Enhanced performance torroidal coolant-collection manifold

Power plants – Reaction motor – Including heat exchange means

Reexamination Certificate

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Details

C060S752000

Reexamination Certificate

active

07373774

ABSTRACT:
A system for cooling a combustion chamber of an engine, such as a rocket engine, is provided. The system has a plurality of coolant tubes or passages surrounding the combustion chamber, a torroidal coolant-collection manifold for receiving coolant from the coolant tubes or passages and for discharging the coolant through a discharge port, and a plurality of turning vanes within the torroidal manifold for reducing pressure loss and improving pressure uniformity associated with the torroidal coolant-collection manifold.

REFERENCES:
patent: 3001726 (1961-09-01), Hasbrouck
patent: 3062566 (1962-11-01), Coburn
patent: 6829884 (2004-12-01), Fint et al.
patent: 2004/0011023 (2004-01-01), Wherley et al.
patent: 0 697 515 (1996-02-01), None
patent: 2 196 392 (1988-04-01), None
patent: 6-330816 (1994-01-01), None

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