GB2452026B - Instrumentation rake and aerofoil having instrumentation elements and method of manufacture therefor - Google Patents

Instrumentation rake and aerofoil having instrumentation elements and method of manufacture therefor

Info

Publication number
GB2452026B
GB2452026B GB0714652A GB0714652A GB2452026B GB 2452026 B GB2452026 B GB 2452026B GB 0714652 A GB0714652 A GB 0714652A GB 0714652 A GB0714652 A GB 0714652A GB 2452026 B GB2452026 B GB 2452026B
Authority
GB
United Kingdom
Prior art keywords
instrumentation
aerofoil
rake
elements
manufacture therefor
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 - Fee Related
Application number
GB0714652A
Other versions
GB2452026A (en
GB2452026A9 (en
GB0714652D0 (en
Inventor
Robert Gilbert Hemmings
Barry L Stephens
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.)
ASSYSTEM
Original Assignee
ASSYSTEM
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 ASSYSTEM filed Critical ASSYSTEM
Priority to GB0714652A priority Critical patent/GB2452026B/en
Publication of GB0714652D0 publication Critical patent/GB0714652D0/en
Publication of GB2452026A publication Critical patent/GB2452026A/en
Publication of GB2452026A9 publication Critical patent/GB2452026A9/en
Application granted granted Critical
Publication of GB2452026B publication Critical patent/GB2452026B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • 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
    • 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
    • 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
    • G01F1/05—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 mechanical effects
    • G01F1/34—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 mechanical effects by measuring pressure or differential pressure
    • G01F1/36—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 mechanical effects by measuring pressure or differential pressure the pressure or differential pressure being created by the use of flow constriction
    • G01F1/40—Details of construction of the flow constriction devices
    • G01F1/46—Pitot tubes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00—Details 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
    • G01M9/065—Measuring arrangements specially adapted for aerodynamic testing dealing with flow
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • G01P5/165—Arrangements or constructions of Pitot tubes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00—Products made by additive manufacturing

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB0714652A 2007-07-27 2007-07-27 Instrumentation rake and aerofoil having instrumentation elements and method of manufacture therefor Expired - Fee Related GB2452026B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0714652A GB2452026B (en) 2007-07-27 2007-07-27 Instrumentation rake and aerofoil having instrumentation elements and method of manufacture therefor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0714652A GB2452026B (en) 2007-07-27 2007-07-27 Instrumentation rake and aerofoil having instrumentation elements and method of manufacture therefor

Publications (4)

Publication Number Publication Date
GB0714652D0 GB0714652D0 (en) 2007-09-05
GB2452026A GB2452026A (en) 2009-02-25
GB2452026A9 GB2452026A9 (en) 2009-07-08
GB2452026B true GB2452026B (en) 2010-05-05

Family

ID=38512961

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0714652A Expired - Fee Related GB2452026B (en) 2007-07-27 2007-07-27 Instrumentation rake and aerofoil having instrumentation elements and method of manufacture therefor

Country Status (1)

Country Link
GB (1) GB2452026B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10717514B2 (en) 2018-03-09 2020-07-21 Senior Ip Gmbh Integrated drain mast structure
RU2757091C2 (en) * 2017-05-05 2021-10-11 Сафран Аэро Бустерс Са Turbulence sensor of turbomachine compressor

