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U.S. Department of Energy
Office of Scientific and Technical Information

Fuel injectors for turbine engines

Patent ·
OSTI ID:6342319
This patent describes a turbine engine. It comprises: a rotatable turbine wheel; a rotary compressor coupled to the turbine wheel; an annular combustor for receiving compressed air from the compressor and fuel from a fuel source and burning the same to provide gases of combustion to drive the turbine wheel; angularly spaced injector assemblies mounted on the outer wall and extending through the inner wall into the combustion zone; and a venturi surface.
Assignee:
Sundstrand Corp., Rockford, IL (USA)
Patent Number(s):
A; US 4955201
Application Number:
PPN: US s 7-133491
OSTI ID:
6342319
Country of Publication:
United States
Language:
English

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