Aircraft engine layout

Details Aircraft engine layout Aircraft engine layout

1993-11-29

1995-05-02

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3983, 244 53B, F02C 704, F02C 712

Patent

active

054108705

ABSTRACT:
Aircraft engine, whose ancillary equipment forms a unitary assembly wherein the equipment is located to the rear of the air intake duct in a substantially closed central compartment just upstream of the gas generator. The equipment positioned along the engine axis, which, inter alia, leads to low engine drag in operation.

REFERENCES:
patent: 2400714 (1946-05-01), Rowledge et al.
patent: 2441135 (1948-05-01), Chalupa
patent: 2548858 (1951-04-01), Benedict
patent: 2618119 (1952-11-01), Redding et al.
patent: 3859785 (1975-01-01), Leto et al.
patent: 5123242 (1992-06-01), Miller

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