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DE102008025869A1 (en) * 2008-05-31 2009-12-03 Mtu Aero Engines Gmbh Measuring probe and method for producing a measuring probe
FR2952713B1 (en) * 2009-11-16 2014-01-03 Snecma PROCESS FOR MANUFACTURING A MEASURING COMB WITH MEASURING MEANS FOR MEASURING PARAMETERS IN AN EXPERIMENTAL TURBOJET AIR FLOW
DE102009057875A1 (en) * 2009-12-11 2011-06-16 Mtu Aero Engines Gmbh Shovel, particularly guide vane for combustion turbine, comprises aerodynamically formed sheet, front edge, rear edge, and primary surface that range from front edge up to rear edge
US8011251B1 (en) * 2010-03-24 2011-09-06 General Electric Company Bifurcated pressure instrumentation rake
US20120096961A1 (en) * 2010-10-21 2012-04-26 General Electric Company Probe holder for turbine engine sensor
US8944678B2 (en) 2011-05-13 2015-02-03 General Electric Company Instrumentation rake assembly
US9289826B2 (en) 2012-09-17 2016-03-22 Honeywell International Inc. Turbine stator airfoil assemblies and methods for their manufacture
US20140182292A1 (en) * 2012-12-29 2014-07-03 United Technologies Corporation Integral instrumentation in additively manufactured components of gas turbine engines
US9027392B2 (en) 2013-05-07 2015-05-12 Honeywell International Inc. Multi-hole probes and methods for manufacturing multi-hole probes
FR3012169B1 (en) 2013-10-21 2018-01-12 Safran Aircraft Engines INSTRUMENTED BLADE
EP3102806B1 (en) * 2014-02-05 2020-09-09 United Technologies Corporation Pressure probe for gas turbine
FR3017459B1 (en) 2014-02-07 2017-07-21 Snecma AUBE INSTRUMENTEE A TUBE REPORTED IN A GROOVE
FR3021741B1 (en) 2014-05-27 2017-11-24 Snecma METHOD FOR MEASURING THE FLOW OF GAS AT THE EXIT OF A TURBOMACHINE COMBUSTION CHAMBER
EP2949864B1 (en) * 2014-05-28 2017-07-05 Ansaldo Energia IP UK Limited Component with sensor and sensor installation method
FR3025884B1 (en) * 2014-09-15 2016-12-23 Snecma RADIAL ARM FOR MEASURING REPRESENTATIVE FLOW VALUES FOR TURBOMACHINE
CN104483454A (en) * 2014-12-30 2015-04-01 国家电网公司 Gas detecting joint device
US20160238456A1 (en) * 2015-02-12 2016-08-18 Rosemount Aerospace Inc. Air temperature sensor and fabrication
CN104764475A (en) * 2015-03-10 2015-07-08 中国船舶重工集团公司第七�三研究所 Measurement probe rotating mechanism
FR3039515B1 (en) * 2015-07-28 2017-09-01 Thales Sa HEATING FOR AERONAUTICAL EQUIPMENT
FR3039513B1 (en) * 2015-07-28 2017-09-01 Thales Sa PROCESS FOR THE ADDITIVE MANUFACTURE OF AERONAUTICAL EQUIPMENT
FR3043464B1 (en) * 2015-11-06 2017-11-10 Snecma MEASURING DEVICE FOR A GAS FLOWING VEIN OF A TURBOMACHINE
FR3044412B1 (en) * 2015-11-30 2018-11-09 Safran Aircraft Engines INSTRUMED VEIN OF TURBOMACHINE
US10139023B2 (en) * 2016-01-11 2018-11-27 United Technologies Corporation Advanced braze joint for tube-to-tube connection
US10794281B2 (en) * 2016-02-02 2020-10-06 General Electric Company Gas turbine engine having instrumented airflow path components
US10753278B2 (en) 2016-03-30 2020-08-25 General Electric Company Translating inlet for adjusting airflow distortion in gas turbine engine
US11073090B2 (en) 2016-03-30 2021-07-27 General Electric Company Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
FR3051044B1 (en) * 2016-05-06 2019-05-03 Safran Aircraft Engines DEVICE FOR MEASURING CHARACTERISTICS OF A FLOW
CN106482923B (en) * 2016-10-28 2019-09-06 北京航天长征飞行器研究所 A kind of flow field calibration test device suitable under hot environment
US10330404B2 (en) * 2016-12-16 2019-06-25 Hamilton Sundstrand Corporation Heat exchanger component with embedded sensor
FR3065523B1 (en) * 2017-04-21 2021-05-14 Safran Aircraft Engines DEVICE FOR MEASURING PARAMETERS OF AN AERODYNAMIC FLOW, VEIN EQUIPPED WITH SUCH A DEVICE, TURBOMACHINE EQUIPPED WITH SUCH A VEIN AND PROCESS FOR INSTALLING SUCH A DEVICE IN A VEIN
FR3066020B1 (en) * 2017-05-05 2019-08-02 Safran Aircraft Engines DEVICE FOR MEASURING PARAMETERS OF AERODYNAMIC FLOW OF A TURBOMACHINE AND TURBOMACHINE EQUIPPED WITH SUCH A DEVICE
EP3462153B1 (en) * 2017-09-29 2021-09-22 General Electric Technology GmbH Method for determining a local hot gas temperature in a hot gas duct, and devices for carrying out the method
CN107917793B (en) * 2017-11-14 2020-09-25 中国空气动力研究与发展中心高速空气动力研究所 Multirow pressure measurement harrow device for experiments
GB201818550D0 (en) * 2018-09-28 2018-12-26 Rolls Royce Plc Flow sensor rake assembly
BE1027043B1 (en) * 2019-02-08 2020-09-08 Safran Aero Boosters Sa TOTAL PRESSURE AND TOTAL TEMPERATURE MEASUREMENT IN A TURBOMACHINE
RU192877U1 (en) * 2019-07-10 2019-10-04 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Device for measuring the temperature of the working environment
CN112539909B (en) * 2020-11-30 2023-03-24 中国空气动力研究与发展中心 Gantry crane device for boundary layer measurement in pulse wind tunnel
CN113267313B (en) * 2021-07-19 2021-09-14 中国空气动力研究与发展中心高速空气动力研究所 Pressure measuring rake and stabilizing method thereof
RU2767580C1 (en) * 2021-11-29 2022-03-17 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Cooled nozzle blade of a high-pressure turbine of a turbojet engine
RU2770976C1 (en) * 2021-12-29 2022-04-25 АО "ОДК - Авиадвигатель" Cooled nozzle blade of high-pressure turbine of turbojet engine with replaceable nose for bench tests

