|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3936 ; 60/743 ; 60/760|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 12 인용 특허 : 0|
Improved fuel atomization for turbine engines utilizing high viscosity fuels is accomplished in an engine having an annular combustor (26) by providing an air injector (52) which produces an air stream (50) generally tangentially directed into the combustor (26) to intersect a fuel spray or film (46) also generally tangentially directed into the combustor (26) by a fuel injector (48) to atomize fuel for ignition by an igniter (60) in an annular outer wall (34) of the combustor (26).
A turbine engine, comprising: a rotary compressor; a turbine wheel coupled to said compressor for driven movement thereof; an annular combustor defining an annular combustion space disposed about said turbine wheel and in fluid communication with both said compressor and said nozzle, said combustor having at least one igniter mounted therein, said combustor being adapted to receive fuel from a source and air from said compressor and to combust fuel and air in said combustion space to generate said gases of combustion; impingement pressure fuel injection ...