JPS6349056B2 - - Google Patents

Info

Publication number
JPS6349056B2
JPS6349056B2 JP55006386A JP638680A JPS6349056B2 JP S6349056 B2 JPS6349056 B2 JP S6349056B2 JP 55006386 A JP55006386 A JP 55006386A JP 638680 A JP638680 A JP 638680A JP S6349056 B2 JPS6349056 B2 JP S6349056B2
Authority
JP
Japan
Prior art keywords
leading edge
band platform
airfoil
measurement probe
edge portion
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.)
Expired
Application number
JP55006386A
Other languages
English (en)
Japanese (ja)
Other versions
JPS55113924A (en
Inventor
Kureigu Sukotsuto Jon
Jirugu Hoiyaa Jon
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 JPS55113924A publication Critical patent/JPS55113924A/ja
Publication of JPS6349056B2 publication Critical patent/JPS6349056B2/ja
Granted legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K1/00—Details of thermometers not specially adapted for particular types of thermometer
    • G01K1/14—Supports; Fastening devices; Arrangements for mounting thermometers in particular locations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/02—Arrangement of sensing elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/68—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using thermal effects
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/68—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using thermal effects
    • G01F1/684—Structural arrangements; Mounting of elements, e.g. in relation to fluid flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Measuring Fluid Pressure (AREA)
  • Measuring Temperature Or Quantity Of Heat (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Control Of Turbines (AREA)
JP638680A 1979-02-01 1980-01-24 Measuring probe Granted JPS55113924A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/008,361 US4244222A (en) 1979-02-01 1979-02-01 Instrumentation probe

Publications (2)

Publication Number Publication Date
JPS55113924A JPS55113924A (en) 1980-09-02
JPS6349056B2 true JPS6349056B2 (US20100268047A1-20101021-C00003.png) 1988-10-03

Family

ID=21731198

Family Applications (1)

Application Number Title Priority Date Filing Date
JP638680A Granted JPS55113924A (en) 1979-02-01 1980-01-24 Measuring probe

Country Status (7)

Country Link
US (1) US4244222A (US20100268047A1-20101021-C00003.png)
JP (1) JPS55113924A (US20100268047A1-20101021-C00003.png)
CA (1) CA1135978A (US20100268047A1-20101021-C00003.png)
DE (1) DE3003169A1 (US20100268047A1-20101021-C00003.png)
FR (1) FR2448136A1 (US20100268047A1-20101021-C00003.png)
GB (1) GB2041104B (US20100268047A1-20101021-C00003.png)
IT (1) IT1129776B (US20100268047A1-20101021-C00003.png)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2124706B (en) * 1982-08-04 1986-05-14 Gen Electric Gas turbine engine airflow temperature sensor
US4467134A (en) * 1983-06-30 1984-08-21 General Electric Company Thermocouple with out-of-line aspiration holes
US4605315A (en) * 1984-12-13 1986-08-12 United Technologies Corporation Temperature probe for rotating machinery
US4595298A (en) * 1985-05-01 1986-06-17 The United States Of America As Represented By The Secretary Of The Air Force Temperature detection system for use on film cooled turbine airfoils
US5185996A (en) * 1990-12-21 1993-02-16 Allied-Signal Inc. Gas turbine engine sensor probe
CA2103782A1 (en) * 1992-08-31 1994-03-01 Robert Frank Tammera Aerodynamic instrumentation probe
US5632556A (en) * 1993-11-29 1997-05-27 Sivco, Inc. Thermowell apparatus for sensing temperature in petrochemical applications
DE4421807A1 (de) * 1994-06-22 1996-01-04 Abb Management Ag Emissionssonde zur Entnahme von Abgas aus der Brennkammer einer Gasturbine sowie Verfahren zur Herstellung und Anwendung derselben
DE19618588A1 (de) * 1996-05-09 1997-11-13 Asea Brown Boveri Temperatursonde
GB2370632B (en) * 2000-11-30 2004-11-17 Rolls Royce Plc A gas turbine engine guide vane and temperature monitor therefor
JP3749135B2 (ja) * 2001-03-13 2006-02-22 横河電子機器株式会社 温度測定装置
US6843061B2 (en) * 2002-02-15 2005-01-18 Siemens Westinghouse Power Corporation Gas turbine with flexible combustion sensor connection
US7111982B1 (en) 2004-01-30 2006-09-26 Swonger Jr Karl William Combined temperature and pressure probe for a gas turbine engine
US7056085B2 (en) * 2004-07-09 2006-06-06 General Electric Company Methods and apparatus for sensing parameters of air flows
FR2933884B1 (fr) * 2008-07-16 2012-07-27 Snecma Procede de fabrication d'une piece d'aubage.
CN103056599B (zh) * 2011-10-24 2015-10-28 沈阳黎明航空发动机(集团)有限责任公司 一种精密多连铸叶片蜡模叶身成型活块的制备方法
US8888442B2 (en) * 2012-01-30 2014-11-18 Pratt & Whitney Canada Corp. Stress relieving slots for turbine vane ring
GB201213576D0 (en) * 2012-07-31 2012-09-12 Rolls Royce Plc Total temperature probe
US9488534B2 (en) 2013-09-05 2016-11-08 Rosemount Aerospace Inc. Supercritical total air temperature sensors
US9624787B2 (en) 2013-09-30 2017-04-18 Rosemount Aerospace Inc. Total air temperature sensors
FR3012169B1 (fr) * 2013-10-21 2018-01-12 Safran Aircraft Engines Pale instrumentee
FR3025885B1 (fr) * 2014-09-15 2017-11-24 Snecma Dispositif de mesure de grandeurs aerodynamiques destine a etre place dans une veine d'ecoulement d'une turbomachine
CN104439062B (zh) * 2014-12-08 2016-11-16 中国南方航空工业(集团)有限公司 用于铸造过程中测量温度的模具及其制造方法
FR3043775B1 (fr) * 2015-11-12 2017-11-10 Snecma Dispositif de mesure de grandeurs aerodynamiques destine a etre place dans une veine d'ecoulement d'une turbomachine
US10704413B2 (en) * 2018-09-06 2020-07-07 Raytheon Technologies Corporation Systems and methods for variable alignment aerodynamic probes
FR3087829B1 (fr) * 2018-10-29 2022-11-11 Safran Aircraft Engines Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module
US11230927B2 (en) 2019-06-03 2022-01-25 Raytheon Technologies Corporation Vane airfoil shapes for embedded members
US20220090513A1 (en) * 2020-09-18 2022-03-24 Ge Avio S.R.L. Probe placement within a duct of a gas turbine engine
US11692455B1 (en) * 2022-09-19 2023-07-04 Pratt & Whitney Canada Corp. Passively orientable pressure probe

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2291448A (en) * 1939-10-28 1942-07-28 Standard Oil Dev Co Shielded high velocity thermocouple
US2688844A (en) * 1945-03-05 1954-09-14 Power Jets Res & Dev Ltd Rotary compressor and its control, and application thereof in combustion turbine power plant
US2756596A (en) * 1952-03-14 1956-07-31 Gen Motors Corp Compressor temperature sensing system
GB759268A (en) * 1953-07-14 1956-10-17 Power Jets Res & Dev Ltd Method of mounting instruments in turbines and compressors
CH326686A (de) * 1953-07-14 1957-12-31 Power Jets Res & Dev Ltd Leitschaufel einer Turbomaschine mit eingebautem Messinstrument
US2971997A (en) * 1958-03-06 1961-02-14 Gen Motors Corp Sampling thermocouple
DE1133912B (de) * 1959-03-02 1962-07-26 Dr Hermann C Schutt Umleitungsstueck fuer einen Stroemungskanal mit Temperaturfuehler
GB1088032A (en) * 1964-06-12 1967-10-18 English Electric Co Ltd Turbine blades
US3451862A (en) * 1966-09-06 1969-06-24 Usa Temperature sensor probe
US3653976A (en) * 1967-05-05 1972-04-04 Gen Motors Corp Thermocouple probe assembly with nickel aluminide tip
US3592061A (en) * 1969-08-22 1971-07-13 Gen Motors Corp Gas turbine airfoil having integral thermocouple
US3940988A (en) * 1974-03-11 1976-03-02 John Zink Company Velocity thermocouple

Also Published As

Publication number Publication date
DE3003169A1 (de) 1980-08-14
US4244222A (en) 1981-01-13
GB2041104A (en) 1980-09-03
GB2041104B (en) 1983-07-27
CA1135978A (en) 1982-11-23
IT1129776B (it) 1986-06-11
FR2448136A1 (fr) 1980-08-29
IT8019420A0 (it) 1980-01-24
FR2448136B1 (US20100268047A1-20101021-C00003.png) 1984-10-26
JPS55113924A (en) 1980-09-02

Similar Documents

Publication Publication Date Title
JPS6349056B2 (US20100268047A1-20101021-C00003.png)
US7631484B2 (en) High pressure ratio aft fan
US4604031A (en) Hollow fluid cooled turbine blades
US11353370B2 (en) Air temperature sensor
EP3205826A1 (en) Airfoil assembly with leading edge element
US7410343B2 (en) Gas turbine
US10605675B2 (en) Air temperature sensor
US20200291801A1 (en) Turbine engine airfoil and method
JP2017082771A (ja) タービンブレード
US11952900B2 (en) Variable guide vane sealing
JP2001200704A (ja) ガスタービン・エンジンの冷却された翼形部及びその製造方法
CA2956979A1 (en) Impingement holes for a turbine engine component
US10443400B2 (en) Airfoil for a turbine engine
EP3431710A1 (en) Shield for a turbine engine airfoil
US20230243268A1 (en) Airfoils for gas turbine engines
US10815821B2 (en) Variable airfoil with sealed flowpath
EP3418703B1 (en) Air temperature sensor
US11624662B2 (en) Exhaust gas temperature sensor
US20200041352A1 (en) Air temperature sensor having a bushing
US20180363482A1 (en) Shroud for a turbine engine
US11939880B1 (en) Airfoil assembly with flow surface
EP3677750B1 (en) Gas turbine engine component with a trailing edge discharge slot
USRE32238E (en) Turbine arrangement