Combustor of high pressure burner for rocket engine and method o

Details Combustor of high pressure burner for rocket engine and method o Combustor of high pressure burner for rocket engine and method o

1989-04-13

1990-03-20

Casaregola, Louis J.

Power plants

Reaction motor

Liquid oxidizer

60267, 2311271, F02K 904

Patent

active

049090321

ABSTRACT:
An inner tube tube an outer surface of which is machined to define regerative coolant grooves for flowing a coolant to cool a combustor is split at a throat into upper and lower portions which in turn are fitted into an outer tube fabricated as a unitary structure. The upper and lower inner tube portions and the inner and outer tubes are integrally joined together.

REFERENCES:
patent: 2705399 (1955-04-01), Allen
patent: 2900168 (1959-08-01), Nyborg
patent: 3057148 (1962-10-01), Kimpel
patent: 3154914 (1964-11-01), Stockel
patent: 3605412 (1971-09-01), Stockel
patent: 3630449 (1971-12-01), Butler

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