|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3936 ; 60/738|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 11 인용 특허 : 12|
A fuel injector 46 for a turbine engine includes an elongated, generally cylindrical metal casting 76 having a cylindrical surface 78 terminating in an end 84 having a frustoconical surface 86. A bore 88 having an axis 89 normal to the frustoconical surface 86 extends through the casting 76 to provide an air inlet 90 in the cylindrical surface 78 and a fuel and air outlet 94 in the frustoconical surface 86. The bore 88 is narrowed at the outlet to provide a constriction 110 thereat. A curved tube 96 of substantially lesser diameter than the bore 88 is lo...
A fuel injector for a turbine engine comprising: an elongated, generally cylindrical metal casting having a cylindrical surface terminating in an end having a frustoconical surface; a bore having an axis normal to said frustoconical surface and extending through said casting to provide an air inlet in said cylindrical surface and a fuel and air outlet in said frustoconical surface, said bore being narrowed at said outlet to provide a constriction thereat; a curved tube of substantially lesser diameter than said bore and at least partially within said bor...