Rocket augmentation for combined cycle turboaccelerator jet...

Details Rocket augmentation for combined cycle turboaccelerator jet... Rocket augmentation for combined cycle turboaccelerator jet...

2007-12-11

2007-12-11

Kim, Ted (Department: 3746)

Power plants

Reaction motor

Method of operation

C060S761000, C060S039461

Reexamination Certificate

active

10918003

ABSTRACT:
An engine for creating a propulsive force includes turbomachinery for generating a flow of hot exhaust gases and an initial thrust force, an augmentor positioned aft of the turbomachinery, and a system for injecting an oxidizer, which preferably undergoes thermal decomposition, into the hot exhaust gases so as to significantly increase the thrust force generated by the engine. In a preferred embodiment of the present invention, the oxidizer comprises liquid high test peroxide.

REFERENCES:
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patent: 4044971 (1977-08-01), Pharris
patent: 4907943 (1990-03-01), Kelch
patent: 5160080 (1992-11-01), Hines et al.
patent: 5272870 (1993-12-01), Grieb et al.
patent: 2003/0079463 (2003-05-01), McKinney
patent: 2235249 (1991-02-01), None
“Jet engines for supersonic flight” by R.I. Kurziner, Moscow, Maschinostroenie, 1977, pp. 145-146, Fig. 5.2.

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