Annular combustion chamber in a turbine engine

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United States of America Patent

PATENT NO 9581334
SERIAL NO

14348966

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Abstract

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An annular combustion chamber of a turbine engine, the chamber including inner and outer coaxial walls forming two surfaces of revolution, which are connected together upstream by an annular chamber end wall including injection systems passing therethrough, each including an injector and at least one swirler for producing a rotating air stream that mixes downstream with fuel from the injector, and at least one ignition spark plug mounted in an orifice of the outer wall downstream from the injection systems. The spark plug is situated circumferentially between two adjacent injection systems that are configured to produce two air/fuel mixture sheets rotating in opposite directions.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINESPARIS FRA PARIS PARIS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bourgois, Sebastien Alain Christophe Saint Germain les Corbeil, FR 7 34
Sandelis, Denis Jean Maurice Nangis, FR 46 692

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