FR1382232A - Perfectionnements apportés aux moteurs à turbine à gaz - Google Patents

Perfectionnements apportés aux moteurs à turbine à gaz

Info

Publication number
FR1382232A
FR1382232A FR952144A FR952144A FR1382232A FR 1382232 A FR1382232 A FR 1382232A FR 952144 A FR952144 A FR 952144A FR 952144 A FR952144 A FR 952144A FR 1382232 A FR1382232 A FR 1382232A
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
engines
gas
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
Application number
FR952144A
Other languages
English (en)
Inventor
James Alexander Petrie
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 FR1382232A publication Critical patent/FR1382232A/fr
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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • F01D25/125—Cooling of bearings
    • 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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Rolling Contact Bearings (AREA)
FR952144A 1962-11-09 1963-10-29 Perfectionnements apportés aux moteurs à turbine à gaz Expired FR1382232A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB42513/62A GB969579A (en) 1962-11-09 1962-11-09 Gas turbine engine

Publications (1)

Publication Number Publication Date
FR1382232A true FR1382232A (fr) 1964-12-18

Family

ID=10424766

Family Applications (1)

Application Number Title Priority Date Filing Date
FR952144A Expired FR1382232A (fr) 1962-11-09 1963-10-29 Perfectionnements apportés aux moteurs à turbine à gaz

Country Status (4)

Country Link
US (1) US3250512A (fr)
DE (1) DE1242942C2 (fr)
FR (1) FR1382232A (fr)
GB (1) GB969579A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4101242A (en) * 1975-06-20 1978-07-18 Rolls-Royce Limited Matching thermal expansion of components of turbo-machines
FR2528494A1 (fr) * 1982-06-10 1983-12-16 Rolls Royce Element de distribution de charge pour une turbine d'un moteur a turbine a gaz et ensemble comportant deux tels elements

