GB2083420B - Disposition of engine on aircraft - Google Patents
Disposition of engine on aircraftInfo
- Publication number
- GB2083420B GB2083420B GB8124046A GB8124046A GB2083420B GB 2083420 B GB2083420 B GB 2083420B GB 8124046 A GB8124046 A GB 8124046A GB 8124046 A GB8124046 A GB 8124046A GB 2083420 B GB2083420 B GB 2083420B
- Authority
- GB
- United Kingdom
- Prior art keywords
- disposition
- aircraft
- engine
- Prior art date
- 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
- 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
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19803033101 DE3033101C2 (de) | 1980-09-03 | 1980-09-03 | Anordnung zur Erhöhung der resultierenden Vortriebskraft bei Flugzeugen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB2083420A GB2083420A (en) | 1982-03-24 |
| GB2083420B true GB2083420B (en) | 1984-06-27 |
Family
ID=6111003
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8124046A Expired GB2083420B (en) | 1980-09-03 | 1981-08-06 | Disposition of engine on aircraft |
Country Status (4)
| Country | Link |
|---|---|
| JP (1) | JPS5777295A (enExample) |
| DE (1) | DE3033101C2 (enExample) |
| FR (1) | FR2489245A1 (enExample) |
| GB (1) | GB2083420B (enExample) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4478378A (en) * | 1981-10-15 | 1984-10-23 | Aeritalia-Societa Aerospaziale Italiana-Per Azioni | Aircraft with jet propulsion |
| AU555526B2 (en) * | 1982-10-29 | 1986-09-25 | General Electric Company | Aircraft engine nacelle |
| GB2149456B (en) * | 1983-11-08 | 1987-07-29 | Rolls Royce | Exhaust mixing in turbofan aeroengines |
| DE3345154C2 (de) * | 1983-12-14 | 1987-02-12 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Tragflügel für Luftfahrzeuge |
| CA1324999C (en) * | 1986-04-30 | 1993-12-07 | Walter M. Presz, Jr. | Bodies with reduced surface drag |
| GB2207468A (en) * | 1987-06-01 | 1989-02-01 | Secr Defence | Vortex silencing in gas turbine engines |
| JP2606289Y2 (ja) * | 1993-06-07 | 2000-10-10 | 富士重工業株式会社 | 航空機のナセル装置 |
| US10723464B2 (en) | 2015-08-26 | 2020-07-28 | Rohr, Inc. | Injector nozzle configuration for swirl anti-icing system |
| US10393020B2 (en) | 2015-08-26 | 2019-08-27 | Rohr, Inc. | Injector nozzle configuration for swirl anti-icing system |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2641468C2 (de) * | 1976-09-15 | 1985-06-13 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Flugzeug mit oberhalb der Tragflügel angeordneten Triebwerken |
-
1980
- 1980-09-03 DE DE19803033101 patent/DE3033101C2/de not_active Expired
-
1981
- 1981-08-06 GB GB8124046A patent/GB2083420B/en not_active Expired
- 1981-09-03 FR FR8116790A patent/FR2489245A1/fr active Granted
- 1981-09-03 JP JP13785481A patent/JPS5777295A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5777295A (en) | 1982-05-14 |
| DE3033101A1 (de) | 1982-03-11 |
| DE3033101C2 (de) | 1984-11-22 |
| FR2489245A1 (fr) | 1982-03-05 |
| FR2489245B3 (enExample) | 1983-06-03 |
| GB2083420A (en) | 1982-03-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB2074962B (en) | Engine mounting arrangement | |
| JPS5740382A (en) | Aircraft engine starting and generating device | |
| GB2070161B (en) | Aircraft generator starter-drive | |
| JPS5797018A (en) | Reciprocal cooling system of engine | |
| GB2071266B (en) | Engine mounting structure | |
| JPS57330A (en) | Aircraft gasturbine engine | |
| JPS57108414A (en) | Car engine | |
| JPS57124035A (en) | Engine system | |
| IL63566A0 (en) | Management system for an aircraft engine | |
| JPS57126507A (en) | Expansion engine | |
| GB2469613B (en) | Aircraft | |
| DE3171462D1 (en) | Engine mounting structure | |
| JPS56135721A (en) | Turbine engine system | |
| GB2083420B (en) | Disposition of engine on aircraft | |
| GB2082520B (en) | Cooling of vehicle engines | |
| GB2132577B (en) | Launching aircraft | |
| JPS56129736A (en) | Combustion engine | |
| JPS5744701A (en) | Pinston engine | |
| JPS54153499A (en) | Mounting device of aircraft engine | |
| JPS5613266A (en) | Method of mounting engine | |
| GB2105800B (en) | Transmission-responsive engine governor | |
| GB2105271A (en) | Aircraft engine mount | |
| JPS57138500A (en) | Aircraft | |
| ZA813912B (en) | Supercharged engine | |
| JPS5722981A (en) | Mounting structure for fair ring of autobicycle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |