US20130315753A1 - Speed control of engine pump via summing differential - Google Patents
Speed control of engine pump via summing differential Download PDFInfo
- Publication number
- US20130315753A1 US20130315753A1 US13/480,542 US201213480542A US2013315753A1 US 20130315753 A1 US20130315753 A1 US 20130315753A1 US 201213480542 A US201213480542 A US 201213480542A US 2013315753 A1 US2013315753 A1 US 2013315753A1
- Authority
- US
- United States
- Prior art keywords
- engine
- pump
- motor
- summing differential
- flow
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B9/00—Piston machines or pumps characterised by the driving or driven means to or from their working members
- F04B9/02—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M39/00—Arrangements of fuel-injection apparatus with respect to engines; Pump drives adapted to such arrangements
- F02M39/02—Arrangements of fuel-injection apparatus to facilitate the driving of pumps; Arrangements of fuel-injection pumps; Pump drives
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
- F02M59/10—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
- F02M59/102—Mechanical drive, e.g. tappets or cams
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B17/00—Pumps characterised by combination with, or adaptation to, specific driving engines or motors
- F04B17/03—Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B17/00—Pumps characterised by combination with, or adaptation to, specific driving engines or motors
- F04B17/05—Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by internal-combustion engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/06—Control using electricity
- F04B49/065—Control using electricity and making use of computers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/20—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by changing the driving speed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B2203/00—Motor parameters
- F04B2203/02—Motor parameters of rotating electric motors
- F04B2203/0209—Rotational speed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B2205/00—Fluid parameters
- F04B2205/09—Flow through the pump
Definitions
- the subject matter disclosed herein generally pertains to the field of a control system for a pump that provides a fluid flow in an engine.
- Engines require various fluid flows during operation, for purposes such as cooling, lubrication, and providing fuel for combustion. Fluid flows may be propelled by a pump through a network of pipes and valves on an engine. The flow rate and pressure of a fluid flow that is needed for an engine may vary based on the operation of the engine. Providing fluid flows tailored to engine operation with relative accuracy may require complex control hardware on the engine.
- Engine gearbox-driven pumping systems comprising a fixed gearbox may be used for various fluid flow applications in an engine. A gearbox pumping and control system transfers mechanical power from the engine to the pump via the gearbox to provide the fluid flow in the engine, and may deliver relatively accurate flows and pressures.
- a gearbox-driven pumping system may require additional air cooling or a return to tank path in order to maintain a target fluid temperature, as fuel recirculation around pump may generate extra heat in the pumping system that needs to be dissipated.
- a fluid pumping system for an engine includes a pump; a summing differential connected to the pump; a gearbox connected to the summing differential, wherein the gearbox causes the pump to rotate to provide a fluid flow in the engine via the summing differential; and a motor connected to the summing differential, wherein the motor adjusts a rotational speed of the pump via the summing differential.
- a method for speed control of a pump to provide a fluid flow in an engine includes powering the pump to rotate by a gearbox connected to a summing differential to provide the fluid flow in the engine; and adjusting a rotational speed of the pump by a motor connected to the summing differential.
- FIG. 1 illustrates a block diagram of an embodiment of a system for speed control of an engine pump via a summing differential
- FIG. 2 illustrates another embodiment of a system for speed control of an engine pump via a summing differential
- FIG. 3 illustrates a flowchart of a method for speed control of an engine pump via a summing differential.
- a gearbox-driven pumping system may be used in conjunction with a summing differential and a motor to provide a fluid flow in an engine.
- the gearbox may provide the primary power source to the pump from the engine, while the motor may be used to increase or decrease the rotational speed of the pump in order to meet a target flow requirement (e.g., flow rate and pressure) for the fluid flow in the engine.
- the gearbox may be sized to input power to the pump from the engine to produce a base rotational pump speed that is determined based on the design of the pump and the requirements of the pumping application.
- the motor input to the differential may add or subtract rotational speed from the pump shaft in order to make adjustments in the pump speed, as the actual pump flow demand in the engine may vary.
