BE557040A - - Google Patents
Info
- Publication number
- BE557040A BE557040A BE557040DA BE557040A BE 557040 A BE557040 A BE 557040A BE 557040D A BE557040D A BE 557040DA BE 557040 A BE557040 A BE 557040A
- 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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
- F02K1/625—Reversing jet main flow by blocking the rearward discharge by means of flaps the aft end of the engine cowling being movable to uncover openings for the reversed flow
-
- 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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Instruments For Viewing The Inside Of Hollow Bodies (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB339498X | 1956-04-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE557040A true BE557040A (de) |
Family
ID=10359469
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE557040D BE557040A (de) | 1956-04-27 |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE557040A (de) |
| CH (1) | CH339498A (de) |
| FR (1) | FR1187684A (de) |
| GB (1) | GB806038A (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0524875A1 (de) * | 1991-07-24 | 1993-01-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Schubumkehrvorrichtung für einen Strahlmotor mit hydraulischer Betätitungseinrichtung mit integrierter Sicherheitseinrichtung |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2156004A (en) * | 1984-03-15 | 1985-10-02 | Gen Electric | Thrust modulation device for a gas turbine engine |
-
0
- BE BE557040D patent/BE557040A/xx unknown
-
1956
- 1956-04-27 GB GB12946/56A patent/GB806038A/en not_active Expired
-
1957
- 1957-04-26 CH CH339498D patent/CH339498A/fr unknown
- 1957-04-27 FR FR1187684D patent/FR1187684A/fr not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0524875A1 (de) * | 1991-07-24 | 1993-01-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Schubumkehrvorrichtung für einen Strahlmotor mit hydraulischer Betätitungseinrichtung mit integrierter Sicherheitseinrichtung |
| FR2679605A1 (fr) * | 1991-07-24 | 1993-01-29 | Snecma | Inverseur de poussee de turboreacteur muni d'un dispositif de securite integre au systeme de commande hydraulique. |
| US5381654A (en) * | 1991-07-24 | 1995-01-17 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A) | Thrust reverser safety system |
Also Published As
| Publication number | Publication date |
|---|---|
| CH339498A (fr) | 1959-06-30 |
| FR1187684A (fr) | 1959-09-15 |
| GB806038A (en) | 1958-12-17 |