US20170130581A1 - An air motor - Google Patents
An air motor Download PDFInfo
- Publication number
- US20170130581A1 US20170130581A1 US15/322,265 US201515322265A US2017130581A1 US 20170130581 A1 US20170130581 A1 US 20170130581A1 US 201515322265 A US201515322265 A US 201515322265A US 2017130581 A1 US2017130581 A1 US 2017130581A1
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- United States
- Prior art keywords
- motor
- chambers
- ports
- chamber
- fluid
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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- 239000012530 fluid Substances 0.000 claims description 18
- 230000000712 assembly Effects 0.000 claims description 2
- 238000000429 assembly Methods 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 238000012384 transportation and delivery Methods 0.000 abstract description 4
- 208000034423 Delivery Diseases 0.000 abstract 1
- 238000010276 construction Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B11/00—Reciprocating-piston machines or engines without rotary main shaft, e.g. of free-piston type
- F01B11/004—Reciprocating-piston machines or engines without rotary main shaft, e.g. of free-piston type in which the movement in the two directions is obtained by two single acting piston motors, each acting in one direction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B19/00—Positive-displacement machines or engines of flexible-wall type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B23/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01B23/08—Adaptations for driving, or combinations with, pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L23/00—Valves controlled by impact by piston, e.g. in free-piston machines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/36—Engines with parts of combustion- or working-chamber walls resiliently yielding under pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B71/00—Free-piston engines; Engines without rotary main shaft
- F02B71/04—Adaptations of such engines for special use; Combinations of such engines with apparatus driven thereby
Definitions
- the present invention relates to motors that use a compressed gas as a driving fluid to drive the motor, and more particularly but not exclusively to air motors that receive compressed air to drive the motor.
- Air motors are known to have a number of working chambers to which compressed gas is delivered to drive pistons at least partly enclosing the working chambers.
- Valve mechanisms co-ordinate the delivery of compressed air sequentially to the chambers, as well as provide for exhausting air from the chambers, to cause reciprocation of the pistons.
- the pistons are connected by a single shaft, with the pistons reciprocating along the axis of the shaft.
- An example of such an air motor is described in International Patent Application PCT/AU2010/000226.
- a further apparatus such as a pump, is connected to the abovementioned shaft so as to be driven by the abovementioned air motor.
- a motor that is driven by a compressed fluid including:
- a first piston at least aiding in enclosing the first chamber
- a second piston at least aiding in enclosing the second chamber
- valve assembly enables passage of the fluid between the two chambers.
- valve assemblies is configured to sequentially connect each the chambers to the air inlet and air outlet, with the chambers being connected to enable the fluid to be transferred therebetween before one of the chambers is connected to the inlet.
- the motor further includes a controller to control operation of the valve assembly.
- valve assembly is a primary valve assembly
- controller is a pilot valve assembly
- the primary valve assembly includes a movable valve member having a plurality of passages, and a plurality of ports surrounding the valve member, with the passages in the movable valve member connecting the ports to provide for the flow of the fluid through the valve assembly.
- the ports include a plurality of ports connected to the inlet, a plurality of ports connected to the outlet, and a plurality of ports connecting the chambers, with the valve member being moved to sequentially connect the chambers to the inlet and outlet, and to connect the chambers.
- the motor includes:
- valve cavity within which the movable valve member is located.
- the movable valve member has a longitudinal axis, with passages being located at longitudinally spaced locations along the movable valve member.
- the ports are located, relative to said longitudinal axis, at longitudinally spaced positions.
- the motor is configured to receive compressed air as the driving fluid.
- FIG. 1 is a schematic sectioned top plan of an air motor
- FIG. 2 is a series of schematic side elevations of a primary valve employed in the air motor of FIG. 1 , with the movable valve member in positions A, B, C and D.
- the air motor 10 receives compressed air in order to be driven.
- the air motor 10 includes a central valve assembly 11 including a base 12 .
- the base 12 is of a unitary construction, that is it is formed of a single piece.
- the base 12 has opposite side faces 13 to which there are sealingly attached caps (covers) 14 that, in co-operation with flexible diaphragms 15 provide working chambers 16 and 17 .
- Each of the diaphragms 15 has secured to it a piston 18 , with pistons 18 being connected by a piston rod (connecting member) 19 so that the pistons 18 reciprocate linearly in unison along the longitudinal axis 20 of the piston rod 19 .
- a clamp member 21 To aid in securing each diaphragm 15 to its associated piston 18 there is provided a clamp member 21 .
- the piston rod 19 extends through passage 48 .
- the axis 20 is also the longitudinal axis of the passage 48 .
- Each diaphragm 15 has a portion abutting the adjacent piston 18 that effectively forms part of the piston 18 .
- the faces 13 are generally parallel but spaced along the axis 20 and generally perpendicular thereto.
- a pilot valve 51 is located in the base 12 and includes a first cavity 22 with a longitudinal axis 23 (generally parallel to the axis 20 ), within which there is located a movable valve member 24 . Also located in the base 12 is a primary valve 52 that includes a second cavity 25 within which there is located a movable valve member 26 .
- seals 27 Extending between the member 24 and surfaces of the base 12 , surrounding the member, are seals 27 .
- the cavity 25 has a longitudinal axis 28 along which the member 26 moves, with the axis 28 being generally parallel to the axis 20 .
- the base 12 includes inlet ducting 50 , exhaust (outlet) ducting 29 , and intermediate ducting 30 .
- the inlet ducting 50 communicates with an inlet port member 31 providing a threaded passage 32 that would typically be threadably engaged with a high pressure hose via which compressed air is delivered to the motor 10 .
- the ducting 29 communicates with a threaded outlet passage 33 , of the outlet port member 31 , that would be typically attached to a muffler and via which exhaust air gas exits the motor 10 .
- the intermediate ducting 30 connects the first chamber 22 with the second chamber 25 .
- Fourth ducting 34 and 54 respectively connect the chambers 16 and 17 with the second chamber 25 .
- valve member 24 projects beyond the base 12 so as to extend into each of the chambers 16 and 17 .
- compressed air is delivered to the passage 32 from where it is delivered to the chamber 22 .
- Air is simultaneously delivered to the chamber 25 from passage 32 for delivery to the chamber 17 (with reference to FIG. 1 ).
- compressed air is also delivered from cavity 22 to the chamber 25 via ducting 30 and 42 to apply pressure to the end face 35 of the member 26 so that compressed air is delivered to chamber 17 .
- the compressed air in the chamber 17 forces the piston 18 in the direction 36 .
- the pistons 18 are connected by the rod 19 , ultimately the piston 18 of the chamber 16 engages the end of the valve member 24 and forces it in the direction 36 .
- compressed air is then redirected to the chamber 16 to cause movement of the piston rod 18 in a direction opposite the direction 36 .
- valve member 24 Simultaneously air is directed via valve member 24 away from the end face 35 of valve cavity 25 to the exhaust ducting 29 through valve chamber 22 , while air is being directed into the cavity so as to apply pressure to the end face 37 to force the valve member 26 in a direction opposite the direction 36 so that the compressed air from passage 28 is now delivered to the chamber 16 .
- This movement of the valve member 26 also alternately connects the chambers 16 and 17 to the exhaust ducting 29 .
- the chamber 17 is connected to the exhaust ducting 29 .
- the chamber 16 receives compressed air
- the chamber 16 is connected to the exhaust ducting 29 .
- the valves 51 and 52 are operated to alternately connect the chambers 16 and 17 to the inlet passage 32 and the exhaust passage 33 .
- the valve 52 includes a sleeve 55 located in the chamber 25 , and within which the valve member 26 is slidably located. Seals 56 sealingly connect the sleeve 55 and member 26 .
- the sleeve 55 has ports 61 to 68 which are arranged as follows:
- ports 61 and 64 communicate with the ducting 34 ;
- ports 65 and 68 communicate with the ducting 54 ;
- ports 63 and 66 communicate with the ducting 50 .
