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:
Jan. 26, 1999

Filed:

Feb. 27, 1997
Applicant:
Inventor:

John S Richardson, Nottingham, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R / ; F23R / ;
U.S. Cl.
CPC ...
60737 ; 60747 ;
Abstract

A double annular combustor for a gas turbine engine is provided with annular arrays of main and pilot fuel injection modules. The main fuel injection modules are of the premix type so as to vaporise fuel. However, the pilot fuel injection modules are configured so as to function as both premix and airspray fuel injectors. During starting and low power conditions, the pilot fuel injectors are operational alone in their airspray mode. However during high power conditions, both the main and pilot fuel injection modules function as premix injectors. The arrangement reduces noxious emissions.


Find Patent Forward Citations

Richardson, John. (1999). Gas turbine engine combustion equipment (U.S. Patent No. 5862668). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/5862668

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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