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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
US4733975A (en) * 1986-07-03 1988-03-29 The United States Of America As Represented By The Secretary Of The Air Force Unitized high temperature probes
GB2272768A (en) * 1992-11-20 1994-05-25 Rolls Royce Plc Pressure or temperature measuring apparatus and a cartridge of sensors for use in the same
US5595062A (en) * 1992-02-17 1997-01-21 Chabry; Alexander Internal combustion engine intake and exhaust systems
US6595062B1 (en) * 2000-10-16 2003-07-22 Lockheed Martin Corporation High temperature rake for suspersonic flow
US20040042527A1 (en) * 2002-08-28 2004-03-04 E.G.O. Elektro-Geraetebau Gmbh Device for determining the temperature of a medium flowing through a duct
US20040202886A1 (en) * 2002-09-23 2004-10-14 Siemens Westinghouse Power Corporation Method and apparatus for instrumenting a gas turbine component having a barrier coating

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US4733975A (en) * 1986-07-03 1988-03-29 The United States Of America As Represented By The Secretary Of The Air Force Unitized high temperature probes
US5595062A (en) * 1992-02-17 1997-01-21 Chabry; Alexander Internal combustion engine intake and exhaust systems
GB2272768A (en) * 1992-11-20 1994-05-25 Rolls Royce Plc Pressure or temperature measuring apparatus and a cartridge of sensors for use in the same
US6595062B1 (en) * 2000-10-16 2003-07-22 Lockheed Martin Corporation High temperature rake for suspersonic flow
US20040042527A1 (en) * 2002-08-28 2004-03-04 E.G.O. Elektro-Geraetebau Gmbh Device for determining the temperature of a medium flowing through a duct
US20040202886A1 (en) * 2002-09-23 2004-10-14 Siemens Westinghouse Power Corporation Method and apparatus for instrumenting a gas turbine component having a barrier coating

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2757091C2 (en) * 2017-05-05 2021-10-11 Сафран Аэро Бустерс Са Turbulence sensor of turbomachine compressor
US10717514B2 (en) 2018-03-09 2020-07-21 Senior Ip Gmbh Integrated drain mast structure

Also Published As

Publication number Publication date
GB2452026A (en) 2009-02-25
GB2452026A9 (en) 2009-07-08
GB0714652D0 (en) 2007-09-05

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20190727