The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 04, 1992

Filed:

May. 16, 1990
Applicant:
Inventors:

Michael T Todman, Leamington SPA, GB;

Simon A James, Conventry, GB;

Michael L Parker, Conventry, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C / ;
U.S. Cl.
CPC ...
60 3937 ; 60 39511 ;
Abstract

In a gas turbine engine power unit the gas turbine engine is provided with combustion chambers whose axes are perpendicular to the engine longitudinal axis. Each combustion chamber is located within and supported by a corresponding tubular member. Each tubular member is supported from a first annular manifold and in turn supports a second annular manifold which is located wholly within the first manifold. The first manifold receives air from the gas turbine engine compressor and directs it to a regenerative heat exchanger. Heated air returned from the regenerative heat exchanger is directed to the second manifold from where it flows through apertures in the tubular members to the combustion chambers. The manner in which the manifolds and combustion chambers are mounted reduces stresses arising from thermal gradients.


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