DE69503134D1 - Fangvorrichtung für ein turbinenrad - Google Patents

Fangvorrichtung für ein turbinenrad

Info

Publication number
DE69503134D1
DE69503134D1 DE69503134T DE69503134T DE69503134D1 DE 69503134 D1 DE69503134 D1 DE 69503134D1 DE 69503134 T DE69503134 T DE 69503134T DE 69503134 T DE69503134 T DE 69503134T DE 69503134 D1 DE69503134 D1 DE 69503134D1
Authority
DE
Germany
Prior art keywords
turbine wheel
collective device
collective
turbine
wheel
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
DE69503134T
Other languages
English (en)
Other versions
DE69503134T2 (de
Inventor
Andrew Kulak
Richard White
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69503134D1 publication Critical patent/DE69503134D1/de
Application granted granted Critical
Publication of DE69503134T2 publication Critical patent/DE69503134T2/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
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
    • 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
DE69503134T 1994-04-29 1995-04-24 Fangvorrichtung für ein turbinenrad Expired - Lifetime DE69503134T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/236,756 US5409349A (en) 1994-04-29 1994-04-29 Turbofan containment structure
PCT/US1995/004992 WO1995030077A1 (en) 1994-04-29 1995-04-24 Turbofan containment structure

Publications (2)

Publication Number Publication Date
DE69503134D1 true DE69503134D1 (de) 1998-07-30
DE69503134T2 DE69503134T2 (de) 1999-02-18

Family

ID=22890822

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69503134T Expired - Lifetime DE69503134T2 (de) 1994-04-29 1995-04-24 Fangvorrichtung für ein turbinenrad

Country Status (5)

Country Link
US (1) US5409349A (de)
EP (1) EP0763164B1 (de)
JP (1) JP3599340B2 (de)
DE (1) DE69503134T2 (de)
WO (1) WO1995030077A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6007894A (en) * 1997-07-10 1999-12-28 Mcdonnell Dougal Corporation Quasi-isotropic composite isogrid structure and method of making same
US6612217B1 (en) 1998-06-02 2003-09-02 Sri International Penetration resistant fabric structures and materials
GB2361033B (en) * 2000-04-08 2004-06-09 Rolls Royce Plc A gas turbine engine blade containment assembly
FR2872485B1 (fr) * 2004-07-05 2006-09-15 Snecma Moteurs Sa Raidisseur pour compresseur basse pression d'un moteur d'aeronef
GB0803479D0 (en) * 2008-02-27 2008-04-02 Rolls Royce Plc Fan track liner assembly
GB2459646B (en) * 2008-04-28 2011-03-30 Rolls Royce Plc A fan assembly
US8092169B2 (en) * 2008-09-16 2012-01-10 United Technologies Corporation Integrated inlet fan case
US8202041B2 (en) * 2008-10-31 2012-06-19 Pratt & Whitney Canada Corp Fan case for turbofan engine
US8827629B2 (en) * 2011-02-10 2014-09-09 United Technologies Corporation Case with ballistic liner
US8500390B2 (en) 2010-05-20 2013-08-06 Pratt & Whitney Canada Corp. Fan case with rub elements
US9126374B2 (en) 2010-09-28 2015-09-08 Russell B. Hanson Iso-grid composite component
US9109462B2 (en) * 2011-12-15 2015-08-18 United Technologies Corporation Energy-absorbing fan case for a gas turbine engine
US10024191B2 (en) 2013-03-11 2018-07-17 Rolls-Royce Corporation Fan track liner designed to yield next to fan case hook
US10563537B2 (en) * 2016-02-05 2020-02-18 United Technologies Corporation Energy absorbing beam and sandwich panel structure
US10487684B2 (en) 2017-03-31 2019-11-26 The Boeing Company Gas turbine engine fan blade containment systems
US10550718B2 (en) 2017-03-31 2020-02-04 The Boeing Company Gas turbine engine fan blade containment systems
GB201816989D0 (en) * 2018-10-18 2018-12-05 Rolls Royce Plc Debris retention
GB201816990D0 (en) * 2018-10-18 2018-12-05 Rolls Royce Plc Debris retention
US11015482B2 (en) 2018-11-27 2021-05-25 Honeywell International Inc. Containment system for gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4012549A (en) * 1974-10-10 1977-03-15 General Dynamics Corporation High strength composite structure
US4397608A (en) * 1980-05-01 1983-08-09 Automation Industries, Inc. Energy-absorbing turbine missile shield
US4490092A (en) * 1981-12-21 1984-12-25 United Technologies Corporation Containment structure
US4417848A (en) * 1982-02-01 1983-11-29 United Technologies Corporation Containment shell for a fan section of a gas turbine engine
FR2574476B1 (fr) * 1984-12-06 1987-01-02 Snecma Carter de retention pour soufflante de turboreacteur
DE3814954A1 (de) * 1988-05-03 1989-11-16 Mtu Muenchen Gmbh Berstschutzring fuer ein triebwerksgehaeuse

Also Published As

Publication number Publication date
EP0763164B1 (de) 1998-06-24
DE69503134T2 (de) 1999-02-18
JPH09512612A (ja) 1997-12-16
JP3599340B2 (ja) 2004-12-08
WO1995030077A1 (en) 1995-11-09
US5409349A (en) 1995-04-25
EP0763164A1 (de) 1997-03-19

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Legal Events

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8364 No opposition during term of opposition