FR2354449A1 - Dispositif de mesure de la temperature de l'air penetrant dans le compresseur d'un moteur a turbine a gaz - Google Patents

Dispositif de mesure de la temperature de l'air penetrant dans le compresseur d'un moteur a turbine a gaz

Info

Publication number
FR2354449A1
FR2354449A1 FR7712164A FR7712164A FR2354449A1 FR 2354449 A1 FR2354449 A1 FR 2354449A1 FR 7712164 A FR7712164 A FR 7712164A FR 7712164 A FR7712164 A FR 7712164A FR 2354449 A1 FR2354449 A1 FR 2354449A1
Authority
FR
France
Prior art keywords
compressor
gas turbine
temperature
measuring
particle separator
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.)
Granted
Application number
FR7712164A
Other languages
English (en)
Other versions
FR2354449B1 (fr
Inventor
Neil Roger Brookes
Martin George Ray
Joseph David Cohen
Thomas Joseph Mccarey
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2354449A1 publication Critical patent/FR2354449A1/fr
Application granted granted Critical
Publication of FR2354449B1 publication Critical patent/FR2354449B1/fr
Granted legal-status Critical Current

Links

Classifications

    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00—Thermometers specially adapted for specific purposes
    • G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • G01K13/028—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow for use in total air temperature [TAT] probes
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Measuring Temperature Or Quantity Of Heat (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Measuring Volume Flow (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

Dispositif présentant des temps de réponse améliorés sans nuire au rendement du moteur. Il comprend une canalisation d'amenée 50 qui comporte un orifice d'entrée 52 placée entre l'entrée d'admission du moteur et le séparateur de particule, et un orifice de sortie 54 placé entre le séparateur de particules 18 et le compresseur, de façon à ce que chute de pression dans le séparateur de particules crée une circulation d'air dans la canalisation d'amenée, et une sonde sensible à la température 58 placée dans la première canalisation capable de transmettre à distance des signaux de température. Application aux moteurs à turbine à gaz d'avion.
FR7712164A 1976-04-28 1977-04-22 Dispositif de mesure de la temperature de l'air penetrant dans le compresseur d'un moteur a turbine a gaz Granted FR2354449A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/680,909 US4047379A (en) 1976-04-28 1976-04-28 Transient air temperature sensing system

Publications (2)

Publication Number Publication Date
FR2354449A1 true FR2354449A1 (fr) 1978-01-06
FR2354449B1 FR2354449B1 (fr) 1983-10-28

Family

ID=24733018

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7712164A Granted FR2354449A1 (fr) 1976-04-28 1977-04-22 Dispositif de mesure de la temperature de l'air penetrant dans le compresseur d'un moteur a turbine a gaz

Country Status (6)

