FR2128375B1 - - Google Patents
Info
- Publication number
- FR2128375B1 FR2128375B1 FR7206680A FR7206680A FR2128375B1 FR 2128375 B1 FR2128375 B1 FR 2128375B1 FR 7206680 A FR7206680 A FR 7206680A FR 7206680 A FR7206680 A FR 7206680A FR 2128375 B1 FR2128375 B1 FR 2128375B1
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
- B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB569271A GB1388852A (en) | 1971-03-01 | 1971-03-01 | Nozzle structure for jet propulsion engines |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2128375A1 FR2128375A1 (fr) | 1972-10-20 |
FR2128375B1 true FR2128375B1 (fr) | 1976-06-11 |
Family
ID=9800855
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7206680A Expired FR2128375B1 (fr) | 1971-03-01 | 1972-02-28 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3806068A (fr) |
DE (1) | DE2209748A1 (fr) |
FR (1) | FR2128375B1 (fr) |
GB (1) | GB1388852A (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3863867A (en) * | 1973-12-26 | 1975-02-04 | Boeing Co | Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor |
US4358074A (en) * | 1979-05-24 | 1982-11-09 | The Boeing Company | Propulsion system for V/STOL aircraft |
FR2507558B1 (fr) * | 1981-06-11 | 1985-11-15 | Do G P | Groupe moteur de sustentation et de propulsion d'un vehicule de transport a coussin d'air |
US4648571A (en) * | 1984-07-19 | 1987-03-10 | Northrop Corporation | Transverse thrust lift augmentation system |
US5150862A (en) * | 1991-01-11 | 1992-09-29 | United Technologies Corporation | In-flight reverser |
US5161752A (en) * | 1991-01-11 | 1992-11-10 | United Technologies Corporation | In-flight reverser |
GB2346593B (en) * | 1999-02-09 | 2003-01-08 | Airship Tech Serv Ltd | Airship bow thruster apparatus |
US7559191B2 (en) | 2004-09-17 | 2009-07-14 | Aurora Flight Sciences Corporation | Ducted spinner for engine cooling |
WO2006137869A2 (fr) * | 2004-09-17 | 2006-12-28 | Aurora Flight Sciences | Systeme et procede pour le controle de la vitesse angulaire de roulis d'un aeronef a voilure libre desaccouplee en torsion |
US7506837B2 (en) | 2004-09-17 | 2009-03-24 | Aurora Flight Sciences Corporation | Inbound transition control for a tail-sitting vertical take off and landing aircraft |
US7364115B2 (en) * | 2004-09-17 | 2008-04-29 | Aurora Flight Sciences Corporation | System and method for controlling engine RPM of a ducted fan aircraft |
US20070221783A1 (en) * | 2004-09-17 | 2007-09-27 | Robert Parks | Adaptive landing gear |
US8001764B2 (en) * | 2004-09-17 | 2011-08-23 | Aurora Flight Sciences Corporation | Vibration isolation engine mount system and method for ducted fans |
EP2074301B1 (fr) * | 2006-10-12 | 2016-02-24 | United Technologies Corporation | Turboréacteur à double-flux avec une tuyère de poussée controlée pour décollage et atterrissage |
US7883051B2 (en) * | 2008-03-27 | 2011-02-08 | Johann Q. Sammy | Ducted propulsion vector system |
US9394852B2 (en) * | 2012-01-31 | 2016-07-19 | United Technologies Corporation | Variable area fan nozzle with wall thickness distribution |
US8375699B1 (en) | 2012-01-31 | 2013-02-19 | United Technologies Corporation | Variable area fan nozzle with wall thickness distribution |
EP2971595B1 (fr) * | 2013-03-15 | 2020-01-01 | United Technologies Corporation | Tuyère de soufflante à géométrie variable avec distribution d'épaisseur de paroi |
US20170058828A1 (en) * | 2015-08-26 | 2017-03-02 | Rohr, Inc. | Cascade with varying vane trailing edge thickness |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3068646A (en) * | 1959-01-28 | 1962-12-18 | Rolls Royce | Improvements in by-pass type gas turbine engines |
US3248878A (en) * | 1963-09-18 | 1966-05-03 | Gen Electric | Thrust deflector and reverser |
GB1247691A (en) * | 1968-08-08 | 1971-09-29 | Rolls Royce | Improvements in or relating to fan ducts for gas turbine ducted fan engines |
GB1246136A (en) * | 1968-09-14 | 1971-09-15 | Rolls Royce | Jet propulsion nozzle |
DE1927280A1 (de) * | 1969-05-29 | 1970-12-03 | Motoren Turbinen Union | Flugzeug,mit einem oder mehreren im Rumpfheck oder in Gondeln angeordneten,mit Schubumkehreinrichtungen ausgeruesteten Turbinenstrahltriebwerken |
-
1971
- 1971-03-01 GB GB569271A patent/GB1388852A/en not_active Expired
-
1972
- 1972-02-26 DE DE19722209748 patent/DE2209748A1/de active Pending
- 1972-02-28 US US00229983A patent/US3806068A/en not_active Expired - Lifetime
- 1972-02-28 FR FR7206680A patent/FR2128375B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3806068A (en) | 1974-04-23 |
GB1388852A (en) | 1975-03-26 |
FR2128375A1 (fr) | 1972-10-20 |
DE2209748A1 (de) | 1972-09-07 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |