DE69302813T2 - Rotor für gasturbinen - Google Patents

Rotor für gasturbinen

Info

Publication number
DE69302813T2
DE69302813T2 DE69302813T DE69302813T DE69302813T2 DE 69302813 T2 DE69302813 T2 DE 69302813T2 DE 69302813 T DE69302813 T DE 69302813T DE 69302813 T DE69302813 T DE 69302813T DE 69302813 T2 DE69302813 T2 DE 69302813T2
Authority
DE
Germany
Prior art keywords
rotor
gas turbines
turbines
gas
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
DE69302813T
Other languages
English (en)
Other versions
DE69302813D1 (de
Inventor
David Knott
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
Application granted granted Critical
Publication of DE69302813D1 publication Critical patent/DE69302813D1/de
Publication of DE69302813T2 publication Critical patent/DE69302813T2/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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
DE69302813T 1992-05-07 1993-04-27 Rotor für gasturbinen Expired - Lifetime DE69302813T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB929209895A GB9209895D0 (en) 1992-05-07 1992-05-07 Rotors for gas turbine engines
PCT/GB1993/000873 WO1993022539A1 (en) 1992-05-07 1993-04-27 Rotors for gas turbine engines

Publications (2)

Publication Number Publication Date
DE69302813D1 DE69302813D1 (de) 1996-06-27
DE69302813T2 true DE69302813T2 (de) 1996-09-26

Family

ID=10715166

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69302813T Expired - Lifetime DE69302813T2 (de) 1992-05-07 1993-04-27 Rotor für gasturbinen

Country Status (5)

Country Link
US (1) US5464326A (de)
EP (1) EP0640172B1 (de)
DE (1) DE69302813T2 (de)
GB (1) GB9209895D0 (de)
WO (1) WO1993022539A1 (de)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2716502B1 (fr) * 1994-02-23 1996-04-05 Snecma Garniture d'étanchéité entre des aubes et des plates-formes intermédiaires.
GB9602129D0 (en) * 1996-02-02 1996-04-03 Rolls Royce Plc Rotors for gas turbine engines
US6217283B1 (en) * 1999-04-20 2001-04-17 General Electric Company Composite fan platform
GB9915637D0 (en) * 1999-07-06 1999-09-01 Rolls Royce Plc A rotor seal
JP4748345B2 (ja) * 2001-07-11 2011-08-17 株式会社Ｉｈｉ ジェットエンジンのファンプラットフォームのシール
EP1448874B1 (de) 2001-09-25 2007-12-26 ALSTOM Technology Ltd Dichtungsanordnung zur dichtspaltreduzierung innerhalb einer strömungsrotationsmaschine
FR2858351B1 (fr) * 2003-07-31 2006-01-13 Snecma Moteurs Plate-forme inter-aubes a flechissement lateral, pour un support d'aubes de turboreacteur
US20070048140A1 (en) * 2005-08-24 2007-03-01 General Electric Company Methods and apparatus for assembling gas turbine engines
GB0611031D0 (en) * 2006-06-06 2006-07-12 Rolls Royce Plc An aerofoil stage and a seal for use therein
GB0614518D0 (en) * 2006-07-21 2006-08-30 Rolls Royce Plc A fan blade for a gas turbine engine
GB0614640D0 (en) * 2006-07-22 2006-08-30 Rolls Royce Plc An annulus filler seal
US7762781B1 (en) 2007-03-06 2010-07-27 Florida Turbine Technologies, Inc. Composite blade and platform assembly
GB0814718D0 (en) 2008-08-13 2008-09-17 Rolls Royce Plc Annulus filler
FR2939836B1 (fr) * 2008-12-12 2015-05-15 Snecma Joint d'etancheite de plateforme dans un rotor de turbomachine
GB201020857D0 (en) 2010-12-09 2011-01-26 Rolls Royce Plc Annulus filler
US9200527B2 (en) * 2011-01-04 2015-12-01 General Electric Company Systems, methods, and apparatus for a turbine interstage rim seal
GB201106278D0 (en) 2011-04-14 2011-05-25 Rolls Royce Plc Annulus filler system
US8777576B2 (en) 2011-08-22 2014-07-15 General Electric Company Metallic fan blade platform
GB201119655D0 (en) 2011-11-15 2011-12-28 Rolls Royce Plc Annulus filler
US10024177B2 (en) * 2012-05-15 2018-07-17 United Technologies Corporation Detachable fan blade platform and method of repairing same
FR2992676B1 (fr) * 2012-06-29 2014-08-01 Snecma Plateforme inter-aubes pour une soufflante, rotor d'une soufflante et procede de fabrication associe
US10344601B2 (en) 2012-08-17 2019-07-09 United Technologies Corporation Contoured flowpath surface
US9297268B2 (en) * 2012-09-06 2016-03-29 United Technologies Corporation Fan blade platform flap seal
US20140169979A1 (en) * 2012-12-14 2014-06-19 United Technologies Corporation Gas turbine engine fan blade platform seal
US9650902B2 (en) * 2013-01-11 2017-05-16 United Technologies Corporation Integral fan blade wear pad and platform seal
US9845699B2 (en) * 2013-03-15 2017-12-19 Gkn Aerospace Services Structures Corp. Fan spacer having unitary over molded feature
US10156151B2 (en) 2014-10-23 2018-12-18 Rolls-Royce North American Technologies Inc. Composite annulus filler
US20160305260A1 (en) * 2015-03-04 2016-10-20 Rolls-Royce North American Technologies, Inc. Bladed wheel with separable platform
FR3052822B1 (fr) * 2016-06-16 2020-03-27 Safran Aircraft Engines Aube de turbomachine equipee d'un joint en elastomere
US10563666B2 (en) * 2016-11-02 2020-02-18 United Technologies Corporation Fan blade with cover and method for cover retention
GB201718600D0 (en) * 2017-11-10 2017-12-27 Rolls Royce Plc Annulus filler
US11028714B2 (en) * 2018-07-16 2021-06-08 Raytheon Technologies Corporation Fan platform wedge seal
US11092020B2 (en) 2018-10-18 2021-08-17 Raytheon Technologies Corporation Rotor assembly for gas turbine engines
US11306601B2 (en) 2018-10-18 2022-04-19 Raytheon Technologies Corporation Pinned airfoil for gas turbine engines
US11359500B2 (en) * 2018-10-18 2022-06-14 Raytheon Technologies Corporation Rotor assembly with structural platforms for gas turbine engines
US10822969B2 (en) 2018-10-18 2020-11-03 Raytheon Technologies Corporation Hybrid airfoil for gas turbine engines
US11136888B2 (en) * 2018-10-18 2021-10-05 Raytheon Technologies Corporation Rotor assembly with active damping for gas turbine engines
US11268397B2 (en) * 2020-02-07 2022-03-08 Raytheon Technologies Corporation Fan blade platform seal and method for forming same

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3464709A (en) * 1966-05-20 1969-09-02 Us Industries Inc Laminated packer
GB1331209A (en) * 1969-10-28 1973-09-26 Secr Defence Bladed rotors for fluid flow machines
GB1232506A (de) * 1969-10-28 1971-05-19
US3936230A (en) * 1974-05-09 1976-02-03 The United States Of America As Represented By The Secretary Of The Air Force Self-supported, self-locating seal for turbine engines
US4045149A (en) * 1976-02-03 1977-08-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Platform for a swing root turbomachinery blade
US4183720A (en) * 1978-01-03 1980-01-15 The United States Of America As Represented By The Secretary Of The Air Force Composite fan blade platform double wedge centrifugal seal
US4580946A (en) * 1984-11-26 1986-04-08 General Electric Company Fan blade platform seal
GB2171151B (en) * 1985-02-20 1988-05-18 Rolls Royce Rotors for gas turbine engines
FR2608674B1 (fr) * 1986-12-17 1991-04-19 Snecma Roue de turbine a aubes ceramique
FR2639402B1 (fr) * 1988-11-23 1990-12-28 Snecma Disque ailete de rotor de turbomachine
US5277548A (en) * 1991-12-31 1994-01-11 United Technologies Corporation Non-integral rotor blade platform

Also Published As

Publication number Publication date
WO1993022539A1 (en) 1993-11-11
EP0640172B1 (de) 1996-05-22
EP0640172A1 (de) 1995-03-01
GB9209895D0 (en) 1992-06-24
DE69302813D1 (de) 1996-06-27
US5464326A (en) 1995-11-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition