ATE532032T1 - Vorrichtung und verfahren zur messung der erosion einer kante einer turbomaschinentragfläche - Google Patents

Vorrichtung und verfahren zur messung der erosion einer kante einer turbomaschinentragfläche

Info

Publication number
ATE532032T1
ATE532032T1 AT09776735T AT09776735T ATE532032T1 AT E532032 T1 ATE532032 T1 AT E532032T1 AT 09776735 T AT09776735 T AT 09776735T AT 09776735 T AT09776735 T AT 09776735T AT E532032 T1 ATE532032 T1 AT E532032T1
Authority
AT
Austria
Prior art keywords
edge
distance
fan blade
computer
erosion
Prior art date
Application number
AT09776735T
Other languages
English (en)
Inventor
Craig Robinson
Stephen Roche
Conall Fee
David Bauer
Original Assignee
Rolls Royce Plc
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 Rolls Royce Plc filed Critical Rolls Royce Plc
Application granted granted Critical
Publication of ATE532032T1 publication Critical patent/ATE532032T1/de

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/24—Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • 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
    • F01D5/005—Repairing methods or devices
    • 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
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0292—Stop safety or alarm devices, e.g. stop-and-go control; Disposition of check-valves
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)
AT09776735T 2008-07-09 2009-06-16 Vorrichtung und verfahren zur messung der erosion einer kante einer turbomaschinentragfläche ATE532032T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0812478.6A GB0812478D0 (en) 2008-07-09 2008-07-09 An apparatus and a method of measuring erosion of an edge of a turbomachine aerofoil
PCT/EP2009/004314 WO2010003512A1 (en) 2008-07-09 2009-06-16 An apparatus and a method of measuring erosion of an edge of a turbomachine aerofoil

Publications (1)

Publication Number Publication Date
ATE532032T1 true ATE532032T1 (de) 2011-11-15

Family

ID=39718154

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09776735T ATE532032T1 (de) 2008-07-09 2009-06-16 Vorrichtung und verfahren zur messung der erosion einer kante einer turbomaschinentragfläche

Country Status (7)

Country Link
US (1) US7990547B2 (de)
EP (1) EP2294358B1 (de)
JP (1) JP5329659B2 (de)
AT (1) ATE532032T1 (de)
CA (1) CA2729826A1 (de)
GB (1) GB0812478D0 (de)
WO (1) WO2010003512A1 (de)

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JP2012137078A (ja) * 2010-12-28 2012-07-19 Jfe Steel Corp 排ガス送風機用インペラーの振動防止方法
GB2491398B (en) 2011-06-03 2013-11-27 Rolls Royce Plc An apparatus and a method of shaping an edge of an aerofoil
GB2496903B (en) * 2011-11-28 2015-04-15 Rolls Royce Plc An apparatus and a method of inspecting a turbomachine
US20150132127A1 (en) * 2013-11-12 2015-05-14 General Electric Company Turbomachine airfoil erosion determination
FR3021993B1 (fr) * 2014-06-06 2016-06-10 Snecma Procede de dimensionnement d'une turbomachine
WO2016003721A1 (en) 2014-07-01 2016-01-07 Sikorsky Aircraft Corporation Blade geometry characterization tool
JP2016109597A (ja) * 2014-12-09 2016-06-20 ゼネラル・エレクトリック・カンパニイ ターボ機械エアフォイルの腐食判断
US9835440B2 (en) * 2015-12-17 2017-12-05 General Electric Company Methods for monitoring turbine components
CN108844491A (zh) * 2018-08-23 2018-11-20 江南大学 一种航空叶片前后缘激光轮廓仪
US10845189B2 (en) * 2019-03-27 2020-11-24 Raythoen Technologies Corporation Calibration for laser inspection
CN112013788B (zh) * 2020-10-22 2021-01-26 四川大学 基于叶片局部前缘曲线特征标定转动中心的方法
KR20240071912A (ko) * 2022-11-16 2024-05-23 한국전력공사 터빈 블레이드 침식량 측정 시스템

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US3513692A (en) * 1966-09-19 1970-05-26 Thiokol Chemical Corp Erosion measuring device
US3699334A (en) * 1969-06-16 1972-10-17 Kollsman Instr Corp Apparatus using a beam of positive ions for controlled erosion of surfaces
US3744911A (en) * 1970-06-11 1973-07-10 G C Optronics Inc Holographic method for interferometric measurement of material corrosion and erosion on arbitrary surfaces
US4025192A (en) * 1975-11-25 1977-05-24 Aga Aktiebolag Optical measuring method
JPS63246637A (ja) 1987-04-01 1988-10-13 Hitachi Ltd タ−ビン翼の浸蝕監視装置
SU1666920A1 (ru) 1988-05-25 1991-07-30 Научно-Производственное Объединение По Исследованию И Проектированию Энергетического Оборудования Им.И.И.Ползунова Устройство дл измерени эрозионного износа рабочих лопаток паровых турбин
US5570186A (en) * 1992-04-28 1996-10-29 Mtu Motoren- Und Turbinen-Union Munich Gmbh Method for inspecting the curvature of a profile, such an edge of a turbine blade
JPH06201343A (ja) * 1993-01-05 1994-07-19 Ishikawajima Harima Heavy Ind Co Ltd ロータブレードの摩耗量測定装置
RU2089878C1 (ru) 1993-12-06 1997-09-10 Шелест Сергей Орестович Способ измерения эрозионного износа кромок рабочих лопаток турбины и устройство для его осуществления
US6970590B2 (en) * 2002-03-28 2005-11-29 General Electric Company Side lit, 3D edge location method
JP3938721B2 (ja) * 2002-07-01 2007-06-27 オリンパス株式会社 計測用内視鏡装置
US6915236B2 (en) * 2002-11-22 2005-07-05 General Electric Company Method and system for automated repair design of damaged blades of a compressor or turbine
AU2003266505A1 (en) * 2003-09-10 2005-04-06 Hitachi, Ltd. Turbine rotor blade
US7681325B2 (en) * 2006-11-02 2010-03-23 General Electric Company Apparatus for measuring a turbine blade

Also Published As

Publication number Publication date
CA2729826A1 (en) 2010-01-14
WO2010003512A1 (en) 2010-01-14
JP5329659B2 (ja) 2013-10-30
GB0812478D0 (en) 2008-08-13
US20110090514A1 (en) 2011-04-21
EP2294358B1 (de) 2011-11-02
US7990547B2 (en) 2011-08-02
JP2011527395A (ja) 2011-10-27
EP2294358A1 (de) 2011-03-16

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