FR2996257B1 - Procede et un dispositif de determination du prelevement d'air sur un turboreacteur d'aeronef - Google Patents

Procede et un dispositif de determination du prelevement d'air sur un turboreacteur d'aeronef

Info

Publication number
FR2996257B1
FR2996257B1 FR1259405A FR1259405A FR2996257B1 FR 2996257 B1 FR2996257 B1 FR 2996257B1 FR 1259405 A FR1259405 A FR 1259405A FR 1259405 A FR1259405 A FR 1259405A FR 2996257 B1 FR2996257 B1 FR 2996257B1
Authority
FR
France
Prior art keywords
turbojet engine
air collection
determining air
aircraft turbojet
aircraft
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
FR1259405A
Other languages
English (en)
Other versions
FR2996257A1 (fr
Inventor
Bruno Robert Gaully
Jerome Guy Roger Sebaa
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 FR1259405A priority Critical patent/FR2996257B1/fr
Priority to US14/043,140 priority patent/US9310276B2/en
Publication of FR2996257A1 publication Critical patent/FR2996257A1/fr
Application granted granted Critical
Publication of FR2996257B1 publication Critical patent/FR2996257B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • G01M15/02—Details or accessories of testing apparatus
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • 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
    • F05D2260/84—Redundancy
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/10—Purpose of the control system to cope with, or avoid, compressor flow instabilities
    • F05D2270/101—Compressor surge or stall
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • F05D2270/3013—Outlet pressure
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • F05D2270/3015—Pressure differential pressure
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Measuring Fluid Pressure (AREA)
FR1259405A 2012-10-03 2012-10-03 Procede et un dispositif de determination du prelevement d'air sur un turboreacteur d'aeronef Active FR2996257B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1259405A FR2996257B1 (fr) 2012-10-03 2012-10-03 Procede et un dispositif de determination du prelevement d'air sur un turboreacteur d'aeronef
US14/043,140 US9310276B2 (en) 2012-10-03 2013-10-01 Method and device for determining the air bleed on an aircraft turbojet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1259405A FR2996257B1 (fr) 2012-10-03 2012-10-03 Procede et un dispositif de determination du prelevement d'air sur un turboreacteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2996257A1 FR2996257A1 (fr) 2014-04-04
FR2996257B1 true FR2996257B1 (fr) 2014-10-10

Family

ID=47356144

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1259405A Active FR2996257B1 (fr) 2012-10-03 2012-10-03 Procede et un dispositif de determination du prelevement d'air sur un turboreacteur d'aeronef

Country Status (2)

Country Link
US (1) US9310276B2 (fr)
FR (1) FR2996257B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170067578A1 (en) * 2015-09-09 2017-03-09 Honeywell International Inc. Detection of high stage valve leakage by pressure lockup
FR3072723B1 (fr) 2017-10-20 2019-11-01 Safran Aircraft Engines Procede et systeme de regulation d'une temperature associee a un ensemble d'echange thermique d'une turbomachine
US10822996B2 (en) 2018-03-12 2020-11-03 General Electric Company Gas turbine engine health determination
US10974835B2 (en) * 2018-03-19 2021-04-13 Hamilton Sundstrand Corporation Bleed air temperature and flow control system
US10801509B2 (en) * 2018-07-26 2020-10-13 Honeywell International Inc. Bleed air selector valve
FR3097963B1 (fr) * 2019-06-27 2021-06-04 Liebherr Aerospace Toulouse Sas Surveillance de l’état d’un échangeur dans un circuit d’air d’un aéronef
FR3105300B1 (fr) * 2019-12-24 2022-06-17 Safran Aircraft Engines Procédé de commande d’une vanne haute pression d’un système de prélèvement d’air d’un turboréacteur d’aéronef
CN111984514B (zh) * 2020-09-02 2023-05-23 大连大学 基于Prophet-bLSTM-DTW的日志异常检测方法
US11549446B1 (en) 2022-02-04 2023-01-10 Pratt & Whitney Canada Corp. Method and apparatus for measuring compressor bleed flow

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5155991A (en) * 1991-04-01 1992-10-20 United Technologies Corporation Bleed air flow regulators with flow balance
US5161364A (en) * 1991-04-01 1992-11-10 United Technologies Corporation Control of aircraft bleed air stage mixing
US6494047B2 (en) * 2000-12-07 2002-12-17 Honeywell International Inc. Airflow sharing
GB0224625D0 (en) * 2002-10-23 2002-12-04 Honeywell Normalair Garrett Method of balancing the supply of bleed air from a plurality of engines
US7536865B2 (en) * 2005-02-09 2009-05-26 Honeywell International Inc. Method and system for balancing bleed flows from gas turbine engines
JP4332740B2 (ja) * 2005-04-08 2009-09-16 株式会社島津製作所 航空機用抽気システム
US8033118B2 (en) * 2008-01-31 2011-10-11 EMBRAER—Empresa Brasileira de Aeronautica S.A. Bleed airflow balancing control using simplified sensing
US8452515B2 (en) * 2011-09-15 2013-05-28 General Electric Company System and method for simulating a gas turbine compressor

Also Published As

Publication number Publication date
US9310276B2 (en) 2016-04-12
US20140090458A1 (en) 2014-04-03
FR2996257A1 (fr) 2014-04-04

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