- the motor may be controlled based on a flow sensor in the engine in order to meet a target flow requirement for the fluid flow.
- the flow sensor may be part of an electronic engine controller of the engine in some embodiments. In one embodiment, by matching the pumping to the flow requirement, less heat is created in the pumping system, eliminating the need to return fuel to the aircraft tank. This may eliminate the need for relatively complex plumbing and valve systems.
- the motor may also act as a back-up power source for the pump in the event of a failure in the power transmission path comprising the gearbox.
- Embodiments of speed control of an engine pump via a summing differential may be used in conjunction with any appropriate type of engine, including but not limited to an aircraft engine, such as an airplane or helicopter engine, a ground vehicle, a relatively large industrial engine, or a ground-based electric generator.
- the pump that is powered via the summing differential may provide any appropriate fluid flow in the engine, including but not limited to fuel, oil, air, or glycol.
- the motor may comprise an electric motor, and may be powered by any appropriate power source, including but not limited to a power grid, an auxiliary power unit (APU), or the engine itself via a generator.
- the target flow requirement may be based on a current operating condition of the engine.
- the pump flow target may be low, so the motor may subtract speed from the pump by way of the summing differential to provide a desired flow in the engine.
- the motor may provide relatively little or no speed adjustment to the pump, and so that the motor requires relatively little power to maintain the flow at the desired level in the engine.
- FIG. 1 illustrates a block diagram an embodiment of a system 100 for speed control of an engine pump via a summing differential.
- Summing differential 103 receives power inputs from motor 101 and gearbox 102 , and causes pump 104 to rotate to provide a fluid flow in engine 105 .
- the fluid flow provided by pump 104 is measured by flow meter 106 .
- Gearbox 102 transfers rotational power from the engine 105 to the pump 104 via the summing differential 103 .
- Motor 101 which may comprise an electric motor, is controlled based by a motor control module 107 , which receives input from the flow meter 106 .
- Motor 101 is controlled by the motor control module 107 to speed up or slow down the rotation of the pump 104 (via the summing differential 103 ) as needed to adjust the fluid flow output by the pump 104 to meet a target flow requirement based on input from the flow meter 106 .
- the motor control module 107 may further control the motor 101 based on the current rotational speed of the motor 101 , the current rotational speed of the pump 104 , and the current operating conditions of the engine 105 in various embodiments.
- Motor control module 107 may be part of an electronic engine controller of the engine 105 in some embodiments.
- the motor control module 107 may be located in any appropriate location with respect to the engine 105 .
- FIG. 2 illustrates another embodiment of a system 200 for speed control of an engine pump via a summing differential.
- Summing differential 206 comprises a first leg 207 a and a second leg 207 b.
- Gearbox 203 is connected to the first leg 207 a of the summing differential 206 .
- Gearbox 203 transfers power received from the engine via engine power input 204 to the pump 205 via the summing differential 206 , causing pump 205 to rotate and provide a fluid flow in the engine.
- Motor 201 is connected to the second leg 207 b of the summing differential 206 , and is controlled via flow sensor-based motor control input 202 , which controls the motor 201 based on the state of the fluid flow in the engine.
- the motor 201 acts to speed up or slow down the rotation of the pump 205 via summing differential 206 , as needed, to meet a target flow requirement for the fluid flow produced by the pump 205 in the engine.
- the target flow requirement may be based on a current operating condition of the engine.
- FIG. 3 illustrates a flowchart of an embodiment of a method 300 for speed control of an engine pump via a summing differential.
- the pump is powered to rotate by the engine via the gearbox and summing differential, thereby providing a fluid flow in the engine.
- the speed of the pump is adjusted up or down, as needed, by a motor via the summing differential to meet a target flow requirement for the fluid flow in the engine.
- the motor is controlled based on a flow sensor that measures the fluid flow in the engine.
- the target flow requirement may be based on a current operating condition of the engine.
- the technical effects and benefits of exemplary embodiments include reduction of complexity in a fluid pumping system for an engine while providing fluid flows that may relatively accurately meet engine requirements.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Computer Hardware Design (AREA)
- Control Of Positive-Displacement Pumps (AREA)
- Control Of Non-Positive-Displacement Pumps (AREA)
Abstract
A fluid pumping system for an engine includes a pump; a summing differential connected to the pump; a gearbox connected to the summing differential, wherein the gearbox causes the pump to rotate to provide a fluid flow in the engine via the summing differential; and a motor connected to the summing differential, wherein the motor adjusts a rotational speed of the pump via the summing differential
Description
- The subject matter disclosed herein generally pertains to the field of a control system for a pump that provides a fluid flow in an engine.
- Engines require various fluid flows during operation, for purposes such as cooling, lubrication, and providing fuel for combustion. Fluid flows may be propelled by a pump through a network of pipes and valves on an engine. The flow rate and pressure of a fluid flow that is needed for an engine may vary based on the operation of the engine. Providing fluid flows tailored to engine operation with relative accuracy may require complex control hardware on the engine. Engine gearbox-driven pumping systems comprising a fixed gearbox may be used for various fluid flow applications in an engine. A gearbox pumping and control system transfers mechanical power from the engine to the pump via the gearbox to provide the fluid flow in the engine, and may deliver relatively accurate flows and pressures. However, a gearbox-driven pumping system may require additional air cooling or a return to tank path in order to maintain a target fluid temperature, as fuel recirculation around pump may generate extra heat in the pumping system that needs to be dissipated.
- According to one aspect, a fluid pumping system for an engine includes a pump; a summing differential connected to the pump; a gearbox connected to the summing differential, wherein the gearbox causes the pump to rotate to provide a fluid flow in the engine via the summing differential; and a motor connected to the summing differential, wherein the motor adjusts a rotational speed of the pump via the summing differential.
- According to another aspect, a method for speed control of a pump to provide a fluid flow in an engine includes powering the pump to rotate by a gearbox connected to a summing differential to provide the fluid flow in the engine; and adjusting a rotational speed of the pump by a motor connected to the summing differential.
- Other aspects, features, and techniques of the invention will become more apparent from the following description taken in conjunction with the drawings.
- Referring now to the drawings wherein like elements are numbered alike in the several FIGURES:
-
FIG. 1 illustrates a block diagram of an embodiment of a system for speed control of an engine pump via a summing differential; -
FIG. 2 illustrates another embodiment of a system for speed control of an engine pump via a summing differential; and -
FIG. 3 illustrates a flowchart of a method for speed control of an engine pump via a summing differential. - Embodiments of systems and methods for speed control of an engine pump via a summing differential are provided, with exemplary embodiments being discussed below in detail. A gearbox-driven pumping system may be used in conjunction with a summing differential and a motor to provide a fluid flow in an engine. The gearbox may provide the primary power source to the pump from the engine, while the motor may be used to increase or decrease the rotational speed of the pump in order to meet a target flow requirement (e.g., flow rate and pressure) for the fluid flow in the engine. The gearbox may be sized to input power to the pump from the engine to produce a base rotational pump speed that is determined based on the design of the pump and the requirements of the pumping application. The motor input to the differential may add or subtract rotational speed from the pump shaft in order to make adjustments in the pump speed, as the actual pump flow demand in the engine may vary. The motor may be controlled based on a flow sensor in the engine in order to meet a target flow requirement for the fluid flow. The flow sensor may be part of an electronic engine controller of the engine in some embodiments. In one embodiment, by matching the pumping to the flow requirement, less heat is created in the pumping system, eliminating the need to return fuel to the aircraft tank. This may eliminate the need for relatively complex plumbing and valve systems. The motor may also act as a back-up power source for the pump in the event of a failure in the power transmission path comprising the gearbox.
- Embodiments of speed control of an engine pump via a summing differential may be used in conjunction with any appropriate type of engine, including but not limited to an aircraft engine, such as an airplane or helicopter engine, a ground vehicle, a relatively large industrial engine, or a ground-based electric generator. The pump that is powered via the summing differential may provide any appropriate fluid flow in the engine, including but not limited to fuel, oil, air, or glycol. The motor may comprise an electric motor, and may be powered by any appropriate power source, including but not limited to a power grid, an auxiliary power unit (APU), or the engine itself via a generator. The target flow requirement may be based on a current operating condition of the engine. For example, in embodiments where the engine comprises an aircraft engine, during ground idle or at the top of a descent the pump flow target may be low, so the motor may subtract speed from the pump by way of the summing differential to provide a desired flow in the engine. When the aircraft engine is at full power (for example, at takeoff), there is high flow demand, and the motor adds speed to the pump for increased flow. During straight and level flight (for example, during cruising), the motor may provide relatively little or no speed adjustment to the pump, and so that the motor requires relatively little power to maintain the flow at the desired level in the engine.
-
FIG. 1 illustrates a block diagram an embodiment of asystem 100 for speed control of an engine pump via a summing differential. Summingdifferential 103 receives power inputs frommotor 101 andgearbox 102, and causespump 104 to rotate to provide a fluid flow inengine 105. The fluid flow provided bypump 104 is measured byflow meter 106. Gearbox 102 transfers rotational power from theengine 105 to thepump 104 via the summingdifferential 103.Motor 101, which may comprise an electric motor, is controlled based by amotor control module 107, which receives input from theflow meter 106.Motor 101 is controlled by themotor control module 107 to speed up or slow down the rotation of the pump 104 (via the summing differential 103) as needed to adjust the fluid flow output by thepump 104 to meet a target flow requirement based on input from theflow meter 106. Themotor control module 107 may further control themotor 101 based on the current rotational speed of themotor 101, the current rotational speed of thepump 104, and the current operating conditions of theengine 105 in various embodiments.Motor control module 107 may be part of an electronic engine controller of theengine 105 in some embodiments. Themotor control module 107 may be located in any appropriate location with respect to theengine 105. -
FIG. 2 illustrates another embodiment of asystem 200 for speed control of an engine pump via a summing differential. Summingdifferential 206 comprises a first leg 207 a and asecond leg 207 b. Gearbox 203 is connected to the first leg 207 a of the summingdifferential 206. Gearbox 203 transfers power received from the engine viaengine power input 204 to the pump 205 via the summingdifferential 206, causing pump 205 to rotate and provide a fluid flow in the engine.Motor 201 is connected to thesecond leg 207 b of the summingdifferential 206, and is controlled via flow sensor-based motor control input 202, which controls themotor 201 based on the state of the fluid flow in the engine. Themotor 201 acts to speed up or slow down the rotation of the pump 205 via summingdifferential 206, as needed, to meet a target flow requirement for the fluid flow produced by the pump 205 in the engine. The target flow requirement may be based on a current operating condition of the engine. -
FIG. 3 illustrates a flowchart of an embodiment of amethod 300 for speed control of an engine pump via a summing differential. Inblock 301, the pump is powered to rotate by the engine via the gearbox and summing differential, thereby providing a fluid flow in the engine. Inblock 302, the speed of the pump is adjusted up or down, as needed, by a motor via the summing differential to meet a target flow requirement for the fluid flow in the engine. The motor is controlled based on a flow sensor that measures the fluid flow in the engine. The target flow requirement may be based on a current operating condition of the engine. - The technical effects and benefits of exemplary embodiments include reduction of complexity in a fluid pumping system for an engine while providing fluid flows that may relatively accurately meet engine requirements.
- The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. While the description of the present invention has been presented for purposes of illustration and description, it is not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications, variations, alterations, substitutions, or equivalent arrangement not hereto described will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the invention. Additionally, while various embodiment of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments. Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
Claims (20)
1. A fluid pumping system for an engine, comprising:
a pump;
a summing differential connected to the pump;
a gearbox connected to the summing differential, wherein the gearbox causes the pump to rotate to provide a fluid flow in the engine via the summing differential; and
a motor connected to the summing differential, wherein the motor adjusts a rotational speed of the pump via the summing differential.
2. The fluid pumping system of claim 1 , wherein the gearbox transfers power from the engine to the pump via the summing differential.
3. The fluid pumping system of claim 1 , wherein the gearbox is connected to a first leg of the summing differential, and wherein the motor is connected to a second leg of the summing differential.
4. The fluid pumping system of claim 1 , wherein the motor reduces or increases the rotational speed of the pump based on a flow meter that measures the fluid flow in the engine.
5. The fluid pumping system of claim 4 , wherein the motor is controlled by an electronic engine controller of the engine based on input from the flow meter.
6. The fluid pumping system of claim 1 , wherein the motor comprises an electric motor.
7. The fluid pumping system of claim 6 , wherein the motor is powered by one of a power grid, an auxiliary power unit (APU), and an engine electrical generator.
8. The fluid pumping system of claim 1 , wherein the fluid flow comprises one of a liquid or a gas.
9. The fluid pumping system of claim 8 , wherein the fluid flow comprises one of fuel, oil, air, or glycol
10. The fluid pumping system of claim 1 , wherein the motor adjusts the rotational speed of the pump to meet a target flow requirement of the fluid flow.
11. The fluid pumping system of claim 10 , wherein the target flow requirement is based on a target operating condition of the engine.
12. A method for speed control of a pump to provide a fluid flow in an engine, the method comprising:
powering the pump to rotate by a gearbox connected to a summing differential to provide the fluid flow in the engine; and
adjusting a rotational speed of the pump by a motor connected to the summing differential.
13. The method of claim 12 , wherein the motor adjusts the rotational speed of the pump based on a flow sensor of the fluid flow in the engine to meet a target flow requirement of the fluid flow, wherein the target flow requirement is based on a target operating condition of the engine.
14. The method of claim 13 , wherein, in the event the operating condition of the engine is high, the motor is configured to increase the rotational speed of the pump.
15. The method of claim 13 , wherein, in the event the operating condition of the engine is low, the motor is configured to reduce the rotational speed of the pump.
16. The method of claim 13 , wherein, in the event the operating condition of the engine is steady, the motor is configured to perform no change of the rotational speed of the pump.
17. The method of claim 12 , wherein the gearbox is configured to transfer power from the engine to the pump.
18. The method of claim 12 , wherein the gearbox is connected to a first leg of the summing differential, and wherein the motor is connected to a second leg of the summing differential.
19. The method of claim 12 , wherein the motor reduces or increases the rotational speed of the pump based on a flow meter that measures the fluid flow in the engine.
20. The method of claim 19 , wherein the motor is controlled by an electronic engine controller of the engine based on input from the flow meter.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/480,542 US20130315753A1 (en) | 2012-05-25 | 2012-05-25 | Speed control of engine pump via summing differential |
GB1307786.2A GB2503775A (en) | 2012-05-25 | 2013-04-30 | Speed control of engine pump via summing differential |
CA2814689A CA2814689A1 (en) | 2012-05-25 | 2013-05-03 | Speed control of engine pump via summing differential |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/480,542 US20130315753A1 (en) | 2012-05-25 | 2012-05-25 | Speed control of engine pump via summing differential |
Publications (1)
Publication Number | Publication Date |
---|---|
US20130315753A1 true US20130315753A1 (en) | 2013-11-28 |
Family
ID=48627066
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/480,542 Abandoned US20130315753A1 (en) | 2012-05-25 | 2012-05-25 | Speed control of engine pump via summing differential |
Country Status (3)
Country | Link |
---|---|
US (1) | US20130315753A1 (en) |
CA (1) | CA2814689A1 (en) |
GB (1) | GB2503775A (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3985468A (en) * | 1974-12-24 | 1976-10-12 | The Garrett Corporation | Gas turbine fuel delivery system |
US20030059310A1 (en) * | 2001-09-21 | 2003-03-27 | Melissa Koenig | Hydraulic transmission pump assembly having a differential actuation and integrated line pressure control |
US20100018182A1 (en) * | 2008-07-25 | 2010-01-28 | Snecma | Regulating the flow rate of fuel taken from a fuel circuit of an aircraft propelled by an engine |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3343660B2 (en) * | 1992-12-10 | 2002-11-11 | 本田技研工業株式会社 | Oil pump drive |
JP3547735B2 (en) * | 2001-11-22 | 2004-07-28 | 本田技研工業株式会社 | Engine system, operating method thereof, and engine starting device |
JP5131460B2 (en) * | 2008-02-12 | 2013-01-30 | 株式会社ジェイテクト | Oil pump drive system |
-
2012
- 2012-05-25 US US13/480,542 patent/US20130315753A1/en not_active Abandoned
-
2013
- 2013-04-30 GB GB1307786.2A patent/GB2503775A/en not_active Withdrawn
- 2013-05-03 CA CA2814689A patent/CA2814689A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3985468A (en) * | 1974-12-24 | 1976-10-12 | The Garrett Corporation | Gas turbine fuel delivery system |
US20030059310A1 (en) * | 2001-09-21 | 2003-03-27 | Melissa Koenig | Hydraulic transmission pump assembly having a differential actuation and integrated line pressure control |
US20100018182A1 (en) * | 2008-07-25 | 2010-01-28 | Snecma | Regulating the flow rate of fuel taken from a fuel circuit of an aircraft propelled by an engine |
Also Published As
Publication number | Publication date |
---|---|
GB201307786D0 (en) | 2013-06-12 |
GB2503775A (en) | 2014-01-08 |
CA2814689A1 (en) | 2013-11-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11492969B2 (en) | Engine thermal management methods and control systems | |
US9388744B2 (en) | Distributed gas turbine engine control system with remote interface units | |
EP3051103B1 (en) | Fuel system | |
EP3203537B1 (en) | Gas turbine engine with thermoelectric system | |
US9133772B2 (en) | Fuel system | |
EP3102809B1 (en) | Technique for optimizing engine performance using fuel temperature | |
US9151180B2 (en) | Lubrication driven gas turbine engine actuation system | |
US20150113996A1 (en) | Cascaded Multi-Variable Control System for a Turboshaft Engine | |
US20130333365A1 (en) | Controlling method and system for compressed air supply to a pneumatic network, in particular in an aircraft | |
US20180050812A1 (en) | Aircraft fuel pump systems | |
CN106275412A (en) | The method of three engine power equipment of regulation rotor craft | |
US11001391B2 (en) | Automatic adjusting fuel boost pump | |
CN111720353B (en) | Method for controlling compressed air to a pneumatic system | |
US20180371945A1 (en) | System and method for supplying lubrication fluid to at least one member of an aircraft propulsion assembly | |
EP3034839B1 (en) | Means and arrangement for fuel icing protection | |
US20130315753A1 (en) | Speed control of engine pump via summing differential | |
EP4253250A1 (en) | Method and system for reducing noise of hybrid power plant | |
US20200198795A1 (en) | Device For Providing Power Or Thrust To An Aerospace Vehicle And Method For Controlling A Device For Providing Power To An Aerospace Vehicle | |
EP3036161B1 (en) | Single stage engine bleed | |
US11761382B2 (en) | Fuel supply device | |
CN111262281B (en) | Distributed power generation for a vehicle system | |
US20240392774A1 (en) | Active displacement control against temperature target | |
CN107061021A (en) | A kind of engine mechanical-hydraulic fuel flow submeter adjusting means | |
US20150308373A1 (en) | Method of scheduling pressure in variable pressure actuation systems | |
EROFEEV et al. | Local hydraulic system with adaptive pressure control for long-haul aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: HAMILTON SUNDSTRAND CORPORATION, CONNECTICUT Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:HIGGINS, ROBERT L.;ZEBROWSKI, THADDEUS J.;VERSAILLES, RICHARD E.;REEL/FRAME:028268/0997 Effective date: 20120524 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |