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
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/026—Shaft to shaft connections
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
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)
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 |
CA2760454C (fr) | 2010-12-03 | 2019-02-19 | Pratt & Whitney Canada Corp. | Element de confinement de rotor turbine a gaz |
ES2963067T3 (es) * | 2016-03-14 | 2024-03-25 | Equinor Energy As | Craqueo de amoníaco |
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)
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 |
-
1975
- 1975-07-09 FR FR7521500A patent/FR2317501A1/fr active Granted
-
1976
- 1976-06-30 US US05/701,418 patent/US4037404A/en not_active Expired - Lifetime
- 1976-07-06 GB GB27987/76A patent/GB1504820A/en not_active Expired
- 1976-07-07 DE DE2630558A patent/DE2630558C2/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2630558A1 (de) | 1977-01-20 |
DE2630558C2 (de) | 1983-08-11 |
FR2317501A1 (fr) | 1977-02-04 |
US4037404A (en) | 1977-07-26 |
GB1504820A (en) | 1978-03-22 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licences | ||
ST | Notification of lapse |