GB2307013A - Compressed gas motor - Google Patents

Compressed gas motor Download PDF

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Publication number
GB2307013A
GB2307013A GB9622999A GB9622999A GB2307013A GB 2307013 A GB2307013 A GB 2307013A GB 9622999 A GB9622999 A GB 9622999A GB 9622999 A GB9622999 A GB 9622999A GB 2307013 A GB2307013 A GB 2307013A
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GB
United Kingdom
Prior art keywords
cylinder
control
gas
piston
motor
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.)
Granted
Application number
GB9622999A
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GB2307013B (en
GB9622999D0 (en
Inventor
Deborah Ann Wrigley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ROBERT CORT Ltd
Original Assignee
ROBERT CORT Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by ROBERT CORT Ltd filed Critical ROBERT CORT Ltd
Publication of GB9622999D0 publication Critical patent/GB9622999D0/en
Publication of GB2307013A publication Critical patent/GB2307013A/en
Application granted granted Critical
Publication of GB2307013B publication Critical patent/GB2307013B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B11/00Reciprocating-piston machines or engines without rotary main shaft, e.g. of free-piston type
    • F01B11/001Reciprocating-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 one double acting piston motor

Description

A 1 COMPRESSED GAS MOTOR 2307013 The present invention relates to a motor
which is powered by compressed gas (typically air), and to a fluid 5 pump which uses such a gas motor to effect pumping.
Known reciprocating gas pumps all use valves for directing compressed gas alternately to one side and the other side of a piston in a cylinder, for causing the piston to reciprocate. Various mechanisms are used for triggering the switching of the valve. These include designs involving push-rods, pneumatic timing ports, magnetic pilot valves, and special seals. In all cases, whatever the nature of the triggering event, the movement of the main valve is actually caused by allowing some of the compressed gas supply to act upon the end of the valve. This makes it very difficult to achieve a rapid and accurate response. Consequently known gas motors tend to be inefficient, with the pistons not reliably travelling for the full intended stroke. There are particular problems if the motors are intended to operate over a range of speeds, and particularly at high speed.
The present invention concerns a gas motor having a main (gas-driven) piston/cylinder arrangement, and also at least one secondary piston/cylinder arrangement which effects compression of a secondary gas supply when the main piston is nearing the end of an intended stroke. The compressed secondary gas supply is used to move the main switching valve.
2 The secondary gas may be atmospheric air.
The secondary piston/cylinder arrangement may employ a secondary piston which is linked with the main piston so that it reciprocates synchronously, in its own cylinder. This secondary piston/cylinder may serve as a fluid pump, as well as having a switching function. Thus the second cylinder may have a port communicating with atmospheric air, which port is arranged to be closed as the secondary piston moves towards one end of its stroke.
Thus further movement in the same direction compresses air trapped in the cylinder. This compressed air then serves for moving the main switching valve.
In a preferred arrangement, the main piston and cylinder are coaxial with a pair of smaller secondary piston/cylinder assemblies. All three pistons are connected so as to reciprocate together. one end region of each secondary cylinder may serve as a fluid pump/ there being check valves so that, in a generally conventional way, fluid is sucked in and pushed out as the secondary pistons reciprocate. On the other sides of the secondary pumps, there are air spaces in the secondary cylinders, each having a port communicating with the atmosphere. As the main piston approaches the end of its intended stroke, one of the secondary pistons moves to obstruct its port. Continuing movement therefore compresses the atmospheric air in the associated air space. The air spaces are communicated with the main valve controlling the gas supply to the 3 main cylinder, so that this is switched.
Thus in the present design, the task of moving the switching valve is removed from the main gas (usually air) supply, and devolved to a secondary fluid system, usually using atmospheric air. Thus there are independent signals to switch the valve, giving repeatable and continuous operation under a wider range of operating conditions. The pressure required to switch the valve can accumulate over a relatively long period, during which the powering of the main piston is not affected. Thus the main piston will carry out full strokes. The main piston can operate at quite low pressure particularly if (as would normally be the case) the secondary cylinders are of much smaller area, giving high compression.
An embodiment of the invention will now be described in more detail with reference to the accompanying drawings, in which:
Fig. 1 is a schematic sectional view of an air driven fluid pump embodying the invention and Fig. 2 is a like view of the pump, showing the pistons in a different configuration.
The illustrated pump has a casing 10 defining a large primary cylinder 12 and two small coaxial cylinders 14, 16, one on each side. The main cylinder contains a main piston 18, and the smaller cylinders contain smaller pistons 20,22. They are linked by a coaxial rod 24. Between the main cylinder 12 and each small cylinder 4 14,16, the rod passes through a sliding seal 26.
in the main cylinder, there are two ports 28,30, disposed so that they are generally on different axial sides of the piston 18. The ports are coupled to a main valve 32 which, at any given time, links one of the ports to a compressed air supply, while connecting the other port to exhaust.
The two lesser piston/cylinder arrangements are identical to each other. At one end of the cylinder (e.g. cylinder 14) (in this embodiment, the outer end) there are a pair of ports 34 containing oppositelyoriented check valves. They will generally be connected to a hydraulic fluid system so that, as the piston (e.g 20) reciprocates, it pumps hydraulic fluid. On the other side of the piston (e.g. 20) there is defined an air space 36. There is a port 38 normally communicating this to atmosphere. Thus, looking at the situation shown in Fig. 1, the pistons are moving to the left so that the air space 36 of the left cylinder 14 is growing, and air is passing in through the port 38. The air space 36 of the right hand cylinder 16 is decreasing, and so air is passing out through the port 38. However continued movement beyond the configuration shown in Fig. 1 causes the port 38 of the right hand cylinder 16 to be closed by the piston 22. Further movement of the piston 22 then compresses the air in the air space 36.
The air spaces 36 are communicated by pilot lines 40 to the main valve 32. The main valve is arranged so that it switches its configuration on receiving high pressure air through a pilot line. Thus Fig. 1 shows the valve 32 in the configuration for leftward movement. When the leftward movement is essentially complete, this causes a high-pressure air signal to be sent through the righthand pilot line 40, causing the valve 32 to switch to the configuration shown in Fig. 2. The main compressed air supply then passes into the left-hand end of the main air cylinder 12, causing the pistons to be driven to the right.
6

