Propulsion system for supersonic aircraft

Details Propulsion system for supersonic aircraft Propulsion system for supersonic aircraft

1977-08-25

1980-01-15

Casaregola, Louis J.

Power plants

Reaction motor

Interrelated reaction motors

60 3926B, F02K 304, F02K 1100

Patent

active

041832116

ABSTRACT:
An optimized propulsion system for aircraft whose flight range extends over wide range of speeds. It comprises an outer turbojet engine and an inner turbojet engine housed within a single engine nacelle and arranged concentrically, the outer turbojet engine extending axially and around a narrow portion of the casing of the inner turbojet engine. The invention may be used in the field of variable-cycle engines, and particularly in the field of supersonic transport aircraft.

REFERENCES:
patent: 3659422 (1972-05-01), Hope
patent: 3677012 (1972-07-01), Batscha
patent: 3841091 (1974-10-01), Sargisson et al.
patent: 4033119 (1977-07-01), Nichols
patent: 4054030 (1977-10-01), Pedersen

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