Turbo-ram-jet engine

Details Turbo-ram-jet engine Turbo-ram-jet engine

1983-07-07

1985-10-01

Casaregola, Louis J.

Power plants

Reaction motor

Plural motive fluid generating means or plural outlets

602701, 60 3933, F02G 100

Patent

active

045437858

ABSTRACT:
A high speed, high-altitude jet aircraft engine operable as a ram-jet and/or turbo-jet using a single combustion chamber in a main housing receiving compressed air and also a variable flow of ram air bypassing the compressor. Primary and secondary burners in different parts of the combustion chamber produce respectively a major high temperature portion of burnt gas exhausted direct through a main nozzle and a minor lower temperature portion ducted off to drive the turbine which is in a side housing, the minor portion being exhausted through a subordinate nozzle.

REFERENCES:
patent: 2672726 (1954-03-01), Wolf et al.
patent: 2952973 (1960-09-01), Hall et al.
patent: 4122670 (1978-10-01), Reider
patent: 4271666 (1981-06-01), Hurley et al.

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