FR2277239B2 - - Google Patents
Info
- Publication number
- FR2277239B2 FR2277239B2 FR7423233A FR7423233A FR2277239B2 FR 2277239 B2 FR2277239 B2 FR 2277239B2 FR 7423233 A FR7423233 A FR 7423233A FR 7423233 A FR7423233 A FR 7423233A FR 2277239 B2 FR2277239 B2 FR 2277239B2
- 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
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
-
- 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)
- Nozzles (AREA)
- Sampling And Sample Adjustment (AREA)
- Control Of Turbines (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7423233A FR2277239A2 (fr) | 1974-07-04 | 1974-07-04 | Dispositif de commande de volets de tuyere d'ejection |
| GB2763475A GB1478075A (en) | 1974-07-04 | 1975-07-01 | Variable-area nozzles or other tubular members |
| DE2529543A DE2529543C2 (de) | 1974-07-04 | 1975-07-02 | Vorrichtung zur Betätigung der beweglichen Klappen von Schubdüsen |
| US05/593,177 US3954225A (en) | 1974-07-04 | 1975-07-03 | Apparatus for controlling exhaust nozzle flaps |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7423233A FR2277239A2 (fr) | 1974-07-04 | 1974-07-04 | Dispositif de commande de volets de tuyere d'ejection |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2277239A2 FR2277239A2 (fr) | 1976-01-30 |
| FR2277239B2 true FR2277239B2 (cg-RX-API-DMAC10.html) | 1979-08-03 |
Family
ID=9140871
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7423233A Granted FR2277239A2 (fr) | 1974-07-04 | 1974-07-04 | Dispositif de commande de volets de tuyere d'ejection |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3954225A (cg-RX-API-DMAC10.html) |
| DE (1) | DE2529543C2 (cg-RX-API-DMAC10.html) |
| FR (1) | FR2277239A2 (cg-RX-API-DMAC10.html) |
| GB (1) | GB1478075A (cg-RX-API-DMAC10.html) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4181260A (en) * | 1977-03-17 | 1980-01-01 | General Electric Company | Hydraulic actuation ring |
| FR2714421B1 (fr) * | 1980-01-14 | 1996-03-01 | Snecma | Tuyère comportant un convergent-divergent réglable, notamment pour moteur à réaction. |
| FR2724977B1 (fr) * | 1980-12-30 | 1996-12-13 | Snecma | Tuyere convergente-divergente en particulier pour turboreacteur |
| FR2723145B1 (fr) * | 1981-11-24 | 1996-12-13 | Snecma | Tuyere convergente-divergente, en particulier pour turboreacteur |
| FR2732408A1 (fr) * | 1983-03-16 | 1996-10-04 | Snecma | Tuyere, en particulier pour turboreacteur |
| US5140809A (en) * | 1990-02-12 | 1992-08-25 | General Electric Company | Exhaust nozzle idle thrust spoiling method |
| US5235808A (en) * | 1990-02-12 | 1993-08-17 | General Electric Company | Exhaust nozzle including idle thrust spoiling |
| US5082182A (en) * | 1990-08-23 | 1992-01-21 | United Technologies Corporation | Thrust vectoring exhaust nozzle |
| US5261605A (en) * | 1990-08-23 | 1993-11-16 | United Technologies Corporation | Axisymmetric nozzle with gimbled unison ring |
| US5176323A (en) * | 1991-04-15 | 1993-01-05 | General Electric Company | Reduced weight nozzle actuation mechanism |
| US5285637A (en) * | 1992-11-02 | 1994-02-15 | United Technologies Corporation | Seal centering and restraining device for an axisymmetric convergent/divergent nozzle |
| US5328098A (en) * | 1993-07-09 | 1994-07-12 | United Technologies Corporation | Thrust vectoring ejector nozzle |
| ES2136475B1 (es) * | 1994-05-20 | 2000-05-16 | Sener Ing & Sist | Perfeccionamientos en toberas axisimetricas de geometria variable y orientacion del flujo destinadas a propulsores de turbina de gas. |
| FR2723764B1 (fr) * | 1994-08-18 | 1996-12-20 | Snecma | Etancheite entre volets suiveurs divergents et convergents d'une tuyere d'ejection de turboreacteur |
| US7458221B1 (en) * | 2003-10-23 | 2008-12-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths |
| FR2873757B1 (fr) * | 2004-07-28 | 2006-09-29 | Snecma Moteurs Sa | Tuyere convergente de turboreacteur |
| FR2875853B1 (fr) * | 2004-09-29 | 2006-12-22 | Snecma Moteurs Sa | Turboreacteur avec une tuyere a section variable dont chaque volet pivote autour d'un axe, axes pour les volets |
| WO2008045069A1 (en) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Fan variable area nozzle with electromechanical actuator |
| US10023302B2 (en) | 2007-12-06 | 2018-07-17 | Roller Bearing Company Of America, Inc. | Actuation system for a lift assisting device and lined track rollers used therein |
| US9261132B2 (en) | 2009-04-24 | 2016-02-16 | Roller Bearing Company Of America, Inc. | Low friction bearing assembly and link apparatus |
| US8931281B2 (en) | 2010-06-07 | 2015-01-13 | United Technologies Corporation | External flap retaining mechanism |
| US20130163905A1 (en) * | 2011-12-06 | 2013-06-27 | Roller Bearing Company Of America, Inc. | High-cycle, short range-of-motion linkage apparatus for gas turbine engine applications |
| EP2844886B1 (en) | 2012-04-30 | 2018-11-07 | Roller Bearing Company of America, Inc. | Hybrid bearing assembly with rolling elements and plain bearing |
| US20220325677A1 (en) * | 2021-04-12 | 2022-10-13 | Detonation Space Inc. | Adjustable exhaust nozzle for detonation engines |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2697907A (en) * | 1948-11-12 | 1954-12-28 | Gen Motors Corp | Multiplate variable area jet nozzle |
| US2811831A (en) * | 1951-06-29 | 1957-11-05 | United Aircraft Corp | Variable area nozzle |
| FR1376576A (fr) * | 1963-08-02 | 1964-10-31 | Snecma | Silencieux pour réacteurs |
| FR1478474A (fr) * | 1966-03-02 | 1967-04-28 | Snecma | Dispositif de commande de volets de tuyère d'éjection |
-
1974
- 1974-07-04 FR FR7423233A patent/FR2277239A2/fr active Granted
-
1975
- 1975-07-01 GB GB2763475A patent/GB1478075A/en not_active Expired
- 1975-07-02 DE DE2529543A patent/DE2529543C2/de not_active Expired
- 1975-07-03 US US05/593,177 patent/US3954225A/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| FR2277239A2 (fr) | 1976-01-30 |
| US3954225A (en) | 1976-05-04 |
| GB1478075A (en) | 1977-06-29 |
| DE2529543A1 (de) | 1976-01-22 |
| DE2529543C2 (de) | 1982-11-25 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| CL | Concession to grant licences |