FR3012420B1 - Procede de detection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aeronef - Google Patents

Procede de detection d'une panne d'une vanne de retour de carburant d'un circuit carburant d'un moteur d'aeronef

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Publication number
FR3012420B1
FR3012420B1 FR1360636A FR1360636A FR3012420B1 FR 3012420 B1 FR3012420 B1 FR 3012420B1 FR 1360636 A FR1360636 A FR 1360636A FR 1360636 A FR1360636 A FR 1360636A FR 3012420 B1 FR3012420 B1 FR 3012420B1
Authority
FR
France
Prior art keywords
fuel
failure
detecting
return valve
aircraft engine
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.)
Active
Application number
FR1360636A
Other languages
English (en)
Other versions
FR3012420A1 (fr
Inventor
Antoine Veyrat-Masson
Nicolas Gomes
Lauranne Mottet
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1360636A priority Critical patent/FR3012420B1/fr
Priority to US15/033,007 priority patent/US10082444B2/en
Priority to PCT/FR2014/052723 priority patent/WO2015063400A2/fr
Publication of FR3012420A1 publication Critical patent/FR3012420A1/fr
Application granted granted Critical
Publication of FR3012420B1 publication Critical patent/FR3012420B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00Testing of engines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/005Accessories not provided for in the groups B64D37/02 - B64D37/28
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/14Filling or emptying
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/32Safety measures not otherwise provided for, e.g. preventing explosive conditions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/22Fuel supply systems
    • F02C7/232Fuel valves; Draining valves or systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K37/00Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K37/00Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
    • F16K37/0025Electrical or magnetic means
    • F16K37/005Electrical or magnetic means for measuring fluid parameters
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00Details 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
    • G01L19/0092Pressure sensor associated with other sensors, e.g. for measuring acceleration or temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/80Diagnostics

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)
FR1360636A 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 Active FR3012420B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
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
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
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

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
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
FR3012420A1 FR3012420A1 (fr) 2015-05-01
FR3012420B1 true FR3012420B1 (fr) 2015-10-23

Family

ID=49876882

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1360636A Active 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

Country Status (3)

Country Link
US (1) US10082444B2 (fr)
FR (1) FR3012420B1 (fr)
WO (1) WO2015063400A2 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
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
CN109863249A (zh) * 2016-08-10 2019-06-07 纽约基因组中心 超低覆盖度基因组测序及其应用
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

Family Cites Families (10)

* Cited by examiner, † Cited by third party
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
US5493902A (en) * 1994-03-02 1996-02-27 Ford Motor Company On-board detection of pressure regulator malfunction
JP3000675B2 (ja) * 1996-02-29 2000-01-17 三菱自動車工業株式会社 内燃機関用燃料供給装置
US5685268A (en) * 1996-05-20 1997-11-11 Siemens Automotive Corporation Fuel leakage detector system
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

Also Published As

Publication number Publication date
FR3012420A1 (fr) 2015-05-01
US20160238484A1 (en) 2016-08-18
US10082444B2 (en) 2018-09-25
WO2015063400A3 (fr) 2015-09-11
WO2015063400A2 (fr) 2015-05-07

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