FR2317501B1 - - Google Patents

Info

Publication number
FR2317501B1
FR2317501B1 FR7521500A FR7521500A FR2317501B1 FR 2317501 B1 FR2317501 B1 FR 2317501B1 FR 7521500 A FR7521500 A FR 7521500A FR 7521500 A FR7521500 A FR 7521500A FR 2317501 B1 FR2317501 B1 FR 2317501B1
Authority
FR
France
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
FR7521500A
Other versions
FR2317501A1 (fr
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR7521500A priority Critical patent/FR2317501A1/fr
Priority to US05/701,418 priority patent/US4037404A/en
Priority to GB27987/76A priority patent/GB1504820A/en
Priority to DE2630558A priority patent/DE2630558C2/de
Publication of FR2317501A1 publication Critical patent/FR2317501A1/fr
Application granted granted Critical
Publication of FR2317501B1 publication Critical patent/FR2317501B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/026Shaft to shaft connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR7521500A 1975-07-09 1975-07-09 Dispositif d'accouplement pour moteur a turbine a gaz Granted FR2317501A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7521500A FR2317501A1 (fr) 1975-07-09 1975-07-09 Dispositif d'accouplement pour moteur a turbine a gaz
US05/701,418 US4037404A (en) 1975-07-09 1976-06-30 Coupling device for gas turbine engine
GB27987/76A GB1504820A (en) 1975-07-09 1976-07-06 Gas turbine engines
DE2630558A DE2630558C2 (de) 1975-07-09 1976-07-07 Gasturbinentriebwerk

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7521500A FR2317501A1 (fr) 1975-07-09 1975-07-09 Dispositif d'accouplement pour moteur a turbine a gaz

Publications (2)

Publication Number Publication Date
FR2317501A1 FR2317501A1 (fr) 1977-02-04
FR2317501B1 true FR2317501B1 (fr) 1981-01-16

Family

ID=9157690

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7521500A Granted FR2317501A1 (fr) 1975-07-09 1975-07-09 Dispositif d'accouplement pour moteur a turbine a gaz

Country Status (4)

Country Link
US (1) US4037404A (fr)
DE (1) DE2630558C2 (fr)
FR (1) FR2317501A1 (fr)
GB (1) GB1504820A (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ZA922942B (en) * 1991-04-29 1993-11-23 Trico Folberth Ltd Housing for a rotatable shaft
FR2694537B1 (fr) * 1992-08-06 1994-10-28 Aerospatiale Dispositif d'accrochage d'une turbomachine sur une structure d'aéronef.
FR2756542B1 (fr) * 1996-11-29 1999-02-12 Eurocopter France Installation de montage d'un moteur sur un plancher, et de connexion de son arbre de sortie avec au moins un mecanisme entraine
US6691519B2 (en) * 2000-02-18 2004-02-17 Siemens Westinghouse Power Corporation Adaptable modular gas turbine power plant
US20080006641A1 (en) * 2005-02-22 2008-01-10 Pratt & Whitney Canada Corp. Positioning arrangement for components of a pressure vessel and method
US7661260B2 (en) * 2006-09-27 2010-02-16 General Electric Company Gas turbine engine assembly and method of assembling same
JP5010499B2 (ja) * 2008-02-28 2012-08-29 三菱重工業株式会社 ガスタービン及びガスタービンの保守点検方法
US8650885B2 (en) * 2009-12-22 2014-02-18 United Technologies Corporation Retaining member for use with gas turbine engine shaft and method of assembly
US9291070B2 (en) 2010-12-03 2016-03-22 Pratt & Whitney Canada Corp. Gas turbine rotor containment
CN108884761B (zh) * 2016-03-14 2022-09-02 艾奎诺能源公司 氨裂解
CN106089311B (zh) * 2016-08-12 2018-04-03 上海电气燃气轮机有限公司 燃气轮机转子轮盘的拉杆连接结构
IT202100010781A1 (it) * 2021-04-28 2022-10-28 Nuovo Pignone Tecnologie Srl Rotore di turbomacchina con giranti impilate e turbomacchina
CN113898414B (zh) * 2021-12-09 2022-03-18 成都中科翼能科技有限公司 一种燃气轮机高压转子防热振动变形的补强结构

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2757857A (en) * 1951-06-19 1956-08-07 United Aircraft Corp Locking means between compressor and turbine
DE1030622B (de) * 1954-02-16 1958-05-22 Napier & Son Ltd Sicherheitsregeleinrichtung fuer Propellerturbinen-Triebwerke mit Verstelluftschraube
GB837309A (en) * 1956-11-08 1960-06-09 Rolls Royce Improvements in or relating to gas-turbine engines
US2930189A (en) * 1957-04-08 1960-03-29 Rolls Royce Gas turbine engine with shaft-failure control
DE1131948B (de) * 1957-04-08 1962-06-20 Rolls Royce Sicherheitseinrichtung gegen UEberdrehzahl von Gasturbinen
US3050939A (en) * 1960-05-05 1962-08-28 Rolls Royce Gas turbine engine with shaft failure control
US3159166A (en) * 1961-10-16 1964-12-01 Gen Motors Corp Engine safety control
GB1107325A (en) * 1965-05-01 1968-03-27 Bristol Siddeley Engines Ltd Shaft means for connecting a driving rotor to a rotor to be driven thereby

Also Published As

Publication number Publication date
GB1504820A (en) 1978-03-22
US4037404A (en) 1977-07-26
DE2630558A1 (de) 1977-01-20
FR2317501A1 (fr) 1977-02-04
DE2630558C2 (de) 1983-08-11

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Legal Events

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ST Notification of lapse