Easily demountable combustion chamber with improved...

Power plants – Combustion products used as motive fluid – Having mounting or supporting structure

Reexamination Certificate

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C060S804000, C060S796000

Reexamination Certificate

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07637111

ABSTRACT:
The component elements of a jet engine combustion chamber are assembled together in a manner that is designed to facilitate maintenance while also improving aerodynamic performance. In an embodiment, the outer cap and the inner cap have tongues and the chamber end wail has corresponding tongues, and the tongues of the caps are assembled to the tongues of the chamber end wall.

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patent: 7415826 (2008-08-01), McMasters et al.
patent: 2005/0000228 (2005-01-01), De Sousa et al.
patent: 2.219.311 (1974-09-01), None
U.S. Appl. No. 12/199,182, filed Aug. 27, 2008, Pieussergues, et al.

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