Country Link
US (1) US4047379A (fr)
JP (1) JPS605776B2 (fr)
DE (1) DE2718663A1 (fr)
FR (1) FR2354449A1 (fr)
GB (1) GB1515499A (fr)
IT (1) IT1084621B (fr)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4351150A (en) * 1980-02-25 1982-09-28 General Electric Company Auxiliary air system for gas turbine engine
GB2089035B (en) * 1980-12-06 1984-10-24 Rolls Royce Temperature sensor
GB2124706B (en) * 1982-08-04 1986-05-14 Gen Electric Gas turbine engine airflow temperature sensor
US4685942A (en) * 1982-12-27 1987-08-11 General Electric Company Axial flow inlet particle separator
US4608819A (en) * 1983-12-27 1986-09-02 General Electric Company Gas turbine engine component cooling system
US4644806A (en) * 1985-04-22 1987-02-24 General Electric Company Airstream eductor
US5018873A (en) * 1985-04-22 1991-05-28 General Electric Company Air temperature measurement
US4668102A (en) * 1985-05-08 1987-05-26 Honeywell Inc. Temperature and flow station
US4770544A (en) * 1985-11-15 1988-09-13 General Electric Company Temperature sensor
US4948264A (en) * 1986-07-07 1990-08-14 Hook Jr Richard B Apparatus for indirectly determining the temperature of a fluid
US4783026A (en) * 1987-05-22 1988-11-08 Avco Corporation Anti-icing management system
IL84611A (en) * 1987-11-26 1991-11-21 Ardon Gador Apparatus and method for protection against heat
US5040380A (en) * 1988-08-04 1991-08-20 Super S.E.E.R. Systems Inc. Method and apparatus for the sensing of refrigerant temperatures and the control of refrigerant loading
US5182906A (en) * 1990-10-22 1993-02-02 General Electric Company Hybrid spinner nose configuration in a gas turbine engine having a bypass duct
US5220785A (en) * 1991-07-15 1993-06-22 United Technologies Corporation Side discharge anti-ice manifold
US5302026A (en) * 1992-07-16 1994-04-12 Rosemount, Inc. Temperature probe with fast response time
IL109388A0 (en) * 1993-04-29 1994-07-31 Rosemount Aerospace Inc Temperature sensor with integral debris guard
US5397181A (en) * 1993-10-21 1995-03-14 General Electric Company Compressor discharge temperature sensing system
US5653538A (en) * 1995-06-07 1997-08-05 Rosemount Aerospace Inc. Total temperature probe
US5867977A (en) * 1996-05-14 1999-02-09 The Dow Chemical Company Method and apparatus for achieving power augmentation in gas turbines via wet compression
US5930990A (en) * 1996-05-14 1999-08-03 The Dow Chemical Company Method and apparatus for achieving power augmentation in gas turbines via wet compression
US6609825B2 (en) * 2001-09-21 2003-08-26 Rosemount Aerospace Inc. Total air temperature probe providing improved anti-icing performance and reduced deicing heater error
US6827485B2 (en) * 2002-07-16 2004-12-07 Rosemount Aerospace Inc. Fast response temperature sensor
ITMI20032586A1 (it) * 2003-12-23 2005-06-24 Nuovo Pignone Spa Sistema di montaggio di una termocoppia per una turbina a gas
US7357572B2 (en) * 2005-09-20 2008-04-15 Rosemount Aerospace Inc. Total air temperature probe having improved deicing heater error performance
JP4672565B2 (ja) * 2006-02-06 2011-04-20 三菱重工業株式会社 温度計測装置、燃焼監視装置、及び、ガスタービン
US7313963B2 (en) 2006-02-28 2008-01-01 General Electric Company Isothermal de-iced sensor
US7328623B2 (en) 2006-03-20 2008-02-12 General Electric Company Temperature and/or pressure sensor assembly
US20080047425A1 (en) * 2006-08-23 2008-02-28 United Technologies Corporation Mission adaptable inlet particle separator
DE102006040757A1 (de) 2006-08-31 2008-04-30 Rolls-Royce Deutschland Ltd & Co Kg Fluidrückführung im Trennkörper von Strömungsarbeitsmaschinen mit Nebenstromkonfiguration
US7828477B2 (en) * 2007-05-14 2010-11-09 Rosemount Aerospace Inc. Aspirated enhanced total air temperature probe
US8392141B2 (en) * 2009-11-02 2013-03-05 Rosemount Aerospace Inc. Total air temperature probe and method for reducing de-icing/anti-icing heater error
DE102010014900A1 (de) 2010-04-14 2011-10-20 Rolls-Royce Deutschland Ltd & Co Kg Nebenstromkanal eines Turbofantriebwerkes
US8945254B2 (en) 2011-12-21 2015-02-03 General Electric Company Gas turbine engine particle separator
US8452516B1 (en) 2012-01-31 2013-05-28 United Technologies Corporation Variable vane scheduling based on flight conditions for inclement weather
US10202185B2 (en) 2014-06-10 2019-02-12 United Technologies Corporation Geared turbofan with improved spinner
GB201416928D0 (en) * 2014-09-25 2014-11-12 Rolls Royce Plc A gas turbine and a method of washing a gas turbine engine
US20160376010A1 (en) * 2015-06-26 2016-12-29 Rosemount Aerospace Inc. Systems and methods for preventing ice accumulation
CN105114180A (zh) * 2015-08-26 2015-12-02 成都博世德能源科技股份有限公司 一种用于燃气轮机的保温式进气系统
US10578498B2 (en) * 2017-06-22 2020-03-03 Unison Industries, Llc Air temperature sensor
US10605675B2 (en) * 2017-06-22 2020-03-31 Unison Industries, Llc Air temperature sensor
US11143193B2 (en) * 2019-01-02 2021-10-12 Danfoss A/S Unloading device for HVAC compressor with mixed and radial compression stages
US11840346B2 (en) * 2022-03-28 2023-12-12 Pratt & Whitney Canada Corp. Strut for aircraft engine
US11821363B1 (en) * 2022-05-06 2023-11-21 Pratt & Whitney Canada Corp. Apparatus for removing particulate matter from bleed gas and gas turbine engine including same

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB734702A (en) * 1952-12-16 1955-08-03 Rolls Royce Improvements in measuring gas temperatures
GB746596A (en) * 1953-01-26 1956-03-14 Rolls Royce Improvements in or relating to gas turbine engines having multi-stage compressors
US3000213A (en) * 1955-08-08 1961-09-19 Cook Electric Co Fluid testing probe
CH357885A (de) * 1960-05-06 1961-10-31 Sulzer Ag Anordnung zur Temperaturmessung eines durch eine Rohrleitung strömenden Mediums
GB1029522A (en) * 1964-01-22 1966-05-11 Bristol Siddeley Engines Ltd Apparatus for measuring the temperature of a gas flow
FR2009192A1 (fr) * 1968-05-23 1970-01-30 Rosemount Eng Co Ltd
US3597920A (en) * 1969-08-21 1971-08-10 Chandler Evans Inc Turbine inlet temperature sensor and computer
US3623367A (en) * 1969-12-23 1971-11-30 Westinghouse Electric Corp Apparatus for measuring the average temperature of a gas stream
FR2160993A1 (fr) * 1971-11-23 1973-07-06 Gen Electric
US3940988A (en) * 1974-03-11 1976-03-02 John Zink Company Velocity thermocouple

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE532567A (fr) *
DE951239C (de) * 1953-11-06 1956-10-25 Sulzer Ag Temperaturmesseinrichtung
US3167960A (en) * 1961-08-07 1965-02-02 Holley Carburetor Co Temperature probe
US3832086A (en) * 1971-11-23 1974-08-27 Gen Electric Particle separator with scroll scavenging means

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB734702A (en) * 1952-12-16 1955-08-03 Rolls Royce Improvements in measuring gas temperatures
GB746596A (en) * 1953-01-26 1956-03-14 Rolls Royce Improvements in or relating to gas turbine engines having multi-stage compressors
US3000213A (en) * 1955-08-08 1961-09-19 Cook Electric Co Fluid testing probe
CH357885A (de) * 1960-05-06 1961-10-31 Sulzer Ag Anordnung zur Temperaturmessung eines durch eine Rohrleitung strömenden Mediums
GB1029522A (en) * 1964-01-22 1966-05-11 Bristol Siddeley Engines Ltd Apparatus for measuring the temperature of a gas flow
FR2009192A1 (fr) * 1968-05-23 1970-01-30 Rosemount Eng Co Ltd
US3597920A (en) * 1969-08-21 1971-08-10 Chandler Evans Inc Turbine inlet temperature sensor and computer
US3623367A (en) * 1969-12-23 1971-11-30 Westinghouse Electric Corp Apparatus for measuring the average temperature of a gas stream
FR2160993A1 (fr) * 1971-11-23 1973-07-06 Gen Electric
US3940988A (en) * 1974-03-11 1976-03-02 John Zink Company Velocity thermocouple

Also Published As

Publication number Publication date
JPS52139815A (en) 1977-11-22
JPS605776B2 (ja) 1985-02-14
DE2718663A1 (de) 1977-11-10
IT1084621B (it) 1985-05-25
FR2354449B1 (fr) 1983-10-28
US4047379A (en) 1977-09-13
GB1515499A (en) 1978-06-28
DE2718663C2 (fr) 1989-02-09

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Legal Events

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DL Decision of the director general to leave to make available licences of right
ST Notification of lapse