Combustion chamber structure and its manufacturing process

Power plants – Reaction motor – Including heat exchange means

Reexamination Certificate

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C029S890010

Reexamination Certificate

active

06889496

ABSTRACT:
A combustion chamber structure for a rocket engine or the like, has a combustion chamber liner with cooling channels and at least one manifold for feeding and removing a coolant, particularly a cryogenic fuel. The at least one manifold is brazed together with the combustion chamber liner and the area of the combustion chamber liner that is not covered by the at least one manifold is coated with an electroplated structural jacket. The invention also includes a method for manufacturing the combustion chamber structure.

REFERENCES:
patent: 5233755 (1993-08-01), Vandendriessche
patent: 5701670 (1997-12-01), Fisher et al.
patent: 5732883 (1998-03-01), Beaurain et al.
patent: 20020084190 (2002-07-01), Ewald et al.
patent: 20040244360 (2004-12-01), McMullen
patent: 2519538 (1976-11-01), None
patent: 196 16 838 (1996-10-01), None
patent: 100 61 186 (2002-01-01), None

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