GB1302228A - - Google Patents
Info
- Publication number
- GB1302228A GB1302228A GB5933970A GB1302228DA GB1302228A GB 1302228 A GB1302228 A GB 1302228A GB 5933970 A GB5933970 A GB 5933970A GB 1302228D A GB1302228D A GB 1302228DA GB 1302228 A GB1302228 A GB 1302228A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- fan unit
- jet pipe
- engine
- aircraft
- 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
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5933970 | 1970-12-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1302228A true GB1302228A (ru) | 1973-01-04 |
Family
ID=10483579
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5933970A Expired GB1302228A (ru) | 1970-12-14 | 1970-12-14 |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1302228A (ru) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4544115A (en) * | 1979-05-01 | 1985-10-01 | Edgley Aircraft Limited | Ducted propeller aircraft |
GB2260369A (en) * | 1991-08-30 | 1993-04-14 | United Technologies Corp | Jet propulsion system having ejector shroud |
EP0582522A1 (fr) * | 1992-08-06 | 1994-02-09 | AEROSPATIALE Société Nationale Industrielle | Dispositif d'accrochage d'une turbomachine sur une structure d'aéronef |
FR2698068A1 (fr) * | 1992-11-16 | 1994-05-20 | Airbus Ind | Avion et autre aéronef à moteur pourvu d'ailes. |
-
1970
- 1970-12-14 GB GB5933970A patent/GB1302228A/en not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4544115A (en) * | 1979-05-01 | 1985-10-01 | Edgley Aircraft Limited | Ducted propeller aircraft |
US4657209A (en) * | 1979-05-01 | 1987-04-14 | Optica Industries Limited | Ducted propeller aircraft |
GB2260369A (en) * | 1991-08-30 | 1993-04-14 | United Technologies Corp | Jet propulsion system having ejector shroud |
GB2260369B (en) * | 1991-08-30 | 1994-07-06 | United Technologies Corp | Propulsion system assembly |
EP0582522A1 (fr) * | 1992-08-06 | 1994-02-09 | AEROSPATIALE Société Nationale Industrielle | Dispositif d'accrochage d'une turbomachine sur une structure d'aéronef |
FR2694537A1 (fr) * | 1992-08-06 | 1994-02-11 | Aerospatiale | Dispositif d'accrochage d'une turbomachine sur une structure d'aéronef. |
US5447282A (en) * | 1992-08-06 | 1995-09-05 | Societe Nationale Industrielle Et Aerospatiale Des Poudres Et Explosifs | Device for attaching a turbojet engine to an aircraft structure |
FR2698068A1 (fr) * | 1992-11-16 | 1994-05-20 | Airbus Ind | Avion et autre aéronef à moteur pourvu d'ailes. |
WO1994011248A1 (fr) * | 1992-11-16 | 1994-05-26 | Airbus Industrie | Avion comportant sur chaque aile au moins un groupe de deux moteurs |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |