Variable cycle engine for high altitude aircraft

Details Variable cycle engine for high altitude aircraft Variable cycle engine for high altitude aircraft

1985-02-06

1986-07-08

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 3933, 13762548, F02G 100

Patent

active

045985430

ABSTRACT:
A turboshaft engine is modified to be able to operate as a turbojet or a turboprop by the movement of an annular slide valve that directs gas flow between a high pressure turbine and a low pressure turbine.

REFERENCES:
patent: 690611 (1902-01-01), Roake
patent: 2307654 (1943-01-01), Andrews
patent: 2474143 (1949-06-01), Forsyth
patent: 2580591 (1952-01-01), Pouit
patent: 2587649 (1952-03-01), Pope
patent: 2832192 (1958-04-01), Budish
patent: 3161018 (1964-12-01), Sandre
patent: 3520138 (1970-07-01), Fox
patent: 3678690 (1972-07-01), Shohet et al.
patent: 3810360 (1974-05-01), Leibach
patent: 3867813 (1975-02-01), Leibach
patent: 3893638 (1975-07-01), Kelley
Jane's Aircraft, pp. 341-342.

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