Abstract: A micro gas turbine engine for use in a turbo heater or co-generation application is described. The micro gas turbine engine includes a fuel delivery system which minimizes the development of deposits in the air-fuel passageway. To this end, a fuel delivery channel formed between a fuel deflector and a slinger body is formed with a contoured or undulating surface. A fuel deflector ring is interposed between the fuel delivery channel and the slinger impeller to facilitate the flow of the air-fuel mixture into the combustion chamber.
Type:
Grant
Filed:
November 6, 2009
Date of Patent:
December 11, 2012
Assignee:
JHRG Inc.
Inventors:
Richard W. Gordon, Nancy Ann Gordon, legal representative