Transport plane with stub tail

Aeronautics and astronautics – Aircraft structure – Details

Patent

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Details

244 53B, 244 23R, 244204, 244209, B64D 2702, B64C 2102, B64C 2106

Patent

active

054801109

ABSTRACT:
A transport plane with stub tail, which is preferably propelled by two jet engines. The intake air is fed to the engines directly integrated in the fuselage tail via a diffusor, the diffusor is a short diffusor. The air obtained by boundary layer suction via a suction slot with a combination of ejectors and diffusors is fed into the rest of the intake air.

REFERENCES:
patent: 2399839 (1946-05-01), Vorse
patent: 3289977 (1966-12-01), Staats
patent: 3317162 (1967-05-01), Grant
patent: 3633848 (1972-01-01), Fimml
patent: 3887147 (1975-06-01), Grieb
patent: 4033526 (1977-07-01), Benson
patent: 4643268 (1987-02-01), Jones et al.
patent: 5016837 (1991-05-01), Willis
patent: 5114097 (1992-05-01), Williams
patent: 5299760 (1994-05-01), Finch et al.
patent: 5368258 (1994-11-01), Johnson et al.

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