WO2015063400A3 - Procédé de détection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aéronef - Google Patents
Procédé de détection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aéronef Download PDFInfo
- Publication number
- WO2015063400A3 WO2015063400A3 PCT/FR2014/052723 FR2014052723W WO2015063400A3 WO 2015063400 A3 WO2015063400 A3 WO 2015063400A3 FR 2014052723 W FR2014052723 W FR 2014052723W WO 2015063400 A3 WO2015063400 A3 WO 2015063400A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fuel
- engine
- return valve
- failure
- detecting
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title abstract 14
- 239000002828 fuel tank Substances 0.000 abstract 5
- 230000000903 blocking effect Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/005—Accessories not provided for in the groups B64D37/02 - B64D37/28
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/14—Filling or emptying
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/232—Fuel valves; Draining valves or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K37/00—Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K37/00—Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
- F16K37/0025—Electrical or magnetic means
- F16K37/005—Electrical or magnetic means for measuring fluid parameters
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L19/00—Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
- G01L19/0092—Pressure sensor associated with other sensors, e.g. for measuring acceleration or temperature
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/80—Diagnostics
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Analytical Chemistry (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Fuel-Injection Apparatus (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
L'invention concerne un procédé de détection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aéronef, le circuit carburant comportant • un réservoir de carburant (10); • un système carburant moteur (20) connecté au réservoir de carburant, ledit système carburant moteur étant apte à délivrer un flux de carburant au moteur en fonction d'un régime dudit moteur; • une canalisation (2) de retour de carburant connectée entre le système carburant moteur (20) et le réservoir de carburant; • une vanne (30) de retour carburant agencée pour commuter entre une position ouverte et une position fermée, ladite vanne étant apte à obstruer, en position fermée, la canalisation (2) de retour de carburant et à mettre en communication, en position ouverte, la canalisation de retour de carburant avec le réservoir de carburant; • le procédé comprenant les étapes suivantes mises en oeuvre dans un calculateur : • mesure (El) d'une pression du flux de carburant issu du réservoir de carburant; et si la pression mesurée est inférieure à un seuil prédéterminé, • mesure (E2) du régime du moteur.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/033,007 US10082444B2 (en) | 2013-10-30 | 2014-10-27 | Method for detecting a failure in a fuel return valve of an aircraft engine fuel circuit |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1360636 | 2013-10-30 | ||
FR1360636A FR3012420B1 (fr) | 2013-10-30 | 2013-10-30 | Procede de detection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2015063400A2 WO2015063400A2 (fr) | 2015-05-07 |
WO2015063400A3 true WO2015063400A3 (fr) | 2015-09-11 |
Family
ID=49876882
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2014/052723 WO2015063400A2 (fr) | 2013-10-30 | 2014-10-27 | Procédé de détection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aéronef |
Country Status (3)
Country | Link |
---|---|
US (1) | US10082444B2 (fr) |
FR (1) | FR3012420B1 (fr) |
WO (1) | WO2015063400A2 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3012418B1 (fr) * | 2013-10-30 | 2016-12-30 | Snecma | Procede de detection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aeronef |
US10451509B2 (en) * | 2014-06-04 | 2019-10-22 | United Technologies Corporation | Method for determining a fault within a flow divider |
US11124831B2 (en) * | 2016-08-10 | 2021-09-21 | New York Genome Center | Ultra-low coverage genome sequencing and uses thereof |
FR3055358B1 (fr) * | 2016-08-25 | 2018-08-17 | Safran Aircraft Engines | Procede de gestion d'une panne de vanne de demarrage d'une turbomachine |
US11555638B2 (en) * | 2016-11-30 | 2023-01-17 | Dwyer Instruments, Llc | Venturi vacuum drawback assemblies and dual orifice venturi valve assemblies |
US10920729B2 (en) | 2017-02-08 | 2021-02-16 | Pratt & Whitney Canada Corp. | Method and system for testing operation of solenoid valves |
US10604268B2 (en) * | 2017-02-22 | 2020-03-31 | Pratt & Whitney Canada Corp. | Autothrottle control for turboprop engines |
US11396848B2 (en) | 2019-07-10 | 2022-07-26 | General Electric Company | Modulating fuel for a turbine engine |
FR3103270B1 (fr) * | 2019-11-20 | 2021-12-03 | Safran Aircraft Engines | Procédé et système de détermination du débit massique d’un fluide dans un circuit de fluide pour la commande d’une vanne de dosage du circuit de fluide |
FR3110195B1 (fr) * | 2020-05-18 | 2022-08-19 | Safran Aerosystems | Aéronefs comprenant dans son réservoir de carburant une chambre dotée d'un capteur |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2287102A (en) * | 1994-03-02 | 1995-09-06 | Ford Motor Co | Detection of fuel line pressure regulator malfunction |
US5685268A (en) * | 1996-05-20 | 1997-11-11 | Siemens Automotive Corporation | Fuel leakage detector system |
US5918578A (en) * | 1996-02-29 | 1999-07-06 | Mitsubishi Jidosha Kogyo Kabushiki Kaisha | Fuel feeding system for internal combustion engine |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1539734A (en) * | 1975-06-10 | 1979-01-31 | Rolls Royce | Fuel supply system for a gas turbine engine |
JPS5487319A (en) * | 1977-12-23 | 1979-07-11 | Nissan Motor Co Ltd | Fuel control equipment of gas turbine |
US4608820A (en) * | 1985-05-03 | 1986-09-02 | Chandler Evans Inc. | Dual stepper motor actuator for fuel metering valve |
US6655151B2 (en) * | 2001-09-07 | 2003-12-02 | Honeywell International, Inc. | Method for controlling fuel flow to a gas turbine engine |
US7431015B2 (en) * | 2006-01-31 | 2008-10-07 | Honeywell International Inc. | Fuel metering system proportional bypass valve error compensation system and method |
US7296406B2 (en) * | 2006-02-28 | 2007-11-20 | Honeywell International, Inc. | System for positioning a piston including a fail fixed valve for holding the piston in position during a power interruption and method of using same |
US7836676B2 (en) * | 2007-06-04 | 2010-11-23 | Honeywell International Inc. | Fuel metering valve back-up position control system |
-
2013
- 2013-10-30 FR FR1360636A patent/FR3012420B1/fr active Active
-
2014
- 2014-10-27 WO PCT/FR2014/052723 patent/WO2015063400A2/fr active Application Filing
- 2014-10-27 US US15/033,007 patent/US10082444B2/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2287102A (en) * | 1994-03-02 | 1995-09-06 | Ford Motor Co | Detection of fuel line pressure regulator malfunction |
US5918578A (en) * | 1996-02-29 | 1999-07-06 | Mitsubishi Jidosha Kogyo Kabushiki Kaisha | Fuel feeding system for internal combustion engine |
US5685268A (en) * | 1996-05-20 | 1997-11-11 | Siemens Automotive Corporation | Fuel leakage detector system |
Also Published As
Publication number | Publication date |
---|---|
US10082444B2 (en) | 2018-09-25 |
US20160238484A1 (en) | 2016-08-18 |
FR3012420A1 (fr) | 2015-05-01 |
WO2015063400A2 (fr) | 2015-05-07 |
FR3012420B1 (fr) | 2015-10-23 |
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