- the ports 61 and 64 provide for the flow of the compressed air to and from chambers 16
- the ports 65 and 68 provide for the flow of compressed air to and from the chamber 17
- the ports 62 and 67 provide the exhaust of air from the chambers 16 and 17
- the ports 63 and 66 provide for the delivery of compressed air to the chambers 16 and 17 .
- the seals 72 connect the member 26 and sleeve 55 .
- the sleeve 55 may also be a plurality of spacers (rings) located between the seals 56 , with the seals 56 connecting the member 26 and base 12 .
- the ports 61 to 68 would be annular with respect to the axis 38 .
- FIG. 2 shows the sequence of movements of the movable valve member 26 , from the position at which the valve member 26 is located when the chamber 16 has reached its maximum volume, that is the piston 18 associated therewith has reached its maximum travel.
- valve member 24 When the above has occurred, the valve member 24 is moved to the left (with reference to FIG. 1 ). Upon doing so compressed air is delivered to the chamber 25 , in particular compressed air engages the end face 35 of the member 26 to drive the member 26 in the direction 36 .
- the passage 69 of the member 26 will move from connecting ports 63 and 64 , to a position at which it connects parts 64 and 65 . Simultaneously the passage 71 will move from connecting parts 67 and 68 . Compressed air that was previously in the chamber 16 will be at least partly exhausted into the chamber 17 via parts 63 and 64 (position B). Further movement of the member 26 in the direction 36 will isolate the chamber 16 from the chamber 17 , while connecting the chamber 17 to a supply of compressed air by connecting the ports 65 and 66 with passage 69 . Simultaneously the passage 70 of the member 26 connects the port 61 , 62 so that the chamber 16 is allowed to exhaust (position C).
- the pilot valve 51 can be replaced with an actuator, such as a servo motor or an electrically operated linear actuator, that is coupled to the member 26 and operated to cause the movement thereof as discussed above.
- an actuator such as a servo motor or an electrically operated linear actuator
- the movement and speed at which the member 26 moves between the positions A, B, C and D is governed by the air flow rate provided by the valve 51 .
- piston 18 associated with the chamber 17 , is at its maximum position in the direction 36 , that is the chamber 17 at its maximum volume, piston 18 will have engaged the member 24 and driven it to a position displaced from the position shown in FIG. 1 , that is a position displaced to the right (position D).
- compressed air is then delivered to the chamber 25 adjacent the end face 37 to drive the member 26 in a direction opposite direction 36 .
- the ports 64 and 65 are connected so that compressed air in the chamber 17 can be transferred to the chamber 16 , and then subsequently the chamber 16 and 17 isolated with the chamber 17 then connected to the port 67 , and the chamber 16 connected to the port 63 . That is chamber 17 is able to exhaust, and chamber 16 receiving compressed air.
- the passages 69 , 70 and 71 are annular with their central axis, the axis 38 .
- the passages 69 , 70 and 71 are located at spaced positions along the axis 38 , with the ports 61 to 68 also located at spaced positions longitudinally relative to the axis 38 .
- the base 12 includes a fifth ducting 38 that extends between the opposite faces 13 .
- Each cap 14 is sealingly connected to its associated adjacent face 13 by means of a seal 39 .
- Each seal 39 includes an annular portion 40 that slidably engages the piston rod 19 , as well as having a weakened portion 41 that is aligned with the ducting 38 .
- Holes 45 and 49 alternately provide for the valve member 24 to extend therethrough, along with aligning with ducting 34 to provide for air flow to and from chambers 16 and 17 .
- hole 45 provides the air flow while hole 49 allows the valve member 24 to extend therethrough.
- hole 49 provides the air flow while hole 45 allows the valve member 24 to extend therethrough.
- the base 12 has faces 46 that are engaged by the member 31 .
- the faces 46 are generally perpendicular to the faces 13 and are therefore generally parallel to the axis 20 .
- the ducting 30 , 34 38 , 50 and 54 can be formed through the faces 13 and 46 .
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Fluid-Driven Valves (AREA)
- Actuator (AREA)
Abstract
An air motor (10) that has opposing chambers (16, 17) to which compressed air is alternatively delivered to drive the motor (10). The motor (10) has a primary valve (52) that governs deli very of the compressed air to the chambers (16, 17) so at least part of the compressed air is transferred to the other chamber to aid in driving the pistons (18).
Description
- The present invention relates to motors that use a compressed gas as a driving fluid to drive the motor, and more particularly but not exclusively to air motors that receive compressed air to drive the motor.
- Air motors are known to have a number of working chambers to which compressed gas is delivered to drive pistons at least partly enclosing the working chambers. Valve mechanisms co-ordinate the delivery of compressed air sequentially to the chambers, as well as provide for exhausting air from the chambers, to cause reciprocation of the pistons. Typically the pistons are connected by a single shaft, with the pistons reciprocating along the axis of the shaft. An example of such an air motor is described in International Patent Application PCT/AU2010/000226.
- A further apparatus, such as a pump, is connected to the abovementioned shaft so as to be driven by the abovementioned air motor.
- A disadvantage of known air motors, such as the air motors discussed above, is that they make inefficient use of the driving fluid (compressed air).
- It is the object of the present invention to overcome or substantially ameliorate at least one of the above disadvantages.
- There is disclosed herein a motor that is driven by a compressed fluid, the motor including:
- a first working chamber;
- a first piston at least aiding in enclosing the first chamber;
- a second working chamber;
- a second piston at least aiding in enclosing the second chamber;
- a compressed fluid inlet;
- exhaust fluid outlet;
- ducting and a valve assembly connecting the chambers, inlet and outlet so that the fluid is allowed to enter and leave the chambers to move the pistons; and wherein
- the valve assembly enables passage of the fluid between the two chambers.
- Preferably, the valve assemblies is configured to sequentially connect each the chambers to the air inlet and air outlet, with the chambers being connected to enable the fluid to be transferred therebetween before one of the chambers is connected to the inlet.
- Preferably, the motor further includes a controller to control operation of the valve assembly.
- Preferably, the valve assembly is a primary valve assembly, and the controller is a pilot valve assembly.
- Preferably, the primary valve assembly includes a movable valve member having a plurality of passages, and a plurality of ports surrounding the valve member, with the passages in the movable valve member connecting the ports to provide for the flow of the fluid through the valve assembly.
- Preferably, the ports include a plurality of ports connected to the inlet, a plurality of ports connected to the outlet, and a plurality of ports connecting the chambers, with the valve member being moved to sequentially connect the chambers to the inlet and outlet, and to connect the chambers.
- Preferably, the motor includes:
- a base;
- a piston rod mounted in the base and coupling the piston so that the pistons move in unison; and
- a valve cavity within which the movable valve member is located.
- Preferably, the movable valve member has a longitudinal axis, with passages being located at longitudinally spaced locations along the movable valve member.
- Preferably, the ports are located, relative to said longitudinal axis, at longitudinally spaced positions.
- Preferably, the motor is configured to receive compressed air as the driving fluid.
- A preferred form of the present invention will now be described by way of example only with reference to the accompanying drawings wherein:
-
FIG. 1 is a schematic sectioned top plan of an air motor; and -
FIG. 2 is a series of schematic side elevations of a primary valve employed in the air motor ofFIG. 1 , with the movable valve member in positions A, B, C and D. - in the accompanying drawings there is schematically depicted an
air motor 10. Theair motor 10 receives compressed air in order to be driven. Theair motor 10 includes acentral valve assembly 11 including abase 12. Preferably thebase 12 is of a unitary construction, that is it is formed of a single piece. Thebase 12 has opposite side faces 13 to which there are sealingly attached caps (covers) 14 that, in co-operation withflexible diaphragms 15 provide 16 and 17. Each of theworking chambers diaphragms 15 has secured to it apiston 18, withpistons 18 being connected by a piston rod (connecting member) 19 so that thepistons 18 reciprocate linearly in unison along thelongitudinal axis 20 of thepiston rod 19. To aid in securing eachdiaphragm 15 to its associatedpiston 18 there is provided aclamp member 21. Thepiston rod 19 extends throughpassage 48. Theaxis 20 is also the longitudinal axis of thepassage 48. - Each
diaphragm 15 has a portion abutting theadjacent piston 18 that effectively forms part of thepiston 18. - The
faces 13 are generally parallel but spaced along theaxis 20 and generally perpendicular thereto. - A
pilot valve 51 is located in thebase 12 and includes afirst cavity 22 with a longitudinal axis 23 (generally parallel to the axis 20), within which there is located amovable valve member 24. Also located in thebase 12 is aprimary valve 52 that includes asecond cavity 25 within which there is located amovable valve member 26. - Extending between the
member 24 and surfaces of thebase 12, surrounding the member, areseals 27. - The
cavity 25 has alongitudinal axis 28 along which themember 26 moves, with theaxis 28 being generally parallel to theaxis 20. - The
base 12 includesinlet ducting 50, exhaust (outlet) ducting 29, andintermediate ducting 30. The inlet ducting 50 communicates with aninlet port member 31 providing a threadedpassage 32 that would typically be threadably engaged with a high pressure hose via which compressed air is delivered to themotor 10. The ducting 29 communicates with a threadedoutlet passage 33, of theoutlet port member 31, that would be typically attached to a muffler and via which exhaust air gas exits themotor 10. Theintermediate ducting 30 connects thefirst chamber 22 with thesecond chamber 25. -
34 and 54 respectively connect theFourth ducting 16 and 17 with thechambers second chamber 25. - As seen in
FIG. 1 , thevalve member 24 projects beyond thebase 12 so as to extend into each of the 16 and 17.chambers - In operation of the above described
air motor 10, compressed air is delivered to thepassage 32 from where it is delivered to thechamber 22. Air is simultaneously delivered to thechamber 25 frompassage 32 for delivery to the chamber 17 (with reference toFIG. 1 ). At this time, compressed air is also delivered fromcavity 22 to thechamber 25 via ducting 30 and 42 to apply pressure to theend face 35 of themember 26 so that compressed air is delivered tochamber 17. The compressed air in thechamber 17 forces thepiston 18 in thedirection 36. As thepistons 18 are connected by therod 19, ultimately thepiston 18 of thechamber 16 engages the end of thevalve member 24 and forces it in thedirection 36. In this configuration compressed air is then redirected to thechamber 16 to cause movement of thepiston rod 18 in a direction opposite thedirection 36. Simultaneously air is directed viavalve member 24 away from theend face 35 ofvalve cavity 25 to theexhaust ducting 29 throughvalve chamber 22, while air is being directed into the cavity so as to apply pressure to theend face 37 to force thevalve member 26 in a direction opposite thedirection 36 so that the compressed air frompassage 28 is now delivered to thechamber 16. This movement of thevalve member 26 also alternately connects the 16 and 17 to thechambers exhaust ducting 29. In particular when compressed air is being delivered to thechamber 16, thechamber 17 is connected to theexhaust ducting 29. However when thechamber 17 receives compressed air, thechamber 16 is connected to theexhaust ducting 29. Accordingly, the 51 and 52 are operated to alternately connect thevalves 16 and 17 to thechambers inlet passage 32 and theexhaust passage 33. - The
valve 52 includes asleeve 55 located in thechamber 25, and within which thevalve member 26 is slidably located.Seals 56 sealingly connect thesleeve 55 andmember 26. - The
sleeve 55 hasports 61 to 68 which are arranged as follows: -
61 and 64 communicate with theports ducting 34; -
65 and 68 communicate with theports ducting 54; -
