Turbofan engine bypass and exhaust system

Details Turbofan engine bypass and exhaust system Turbofan engine bypass and exhaust system

1993-05-24

1994-12-06

Bertsch, Richard A.

Power plants

Reaction motor

Interrelated reaction motors

60262, 60271, 60 3931, 23926517, F02K 302

Patent

active

053699548

ABSTRACT:
A turbofan engine bypass and exhaust system has a double-hoop configuration in which a fan exhaust passageway comprises shells of a constant circular contour to resolve air pressure induced stresses and increase in bypass passageway area asymmetrically in the horizontal direction without substantially increasing the overall engine height.

REFERENCES:
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patent: 3806067 (1974-04-01), Kutney
patent: 4132069 (1979-01-01), Adamson et al.
patent: 4327548 (1982-05-01), Woodward
patent: 4449682 (1984-05-01), Gratzer et al.
patent: 4567960 (1986-02-01), Johnson et al.
patent: 4683717 (1987-08-01), Naud
patent: 4802629 (1989-02-01), Klees
patent: 4930725 (1990-06-01), Thompson et al.
patent: 5058379 (1991-10-01), Lardellier
patent: 5097656 (1992-03-01), Napier

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