BE691769A - - Google Patents
Info
- Publication number
- BE691769A BE691769A BE691769DA BE691769A BE 691769 A BE691769 A BE 691769A BE 691769D A BE691769D A BE 691769DA BE 691769 A BE691769 A BE 691769A
- Authority
- BE
- Belgium
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
-
- 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
- F02K1/123—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure
-
- 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
- F02K1/38—Introducing air inside the jet
- F02K1/383—Introducing air inside the jet with retractable elements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US517297A US3391898A (en) | 1965-12-29 | 1965-12-29 | Actuating mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE691769A true BE691769A (en:Method) | 1967-05-29 |
Family
ID=24059220
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE691769D BE691769A (en:Method) | 1965-12-29 | 1966-12-27 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3391898A (en:Method) |
| BE (1) | BE691769A (en:Method) |
| DE (1) | DE1526883B1 (en:Method) |
| FR (1) | FR1506194A (en:Method) |
| GB (1) | GB1167040A (en:Method) |
| NL (1) | NL6618372A (en:Method) |
| SE (1) | SE303103B (en:Method) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3614037A (en) * | 1969-09-22 | 1971-10-19 | Boeing Co | Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser |
| GB1526224A (en) * | 1975-10-28 | 1978-09-27 | Rolls Royce | Gas turbine engine cowls |
| US8615982B2 (en) * | 2011-07-05 | 2013-12-31 | Hamilton Sundstrand Corporation | Integrated electric variable area fan nozzle thrust reversal actuation system |
| FR3012794B1 (fr) * | 2013-11-05 | 2017-03-24 | Aircelle Sa | Liaison entre un actionneur et un inverseur de poussee d'une nacelle de turboreacteur, comportant des jeux |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US788510A (en) * | 1903-04-21 | 1905-05-02 | Crane Co | Valve. |
| US2504006A (en) * | 1947-09-05 | 1950-04-11 | Craig L Davis | Valve device |
| US3057150A (en) * | 1961-03-27 | 1962-10-09 | United Aircraft Corp | Two dimensional floating blow-in-door and flap ejector |
| DE1193733B (de) * | 1961-03-27 | 1965-05-26 | United Aircraft Corp | Ejektor-Schubduese zum Flugzeugantrieb |
-
1965
- 1965-12-29 US US517297A patent/US3391898A/en not_active Expired - Lifetime
-
1966
- 1966-12-16 GB GB56517/66A patent/GB1167040A/en not_active Expired
- 1966-12-22 DE DE19661526883 patent/DE1526883B1/de active Pending
- 1966-12-27 BE BE691769D patent/BE691769A/xx unknown
- 1966-12-28 FR FR5037A patent/FR1506194A/fr not_active Expired
- 1966-12-28 SE SE17806/66A patent/SE303103B/xx unknown
- 1966-12-29 NL NL6618372A patent/NL6618372A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| SE303103B (en:Method) | 1968-08-12 |
| GB1167040A (en) | 1969-10-15 |
| DE1526883B1 (de) | 1971-06-09 |
| NL6618372A (en:Method) | 1967-06-30 |
| FR1506194A (fr) | 1967-12-15 |
| US3391898A (en) | 1968-07-09 |