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)
Abstract
1302228 Gas turbine engines in aircraft HAWKER SIDDELEY AVIATION Ltd 14 Dec 1971 [14 Dec 1970] 59339/70 Heading B7G [Also in Division F1] A gas turbine engine 60, mounted on the wing 61 of an aircraft, discharges, via jet pipe 62, through the turbine of an aft turbo-fan unit 63 which is located in a position at the trailing edge of the wing to receive air flowing both over and under the wing and is mounted on the airframe structure; the jet pipe not being required to bear the load of the fan unit. In some instances it is possible to mount the fan unit as a cantilever off the wing but it is preferably carried alongside the fuselage on mountings on the fuselage structure. The engine 60 is shown mounted in a pod 64 just below the wing, but may be buried in the wing (Fig. 4, not shown), in which case engine, jet pipe and fan unit are substantially coaxial. The engine may also be carried beneath the wing on a pylon (Fig. 6, not shown) and in this case the jet pipe has considerably more curvature to lead up to the fan unit.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5933970 | 1970-12-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1302228A true GB1302228A (en) | 1973-01-04 |
Family
ID=10483579
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5933970A Expired GB1302228A (en) | 1970-12-14 | 1970-12-14 |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1302228A (en) |
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 (en) * | 1992-08-06 | 1994-02-09 | AEROSPATIALE Société Nationale Industrielle | Mounting device of a turbine engine on an aircraft structure |
FR2698068A1 (en) * | 1992-11-16 | 1994-05-20 | Airbus Ind | Aircraft and other powered aircraft with wings. |
-
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 (en) * | 1992-08-06 | 1994-02-09 | AEROSPATIALE Société Nationale Industrielle | Mounting device of a turbine engine on an aircraft structure |
FR2694537A1 (en) * | 1992-08-06 | 1994-02-11 | Aerospatiale | Device for attaching a turbomachine to an aircraft structure. |
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 (en) * | 1992-11-16 | 1994-05-20 | Airbus Ind | Aircraft and other powered aircraft with wings. |
WO1994011248A1 (en) * | 1992-11-16 | 1994-05-26 | Airbus Industrie | Aircraft with at least one set of two engines fitted on each wing |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4712750A (en) | Temperature control device for jet engine nacelle associated structure | |
GB924078A (en) | Aircraft | |
US3229933A (en) | Cruise fan powerplant | |
GB1024894A (en) | Improvements in aircraft jet-propulsion power-plants | |
GB1302228A (en) | ||
GB1041132A (en) | Improvements relating to the propulsion of aircraft | |
GB817507A (en) | Improvements in or relating to aircraft | |
US3146971A (en) | Hypersonic aircraft | |
GB877838A (en) | Improvements relating to gas turbine engine air intakes | |
GB1076152A (en) | Improvements in aircraft power plants | |
Woodward et al. | Measured far-field flight noise of a counterrotation turboprop at cruise conditions | |
GB1032274A (en) | Mounting of ducted fan turbine engines in the tail of an aircraft | |
GB890703A (en) | An improved tiltable pod for jet power units on aircraft | |
Krebs | Advanced Supersonic Technology Study: Engine Program Summary. Supersonic Propulsion: 1971 to 1976 | |
GB1365305A (en) | Aircraft | |
Randall | The XB-70 A air induction system | |
Goodmanson et al. | Installation and integration of transonic transport propulsion systems | |
GB1131378A (en) | Air intake for a gas turbine engine | |
Clark et al. | Development of the AV-8B propulsion system | |
GB1074068A (en) | Mounting arrangement for gas turbine jet propulsion engines | |
GB1392432A (en) | Aircraft | |
GB1215461A (en) | Improvements in or relating to aircraft | |
GB1017377A (en) | Releasable aircraft engine pods | |
Baals et al. | Assessment of Sonic‐Boom Problem for Future Air‐Transport Vehicles | |
Sutcliffe | Aerodynamics II |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |