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Machine translation
1. (WO1981000089) VERTICAL TAKE-OFF AND LANDING AIRCRAFT
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/1981/000089    International Application No.:    PCT/JP1979/000177
Publication Date: 22.01.1981 International Filing Date: 05.07.1979
IPC:
B64C 29/00 (2006.01)
Applicants:
Inventors:
Priority Data:
JP79/00177 05.07.1979 WO
Title (EN) VERTICAL TAKE-OFF AND LANDING AIRCRAFT
(FR) AVION A DECOLLAGE ET ATTERRISSAGE VERTICAUX
Abstract: front page image
(EN)An aircraft includes a cylindrical body having annular intakes (4) and jet outlets (5) about the periphery thereof, as well as a turbo jet engine (2) comprising a compressor (7), combustion chamber (8) and turbine (9), and gas deflection rings (6). The gas deflection ring (6) is rotatable and longitudinally slidable with respect to the cylindrical body (1). Such manipulation of the deflection ring (6) jets the gas from the outlets (5) in a prescribed direction, whereby the aircraft can take-off and land vertically, hover, turn and cruise.
(FR)Un avion comprend un corps cylindrique ayant des entrees (4) et des sorties de reacteur (5) annulaires a sa peripherie, ainsi qu"un turbo reacteur (2) comprenant un compresseur (7), une chambre de combustion (8) et une turbine (9), et des anneaux de deviation des gaz (6). L"anneau de deviation des gaz (6) est rotatif et coulisse longitudinalement par rapport au corps cylindrique (1). Une telle manipulation de l"anneau de deflexion (6) envoie les gaz provenant des sorties (5) suivant une direction predeterminee, permettant a l"avion de decoller et atterrir verticalement, planer, tourner et voler.
Designated States:
Publication Language: Japanese (JA)
Filing Language: Japanese (JA)