Abstract:
A combustor extension for a heat gun where the heat gun has a jet pump for mixing pressurized fuel with air to form an air/fuel mixture and a combustor attachment for combusting the air/fuel mixture. The jet pump has a first electrical connector for providing an electrical charge to an ignition device at the combustor attachment for igniting the air/fuel mixture. The combustor extension includes a hollow conduit having proximal and distal ends for extending between and coupling the combustor attachment to the jet pump. A second electrical connector at the proximal end of the conduit electrically couples to the first electrical connector of the jet pump. A third electrical connector at the distal end of the conduit electrically couples to the ignition device of the combustor attachment. The second and third electrical connectors are electrically connected together.

Description:
RELATED APPLICATION 
     This application is a continuation-in-Part of U.S. Ser. No. 08/966,293 filed Nov. 7, 1997 now U.S. Pat. No. 6,010,329, which claims the benefit of U.S. Provisional Application No. 60/030,770 filed on Nov. 8, 1996, the entire teachings of which are incorporated herein by reference. 
    
    
     BACKGROUND OF THE INVENTION 
     The effectiveness of heat guns is predicated upon the ability of the combustion products to entrain and propel vast amounts of the surrounding air. Two factors have been found to enhance this process: 1) The speed of the combustion products to be as high as possible and 2) the combustor outlet to be in the shape of a slot in order to maximize the gas/air interface and create a fan shaped heat output pattern. 
     The speed of the combustion products is a function of the pressure recovery of the jet pump which is used to aspirate the combustion air by the expansion of the gaseous fuel. The performance of the jet pump is thus linked directly with the effectiveness of the heat gun. 
     One measure to improve the performance of prior art jet pumps has been to lengthen the diffusor to achieve maximum pressure recovery. One drawback of pushing the diffusor to its limits is the attendant tendency for flow separation and pressure fluctuation. The periodic flow separation occurs spontaneously, even in a perfectly draft-free room, but are exacerbated by any disturbance: by moving the heat gun about, by air drafts and even by sound. The result is an uneven flow, noisy combustion, bad emissions and performance fluctuations. 
     Another measure to improve the performance of prior art jet pumps has been to use multiple nozzles in place of a single nozzle. These efforts have aimed to arrange the nozzles to shorten the mixing process and minimize friction losses in the mixing duct of the jet pump. 
     The fan shaped pattern has the advantage of spreading the heat evenly over a wide area. The heated area is a long, narrow zone in line with the combustor slot which the operator sweeps over the object to cover the whole area. 
     The orientation of the slot relative to the handle of the heat gun is usually a matter of personal preference but in some instances also of practical significance. When shrinking a plastic bag over a pallet for instance, it is important to first shrink the bottom of the bag all around to prevent it from riding up. A horizontal orientation of the slot is most efficient for this operation. Subsequently, when shrinking the sides of the bag, a vertical orientation is more effective. Thus it is desirable to change the orientation of the slot easily and quickly. 
     One commercially available heat gun employs a screw with a wing head to fasten the cylindrical combustor inlet to the body of the heat gun so that the operator can adjust its orientation without tools. This arrangement however is awkward in practice since the mounting screw has to be loosened and tightened every time the slot orientation is changed. If the operator neglects to tighten the screw, he runs the risk of losing it. 
     Another need that arises in practice is to extend the length of the heat gun to heat objects which are out of reach. This situation occurs for instance when shrink wrapping tall pallet loads or big boats. In the past this has been accomplished by extension tubes. The extension tube ducts the combustible mixture from the jet pump to the combustor as well as providing an electrical lead and ground from the ignitor to the spark plug. The installation is particularly cumbersome. First the fasteners holding the combustor have to be removed, the spark plug lead disconnected and the combustor taken off. Then the process has to be repeated twice in the reverse order, once to attach the extension to the gun, and again to mount the combustor to the extension. Disassembly is an equally complicated process. An added problem arises in keeping the second set of fasteners from getting lost. 
     A serious ignition problem arises with the extension if the ignition lead is carried inside the extension tube. After operating the gun a few times the spark grows progressively weaker until it is unable to light off the gun. The only solution to this problem in the past has been to mount the ignition lead outside the extension tube. This arrangement is costly and makes the ignition lead vulnerable to damage in use. 
     SUMMARY OF THE INVENTION 
     The present invention is directed to a jet pump for a heat gun including an elongate hollow pump body lying along a longitudinal axis. The pump body has an inlet, a mixing section and an outlet. A nozzle unit is axially aligned with the inlet for directing pressurized fuel into the inlet of the pump body. Movement of the pressurized fuel into the inlet causes air to be drawn into the inlet to mix with the fuel within the pump body. A disk shaped air diverter is axially spaced away from the inlet of the pump body. The diverter has a length and a diameter. The diameter of the diverter is greater than the length of the diverter and larger than the inlet of the pump body. A housing is radially spaced from and surrounds the diverter forming a first annular gap therearound for air outside the housing to pass therethrough. The air moves around the diverter then changes direction between the diverter and the inlet of the pump body before entering the inlet. 
     In preferred embodiments, the nozzle unit is mounted to the diverter. The jet pump housing is radially spaced from and surrounds the pump body forming a second annular gap between the housing and the pump body. The housing includes an opening positioned radially relative to the pump body such that air outside the housing can enter through the opening and pass through the second annular gap to enter the pump body inlet. The diverter is preferably axially spaced from the pump body about 0.5 inches. The ratio of the diverter diameter to the inlet diameter is about 4 and the ratio of the diverter diameter to its length is about 2. 
     The nozzle unit preferably includes a series of elongate nozzle tubes arranged in a circle. The nozzle tubes extend into the inlet of the pump body and are angled radially outwardly for directing the pressurized fuel towards the walls of the pump body. The tip portions are preferably positioned along a circle having a diameter of about 0.28 inches and are at an 12° angle relative to each other. The nozzle tubes each have a stem portion with a first diameter and a first wall thickness. Each nozzle tube also has a tip portion with a second diameter and a second wall thickness. The second diameter at the tip portion is smaller than the first diameter of the stem portion with the ratio of the first diameter to the second diameter being about 1.6. The wall thickness at the tip portion is less than the wall thickness of the stem portion. The wall thickness at the tip portion is preferably about 0.003 inches and the wall thickness at the stem portion is preferably about 0.005 inches. The nozzle tubes are about 0.437 inches long with the tip portion being about 0.06 inches long. 
     The present invention further includes a combustor system including a first spring loaded button protruding radially from the pump body. A combustor attachment combusts an air/fuel mixture received from the outlet of the pump body. The combustor attachment is capable of being releasably coupled to the pump body and has an ignition device for igniting the air/fuel mixture. The combustor attachment has a first hole capable of engaging the first spring loaded button for locking the combustor attachment to the pump body in a first position. The combustor attachment also has a second hole capable of engaging the first spring loaded button for locking the combustor attachment to the pump body in a second position. The combustor system has a first electrical connector positioned in the pump body outlet for providing an electrical charge to the ignition device. The combustor system preferably includes a hollow extension piece having proximal and distal ends capable of being positioned between the pump body and the combustor attachment. The extension piece includes a second electrical connector at the proximal end for engaging the first electrical connector and a third electrical connector at the distal end for engaging the ignition device of the combustor attachment. The second and third electrical connectors are electrically connected together by an electrical conductor. The extension piece includes a proximal hole at the proximal end capable of engaging the first spring loaded button for locking the extension piece to the pump body. The extension piece also has a second spring loaded button at the distal end capable of engaging one of the first and second holes of the combustor attachment for locking the combustor attachment to the extension piece. In one preferred embodiment, the extension piece is telescoping allowing the combustor attachment to be extended or retracted without turning off the jet pump. 
     The present invention provides a jet pump for a heat gun having a high overall output pressure and a short length that promotes complete smooth quiet combustion that can be easily muffled. The combustor attachment permits quick rotation and removal without the use of tools. The extension piece includes an internal ignition lead that maintains electrical contact regardless of the orientation of the combustor attachment. Hydraulic sealing is made at the same time that the electrical connection is made. More than one extension piece can be used in series between the pump body and the combustor attachment. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     The foregoing and other objects, features and advantages of the invention will be apparent from the following more particular description of preferred embodiments of the invention, as illustrated in the accompanying drawings in which like reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the invention. 
     FIG. 1 is a side sectional view of a preferred embodiment of the present heat gun invention. 
     FIG. 2A is a frontal view of the heat gun with the combustor slot in a vertical orientation. 
