DE60120821D1 - Berstschutzeinrichtung für eine Gasturbine - Google Patents

Berstschutzeinrichtung für eine Gasturbine

Info

Publication number
DE60120821D1
DE60120821D1 DE60120821T DE60120821T DE60120821D1 DE 60120821 D1 DE60120821 D1 DE 60120821D1 DE 60120821 T DE60120821 T DE 60120821T DE 60120821 T DE60120821 T DE 60120821T DE 60120821 D1 DE60120821 D1 DE 60120821D1
Authority
DE
Germany
Prior art keywords
gas turbine
protection device
burst protection
burst
turbine
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 - Lifetime
Application number
DE60120821T
Other languages
English (en)
Other versions
DE60120821T2 (de
Inventor
Stephen John Booth
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 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
Publication of DE60120821D1 publication Critical patent/DE60120821D1/de
Application granted granted Critical
Publication of DE60120821T2 publication Critical patent/DE60120821T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE60120821T 2000-04-05 2001-03-09 Berstschutzeinrichtung für eine Gasturbine Expired - Lifetime DE60120821T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0008193 2000-04-05
GBGB0008193.5A GB0008193D0 (en) 2000-04-05 2000-04-05 A gas turbine engine blade containment assembly

Publications (2)

Publication Number Publication Date
DE60120821D1 true DE60120821D1 (de) 2006-08-03
DE60120821T2 DE60120821T2 (de) 2006-10-12

Family

ID=9889118

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60120821T Expired - Lifetime DE60120821T2 (de) 2000-04-05 2001-03-09 Berstschutzeinrichtung für eine Gasturbine

Country Status (4)

Country Link
US (1) US6497550B2 (de)
EP (1) EP1143112B1 (de)
DE (1) DE60120821T2 (de)
GB (1) GB0008193D0 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0117550D0 (en) * 2001-07-19 2001-09-12 Rolls Royce Plc Joint arrangement
ATE503914T1 (de) * 2004-05-17 2011-04-15 Carlton Forge Works Turbinengehäuseverstärkung bei einem gasturbinentriebwerk
US8191254B2 (en) 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
GB2426287B (en) * 2005-05-18 2007-05-30 Rolls Royce Plc Blade containment structure
GB2459646B (en) * 2008-04-28 2011-03-30 Rolls Royce Plc A fan assembly
US8202041B2 (en) * 2008-10-31 2012-06-19 Pratt & Whitney Canada Corp Fan case for turbofan engine
US9062565B2 (en) * 2009-12-31 2015-06-23 Rolls-Royce Corporation Gas turbine engine containment device
US8500390B2 (en) 2010-05-20 2013-08-06 Pratt & Whitney Canada Corp. Fan case with rub elements
US9810077B2 (en) 2012-01-31 2017-11-07 United Technologies Corporation Fan blade attachment of gas turbine engine
EP2904214B1 (de) 2012-10-01 2019-08-07 United Technologies Corporation Reduzierte lüfter-containment-gefahr durch verkleidungs- und schaufeldesign
WO2014055102A1 (en) 2012-10-01 2014-04-10 United Technologies Corporation Low weight large fan gas turbine engine
CN103293002B (zh) * 2013-06-03 2016-01-20 浙江大学 一种基于线型聚能切割技术的机匣包容试验方法
EP2940251B1 (de) 2014-04-28 2019-06-12 Rolls-Royce Corporation Gebläsegehäuse
US9290274B2 (en) 2014-06-02 2016-03-22 Mra Systems, Inc. Acoustically attenuating sandwich panel constructions
AT516322B1 (de) * 2014-10-10 2017-04-15 Facc Ag Fangehäuse für ein Flugzeugtriebwerk
FR3041704B1 (fr) * 2015-09-29 2017-11-03 Snecma Panneau d'echange thermique et de reduction de bruit pour un ensemble propulsif
US10634002B2 (en) * 2016-05-25 2020-04-28 Rolls-Royce Corporation Soft wall containment system for gas turbine engine
CN107829980B (zh) * 2016-09-16 2021-05-25 通用电气公司 沿周向变化厚度的复合风扇壳
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
US11846199B2 (en) * 2022-01-28 2023-12-19 Hamilton Sundstrand Corporation Rotor containment structure

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3974313A (en) * 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
FR2574476B1 (fr) 1984-12-06 1987-01-02 Snecma Carter de retention pour soufflante de turboreacteur
JPH05347098A (ja) 1992-03-16 1993-12-27 Oki Electric Ind Co Ltd 半導体記憶装置
US5267828A (en) * 1992-11-13 1993-12-07 General Electric Company Removable fan shroud panel
US5403148A (en) * 1993-09-07 1995-04-04 General Electric Company Ballistic barrier for turbomachinery blade containment
US5486086A (en) * 1994-01-04 1996-01-23 General Electric Company Blade containment system
GB2288639B (en) * 1994-04-20 1998-10-21 Rolls Royce Plc Ducted fan gas turbine engine nacelle assembly
US5431532A (en) 1994-05-20 1995-07-11 General Electric Company Blade containment system
US5885056A (en) * 1997-03-06 1999-03-23 Rolls-Royce Plc Gas Turbine engine casing construction
GB9812992D0 (en) * 1998-06-17 1998-08-12 Rolls Royce Plc A gas turbine engine containment casing

Also Published As

Publication number Publication date
EP1143112B1 (de) 2006-06-21
GB0008193D0 (en) 2000-05-24
US20010028840A1 (en) 2001-10-11
EP1143112A1 (de) 2001-10-10
US6497550B2 (en) 2002-12-24
DE60120821T2 (de) 2006-10-12

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Legal Events

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