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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/023—Aircraft characterised by the type or position of power plant of rocket type, e.g. for assisting taking-off or braking
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- 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
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- 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
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB339498X | 1956-04-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE557040A true BE557040A (en) |
Family
ID=10359469
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE557040D BE557040A (en) | 1956-04-27 |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE557040A (en) |
| CH (1) | CH339498A (en) |
| FR (1) | FR1187684A (en) |
| GB (1) | GB806038A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0524875A1 (en) * | 1991-07-24 | 1993-01-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Thrust reverser for an aircraft jet engine with hydraulic actuation system with integrated security device |
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/en unknown
- 1957-04-27 FR FR1187684D patent/FR1187684A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0524875A1 (en) * | 1991-07-24 | 1993-01-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Thrust reverser for an aircraft jet engine with hydraulic actuation system with integrated security device |
| FR2679605A1 (en) * | 1991-07-24 | 1993-01-29 | Snecma | TURBOJET DRIVE INVERTER PROVIDED WITH A SAFETY DEVICE INTEGRATED WITH THE HYDRAULIC CONTROL SYSTEM. |
| 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 |
|---|---|
| FR1187684A (en) | 1959-09-15 |
| GB806038A (en) | 1958-12-17 |
| CH339498A (en) | 1959-06-30 |