|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 6 인용 특허 : 0|
A gas turbine engine 10 having a rotor 12 with turbine blades 14 and a nozzle 16 adjacent the turbine blades 14 for directing hot gases of combustion at the turbine blades 14. The engine 10 also includes an annular combustor 18 about the rotor 12 and an annular combustor housing 30 substantially surrounding the combustor 18 in generally concentric spaced relation. A fuel injection system is operatively associated with the combustor 18 for injecting fuel into a combustion space 28 to be combusted with air from a compressor 34. The fuel injection system ma...
A gas turbine engine, comprising: a rotor including turbine blades and a nozzle adjacent said turbine blades for directing hot gases of combustion at said turbine blades; an annular combustor about said rotor defined by spaced inner and outer walls connected by a radially extending wall, said combustor having an outlet leading to said nozzle, said combustor including an annular combustion space upstream of said outlet defined by said inner, outer and radially extending walls; an annular combustor housing substantially surrounding said combustor in genera...