GB1349150A - Aircraft - Google Patents
AircraftInfo
- Publication number
- GB1349150A GB1349150A GB3417270A GB1349150DA GB1349150A GB 1349150 A GB1349150 A GB 1349150A GB 3417270 A GB3417270 A GB 3417270A GB 1349150D A GB1349150D A GB 1349150DA GB 1349150 A GB1349150 A GB 1349150A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- centre line
- aircraft
- nozzle
- jet
- 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
- 239000007789 gas Substances 0.000 abstract 2
- 238000007599 discharging Methods 0.000 abstract 1
- 230000005484 gravity Effects 0.000 abstract 1
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
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Electron Sources, Ion Sources (AREA)
Abstract
1349150 Propelling aircraft DEFENCE SECRETARY OF STATE FOR 26 July 1971 [14 July 1970] 34172/70 Heading B7G An aircraft has a main propulsion engine which may be an aft-fan gas turbine engine on each side of the fore-and-aft centre line of the aircraft and a third jet engine 14 of substantially less maximum thrust than each of the propulsion engines, this third engine discharging its jet at a place which is on said centre line and a substantial distance aft of the centre of gravity of the aircraft, there being means by which the direction of discharge of the jet from the third engine can be varied so as to be inclined upwards or downwards with respect to the centre line, or to one side or the other side of the centre line. Preferably, the third engine 14 having an intake 12 is pitched downwards with respect to the centre line and the nozzle 8 of the engine provides a fixed angle of deflection of the gases with respect to the engine, the angle being greater than the pitch of the engine. The nozzle 8 is rotatable with a ring 16 mounted on the engine. It is stated that the nozzle may be mounted on gimbal rings or deflecting vanes may replace the nozzle.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3417270 | 1971-07-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1349150A true GB1349150A (en) | 1974-03-27 |
Family
ID=10362288
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3417270A Expired GB1349150A (en) | 1971-07-26 | 1971-07-26 | Aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1349150A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2305344A1 (en) * | 1975-03-27 | 1976-10-22 | Boeing Co | AIRCRAFT FUSELAGE POWER UNIT |
| GB2282353A (en) * | 1993-10-04 | 1995-04-05 | Peter William Bishop | Vectored thrust flight control |
| WO1998021092A1 (en) * | 1996-11-12 | 1998-05-22 | Mcdonnell Douglas Corporation | Pylon flap for increasing negative pitching moments |
| CN106986035A (en) * | 2015-09-21 | 2017-07-28 | 通用电气公司 | rear engine for aircraft |
-
1971
- 1971-07-26 GB GB3417270A patent/GB1349150A/en not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2305344A1 (en) * | 1975-03-27 | 1976-10-22 | Boeing Co | AIRCRAFT FUSELAGE POWER UNIT |
| GB2282353A (en) * | 1993-10-04 | 1995-04-05 | Peter William Bishop | Vectored thrust flight control |
| GB2282353B (en) * | 1993-10-04 | 1997-09-24 | Peter William Bishop | Flight control systems for aircraft |
| WO1998021092A1 (en) * | 1996-11-12 | 1998-05-22 | Mcdonnell Douglas Corporation | Pylon flap for increasing negative pitching moments |
| US5779191A (en) * | 1996-11-12 | 1998-07-14 | Brislawn; Mark G. | Pylon flap for increasing negative pitching moments |
| CN106986035A (en) * | 2015-09-21 | 2017-07-28 | 通用电气公司 | rear engine for aircraft |
| CN106986035B (en) * | 2015-09-21 | 2020-09-08 | 通用电气公司 | Rear engine for an aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| CSNS | Application of which complete specification have been accepted and published, but patent is not sealed |