Gas spring

Abstract: A gas spring which provides two stages of resistance to axial movement, by a first head (20) and rod (16) slidably disposed within a second rod (18) with a head (22), with both of the heads subjected to pressurized gas in a common chamber (14) within the cylinder (12). Preferably, a seal (46,77) for each provides sealing engagement when the force of pressurized gas acts upon the seal. Hence, the seal provides sealing engagement without being axially compressed and radially expanded. The seal may be used in single stage and two stage gas springs. Desirably, a positive stop (96,102) for each rod is provided, preferably as a part of the housing (42,44,74,76) for its bearings and seal. Preferably, the seal (46,77) is a flexible annular sealing element which when viewed in cross section is generally a C-shape, with arms constructed and arranged so that the free edges of the seal are biased into sealing engagement by pressurized gas acting on the arms.

Description: This invention relates to a gas spring device according to the preamble of claim 1. A gas spring of that kind (FR-A-2 579 282) has a cylinder and a housing means connected together, the latter enclosing two lip seals of generally C-shaped cross-section with a space between the lip seals which is filled with oil. The lip seals open toward the cylinder, so that the pressure of the gas in the cylinder and the oil in the space, respectively, press the lips against the adjacent walls. This design has the drawback of relative high costs and is bulky. In a gas spring known from (US-A 4,792,128), the bearing and seal assembly comprises housing means composed of front and rear parts, the front part is stationary and the rear part is slidably received in the front housing part, with the gasket or seal therebetween. In use, the seal is compressed axially, so that it expands radially inward into firm sealing engagement with the rod by the force produced by pressurized gas in the chamber acting on the rear housing part. The movement of the housing part causes wear on adjacent parts and wear of the housing itself. A positive stop in the cylinder prevents the head from striking and damaging the bearing and seal assembly. US-A 4,838,527 shows a gas spring which can be operated with either an external source of gas or as a precharged and self-contained unit by changing first and second valves assemblies either of which can be installed in the same cavity in the cylinder. Gas springs are utilized typically to yieldingly resist movement of a body such as a clamping ring for a metal blank in a die in a press for forming sheet metal parts. Such gas springs are charged at a predetermined pressure, such as 13,79 MPa (2000 PSI). The rod can yieldably move toward its retracted position when the force applied externally to the rod exceeds the force produced thereon by the gas in the chamber. When the rod and head are forced into the chamber, the gas therein is compressed to a maximum operating pressure which is usually in the range of about 20,69 MPa to 34,48 MPa (3000 to 5000 PSI), depending on the volume of the chamber and the effective area and stroke of the rod and piston. These gas springs require a substantial force to begin moving their rods toward their retracted positions. This force is often so substantial that a mechanical crankshaft type press may have difficulty producing sufficient force to retract the rod. This may occur because the press produces relatively little force at the beginning of its stroke and most of its force near the very end of its stroke. With conventional presses and dies relatively little force need be applied to the clamping ring during the initial portion of the press stroke and a much greater force is required near the end of the press stroke. Excessive forces cause excessive wear on the crank, crank bearings and die parts. Thus, the desired force across stroke curve for press operations is opposite to that produced by gas springs having a single rod. Gas springs with telescoping pistons and rods are already known (DE-A 28 16 761) and comprise three or more gas pressure cavities connected to one another through damping bores. The total stroke length of the gas spring is increased by the telescope construction. These gas springs do not lend themselves for the use referred-to above. A sealing element as used in the invention is already known from US-A 4,508,356. The invention is defined by claim 1. The seal used in the gas spring of invention is a flexible annular sealing element which when viewed in cross section is generally C-shaped, with arm constructed and arranged, so that the free edges thereof optionally flex and extend when the seal is deformed by pressurized gas. The lip or edge provides additional sealing surface area in contact with an adjacent surface to provide improved sealing. The seal may be used in single stage and two stage gas springs. Desirably, a positive stop for each rod is provided, preferably as a part of the housing for its bearings and seal. The two stage embodiment provides two stages of resistance to axial movement, by an inner head and rod slidably disposed within an outer rod with a head, with both of the heads subjected to pressurized gas in a common chamber within the cylinder. The gas spring device will have improved rod sealing characteristics, will be improved in service useful life, and is durable, reliable, of relatively simple design and economical manufacture and assembly. In the two stage embodiment, the gas spring device will provide a substantially lesser force at the beginning of its stroke in relation to the force at the end of its stroke, and significantly decreases the tendency to slow down or stall a press. These and other objects, features and advantages of this invention will be apparent from the following detailed description, appended claims and accompanying drawings in which: Fig. 1 is a sectional view of a two stage gas spring embodying this invention. Fig. 2 is an enlarged view of the encircled portion of Fig. 1 showing a seal in its relaxed state. Fig. 3 is an enlarged view of the encircled portion of Fig. 1 showing a seal in its extended state. Fig. 4 is a force vs. displacement curve of the two stage gas spring. Fig. 5 is a sectional view of a single stage gas spring embodying this invention. Fig. 1 illustrates a two-stage gas spring 10 embodying this invention. This gas spring 10 has a cylinder 12 defining at least in part a gas chamber 14 in which an inner and outer rod 16 and 18 with head 20, 20 are telescopically received. To provide a spring or cushion, the rods 16, 18 are yieldably urged to their extended positions by pressurized gas in the chamber 14 which acts on the piston cross section of the rods 16, 18. When a force is applied externally to the rods 16, 18, such as through a die plate, which force is greater than the force produced on the rod or rods by the gas in the chamber, initially the inner rod 16 and then subsequently both rods 16, 18 in unison are yieldably moved toward their retracted positions. Preferably, the cylinder 12 has a separate tube 24 and an end cap 26 permanently fixed to the tube by a circumferentially continuous seam weld. A filler and bleed poppet valve assembly 28 is preferably removably received in a valve cavity 30 in the cap 26 and communicates with the chamber 14 through a passage 32. The inner rod 16 is slidably received in a bearing and seal assembly 34 disposed in a bore 36 through the outer rod 18 and releasably therein by ring segments 38 received in a groove 40 in the bore 36. This assembly has a front housing 42 slidably received preferably with an interference fit in a rear housing 44 with a rod seal 46 received between them in a counterbore 48 in the rear housing 44. The clearance between the bore 36 of outer rod 18 and the rear housing 44 is sealed by an O-ring 52 and back-up ring 53 received in a groove 54 therein.The rod 16 is slidably received in bearings 56, 57 received in counterbores 58 in the front and rear housings 42, 44. To prevent contaminants entering the assembly 34, preferably a rod scraper 60 encircles the rod 16 and is received in a recess 62 in the front housing 42, and a dust cap 64 overlies the assembly 34 and is received and frictionally retained in the end 66 of the second rod 18. Similarly, the outer rod 18 is slidably received in a bearing and seal assembly 68 disposed in the tube 24 of the cylinder 12 and releasably retained therein by ring segments 70 received in a groove 72 in the tube 24. This assembly has a front housing 74 slidably received preferably with an interference fit in a rear housing 76 with a rod seal 77 received between them in a counterbore 78 in the rear housing 76. The clearance between the tube 24 and the rear housing 76 is sealed by an O-ring 80 and a back-up ring 81 received in a groove 82 therein. The outer rod 18 is slidably received in bearings 84, 85 which are received in counterbores 86 in the front and rear housings 74, 76. Preferably, to prevent contamination of the assembly 68, a rod scraper 89 is received in a recess 90 in the front housing 74 and a dust cap 92 overlies the bearing assembly 68 and is received and frictionally retained in the end 94 of the tube 24. The bearings 58, 84 are of a suitable material such as sintered bronze. To insure adequate lubrication of the bearings 56, 57, 84, 85, and particularly the rear bearings, they are impregnated with lubricant and a small quantity of a synthetic high temperature lubricating oil is also disposed in the chamber 14. To provide a longer life in service, relatively little clearance is provided between each rod 16, 18 and its bearings 58, 84. This clearance is usually about 0,05 to 0,1 mm (0.002 to 0.004 of an inch) per side or a total clearance of 0,1 to 0,2 mm (0.004 to 0.008 of an inch) between the diameters of each rod and its associated bearings. To achieve these close tolerances, preferably the bearings are sized after being pressed into their housings. Movement of the inner rod 16 to its extended position is limited by a positive stop 96 provided by cooperation of an end face 98 of the rear housing 44 with a complementary shoulder 100 on the head 20 of the inner rod 16. Movement of the outer rod 18 to its extended position is limited by a positive stop 102 provided by engagement of a conical surface 104 on the back face 106 of the rear housing 76 with a complementary surface on the head 22 of the outer rod 18. While the rod seals 46, 77 differ in diameter, preferably they have essentially the same construction and arrangement. The seals 46, 77 comprise a flexible annular sealing element or ring 110, which is circumferentially continuous and as shown in Fig. 2, in a relaxed or unflexed state, has in cross section a generally C-shape with side walls or arms 112, the central portions of which are urged into contact with their adjacent rod and housing surfaces by a circumferentially continuous metal spring element 114 received in the ring 110. Preferably, the ring 110 is made of a low friction and highly wear resistant elastomeric material such as an ultra high molecular weight polyethylene. Preferably, the arms 112 have generally right angular surfaces defining a sharp peripheral edge or lip 116. In assembly, when pressurized gas is admitted to the chamber 14, as shown in Fig. 3, the arms 112 are extended and forced along with the lips 116 into firm sealing engagement with the adjacent surfaces of the rods 16, 18 and housings 44, 76. The pressurized gas forces the ring 110 to engage with and conform to the peripheral surfaces of the cavity in which it is received. It has been found that further improved sealing performance and a significantly decreased tendency for the seal to cock or turn in the groove and thereby leak can be achieved if the outer wall or arm 118 of the ring 110 is substantially thicker than its inner wall or arm 120. Preferably, as illustrated in the drawings, the radial thickness of the outer wall 118 is about 110% to 250% times the radial thickness of the inner wall 120. The interior of each seal 46, 77 continuously communicates with the chamber 14 through one or more passages 123, which are preferably formed by interconnected grooves 124, 125, 126 in the rear bearings 56, 84 which have end faces 127, 128, and inner and outer surfaces 129, 130 (see Fig. 5). Grooves 125, 126 extend radially across the opposed end faces 127, 128 of each rear bearing 56, 84 and are interconnected by groove 124 extending axially across the outer peripheral surface 130 of each bearing 56, 84. Preferably, there are two or three sets of these grooves 124, 125, 126 circumferentially spaced about each bearing 56, 84. To prevent each rear bearing 56, 84 from being moved axially in its rear housing 44, 76 into the seal 46, 77 which might well damage it, these passages 123 also substantially equalize the pressure of gas acting on the opposed end faces 127, 128 of each bearing 56, 84. During charging and use of the gas cylinder 12, there are substantial gas pressure spikes or variations which without these passages 123 would produce a substantial difference in the pressure of the gas acting on opposed end faces 127, 128 of the bearings 56, 84 which would move or shift the bearings 56, 84 axially in their housings 44, 76. This bearing, seal and housing construction permits and facilitates the use of close tolerances and even interference fits between the bearings and housing members. The housing member is not required to move axially to compress and radially expand the seal. Elimination of this movement and use of close tolerances substantially reduces wear on the component parts and greatly extends the useful service life of the gas spring. Moreover, these close tolerances in conjunction with lubrication of the parts further enhances sealing and minimizes leakage of pressurized gas from the chamber. In use, the chamber is precharged with a compressed gas, such as nitrogen, to a relatively high internal pressure such as 13,79 MPa (2000 PSI). As shown in the force versus displacement curve in Fig. 4, a relatively small force is required to initially retract the inner rod 16 and this force increases only modestly as the inner rod 16 is retracted, such as by advancement of the die plate, until the plate also bears on the outer rod 18. This relatively low force for displacement of the inner rod 16 is due to the relatively small area of its cross section and the fact that the movement of the inner rod 16 and head 20 only moderately compresses the gas in the chamber 14 and thereby only moderately increases the force required to continue to move the rod 16 toward its retracted position. However, as indicated in Fig. 4, when the plate bears on the outer rod 18, the total force required to simultaneously displace both rods 16, 18 increase substantially and the total force required to continue to move both rods toward their fully retracted positions increases rapidly. The increase in force required to initiate retraction of the outer rod 18 is due to the gas in the chamber 14 acting on the total cross sectional area of both rods and assembly 34 and the rapid increase of the force required to continue moving both rods 16, 18 toward their fully retracted positions is due to compression of the gas in the cylinder 12 by both heads 20, 22 and rods 16, 18 which rapidly increases its pressure and thus the force it exerts on both rods. Fig. 5 illustrates a modified one-stage gas spring 134 with a single rod 136 and a seal 138. This gas spring 134 illustrates application of the seal 138 and bearing and seal assembly 140 to gas springs having a single rod 136 and head 142. In testing gas springs embodying this invention, and particularly two-rod springs, they have been found to operate at a substantially lower temperature and with substantially less wear on the rod. Indeed, two-rod gas springs embodying this invention have been tested for more than 1,000,000 substantially continuous cycles without any detected wear. In contrast, prior gas springs have failed after as few as 5,000 continuous cycles. In these two-rod gas springs, the inner rod was moved toward its retracted position from 0 to 7,6 cm (0 to 3") by application of a force to its free end which increased generally linearly from about 2744,6 N to 3073,7 N (617 lbs. to 691 lbs.) and then both rods were moved simultaneously and additional 2,54 cm (1") by application of a force to their free end which increased linearly from about 27,17 kN to 43,67 kN (6108 lbs. to 9816 lbs.). In contrast, in comparably sized springs with a cylinder of the same diameter and length and a single rod and head like that of Fig. 5, the rod moved towards its retracted position from 0 to 10,16 cm (0 to 4") by application of a force to its free end which increased generally linearly from 27,17 kN to 43,23 kN (6108 lbs. to 9719 lbs.).

Claims: A gas spring device comprising a cylinder (12) having a hollow for a gas chamber (14), at least a first rod (18; 136) having a head (22; 142) and being telescopically received in said cylinder, at least a first bearing and seal assembly (68; 140) for journalling said rod (18; 136) and sealing said gas chamber (14) which, in the operating condition of the gas spring, is filled by pressure gas, said bearing and seal assembly (68; 140) being in sealing engagement with said rod (18; 136) and including said housing means (74, 76), said housing means (74, 76) defining recess means (86) to receive seal means (77; 138), said seal means (77; 138) comprising a flexible annular sealing element (110) of a generally C-shaped cross section defining side walls or arms (112) with free edges (116), onto which the gas pressure in the gas chamber (14) acts, characterized in that there is only one sealing element (110) for said first rod (18, 136), that the sealing element (110) has a metal spring element (114) of a generally C-shaped cross section included in the annular hollow of the sealing element (110) such that the generally C-shaped surface of the hollow is in corresponding contact with the outer surface of said generally C-shaped metal spring element (110) to urge the central portions of the side walls or arms (112) into engagement with the rod (18; 136) and the housing means (74, 76), respectively, that said sealing element (110) has a relaxed state when said gas chamber (14) is not filled with pressure gas, and in said relaxed state leaves two radially spaced apart outer annular hollows adjacent to the corners of said recess (86) which are arranged in outward moving direction of the rod, said outer annular hollows disappearing caused by deformation of the sealing element (110) when said sealing element (110) being under gas pressure from its inner hollow, and that the housing means (74, 76) is arranged and retained within the cylinder (12). The gas spring device of claim 1 wherein said free edges (116) of said arms (112), in said relaxed state of the sealing element (110), are clear off the rod (18) and housing means (76), respectively, and, in said state under gas pressure, flex and extend toward the rod (18) and housing means (76), respectively, caused by said deformation of the sealing element (110). The gas spring device of claim 1 or 2 wherein said bearing and seal assembly (68; 140) includes a first bearing (84) disposed in a recess (86) in said housing means (74, 76) upstream of said sealing element (77; 138) and in engagement with said rod (18; 136) so as to journal same, said bearing (84) and said recess (86) defining passage means (124, 125, 126) which continuously communicates with said gas chamber (14) and said sealing element (77; 138). The gas spring device of claim 3 wherein said bearing (84) has inner and outer surfaces (129, 130), and first and second end faces (127, 128) and wherein said passage means comprises an axial groove (124) which extends generally axially along said outer surface (130) from the first end face (127) to the second end face (128) and a radial groove (125) which extends radially along said first end face (127) from said inner surface (129) to said axial groove (124) of said outer surface (130) and a radial groove (126) which extends radially along said second end face (128) from said inner surface (129) to said axial groove (124) of said outer surface (130) thereby the difference in gas pressure at said first and second end faces (127 128) of said bearing (84) is minimized. The gas spring device of any of claims 1 to 4 wherein said head (22; 142) has a surface (102) engageable with a surface (104) on said housing means (74, 76) to provide a positive stop limiting the extent to which said rod (18; 136) can be axially extended relative to said cylinder (12). The gas spring device of any of claims 1 to 5 wherein said side walls or arms (112) of said sealing element (110) include an outer arm (118) and an inner arm (120), said outer arm (118) of said sealing element (77; 138) engageable with said housing means has a radial thickness at least about 110 % of the radial thickness of said inner arm (120) of said sealing element engageable with said rod (18; 136). The gas spring device of claim 6 wherein said outer arm (118) has a radial thickness about 110 to 250 % of the radial thickness of said inner arm (120). The gas spring device of any of claims 1 to 7 wherein said housing means (74, 76) includes a front housing (74) and a rear housing (76), each comprising a bearing (84, 85) for the rod (18; 136), the front housing (74) being received by the rear housing (76) with an interference fit. The gas spring device according to any of claims 1 to 8 further comprising a second rod (16) with a second head (20), a bore (36) through said first rod (18), said second rod (16) telescopically received in said first rod (18), and a second bearing and seal assembly (34) for journalling said second rod (16) and sealing said gas chamber (14). The gas spring device of claim 9 wherein said second bearing and seal assembly (34) comprises a second sealing element (46) corresponding to the first sealing element (77; 138) as to construction and second housing means (42, 44).

Inventors: HOLLEY DAVID M, HOLLEY, DAVID M.
Applicants: POWER COMPONENTS INC, POWER COMPONENTS, INC.
Application year: 1991
Main classification: F16F9
IPC codes: F16J15, F16F9, B30B15