Solid propellant air-turborocket

Details Solid propellant air-turborocket Solid propellant air-turborocket

1985-02-06

1993-10-05

Bentley, Stephen C.

Power plants

Reaction motor

Turborocket

60253, 60261, 602701, F02K 500

Patent

active

H00012343

ABSTRACT:
The invention discloses an air-turborocket having a single set of compres blades extending radially from a common rotor. A shroud ring encircles the outer periphery of the compressor blades and holds a plurality of turbine blades on the outer periphery thereof which are driven by hot expanding fuel rich gases obtained from the partial combustion of a solid propellant in a first combustion chamber external to a compressor housing. The hot expanding fuel rich gases drive the turbine blades which drive the compressor blades thereby providing compressed air which is forcibly mixed by a mixer/diffuser with the hot expanding fuel rich gases for further combustion to provide thrust in a second combustion chamber aft to the compressor.

REFERENCES:
patent: 3110153 (1963-11-01), House
patent: 4096803 (1978-06-01), Kesting

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