JPS5252016A - Ejector sleeve support structure for aircraft gas turbine engine - Google Patents
Ejector sleeve support structure for aircraft gas turbine engineInfo
- Publication number
- JPS5252016A JPS5252016A JP51109342A JP10934276A JPS5252016A JP S5252016 A JPS5252016 A JP S5252016A JP 51109342 A JP51109342 A JP 51109342A JP 10934276 A JP10934276 A JP 10934276A JP S5252016 A JPS5252016 A JP S5252016A
- Authority
- JP
- Japan
- Prior art keywords
- support structure
- gas turbine
- turbine engine
- ejector sleeve
- sleeve support
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB37534/75A GB1514305A (en) | 1975-09-12 | 1975-09-12 | Ejector sleeves for aircraft mounted gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5252016A true JPS5252016A (en) | 1977-04-26 |
Family
ID=10397205
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP51109342A Pending JPS5252016A (en) | 1975-09-12 | 1976-09-11 | Ejector sleeve support structure for aircraft gas turbine engine |
Country Status (5)
Country | Link |
---|---|
US (1) | US4049220A (ja) |
JP (1) | JPS5252016A (ja) |
DE (1) | DE2640648C2 (ja) |
FR (1) | FR2323883A1 (ja) |
GB (1) | GB1514305A (ja) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4369937A (en) * | 1981-05-18 | 1983-01-25 | The United States Of America As Represented By The Secretary Of The Army | Hinging and latching apparatus |
US4466587A (en) * | 1981-12-21 | 1984-08-21 | General Electric Company | Nacelle installation |
US5727755A (en) * | 1994-01-21 | 1998-03-17 | Craig; Alfred C. | Aircraft engines with a controllable outer casing |
US5730392A (en) * | 1995-09-22 | 1998-03-24 | Aeronautical Concept Of Exhaust, Ltd. | Adjustable fairing for thrust reversers |
US6938408B2 (en) * | 2001-04-26 | 2005-09-06 | Propulsion Vectoring, L.P. | Thrust vectoring and variable exhaust area for jet engine nozzle |
ES2316257B1 (es) * | 2006-10-31 | 2010-01-12 | Airbus España, S.L. | Cono de cola para aeronave con carena movil y estructura de soporte de unidad auxiliar de energia y de sus elementos anexos. |
FR2936492B1 (fr) * | 2008-10-01 | 2011-04-01 | Aircelle Sa | Nacelle pour turboreacteur. |
FR3015434B1 (fr) * | 2013-12-23 | 2017-12-08 | Snecma | Suspension de turbomachine |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US560141A (en) * | 1896-05-12 | Bicycle-supporting apparatus | ||
US1703496A (en) * | 1927-06-01 | 1929-02-26 | Naud Jack | Dog race track |
US2972860A (en) * | 1958-01-30 | 1961-02-28 | Westinghouse Electric Corp | Combined variable ejector and thrust reverser |
US3084507A (en) * | 1958-06-17 | 1963-04-09 | Douglas Aircraft Co Inc | Jet engine sound suppressor and reverser |
US3067968A (en) * | 1958-12-29 | 1962-12-11 | Heppenstall Charles William | Retractable jet engine noise suppressor |
US3591087A (en) * | 1969-05-08 | 1971-07-06 | Rohr Corp | Apparatus for augmenting the thrust of an aircraft jet engine |
US3516511A (en) * | 1969-05-22 | 1970-06-23 | Rohr Corp | Method and apparatus for augmenting the thrust and suppressing the noise of an aircraft jet engine |
US3583640A (en) * | 1969-11-03 | 1971-06-08 | Rohr Corp | Jet propulsion apparatus and method of operating the same |
DE2031170A1 (de) * | 1970-06-24 | 1971-12-30 | Bosch Gmbh Robert | Transporteinrichtung für Lasten |
US3637042A (en) * | 1970-07-27 | 1972-01-25 | Rohr Corp | Method and apparatus for suppressing the noise of jet-propelled aircraft |
US3581841A (en) * | 1970-07-27 | 1971-06-01 | Rohr Corp | Thrust reversing and noise suppressing apparatus for a jet engine |
-
1975
- 1975-09-12 GB GB37534/75A patent/GB1514305A/en not_active Expired
-
1976
- 1976-08-30 US US05/718,470 patent/US4049220A/en not_active Expired - Lifetime
- 1976-09-09 DE DE2640648A patent/DE2640648C2/de not_active Expired
- 1976-09-10 FR FR7627343A patent/FR2323883A1/fr active Granted
- 1976-09-11 JP JP51109342A patent/JPS5252016A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
FR2323883A1 (fr) | 1977-04-08 |
DE2640648A1 (de) | 1977-04-07 |
DE2640648C2 (de) | 1982-04-22 |
GB1514305A (en) | 1978-06-14 |
US4049220A (en) | 1977-09-20 |
FR2323883B1 (ja) | 1982-09-17 |
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