S-duct for a turbo-jet aircraft engine

Details S-duct for a turbo-jet aircraft engine S-duct for a turbo-jet aircraft engine

1992-07-07

1994-04-05

Barefoot, Galen

Aeronautics and astronautics

Aircraft power plants

244 55, B64D 3302

Patent

active

052997600

ABSTRACT:
An improved S-duct for turbo-jet engined aircraft. The present invention allows a high volume of high energy air to traverse the S-duct at a high pressure recovery ratio.

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patent: 4787421 (1988-11-01), Yu
patent: 4901947 (1990-02-01), Raymer
patent: 4989807 (1991-02-01), Foreman et al.

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