting cylindrical tube and to provide a 180° wrap angle for the seam area as illustrated in Figure 5. The temperature of the seam area was raised to about 90°C, 8°C above the glass transition temperature (Tg) of the charge transport layer, using a toaster oven type filament heater to represent the prior art heat treatment approach. Observation with an infrared sensing camera showed that the seam heat treatment process required over 0.95 minute to reach the desired seam area temperature for softening of the charge transport layer in the seam area to effect seam stress release. Since the supplied heat energy was also being conducted through the belt to the back supporting cylindrical tube, it was noted that the resulting heated seam area required about 1.5 minutes of cooling time for the seam to return to ambient room temperature. It was also noted that the prior art seam heat treatment method, if continued for a plurality of belts, could cause a substantial rise in room ambient temperature. The seam area receiving the heat treatment had a width of about 2 inches over both sides of the seam (i.e. extending a perpendicular distance of 1 inch from the centerline of the seam) and was found to exhibit a substantial amount of imaging member set (i.e. when viewing the seam area from one end of the seam of a belt resting on a flat table top, the treated seam area exhibited a pronounced curve resembling the curvature of the back supporting cylindrical tube). EXAMPLE IV The second electrophotographic imaging member belt of Example II was vacuum held over a hallow aluminum cylindrical holding tube having a 2-inch outer diameter, a 1/4 inch wall thickness, a 2 millimeters slit opening at 3 o'clock and 9 o'clock positions, an end cap, and a vacuum connecting tube at the opposite end to supplied a low 630 millimeters Hg pressure to hold the belt. The cylindrical holding tube was set at horizontal position and the belt having the seam was vacuum held, as that illustrated in Figure 6, to provide an air spacing of about one inch between the top surface of the cylindrical holding tube and the inside surface of the belt under the seam area as well as sustaining the seam and region of the belt adjacent to each side of the seam in-an arcuate shape having a substantially semicircular bend to yield a radius of curvature of about 2 inches. The imaging member belt, with the seam held 12 o'clock position directly over the air gap created by the horizontal cylindrical holding tube, was heat treated by exposure to the toaster oven type filament heater as that described in the Comparative Example III. The temperature of the seam area was raised very quickly to 90°C, 8°C above the Tg of the charge transport layer, in about 2 seconds observed with an infrared sensing camera.. Quick seam area cooling down to room ambient temperature was noted in about 6 seconds after removal of the heat source from the belt assembly. With this invention heat treatment procedure, the entire cycle of seam stress release process was accomplished in just about only 8 seconds. The resulting treated seam area did not exhibit a seam area set like that observed in the prior art seam treatment process demonstrated in Comparative Example III. EXAMPLE V The control electrophotographic imaging member belt, the prior art electrophotographic imaging member belt, and the electrophotographic imaging member belts of the present invention as exemplified by Example II, Comparative Example III, and Example IV, respectively, were each dynamically cycled and print tested in a xerographic machine, having a belt support module comprising a 25.24 mm diameter drive roller, a 25.24 mm diameter stripper roller, and a 29.48 mm diameter tension roller to exert a belt tension of 1.1 pounds per inch. The belt cycling speed was set at 65 prints per minute. The control non-heat treated belt of Example II was cyclic tested to only about 56,000 prints because the testing had to be terminated due to premature seam cracklng/delamination problems. Although the prior art belt of Comparative Example III, with a 6.25 centimeters wide heat treated seam, area cycled to 300,000 prints without exhibiting any evidence of seam failure, the appearance of ripples was observed, the ripples having a 500 micrometers peak-to-peak height and a periodicity of about 35 mm in the imaging zones adjacent to the seam heat treatment area after only 40 prints. These ripples caused copy print-out defects during xerographic imaging. Moreover, the large set in the seam heat treat area formed a 0.5 mm surface hump that interacted with a cleaning blade operation thereby impacting the cleaning efficiency of the blade. When measured for dimensional integrity, the seam heat treatment process of Comparative Example III was found to cause a 0.057 percent circumferential belt shrinkage. When the same belt cycling procedure is repeated with the imaging member belt of Example IV of the present invention, no seam failure was observed up to 300,000 prints. However, in an apparent contrast to the prior art seam heat treatment, the seam stress release heat treatment process of the present invention did not exhibit a belt seam area surface protrusion caused by any set. Moreover, the belt of this invention had no notable ripple appearance in the image zones. Further, the belt of this invention exhibited nil belt treatment induced belt circumference shrinkage. In summary, the seam heat stress release process of the present invention resolves seam cracking/delamination problems, provides a very short treatment processing cycle time to synchronize with the current imaging member belt production ultrasonic seam welding operation, avoids seam area heat induced set problems, prevents the appearance of ripples in the imaging zones adjacent to the seam heat treatment area, and produces a dimensionally stable imaging member belt. These results demonstrate clear advantage of the process of this invention over those used by the prior art seam heat treatment processes.

Claims: A process for treating a seamed flexible electrostatographic imaging belt (10) comprising providing an imaging belt comprising at least one imaging layer comprising a thermoplastic polymer matrix and a seam (30) extending from one edge of the belt to the other, the seam having a region on the belt adjacent each side of the seam and also having an exposed surface on each side of the belt, characterized by supporting the belt with at least one vacuum holding device (100) spaced from the seam while maintaining the seam and region of the belt adjacent each side of the seam in an arcuate shape having at least a substantially semicircular cross section having a radius of curvature of between about 9.5 millimeters and about 50 millimeters, heating the thermoplastic polymer matrix of the imaging layer in the seam and the region of the belt adjacent each side of the seam to at least the glass transition temperature Tg of the thermoplastic polymer matrix without significantly heating the support member, and contacting the exposed surface of the seam and regions on each side of the belt with a gas to rapidly cool the seam and regions on each side of the belt to a temperature below the glass transition temperature of the polymer matrix while maintaining the arcuate shape of the region of the belt adjacent each side of the seam. A process according to claim 1 including substantially instantaneously heating the thermoplastic polymer matrix in the seam (30) and the region of the belt (10) adjacent each side of the seam to a temperature between the glass transition temperature of the polymer matrix and a temperature about 25° greater than the glass transition temperature of the polymer matrix. A process according to claim 1 wherein the electrostatographic imaging belt is an electrophotographic imaging belt comprising a charge generating layer (18) and a charge transport layer (16) and the layer comprising the thermoplastic polymer matrix is the charge transport layer. A process according to claim 3 wherein the thermoplastic polymer matrix in the charge transport layer (16) is polycarbonate resin containing dissolved or molecularly dispersed small charge transport molecules. A process according to claim 1 wherein the electrostatographic imaging belt (10) is an electrographic imaging belt comprising a supporting substrate layer (26) and a dielectric imaging layer, the dielectric imaging layer comprising the thermoplastic polymer matrix. A process according to claim 1 wherein the electrostatographic imaging belt is an intermediate transfer belt comprising a supporting substrate layer (26) and an imaging layer, the imaging layer comprising the thermoplastic polymer matrix. Apparatus for treating an electrostatographic imaging belt (10) comprising at least one imaging layer comprising a thermoplastic polymer matrix and a seam (30) extending from one edge of the belt to the other, the seam having a region (68, 70) on the belt adjacent each side of the seam and also having an exposed major surface (12, 14) on each side of the belt, characterized by comprising at least one vacuum holding device (100) which, in use, is spaced from the seam for maintaining the seam and region of the belt adjacent each side of the seam in an arcuate shape having at least a substantially semicircular cross section having a radius of curvature of between about 9.5 millimeters and about 50 millimeters, and a heating device (122, 124) adjacent to and spaced from the vacuum holding device and adapted to heat the thermoplastic polymer matrix in the seam and the region of the belt adjacent each side of the seam to at least the glass transition temperature Tg of the polymer matrix without significantly heating the supporting vacuum holding device (100). Apparatus according to claim 7 including at least two of the vacuum holding devices (114, 116). Apparatus according to claim 8 wherein one of the two vacuum support members (128, 130) supports the belt below one side of the seam and the other vacuum support member supports the belt below the other side of the seam. Apparatus according to claim 7 including a belt alignment device (104) to position the seam of the belt at a predetermined location.

Inventors: GRABOWSKI EDWARD F, HORGAN ANTHONY M, HSIEH BING R, MISHRA SATCHIDANAND, POST RICHARD L, VON HOENE DONALD C, YU ROBERT C U, GRABOWSKI, EDWARD F., HORGAN, ANTHONY M., HSIEH, BING R., MISHRA, SATCHIDANAND, POST, RICHARD L., VON HOENE, DONALD C., YU, ROBERT C. U.
Applicants: XEROX CORP, XEROX CORPORATION
Application year: 1999
Main classification: G03G5
IPC codes: B32B1, G03G21, G03G15, F16G3, G03G5