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GB759268A - Method of mounting instruments in turbines and compressors - Google Patents

Method of mounting instruments in turbines and compressors

Info

Publication number
GB759268A
GB759268A GB19476/53A GB1947653A GB759268A GB 759268 A GB759268 A GB 759268A GB 19476/53 A GB19476/53 A GB 19476/53A GB 1947653 A GB1947653 A GB 1947653A GB 759268 A GB759268 A GB 759268A
Authority
GB
United Kingdom
Prior art keywords
tube
compressors
turbines
july
mounting instruments
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
GB19476/53A
Inventor
John Douglas Annear
Harry White
Samuel Leonard Holt
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB19476/53A priority Critical patent/GB759268A/en
Priority to US442246A priority patent/US2946221A/en
Publication of GB759268A publication Critical patent/GB759268A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

759,268. Measuring temperature. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. July 5, 1954 [July 11, 1953], No. 19476/53. Class 40(1) [Also in Group XXVI] A. thermocouple enclosed, except for the junction, in a refractory tube 12, is arranged in a tube 4 mounted in a recess of the leading edge of a stator guide vane 2 of a turbine or compressor and deformed to the contour of the vane. The tube 4 is notched at 11 to provide a fluid inlet and drilled at 14 to provide an outlet.
GB19476/53A 1953-07-14 1953-07-14 Method of mounting instruments in turbines and compressors Expired GB759268A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB19476/53A GB759268A (en) 1953-07-14 1953-07-14 Method of mounting instruments in turbines and compressors
US442246A US2946221A (en) 1953-07-14 1954-07-09 Stator blade mounting of condition sensing elements in fluid flow machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19476/53A GB759268A (en) 1953-07-14 1953-07-14 Method of mounting instruments in turbines and compressors

Publications (1)

Publication Number Publication Date
GB759268A true GB759268A (en) 1956-10-17

Family

ID=10129998

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19476/53A Expired GB759268A (en) 1953-07-14 1953-07-14 Method of mounting instruments in turbines and compressors

Country Status (2)

Country Link
US (1) US2946221A (en)
GB (1) GB759268A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4244222A (en) * 1979-02-01 1981-01-13 General Electric Company Instrumentation probe
FR2629871A1 (en) * 1988-04-07 1989-10-13 Messerschmitt Boelkow Blohm THRUST VECTOR CONTROL, IMPROVING THE MANEUVERABILITY OF PROPELLANT AIRCRAFT BY REACTION AND METHOD OF USING THE SAME
EP1615002A1 (en) * 2004-07-09 2006-01-11 General Electric Company Vane assembly and method for measuring a physical property of an air flow
GB2614367A (en) * 2021-12-22 2023-07-05 Unison Ind Llc Turbine engine exhaust gas temperature sensor

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4063228A (en) * 1976-12-22 1977-12-13 General Electric Company Moisture detector for steam line
US4244221A (en) * 1979-02-01 1981-01-13 General Electric Company Removable instrumentation probe
GB9720719D0 (en) * 1997-10-01 1997-11-26 Rolls Royce Plc Gas Turbine Engine Gas Temperature Sensing Device
EP1860282A1 (en) * 2006-05-24 2007-11-28 Siemens Aktiengesellschaft Compressor airfoil with integrated sensing elements and associated compressor
US9207128B2 (en) * 2012-06-05 2015-12-08 General Electric Company Dynamic fiber temperature sensing package and method of assembling the same
FR3012169B1 (en) * 2013-10-21 2018-01-12 Safran Aircraft Engines INSTRUMENTED BLADE
RU2017134423A (en) * 2015-04-23 2019-05-23 Нуово Пиньоне Текнолоджи Срл Measurement of total fluid pressure in a turbomachine
FR3066779B1 (en) * 2017-05-26 2020-04-03 Safran Aircraft Engines DEVICE FOR MEASURING PARAMETERS OF AN AERODYNAMIC FLOW FOR A TURBOMACHINE BLADE, BLADE AND A TURBOMACHINE BLADE EQUIPPED WITH SAID MEASUREMENT DEVICE
FR3072169B1 (en) * 2017-10-09 2019-10-11 Safran Aircraft Engines DEVICE FOR MEASURING AT LEAST ONE PARAMETER OF AERODYNAMIC FLOW OF A TURBOMACHINE EQUIPPED WITH A VIBRATION DAMPING MEANS AND TURBOMACHINE VEIN EQUIPPED WITH SUCH A DEVICE
US11230927B2 (en) 2019-06-03 2022-01-25 Raytheon Technologies Corporation Vane airfoil shapes for embedded members
US11840346B2 (en) * 2022-03-28 2023-12-12 Pratt & Whitney Canada Corp. Strut for aircraft engine
US11692455B1 (en) * 2022-09-19 2023-07-04 Pratt & Whitney Canada Corp. Passively orientable pressure probe

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1885933A (en) * 1928-10-18 1932-11-01 Nat Lock Washer Co Boat meter
US2057645A (en) * 1934-01-08 1936-10-13 Erwin H Hamilton Pressure gauge
US2179500A (en) * 1937-12-01 1939-11-14 Walter S Diehl Pitot-static tube
US2411484A (en) * 1944-06-09 1946-11-19 Budd Co Air speed indicator
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
US2709979A (en) * 1950-07-14 1955-06-07 Hydrofoil Corp Hydrofoil craft
US2741919A (en) * 1952-01-14 1956-04-17 Gen Motors Corp Compressor temperature sensing device
US2756596A (en) * 1952-03-14 1956-07-31 Gen Motors Corp Compressor temperature sensing system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4244222A (en) * 1979-02-01 1981-01-13 General Electric Company Instrumentation probe
FR2629871A1 (en) * 1988-04-07 1989-10-13 Messerschmitt Boelkow Blohm THRUST VECTOR CONTROL, IMPROVING THE MANEUVERABILITY OF PROPELLANT AIRCRAFT BY REACTION AND METHOD OF USING THE SAME
EP1615002A1 (en) * 2004-07-09 2006-01-11 General Electric Company Vane assembly and method for measuring a physical property of an air flow
JP2006022806A (en) * 2004-07-09 2006-01-26 General Electric Co <Ge> Method and device for detecting parameter of air stream
GB2614367A (en) * 2021-12-22 2023-07-05 Unison Ind Llc Turbine engine exhaust gas temperature sensor
US12092025B2 (en) 2021-12-22 2024-09-17 Unison Industries, Llc Turbine engine exhaust gas temperature sensor
GB2614367B (en) * 2021-12-22 2024-12-11 Unison Ind Llc Turbine engine exhaust gas temperature sensor

Also Published As

Publication number Publication date
US2946221A (en) 1960-07-26

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