Keel-rib coolant channels for rocket combustors

Details Keel-rib coolant channels for rocket combustors Keel-rib coolant channels for rocket combustors

1987-07-08

1988-11-01

Casaregola, Louis J.

Power plants

Reaction motor

Liquid oxidizer

60267, F02K 900

Patent

active

047810190

ABSTRACT:
The present invention provides a regeneratively cooled rocket combustor comprising a combustor wall, a plurality of coolant channels extending through the combustor wall and at least one keel-rib extending into each coolant channel from the channel roof and which is bounded on both of its sides by arcuate flutes for providing smooth and continuous surface transition between the keel-rib and adjoining interior surfaces of the coolant channel.

REFERENCES:
patent: 3154914 (1964-11-01), Stockel

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