Integrated turboramjet engine

Details Integrated turboramjet engine Integrated turboramjet engine

1990-04-05

1991-10-22

Bertsch, Richard A.

Power plants

Reaction motor

Interrelated reaction motors

60225, 602701, F02C 7042, F02K 716

Patent

active

050583786

ABSTRACT:
A change-over arrangement for an integrated turboramjet engine has a guide ring which can be displaced in the axial direction and an annular cone which can be displaced against the guide ring. In the turbo-operation, the annular cone is in its front position and the guide ring is in its rear position closing off a ram air inlet duct, and in the ramjet operation, the annular cone, in its rear position, closes off the turbo-inlet duct, and the guide ring opens up the ram air inlet duct. As a result, a low-loss introduction of the air current can take place into the turbo-inlet duct or into the ram air inlet duct, without, at the same time, requiring disadvantageous enlargements of the diameter of the outer casing of the engine.

REFERENCES:
patent: 2955414 (1960-10-01), Hausmann
patent: 3161018 (1964-12-01), Sandre

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