JPS6033981B2 - ガスタ−ビンエンジンの圧縮機 - Google Patents

ガスタ−ビンエンジンの圧縮機

Info

Publication number
JPS6033981B2
JPS6033981B2 JP57048105A JP4810582A JPS6033981B2 JP S6033981 B2 JPS6033981 B2 JP S6033981B2 JP 57048105 A JP57048105 A JP 57048105A JP 4810582 A JP4810582 A JP 4810582A JP S6033981 B2 JPS6033981 B2 JP S6033981B2
Authority
JP
Japan
Prior art keywords
aluminum alloy
alloy plate
casing
compressor
support device
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
JP57048105A
Other languages
English (en)
Japanese (ja)
Other versions
JPS57171033A (en
Inventor
マツクス・アルダ−ソン
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce 1971 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 Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Publication of JPS57171033A publication Critical patent/JPS57171033A/ja
Publication of JPS6033981B2 publication Critical patent/JPS6033981B2/ja
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
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/14—Testing gas-turbine engines or jet-propulsion engines
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00—Vibration-testing of structures; Shock-testing of structures
    • G01M7/08—Shock-testing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP57048105A 1981-03-25 1982-03-25 ガスタ−ビンエンジンの圧縮機 Expired JPS6033981B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8109286A GB2095749B (en) 1981-03-25 1981-03-25 Gas turbine engine having improved resistance for foreign object ingestion damage
GB8109286 1981-03-25

Publications (2)

Publication Number Publication Date
JPS57171033A JPS57171033A (en) 1982-10-21
JPS6033981B2 true JPS6033981B2 (ja) 1985-08-06

Family

ID=10520632

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57048105A Expired JPS6033981B2 (ja) 1981-03-25 1982-03-25 ガスタ−ビンエンジンの圧縮機

Country Status (5)

Country Link
US (1) US4666371A (US20100223739A1-20100909-C00025.png)
JP (1) JPS6033981B2 (US20100223739A1-20100909-C00025.png)
DE (1) DE3209960C2 (US20100223739A1-20100909-C00025.png)
FR (1) FR2502696A1 (US20100223739A1-20100909-C00025.png)
GB (1) GB2095749B (US20100223739A1-20100909-C00025.png)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101426403B1 (ko) * 2012-09-28 2014-08-07 한국전력공사 보일러 튜브의 스케일 제거 방법

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2225587B (en) * 1988-10-29 1992-07-15 Ishikawajima Harima Heavy Ind Interior material for fan case of turbo-fan engine
DE4223496A1 (de) * 1992-07-17 1994-01-20 Asea Brown Boveri Vorrichtung zum Reduzieren der kinetischen Energie von berstenden Teilen
US5447411A (en) * 1993-06-10 1995-09-05 Martin Marietta Corporation Light weight fan blade containment system
DE4329014C1 (de) * 1993-08-28 1995-01-05 Mtu Muenchen Gmbh Rotorgehäuse, insbesondere Gehäuse für Turbotriebwerke
US5472315A (en) * 1993-11-09 1995-12-05 Sundstrand Corporation Abradable coating in a gas turbine engine
CA2166852A1 (en) * 1995-01-17 1996-07-18 Donnie Ray Juen Organosiloxane compositions yielding machinable erosion resistant elastomers
GB2303596A (en) * 1995-07-20 1997-02-26 Rolls Royce Plc Gas turbine engine containment barrier
GB9922618D0 (en) 1999-09-25 1999-11-24 Rolls Royce Plc A gas turbine engine blade containment assembly
DE10020673C2 (de) * 2000-04-27 2002-06-27 Mtu Aero Engines Gmbh Ringstruktur in Metallbauweise
GB0206136D0 (en) * 2002-03-15 2002-04-24 Rolls Royce Plc Improvements in or relating to cellular materials
US6916529B2 (en) * 2003-01-09 2005-07-12 General Electric Company High temperature, oxidation-resistant abradable coatings containing microballoons and method for applying same
DE102004010236A1 (de) * 2004-03-03 2005-09-15 Mtu Aero Engines Gmbh Ringstruktur in Metallbauweise
DE102004018585B4 (de) * 2004-04-16 2013-12-05 Rolls-Royce Deutschland Ltd & Co Kg Triebwerkeinlaufkonus für ein Gasturbinentriebwerk
SE527732C2 (sv) * 2004-10-07 2006-05-23 Volvo Aero Corp Ett hölje för omslutande av en gasturbinkomponent
GB2426287B (en) * 2005-05-18 2007-05-30 Rolls Royce Plc Blade containment structure
US20070197719A1 (en) * 2006-02-21 2007-08-23 United Technologies Corporation Turbine friendly abradable material
US8020875B2 (en) * 2006-02-21 2011-09-20 United Technologies Corporation Turbine friendly abradable material
EP2083148A3 (de) * 2008-01-23 2012-06-06 Rolls-Royce Deutschland Ltd & Co KG Gasturbine mit einem Verdichter mit Einlaufschicht und Verfahren zum Einlaufen von freien Endbereichen von Schaufeln eines Verdichters einer Gasturbine
DE102008005480A1 (de) * 2008-01-23 2009-07-30 Rolls-Royce Deutschland Ltd & Co Kg Gasturbine mit einem Verdichter mit Einlaufschicht mit luftaushärtendem Material
CN102345623A (zh) * 2011-07-20 2012-02-08 浙江义乌星耀风机有限公司 具有防爆定子结构的煤气轴流风机及其制造方法
FR2997499B1 (fr) * 2012-10-31 2015-01-23 Snecma Dispositif de test d'ingestion d'objets par une turbomachine
US10167727B2 (en) * 2014-08-13 2019-01-01 United Technologies Corporation Gas turbine engine blade containment system
US10550718B2 (en) 2017-03-31 2020-02-04 The Boeing Company Gas turbine engine fan blade containment systems
US10487684B2 (en) 2017-03-31 2019-11-26 The Boeing Company Gas turbine engine fan blade containment systems
US10947901B2 (en) * 2018-11-27 2021-03-16 Honeywell International Inc. Gas turbine engine compressor sections and intake ducts including soft foreign object debris endwall treatments

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2742224A (en) * 1951-03-30 1956-04-17 United Aircraft Corp Compressor casing lining
GB868197A (en) * 1956-09-28 1961-05-17 Rolls Royce Improvements in or relating to protective arrangements for use with rotating parts
US3053694A (en) * 1961-02-20 1962-09-11 Gen Electric Abradable material
FR1429834A (fr) * 1964-05-08 1966-02-25 Rolls Royce Perfectionnements apportés aux aubages, notamment pour moteurs à turbine à gaz
US3423070A (en) * 1966-11-23 1969-01-21 Gen Electric Sealing means for turbomachinery
US3575427A (en) * 1969-11-03 1971-04-20 United Aircraft Corp Composite abradable seal
US3603599A (en) * 1970-05-06 1971-09-07 Gen Motors Corp Cooled seal
FR2216174B1 (US20100223739A1-20100909-C00025.png) * 1973-02-02 1978-09-29 Norton Co
US3974313A (en) * 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
GB1485032A (en) * 1974-08-23 1977-09-08 Rolls Royce Gas turbine engine casing
US4149824A (en) * 1976-12-23 1979-04-17 General Electric Company Blade containment device
GB1548836A (en) * 1977-03-17 1979-07-18 Rolls Royce Gasturbine engine
FR2467977A1 (fr) * 1979-10-19 1981-04-30 Snecma Dispositif de securite en cas de rupture d'element rotatif de turbomachine
FR2467978A1 (fr) * 1979-10-23 1981-04-30 Snecma Dispositif de retention pour carter de compresseur d'une turbomachine
FR2470269A1 (fr) * 1979-11-27 1981-05-29 Snecma Structure de retention pour carter de compresseur d'une turbomachine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101426403B1 (ko) * 2012-09-28 2014-08-07 한국전력공사 보일러 튜브의 스케일 제거 방법

Also Published As

Publication number Publication date
GB2095749B (en) 1984-12-12
JPS57171033A (en) 1982-10-21
FR2502696B1 (US20100223739A1-20100909-C00025.png) 1984-05-25
GB2095749A (en) 1982-10-06
DE3209960C2 (de) 1984-04-12
DE3209960A1 (de) 1982-10-14
US4666371A (en) 1987-05-19
FR2502696A1 (fr) 1982-10-01

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