Claims (8)

1. A gas motor comprising: a motor piston/cylinder assembly having a motor piston and a motor cylinder, said cylinder having first and second gas inlets in respective opposite axial end regions; gas supply means; valve means for coupling said gas supply means selectively to either one of said first and second gas inlets of the motor cylinder; a control piston/cylinder assembly comprising a control cylinder and a control piston; said control piston being linked to the motor piston for movement therewith; said control piston/cylinder assembly being arranged to urge compression of a secondary fluid when the control piston is nearing a first end of said control cylinder, thereby to generate a switching pressure; and pilot line means communicating the first end region of the control cylinder to said valve means to communicate said switching pressure thereto; and wherein said valve means is arranged to switch said gas supply means from said first gas inlet to said second gas inlet when said switching pressure is communicated to it.
2. A gas motor according to claim 1 wherein said control piston/cylinder assembly is arranged to urge said compression of a secondary fluid only when the control 7 piston is in a predetermined end region of the control cylinder.
3. A gas motor according to claim 2 wherein said secondary fluid is air and said control cylinder has an opening in its cylinder wall communicating with atmosphere, which opening is closed by the control piston as it moves into said predetermined end region.
4. A gas motor according to any preceding claim wherein said control piston/cylinder assembly is arranged to act as a fluid pump, and has a pumping fluid inlet and a pumping fluid outlet in its second end region which is axially remote from said first end.
5. A gas motor according to any preceding claim wherein said control piston/cylinder assembly comprises a pair of like control cylinders and control pistons which are coaxial with the motor piston/cylinder assembly, each being arranged to urge compression of a secondary fluid to generate a switching pressure, and each having a respective pilot line means for communicating said switching pressure to said valve means; said pair of control cylinders and pistons being arranged to generate said switching pressures out of phase with each other; and wherein said valve means is arranged to switch said gas supply means from said first gas inlet to said second gas inlet when said switching pressure is communicated to 8 it from a first one of said control cylinders; and to switch said gas supply means from said second gas inlet to said first gas inlet when said switching pressure is communicated to it from the other one of said control 5 cylinders.
6. A gas motor according to any preceding claim wherein said motor cylinder is of substantially greater cross sectional area than the or each said control cylinder.
7. A gas motor according to claim 6 wherein said motor cylinder has a cross sectional area which is at least four times that of the or each said control cylinder.
8. A gas motor substantially as herein described with reference to and as illustrated in the accompanying drawings.
GB9622999A 1995-11-07 1996-11-05 Compressed gas motor Expired - Fee Related GB2307013B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9522793.0A GB9522793D0 (en) 1995-11-07 1995-11-07 Compressed gas motor