     FIG. 2B is a frontal view of the heat gun with the combustor slot rotated to a horizontal orientation. 
     FIG. 3 is a vertical cross-section of the nozzle assembly. 
     FIG. 4 is a front view of the nozzle assembly. 
     FIG. 5 is an enlarged side sectional view of an individual nozzle. 
     FIG. 6 is an enlarged side sectional view of the inlet structure of the heat gun. 
     FIG. 7 is an end view of the inlet of the heat gun. 
     FIG. 8 is a side sectional view of another preferred inlet structure. 
     FIG. 9 is an end view of the inlet of FIG.  8 . 
     FIG. 10 is an exploded view of the socket assembly. 
     FIG. 11 is an exploded view of the combustor mounting flange and the combustor. 
     FIG. 12 is a perspective exploded view of the combustor mounting flange and combustor with the internal electrical socket assembly in cross section. 
     FIG. 13A is a side sectional view of the heat gun showing the removal of the combustor. 
     FIG. 13B is a side sectional view of the heat gun showing the insertion of a combustor extension. 
     FIG. 14 is a perspective sectional view of the combustor extension with the locking button in exploded view. 
     FIG. 15A is a side sectional view of the ignitor before firing. 
     FIG. 15B is a side sectional view of the ignitor after firing. 
     FIG. 15C is an enlarged side sectional view of the ignitor after firing showing the ground clip. 
     FIG. 16A is a side sectional view of another preferred combustor extension in the extended position. 
     FIG. 16B is a side sectional view of the combustor extension of FIG. 16A in the contracted position. 
     FIG. 17 is a perspective view of the sliding joint of that combustor extension with a portion in section. 
     FIG. 18 is a performance graph of the present heat gun invention in comparison with a heat gun having a single nozzle jet pump. 
     FIG. 19 is a performance graph of the present heat gun invention as a function of the spread angle of the nozzle tubes. 
     FIG. 20 is a performance graph of the present heat gun invention as a function of the length of the nozzle tubes. 
     FIG. 21 is a graph showing the fluctuation of Output Pressure vs. Time of the present invention compared to prior art heat guns. 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     FIG. 1 shows a cross-sectional view of a heat gun of the present invention. The heat gun comprises a handle  21  which houses a valve  22 , an ignitor  23  and a trigger  24 . A fuel line  25  leads from the handle  21  to the jet pump nozzle  26 . The nozzle  26  is mounted on a flow diverter  30  which is supported by outer struts  31  inside a housing  33  with a rear air inlet  34  and several additional air inlets  35  further forward. Housing  33  also supports a pump body  36 . Internally, the pump body  36  contains a bell mouth inlet  37 , a cylindrical mixing section  40  and an expanding diffuser  41 . A combustor  43  with a flame holder  47  and a spark plug  48  is mounted on a flange  42  of the jet pump  36 . 
     One principal part of the present invention is the construction of the nozzle  26  consisting of multiple nozzle tubes  28  arranged in a circular array diverging from the central axis. This is shown in greater detail in FIGS. 3,  4  and  5 . 
     FIG. 6 shows the preferred placement of the nozzle  26  relative to the bell mouthed entry  37  to the mixing section  40 . The nozzle tubes  28  protrude into the gap l 2  between the flow diverter  30  and the bell mouthed entry  37 . 
     FIG. 7 shows how the nozzle  26  is mounted concentrically relative to the pump body  36  inside the housing  33  by the struts  32 . 
     FIG. 3 shows the divergent angle g of the nozzle tubes  28 . The divergent angle can be varied if the diameter D 4  remains constant. 
     FIG. 4 show a preferred embodiment utilizing an array of  6  nozzle tubes  28 . There are preferably six nozzle tubes  28  but alternatively, more than six or less than six nozzle tubes  28  can be employed. 
     FIG. 5 shows how the nozzle tubes  28  taper down to a smaller diameter D 6  and terminate in a short straight section of length l 8 . The wall thickness w 1 , also tapers down to a thinner wall thickness w 2  at the nozzle outlet. 
     Another principal part of the present invention is the flow diverter  30 . The structure surrounding the flow diverter  30  is shown in greater detail in FIGS. 6 and 7. The flow diverter  30  is cylindrical or disk shaped and is placed in close proximity with the bell shaped jet pump inlet  37 . The outer edges of the flow diverter  30  at the entry to the annular flow passage between it and the housing  33  are rounded as shown by the dimension r 1 . Similarly, the inner edge at the entry into the radial flow passage between the flow diverter  30  and the pump body  36  are rounded as shown by the dimension r 2 . 
     The flow diverter  30  is shown in another preferred embodiment of the present invention in cross-sectional view in FIG. 8, an end view in FIG.  9 . The jet pump inlet is enlarged to form a cylindrical section  38 . The flow diverter  30  is supported by struts  31  inside the cylindrical section  38 . Also shown in this embodiment is a closed cell foam lining  39  on the inside of the cylindrical section  38  for silencing the noise emanating from the nozzle. 
     The quick connect feature of the combustor can be seen in FIGS. 10,  11  and  12 . FIG. 10 shows a socket  59  made of an insulating material such as plastic. It contains a metallic contact spring  66  which is located in the center of the socket body  62  by a axial screw  65  in communication with a cross bore  63 . Cross bore  63  is recessed to receive a O-ring seal  67 . 
     FIG. 11 shows the combustor mounting flange  42  of the pump body  36  with two O-rings  50 . The flange  42  has a cavity  54  in which a button  51  and spring  56  are retained by a bracket  55  with an aperture  52  through which the head of the button can move but through which the button flange  53  cannot pass. The bracket  55  is held in place by two diametrically opposed bosses  58  and the locating holes  57 . 
     The combustor attachment  43  has a beveled edge  45  and a cylindrical section  44  which mates with the O-rings  50 . It also has two locating holes  49  placed at 90 degrees to each other to mate with the button  51 . 
     The working parts which establish the electrical connection are shown in detail in FIG.  12 . The insulated ignition cable  64  feeds into the cross bore  63  of the insulated socket  59 . Screw  65  pierces the cable and holds it in place while simultaneously establishing contact with the spring  66 . Spring  66  mates with spark plug  48  located in the axis of the cylindrical combustor section  44  by a flame holder  47 . 
     FIGS. 13B and 14 show the construction of an extension tube  69 . At its inlet end the extension tube  69  is fashioned like the cylindrical section  44  of the combustor  43 , with a beveled edge  71  and locating holes  72 . The extension ignition lead  74  is located on the axis by the insulated plug holder  73  in position to mate with the socket  59  and contact spring  66 . At its outlet end the extension tube  69  terminates in a mounting flange similar to the mounting flange  42  with O-rings  50 , button  51  and socket  59  with contact spring  66  and screw  65 . One difference in construction is that the extension ignition lead  74  runs axially down the extension tube and feeds axially into the socket body  62 . The extension ignition lead  74  and associated connectors are preferably positioned along the central axis of the extension tube  69  to be away from the walls thereof. If the extension ignition lead  74  is positioned too close to the walls of the extension tube  69 , the extension ignition lead  74  behaves as a capacitor and stores electric charges rather than delivers electric charges to spark plug  48 . 
     The extension tube  69  also carries a metal grounding pin  75  which is spring loaded in the plug holder  73 . Another preferred embodiment in place of the grounding pin  75  is shown if FIGS. 15A,  15 B and  15 C. The insulated ignition lead  64  emanating from the ignitor  23  carries a metal clip  76  which clamps around it and pierces it to establish electrical contact. The metal clip  76  is located on the ignition lead  64  in such a manner that it touches the ignitor link  77  when the trigger  24  is in the released position as shown in FIG.  15 A. When the trigger  24  is depressed the ignitor link  77  rocks to actuate the ignitor  23  and breaks the contact with the metal clip  76 . 
     Another preferred combustor extension is shown in FIGS. 16A,  16 B and  17 . Its distinguishing feature is that it employs two telescoping extension tubes, a inner extension tube  78  and an outer extension tube  79  joined by a compression fitting  83  and a compression nut  87 . The compression fitting  83  has a cone shaped end  85  with serrations  86  which mate with the conical internal diameter of the compression nut  87 . The inner extension tube  78  carries a stop collar  82  with an O-ring seal  83 . Telescoping rod  80  and tube  81  function as an ignition lead. 
     In a typical construction in accordance with the embodiment of FIGS.  1  and  3 - 9  the dimensions may be selected as follows: 
     l 1 =0.750 in. 
     l 2 =0.500 in. 
     l 3 =0.250 in. 
     l 4 =1.400 in. 
     l 5 =5.500 in. 
     l 6 =1.400 in. 
     l 7 =0.437 in. 
     l 8 =0.060 in. 
     l 9 =8.550 in. 
     l 10 =36 in. 
     l 11 =54 in. 
     l 12 =30 in. 
     D 1 =1.500 in. 
     D 2 =2.250 in. 
     D 3 =0.375 in. 
     D 4 =0.280 in. 
     D 5 =0.040 in. 
     D 6 =0.024 in. 
     w 1 =0.005 in. 
     w 2 =0.003 in. 
     a=5 degrees 
     g=12 degrees 
     Actuating the trigger  24  opens the valve  22  admitting the pressurized fuel gas G. The gas is led to the nozzle  26  by the fuel line  25 . At the nozzle, the pressure of the gas is expanded into the kinetic energy of multiple streams issuing from each nozzle tube  28  entraining the surrounding air. The momentum transfer from the gas to the air is accomplished in the straight walled mixing duct  40 . Some of the kinetic energy of the mixture is subsequently transformed to static pressure in the diffusor  41 , and the pressurized mixture is fed into the combustor  43 . 
     In common with other multi-nozzle jet pumps of the prior art, the present invention has the advantage of needing a much shorter mixing duct  40  to accomplish the mixing process than in a single nozzle jet pump. This leads to lower wall friction losses in the mixing duct and enhanced performance. 
     The performance of the present invention is improved further by the diverging placement of the nozzle tubes  28 . This relationship is illustrated in FIG.  19 . The divergent placement of nozzle tubes  28  pushes most of the entrained fluid to the outside of the mixing section. The velocity profile at the exit of the mixing section shows a pronounced peak close to the wall. 
     Aiming the gas nozzles at the walls appears detrimental to performance since forward momentum of the gas is sacrificed and, in addition, wall friction should increase. It is believed however that this velocity profile leads to greater diffusor efficiencies which more than make up for the aforementioned losses. By concentrating the bigger part of the flow energy close to the wall, the separation of the boundary layer of the diffuser is delayed. Stall and separation are thus avoided. As a result, diffusor efficiency is high and a greater overall pressure recovery is possible in spite of possibly higher wall friction due to the higher velocities near the wall. 
     The mixing process is improved by making the wall thickness w 2  of the nozzle tubes  28  as thin as possible to minimize eddy formation in the entrainment process and lengthening them to reach into the vicinity of the bell mouthed entry  37 . The benefits that can be derived by lengthening the nozzle tubes  28  is shown in FIG.  20 . Lengthening the nozzle tubes  28  without undue pressure losses requires a larger nozzle tube diameter D 5 . However, the benefit of enlarging the nozzle tube diameter to minimize gas pressure losses has to be balanced against the draw-back of the increased drag losses in the aspirated air stream. For this reason it is desirable to use as thin a nozzle tube wall w 1  as possible consistent with the requirements of structural strength. 
     The performance is more consistent if the nozzle tubes  28  are fashioned to have a straight section with an L/D of more than  2  after tapering down to the small discharge diameter D 6 . This may be due to the better guidance of the jet discharge direction that this geometry affords. 
     The combustion air is not aspirated into the jet pump by the path of least resistance but is forced to make two right angle turns before entering the jet pump. This is illustrated in FIG.  8 . The air A 1  enters the annular gap between the cylindrical inlet portion  38  and the flow diverter  30  in an axial direction. It is then deflected radially inward in the space between the flow diverter  30  and the pump body  36 . Subsequently, it is again deflected 90 degrees as it enters the bell mouthed inlet  37  to the jet pump in an axial direction. The basic function of the flow diverter  30  is to establish this tortuous flow patter. Without it, the air would rush in unrestrained. To minimize pressure losses at the entry to the annular passage the leading edges are rounded as shown by r 1 . To minimize pressure losses due to turning the flow from an axial to a radial direction the inside corners of the flow diverter  30  are rounded as shown by r 2 . 
     The preferred embodiment of the invention shown in FIG. 6 operates in a similar fashion. The end of the pump body  36  is fashioned to match the flow diverter  30  in size and shape, and it mounts in the housing  33  by the inner struts  32  in the same fashion as the flow diverter  30 . As a result, a second flow pattern is established tor combustion air A 2  drawn in through the front air openings  35  which mirrors the flow pattern of combustion air A 1  drawn in through the rear air opening  34 . 
     The operation of the quick connect feature of the invention is as follows. To change the direction of the combustor slot  46  the operator merely depresses the button  51  and turns the combustor  43  until the button  51  pops into the next locating hole  49 . To disconnect, the operator merely depresses the button  51  and pulls the combustor  43  off. Re-attachment is even simpler since the beveled edge  45  obliviates the need to depress the button by the operator as the combustor  43  is pushed back on. 
     By virtue of the centrally located electrical socket  59  and spark plug  48  the electrical connection is established simultaneously with the hydraulic connection or sealing for the combustion gases without regard to the rotation of the combustor  43  relative to the housing  33 . 
     The installation and removal of an extension tube follows the same pattern. When using the extension and firing the gun repeatedly, a high voltage charge builds up on the internal ignition lead, since the spark plug does not discharge the ignitor completely and the capacitance of the lead inside the extension tube blocks further ignition until the charge is dissipated. To promote a quick discharge the spring loaded grounding pin  75  can be depressed until it contacts the ignition lead  74 . Another, preferred embodiment of this feature is shown in FIG. 15A, FIGS. 15B and 15C. The grounding clip  76  is located so that it automatically discharges any residual voltage in the ignition lead  64  by touching the grounded ignitor link  77  when the trigger  24  is released. 
     As shown in FIGS. 16A and 16B, the telescoping extension tube facilitates an easy change in the length of the extension to reach both near and far while the heat gun is running. The operator merely loosens the compression nut  87 . This releases the pressure on the conical serrated compression fitting  84  and the inner extension tube can be slid out to the desired length. 
     A jet pump built with the dimensions shown in FIGS. 1-6 was compared to a jet pump with a single nozzle of the same gas consumption. The dimensions of the single nozzle pump were kept the same except for using a longer and bigger diameter mixing section  30  to achieve optimum performance. The single nozzle pump thus had to be 3 inches longer. 
     Both pumps were set up to run on pressurized air at 22 psi entraining ambient air. The output pressure was measured by a pressure gage. The output volume was controlled with a Gate Valve and measured by a Flow Meter. The results of a representative test are shown in FIG. 18 as a plot of output pressure versus pump volume. From this data the power output and pump efficiencies of the two pumps can be calculated, also shown in FIG.  18 . 
     The present invention achieves a pump efficiency of 24% compared to 17% achievable in the prior art, a 40% improvement in output power. Yet it is 3 inches, or 25% shorter. 
     To demonstrate the improvement that can be achieved with the flow diverter of the present invention compared to the prior art, another bench test was performed. A jet pump built with the dimensions according to the present invention was set up running on pressurized air at 22 psi entraining ambient air. The output pressure was monitored with a pressure transducer connected to a strip chart recorder. The output volume was controlled with a gate valve and measured by an orifice plate. After running for 2 minutes the flow diverter  30  was removed to simulate the prior art and the test was continued for another 2 minutes. The results of a representative test are shown in FIG.  21 . 
     Both pumps achieve the same peak pressure of 1.10″ water column, but the jet pump of the present invention has a fluctuation of only 0.02″ compared to a fluctuation of 0.07″ of the prior art, more than a three fold improvement in output pressure fluctuation. 
     In addition to running more smoothly, the jet pump of the present invention also has a discernibly higher average output pressure: 1.09″ vs. 1.06″. While this improvement is only slight it is significant in that the invention achieves the goal of smoother output without any loss in performance. On the contrary, there is a net gain in performance. 
     This is remarkable inasmuch as the invention introduces two right angle turns to the incoming flow. Given the pressure losses due to the turns of the flow of the present invention, the reasonable expectation is that it should suffer from a drop, not a gain in performance. 
     EQUIVALENTS 
     While this invention has been particularly shown and described with references to preferred embodiments thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims. Those skilled in the art will recognize or be able to ascertain using no more than routine experimentation, many equivalents to the specific embodiments of the invention described specifically herein. Such equivalents are intended to be encompassed in the scope of the claims. 
     For example, the jet pump of the present invention can be used for other suitable purposes other than on a heat gun.