Heat transfer enhancement features for a tubular wall...

Power plants – Reaction motor – Including heat exchange means

Reexamination Certificate

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C060S759000, C431S353000

Reexamination Certificate

active

07464537

ABSTRACT:
A combustion chamber for use in an engine, such as a rocket engine, has an inner wall with a corrugated configuration. The inner wall is formed with a plurality of tubes for carrying a coolant. As a result of the tubular construction, the inner wall has a plurality of spaced apart crowns and a plurality of valleys intermediate with the spaced apart crowns. To enhance the rate of heat flux or transfer in the valleys, a device is installed in each valley to cause local intensification of the turbulence in the hot gas flow in an effective way. The device may take the shape of a chevron or a bump.

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