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1258661C2 (de) * 1964-10-28 1973-12-13 Gasturbine mit eintrittsseitiger abdichtung der kuehlluftzufuehrung
US3303997A (en) * 1965-04-21 1967-02-14 United Aircraft Corp Compressor air seal
GB1504129A (en) * 1974-06-29 1978-03-15 Rolls Royce Matching differential thermal expansions of components in heat engines
US4111596A (en) * 1977-01-10 1978-09-05 The United States Of America As Represented By The Secretary Of The Navy Turbine blade cooling system
GB2062762B (en) * 1979-11-03 1983-03-30 Rolls Royce Bearing arrangement in a modular gas turbine engine
US4369016A (en) * 1979-12-21 1983-01-18 United Technologies Corporation Turbine intermediate case
US4304522A (en) * 1980-01-15 1981-12-08 Pratt & Whitney Aircraft Of Canada Limited Turbine bearing support
FR2484574A1 (fr) * 1980-06-13 1981-12-18 Snecma Palier inter-arbres de turbomachine multi-corps a amortissement par pellicule d'huile
FR2535789A1 (fr) * 1982-11-10 1984-05-11 Snecma Montage d'un palier inter-arbres de turbomachine multi-corps
US4541775A (en) * 1983-03-30 1985-09-17 United Technologies Corporation Clearance control in turbine seals
US4820117A (en) * 1987-07-09 1989-04-11 United Technologies Corporation Crossed I-beam structural strut
US5160251A (en) * 1991-05-13 1992-11-03 General Electric Company Lightweight engine turbine bearing support assembly for withstanding radial and axial loads
US5180282A (en) * 1991-09-27 1993-01-19 General Electric Company Gas turbine engine structural frame with multi-yoke attachment of struts to outer casing
US5236303A (en) * 1991-09-27 1993-08-17 General Electric Company Gas turbine engine structural frame with multi-clevis ring attachment of struts to outer casing
US5685693A (en) * 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control
US5622438A (en) * 1995-07-12 1997-04-22 United Technologies Corporation Fire resistant bearing compartment cover
US6099165A (en) * 1999-01-19 2000-08-08 Pratt & Whitney Canada Corp. Soft bearing support
US20100303608A1 (en) * 2006-09-28 2010-12-02 Mitsubishi Heavy Industries, Ltd. Two-shaft gas turbine
US8215894B2 (en) * 2007-11-13 2012-07-10 United Technologies Corporation Dual configuration seal assembly for a rotational assembly
US9631558B2 (en) 2012-01-03 2017-04-25 United Technologies Corporation Geared architecture for high speed and small volume fan drive turbine
US9239012B2 (en) 2011-06-08 2016-01-19 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US20150345426A1 (en) 2012-01-31 2015-12-03 United Technologies Corporation Geared turbofan gas turbine engine architecture
US10240526B2 (en) 2012-01-31 2019-03-26 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section
US20150192070A1 (en) 2012-01-31 2015-07-09 United Technologies Corporation Geared turbofan gas turbine engine architecture
US8887487B2 (en) 2012-01-31 2014-11-18 United Technologies Corporation Geared turbofan gas turbine engine architecture
US10287914B2 (en) 2012-01-31 2019-05-14 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section and bearing support features
US20130192201A1 (en) * 2012-01-31 2013-08-01 United Technologies Corporation Geared turbofan gas turbine engine architecture
US10138809B2 (en) 2012-04-02 2018-11-27 United Technologies Corporation Geared turbofan engine with a high ratio of thrust to turbine volume
US10125693B2 (en) 2012-04-02 2018-11-13 United Technologies Corporation Geared turbofan engine with power density range
US9074485B2 (en) 2012-04-25 2015-07-07 United Technologies Corporation Geared turbofan with three turbines all counter-rotating
WO2014152123A1 (fr) * 2013-03-14 2014-09-25 United Technologies Corporation Joint de dissuasion à écran thermique pour moteur à turbine à gaz
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
DE102014114473A1 (de) * 2014-10-06 2016-04-07 Rolls-Royce Deutschland Ltd & Co Kg Gasturbine mit wenigstens zwei koaxial zueinander angeordneten und zumindest bereichsweise als Hohlwellen ausgebildeten Wellen
KR101872808B1 (ko) * 2017-04-28 2018-06-29 두산중공업 주식회사 길이조절구조를 포함하는 가스터빈 로터, 및 이를 포함하는 가스터빈
RU2742849C1 (ru) * 2020-02-28 2021-02-11 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Передняя опора ротора турбины низкого давления двухвального газотурбинного двигателя

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH266474A (de) * 1941-10-14 1950-01-31 Vickers Electrical Co Ltd Strahltriebwerk.
US2711074A (en) * 1944-06-22 1955-06-21 Gen Electric Aft frame and rotor structure for combustion gas turbine
BE535079A (fr) * 1954-01-25
GB773499A (en) * 1954-02-12 1957-04-24 Rolls Royce Improvements in or relating to axial-flow compressors and to gas-turbine engines incorporating such compressors
GB790830A (en) * 1954-07-16 1958-02-19 Rolls Royce Improvements relating to gas-turbine engines
DE1062987B (de) * 1956-01-05 1959-08-06 Power Jets Res & Dev Ltd Gasturbinenstrahltriebwerk
GB920886A (en) * 1958-11-24 1963-03-13 Rolls Royce Improvements in or relating to gas turbine engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4101242A (en) * 1975-06-20 1978-07-18 Rolls-Royce Limited Matching thermal expansion of components of turbo-machines
FR2528494A1 (fr) * 1982-06-10 1983-12-16 Rolls Royce Element de distribution de charge pour une turbine d'un moteur a turbine a gaz et ensemble comportant deux tels elements

Also Published As

Publication number Publication date
DE1242942B (de) 1967-06-22
DE1242942C2 (de) 1967-12-14
US3250512A (en) 1966-05-10
GB969579A (en) 1964-09-09

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