Variable displacement pumps

Claim 2

An emergency hydraulic supply system comprising: a) a source of hydraulic fluid, b) a rotary variable-displacement hydraulic pump coupled to said source and operable to supply hydraulic fluid under pressure, c) a rotary prime mover coupled to said pump and operable to drive the same, d) pressure-compensated control means coupled to said pump and operable alone, in a first regime of operation of the system, to vary the displacement of said pump, said first regime of operation corresponding to a first rotational speed of said prime mover, and e) a speed control loop comprising said control means, said pump and said prime mover, and additionally comprising: i. combined speed sensor and speed governor means operable to provide a signal representative of the rotational speed of said prime mover, ii. override means coupled to receive said signal and arranged to be inoperable during said first regime of operation and arranged to be rendered operative to override said control means during a second regime of operation of the system corresponding to a second rotational speed of said prime mover, said second rotational speed being lower than said first rotational speed, whereby said pump is maintained at a substantially constant speed during said second regime with the override means varying the displacement of said pump to match available prime mover power.

Claim 3

A pump according to claim 1, wherein the signal related to the rotational speed of the pump is a hydraulic pressure signal.

Claim 4

A pump according to claim 1, wherein the signal related to the rotational speed of the pump is an electrical signal.

Claim 5

A pump according to claim 1, wherein means are provided for adjusting the minimum speed of the pump.

Claim 6

A system according to claim 1, and further including speed governor means coupled to the prime mover, said speed governor being operable during said first regime to govern the speed of said prime mover and being rendered inoperative during said second regime.

Claim 7

A system according to claim 1, wherein the system has a third regime of operation corresponding to a third rotational speed of said prime mover, said third rotational speed being intermediate said first and second rotational speeds, said combined speed governor and speed sensor means and said prime mover speed governor both being inoperative in said third regime, whereby if the demand on said pump increases during said third regime, the speed of the prime mover decreases, with torque remaining substantially constant.

Claim 8

A pump according to claim 1, wherein the prime mover is a ram air turbine.

Claim 9

A pump according to claim 7, wherein the ram air turbine is provided with a speed governor.

Claim 10

A pump according to claim 1, wherein the override means are in the form of a control valve responsive to the signal related to the rotational speed of the pump and operable to apply pump outlet pressure to the displacement means of the pump to de-stroke the pump when the rotational speed of the pump decreases.

Claim 11

A pump according to claim 9 and being in the form of a swash pump, the control valve being operable to apply pump outlet pressure to the displacement of the swash pump to de-stroke the pump when the rotational speed of the pump decreases.

Claim 12

A pump according to claim 9, wherein the control valve is responsive to the output flow of hydraulic fluid from the pump.

Claim 13

A pump according to claim 11, wherein the control valve has a flow sensor connected across the spool thereof.

Claim 14

A system according to claim 1, and further including means for programming the governed speed of said pump.

Claim 15

A pump according to claim 13, wherein the signal related to the rotational speed of the pump is an electrical signal.

Claim 16

A pump according to claim 13, wherein the signal related to the rotational speed of the pump is a hydraulic pressure signal.

Claim 17

A pump according to claim 13, wherein means are provided for adjusting the minimum speed of the pump.

Claim 18

A system according to claim 13, wherein said programme means are associated with said combined speed sensor and speed governor means.

Claim 19

A system according to claim 13 wherein said programme means are associated with said override means and said override means comprise a proportional control hydraulic valve having a housing, a spool slidably mounted in the housing and a return spring acting between said housing and one end of said spool, said programme means being operable to vary the preload of said return spring.

Claim 20

A system according to claim 18, wherein said programme means varies said return spring directly.

Claim 21

A system according to claim 18, wherein aid programme means varies said return spring indirectly via drive means.

Claim 22

A system according to claim 20, wherein said drive means is selected from a solenoid, a motor, motor-driven screw, and hydraulic pressure.

Claim 23

A pump according to claim 13, wherein the override means are in the form of a control valve responsive to the signal related to the rotational speed of the pump and operable to apply pump outlet pressure to the displacement means of the pump to de-stroke the pump when the rotational speed of the pump decreases.

Claim 24

A pump according to claim 22 and being in the form of a swash pump, the control valve being operable to apply pump outlet pressure to the displacement of the swash pump to de-stroke the pump when the rotational speed of the pump decreases.

Claim 25

A pump according to claim 22, wherein the control valve is responsive to the output flow of hydraulic fluid from the pump.

Claim 26

A pump according to claim 24, wherein the control valve has a flow sensor connected across the spool thereof.

Claim 27

In an aircraft, an emergency hydraulic supply system comprising: a) a source of hydraulic fluid, b) a rotary variable-displacement hydraulic pump coupled to said source and operable to supply hydraulic fluid under pressure, c) a prime mover in the form of a ram air turbine coupled to said pump and operable to drive the same, d) pressure-compensated control means coupled to said pump and operable alone, in a first regime of operation of the system, to vary the displacement of said pump, said first regime of operation corresponding to a first rotational speed of said ram air turbine, and e) a speed control loop comprising said control means, said pump and said ram air turbine, and additionally comprising: i. combined speed sensor and speed governor means operable to provide a signal representative of the rotational speed of said ram air turbine, ii. override means coupled to receive said signal arranged to be inoperable during said first regime of operation and arranged to be rendered operative to override said control means during a second regime of operation of the system corresponding to a second rotational speed of said ram air turbine, said second rotational speed being lower than said first rotational speed, whereby said pump is maintained at a substantially constant speed during said second regime with the override means varying the displacement of said pump to match available power from the ram air turbine.

Claim 28

In an aircraft, an emergency hydraulic supply system comprising: a) a source of hydraulic fluid, b) a rotary variable-displacement hydraulic pump coupled to said source and operable to supply hydraulic fluid under pressure, c) a prime mover in the form of a ram air turbine coupled to said pump and operable to drive the same, d) pressure-compensated control means coupled to said pump and operable alone, in a first regime of operation of the system, to vary the displacement of said pump, said first regime of operation corresponding to a first rotational speed of said ram air turbine, and e) a speed control loop comprising said control means, said pump and said ram air turbine, and additionally comprising: i. combined speed sensor and speed governor means operable to provide a signal representative of the rotational speed of said ram air turbine, ii. override means coupled to receive said signal arranged to be inoperable during said first regime of operation and arranged to be rendered operative to override said control means during a second regime of operation of the system corresponding to a second rotational speed of said ram air turbine, said second rotational speed being lower than said first rotational speed, whereby said pump is maintained at a substantially constant speed during said second regime with the override means varying the displacement of said pump to match available power from the ram air turbine.

Claim 29

A system according to claim 26, and further including speed governor means coupled to the arm air turbine, said speed governor being operable during said first regime to govern the speed of said ram air turbine band being rendered inoperative during said second regime.

Claim 30

A system according to claim 26, wherein the system has a third regime of operation corresponding to a third rotational speed of said ram air turbine, said third rotational speed being intermediate said first and second rotational speeds, said combined speed governor and speed sensor means and said ram air turbine speed governor both being inoperative in said third regime, whereby the ram air turbine is a constant pitch and if the demand on said pump increases during said third regime, the speed of the prime mover decreases, with torque remaining substantially constant.

Claim 31

A system according to claim 26, and further including means for programming the governed speed of said pump.

Claim 32

A system according to claim 29 wherein said programme means are associated with said override means and said override means comprise a proportional control hydraulic valve having a housing, a spool slidably mounted in the housing and a return spring acting between said housing and one end of said spool, said programme means being operable to vary the preload of said return spring.

Claim 33

A system according to claim 29, wherein said programme means varies said return spring directly.

Claim 34

A system according to claim 29, wherein aid programme means varies said return spring indirectly via drive means.

Claim 35

A system according to claim 29, wherein said drive means is selected from a solenoid, a motor, motor-driven screw, and hydraulic pressure.

Claim 36

A system according to claim 29, wherein said programme means are associated with said combined speed sensor and speed governor means.