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
Application number
GB5933970A
Other languages
English (en)
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Publication of GB1302228A publication Critical patent/GB1302228A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/10Aircraft characterised by the type or position of power plant of gas-turbine type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB5933970A 1970-12-14 1970-12-14 Expired GB1302228A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5933970 1970-12-14

Publications (1)

Publication Number Publication Date
GB1302228A true GB1302228A (fr) 1973-01-04

Family

ID=10483579

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5933970A Expired GB1302228A (fr) 1970-12-14 1970-12-14

Country Status (1)

Country Link
GB (1) GB1302228A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
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.

Cited By (9)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
US4712750A (en) Temperature control device for jet engine nacelle associated structure
GB1172782A (en) Lift Fan Installations for Vertical Take Off and Landing Aircraft.
US3229933A (en) Cruise fan powerplant
GB1024894A (en) Improvements in aircraft jet-propulsion power-plants
GB1302228A (fr)
GB1041132A (en) Improvements relating to the propulsion of aircraft
GB817507A (en) Improvements in or relating to aircraft
GB1076152A (en) Improvements in aircraft power plants
GB1032274A (en) Mounting of ducted fan turbine engines in the tail of an aircraft
Stern Aircraft Propulsion A Key to Fuel Conservation An Aircraft Manufacturer's View
GB890703A (en) An improved tiltable pod for jet power units on aircraft
GB1365305A (en) Aircraft
Goodmanson et al. Installation and integration of transonic transport propulsion systems
Randall The XB-70 A air induction system
GB1074068A (en) Mounting arrangement for gas turbine jet propulsion engines
Clark et al. Development of the AV-8B propulsion system
GB983051A (en) Aircraft
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
Holbrook et al. Evolution of the turboprop for high speed air transportation
Rose et al. Continuous Spark Ignition for Rapid Relight After Flameout of Gas Turbine Engines
GB793928A (en) Improvements relating to methods and means of operating aircraft
GB1131378A (en) Air intake for a gas turbine engine

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee