GB898360A - Disc-type aircraft - Google Patents

Disc-type aircraft

Info

Publication number
GB898360A
GB898360A GB13790/54A GB1379054A GB898360A GB 898360 A GB898360 A GB 898360A GB 13790/54 A GB13790/54 A GB 13790/54A GB 1379054 A GB1379054 A GB 1379054A GB 898360 A GB898360 A GB 898360A
Authority
GB
United Kingdom
Prior art keywords
aircraft
gases
shutters
annular
ports
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
GB13790/54A
Inventor
John Carver Meadows Frost
Thomas Desmond Earl
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Avro Aircraft Ltd
Original Assignee
Avro Aircraft Ltd
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 by Avro Aircraft Ltd filed Critical Avro Aircraft Ltd
Priority to GB13790/54A priority Critical patent/GB898360A/en
Publication of GB898360A publication Critical patent/GB898360A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/001Flying saucers

Abstract

898,360. Aircraft. AVRO AIRCRAFT Ltd. May 10, 1955 [May 11, 1954], No. 13790/54. Class 4. In an aircraft comprising a generally lentiform structure as described in Specification 898,358, a group of gas turbine engines 37 is positioned between the aerofoil surfaces in a generally radial arrangement with their intakes directed towards the centre of the structure and their outlets directed towards its perimeter. Each engine 37 is attached to a segment 11 and is housed in a cylindrical shell 38 within an annular fuel tank 13 with the aid of mounting means 43; 40, 39. The air intakes of the engines register with openings in an annular plenum chamber between walls 14 and 21, to which air is admitted through ports 29 or through spring closed ports 27, Fig. 8 (not shown), during take-off when the ports 29 are closed to avoid admission of combustion products from the " gas cushion " on which the craft rises. It is stated that, because of this ground cushion effect, the aircraft rises vertically although it may have a weight greater than combined static thrust of all its engines; The gases from the engine outlets, are ejected from the periphery of the aircraft and their flow is controlled to control the aircraft similar to the manner described in Specification 898,359 and as described in Specification 898,362. In " take-off" position a selector handle 80 closes shutters 72 so that all gases are ejected downwardly through an annular nozzle 69, but during flight this handle is moved to allow gases to be ejected from upper and lower nozzles 68, 69, the annular shutters being then eccentrically disposed to close both nozzles at the front and to locate them open to a progressively increasing extent towards the rear. A control handle 79 causesdifferential movement of the shutters so that its movement to port reduces. the proportion of port flowing gases having a downward component and increases the proportion of starboard flowing gases havinga downward component. Rudder pedals 83 control shutters 82 for openings 81 to port and starboard. Specification 892,401 also is referred to.
GB13790/54A 1954-05-11 1954-05-11 Disc-type aircraft Expired GB898360A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB13790/54A GB898360A (en) 1954-05-11 1954-05-11 Disc-type aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13790/54A GB898360A (en) 1954-05-11 1954-05-11 Disc-type aircraft

Publications (1)

Publication Number Publication Date
GB898360A true GB898360A (en) 1962-06-06

Family

ID=10029420

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13790/54A Expired GB898360A (en) 1954-05-11 1954-05-11 Disc-type aircraft

Country Status (1)

Country Link
GB (1) GB898360A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0304614A2 (en) * 1987-08-24 1989-03-01 von Kozierowski, Joachim Flying object taking off and landing vertically

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0304614A2 (en) * 1987-08-24 1989-03-01 von Kozierowski, Joachim Flying object taking off and landing vertically
EP0304614A3 (en) * 1987-08-24 1990-04-25 Joachim Von Kozierowski Centrifugal-force ring

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