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Machine translation
1. (WO1980002681) VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND JET ENGINE THEREFOR
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/1980/002681    International Application No.:    PCT/JP1979/000145
Publication Date: 11.12.1980 International Filing Date: 07.06.1979
IPC:
B64C 29/00 (2006.01)
Applicants:
Inventors:
Priority Data:
JP79/00145 07.06.1979 WO
Title (EN) VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND JET ENGINE THEREFOR
(FR) AVION A DECOLLAGE ET ATTERRISSAGE VERTICAUX ET REACTEUR POUR CELUI-CI
Abstract: front page image
(EN)Vertical take-off and landing aircraft in which a jet engine (2) with its jet nozzle port (13) directed downwardly is mounted underneath a fuselage (1) via a gimbal mechanism so that the jet engine (2) can be tilted in any direction around axes (5) and (6), the jet engine (2) having an especially large diameter for increasing the volume of air flow. Since a rotary portion which mounts a compressor (7) and a turbine (8) also has a large diameter, jetted gas is ejected circularly from the outer peripheral portion of the jet engine (2). Disposing the fuselage (1) in the hollow portion of the rotary portion extracted at the central portion thereof from the rotary portion enables the weight and front area of the aircraft body to be reduced.
(FR)Un avion a decollage et atterrissage verticaux dans lequel un reacteur (2) avec son orifice de tuyere a reaction (13) dirige vers le bas et monte sous un fuselage (1) par l"intermediaire d"un mecanisme a cardan de sorte que le reacteur (2) puisse etre incline dans toutes les directions autour des axes (5 et 6), le reacteur (2) ayant un diametre particulierement grand pour augmenter le debit d"air. Etant donne qu"une portion rotative ou sont montes un compresseur (7) et une turbine (8) possede egalement un grand diametre, les gaz du reacteur sont ejectes de maniere circulaire a partir de la partie peripherique exterieure du reacteur (2). En disposant le fuselage (1) dans la partie creuse de la partie rotative amenagee dans sa partie centrale a partir de la partie rotative, on peut reduire le poids et la surface frontale de l"avion.
Designated States:
Publication Language: Japanese (JA)
Filing Language: Japanese (JA)