Publications (3)

Publication Number Publication Date
GB9622999D0 GB9622999D0 (en) 1997-01-08
GB2307013A true GB2307013A (en) 1997-05-14
GB2307013B GB2307013B (en) 1999-09-29

Family

ID=10783522

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB9522793.0A Pending GB9522793D0 (en) 1995-11-07 1995-11-07 Compressed gas motor
GB9622999A Expired - Fee Related GB2307013B (en) 1995-11-07 1996-11-05 Compressed gas motor

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB9522793.0A Pending GB9522793D0 (en) 1995-11-07 1995-11-07 Compressed gas motor

Country Status (2)

Country Link
EP (1) EP0773346A1 (en)
GB (2) GB9522793D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7284475B2 (en) * 2004-12-30 2007-10-23 Envirodrive Inc. Pneumatic reciprocating motor

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9924283D0 (en) * 1999-10-14 1999-12-15 Potential Makes Work Limited Method and apparatus for generating motive power
US20110308248A1 (en) * 2009-02-23 2011-12-22 Novopower Ltd. Pressurized-gas powered compressor and system comprising same

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB784684A (en) * 1954-08-31 1957-10-16 George Stephen Kammer Improvements in reciprocating motors for actuation by a fluid supplied at substantially constant pressure
GB928078A (en) * 1959-11-23 1963-06-06 T H Paris Inc Hydraulic reversing control
GB1504545A (en) * 1974-12-18 1978-03-22 Ingersoll Rand Co Hydraulic reciprocating motor

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4286929A (en) * 1977-03-23 1981-09-01 Rodney T. Heath Dual pressure gas motor, and method of operation
FR2591659B1 (en) * 1985-12-18 1989-10-27 Fogautolube Sa DISTRIBUTION SYSTEM FOR A RECIPROCATING PNEUMATIC MOTOR
NO170236C (en) * 1989-04-06 1992-09-23 Speeder As LINEAERMOTOR

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB784684A (en) * 1954-08-31 1957-10-16 George Stephen Kammer Improvements in reciprocating motors for actuation by a fluid supplied at substantially constant pressure
GB928078A (en) * 1959-11-23 1963-06-06 T H Paris Inc Hydraulic reversing control
GB1504545A (en) * 1974-12-18 1978-03-22 Ingersoll Rand Co Hydraulic reciprocating motor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7284475B2 (en) * 2004-12-30 2007-10-23 Envirodrive Inc. Pneumatic reciprocating motor

Also Published As

Publication number Publication date
GB9522793D0 (en) 1996-01-10
GB2307013B (en) 1999-09-29
GB9622999D0 (en) 1997-01-08
EP0773346A1 (en) 1997-05-14

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 20011105