|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/738; 060/759; 060/760|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 39 인용 특허 : 0|
A combustor for a gas turbine is provided, the combustor including a reverse flow type combustion chamber defined by an inner cylindrical wall and an outer wall concentric with the inner wall and connected at one end by an annular dome. The outer wall has three successive sections with the first section being cylindrical and of a predetermined diameter, the second outer wall section being of frusto-conical shape, and the third wall section being of cylindrical shape but of reduced diameter compared to the first section. Injectors are provided in the angl...
1. A combustor in a gas turbine engine of the type including a reverse flow annular combustor, the combustor having an inner cylindrical wall, an outer wall concentric with the inner wall about a combustor axis, and an annular dome connecting the inner wall and outer wall, the outer wall having a first cylindrical wall portion adjacent the dome and having a predetermined diameter, a second outer wall portion adjacent the first wall portion and remote from the dome, the second wall portion terminating in a third wall portion of cylindrical shape and of re...