62 and 67 communicate with theports ducting 29; and -
63 and 66 communicate with theports ducting 50. - Accordingly the
61 and 64 provide for the flow of the compressed air to and fromports chambers 16, the 65 and 68 provide for the flow of compressed air to and from theports chamber 17, the 62 and 67 provide the exhaust of air from theports 16 and 17, while thechambers 63 and 66 provide for the delivery of compressed air to theports 16 and 17.chambers - The
seals 72 connect themember 26 andsleeve 55. - The
sleeve 55 may also be a plurality of spacers (rings) located between theseals 56, with theseals 56 connecting themember 26 andbase 12. Theports 61 to 68 would be annular with respect to theaxis 38. -
FIG. 2 shows the sequence of movements of themovable valve member 26, from the position at which thevalve member 26 is located when thechamber 16 has reached its maximum volume, that is thepiston 18 associated therewith has reached its maximum travel. - When the above has occurred, the
valve member 24 is moved to the left (with reference toFIG. 1 ). Upon doing so compressed air is delivered to thechamber 25, in particular compressed air engages theend face 35 of themember 26 to drive themember 26 in thedirection 36. - As the member 26 (position A) initiates movement in the
direction 36, thepassage 69 of themember 26 will move from connecting 63 and 64, to a position at which it connectsports 64 and 65. Simultaneously theparts passage 71 will move from connecting 67 and 68. Compressed air that was previously in theparts chamber 16 will be at least partly exhausted into thechamber 17 viaparts 63 and 64 (position B). Further movement of themember 26 in thedirection 36 will isolate thechamber 16 from thechamber 17, while connecting thechamber 17 to a supply of compressed air by connecting the 65 and 66 withports passage 69. Simultaneously thepassage 70 of themember 26 connects the 61, 62 so that theport chamber 16 is allowed to exhaust (position C). - The
pilot valve 51 can be replaced with an actuator, such as a servo motor or an electrically operated linear actuator, that is coupled to themember 26 and operated to cause the movement thereof as discussed above. - The movement and speed at which the
member 26 moves between the positions A, B, C and D is governed by the air flow rate provided by thevalve 51. - However once the
piston 18, associated with thechamber 17, is at its maximum position in thedirection 36, that is thechamber 17 at its maximum volume,piston 18 will have engaged themember 24 and driven it to a position displaced from the position shown inFIG. 1 , that is a position displaced to the right (position D). Once this occurs compressed air is then delivered to thechamber 25 adjacent theend face 37 to drive themember 26 in a directionopposite direction 36. As this occurs again the 64 and 65 are connected so that compressed air in theports chamber 17 can be transferred to thechamber 16, and then subsequently the 16 and 17 isolated with thechamber chamber 17 then connected to theport 67, and thechamber 16 connected to theport 63. That ischamber 17 is able to exhaust, andchamber 16 receiving compressed air. - The
69, 70 and 71 are annular with their central axis, thepassages axis 38. The 69, 70 and 71 are located at spaced positions along thepassages axis 38, with theports 61 to 68 also located at spaced positions longitudinally relative to theaxis 38. - The
base 12 includes afifth ducting 38 that extends between the opposite faces 13. - Each
cap 14 is sealingly connected to its associatedadjacent face 13 by means of aseal 39. Eachseal 39 includes anannular portion 40 that slidably engages thepiston rod 19, as well as having a weakenedportion 41 that is aligned with theducting 38. There is also ducting (depressions) 42 that provide for the ducting of air to be located adjacent the 35 and 37 when thefaces valve member 26 is to be moved. 45 and 49 alternately provide for theHoles valve member 24 to extend therethrough, along with aligning withducting 34 to provide for air flow to and from 16 and 17. On the side ofchambers chamber 17,hole 45 provides the air flow whilehole 49 allows thevalve member 24 to extend therethrough. On the side ofchamber 16,hole 49 provides the air flow whilehole 45 allows thevalve member 24 to extend therethrough. - The
base 12 hasfaces 46 that are engaged by themember 31. The faces 46 are generally perpendicular to thefaces 13 and are therefore generally parallel to theaxis 20. - The
30, 34 38, 50 and 54 can be formed through theducting 13 and 46.faces - In the above described preferred embodiment rather than totally exhausting the compressed air from the
16 and 17, at least part of the compressed air is transferred to the other chamber to aid in driving thechambers pistons 18. Accordingly less compressed air is used to operate themotor 10.
Claims (11)
1.-10. (canceled)
11. A motor that is driven by a compressed fluid, the motor including:
a first working chamber;
a first piston at least aiding in enclosing the first chamber;
a second working chamber;
a second piston at least aiding in enclosing the second chamber;
a compressed fluid inlet;
an exhaust fluid outlet;
ducting and a valve assembly connecting the chambers, inlet and outlet so that the fluid is allowed to enter and leave the chambers to move the pistons; and wherein
the valve assembly enables passage of the fluid between the two chambers.
12. The motor of claim 1, wherein the valve assemblies is configured to sequentially connect each the chambers to the air inlet and air outlet, with the chambers being connected to enable the fluid to be transferred therebetween before one of the chambers is connected to the inlet.
13. The motor of claim 1, wherein the motor further includes a controller to control operation of the valve assembly.
14. The motor of claim 1, wherein the valve assembly is a primary valve assembly, and the controller is a pilot valve assembly.
15. The motor of claim 4, wherein the primary valve assembly includes a movable valve member having a plurality of passages, and a plurality of ports surrounding the valve member, with the passages in the movable valve member connecting the ports to provide for the flow of the fluid through the valve assembly.
16. The motor of claim 5, wherein the ports include a plurality of ports connected to the inlet, a plurality of ports connected to the outlet, and a plurality of ports connecting the chambers, with the valve member being moved to sequentially connect the chambers to the inlet and outlet, and to connect the chambers.
17. The motor of claim 5, further including:
a base;
a piston rod mounted in the base and coupling the piston so that the pistons move in unison; and
a valve cavity within which the movable valve member is located.
18. The motor of claim 5, wherein the movable valve member has a longitudinal axis, with passages being located at longitudinally spaced locations along the movable valve member.
19. The motor of claim 8, wherein the ports are located, relative to said longitudinal axis, at longitudinally spaced positions.
20. The motor of claim 1, wherein the motor is configured to receive compressed air as the driving fluid.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2014902628 | 2014-07-08 | ||
| AU2014902628A AU2014902628A0 (en) | 2014-07-08 | An air motor | |
| PCT/AU2015/000140 WO2016004453A1 (en) | 2014-07-08 | 2015-03-13 | An air motor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20170130581A1 true US20170130581A1 (en) | 2017-05-11 |
Family
ID=55063380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US15/322,265 Abandoned US20170130581A1 (en) | 2014-07-08 | 2015-03-13 | An air motor |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20170130581A1 (en) |
| AU (1) | AU2015286240B2 (en) |
| WO (1) | WO2016004453A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110374683B (en) * | 2019-07-22 | 2021-04-20 | 六安永贞匠道机电科技有限公司 | A bidirectional intermittent air motor |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6241487B1 (en) * | 1998-11-10 | 2001-06-05 | Warren Rupp, Inc. | Fluid powered diaphragm pump |
| ES2743439T3 (en) * | 2004-11-17 | 2020-02-19 | Proportionair Inc | Control system for a pneumatic diaphragm pump |
| NZ601637A (en) * | 2010-05-14 | 2013-12-20 | Joe Santa & Ass Pty Ltd | An air motor |
-
2015
- 2015-03-13 AU AU2015286240A patent/AU2015286240B2/en active Active
- 2015-03-13 WO PCT/AU2015/000140 patent/WO2016004453A1/en not_active Ceased
- 2015-03-13 US US15/322,265 patent/US20170130581A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| AU2015286240B2 (en) | 2018-08-16 |
| AU2015286240A1 (en) | 2017-01-19 |
| WO2016004453A1 (en) | 2016-01-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: JOE SANTA & ASSOCIATES PTY LIMITED, AUSTRALIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SANTA, DAVID LUIZ;REEL/FRAME:041482/0912 Effective date: 20170123 |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |