IPC분류정보
| 국가/구분 |
United States(US) Patent
등록
|
| 국제특허분류(IPC7판) |
|
| 출원번호 |
US-0398557
(1999-09-17)
|
|
발명자
/ 주소 |
- Dodds, Willard J.
- Heberling, Paul V.
- Taylor, Jack R.
- Halila, Ely E.
|
| 출원인 / 주소 |
|
| 대리인 / 주소 |
Hess, Andrew C.Andes, William Scott
|
| 인용정보 |
피인용 횟수 :
22 인용 특허 :
8 |
초록
▼
A combustor for a gas turbine engine having a longitudinal axis therethrough, including an outer liner having a forward end and an aft end, an inner liner having a forward end and an aft end, a first dome formed upstream of the outer liner forward end so as to define a first combustion zone radially
A combustor for a gas turbine engine having a longitudinal axis therethrough, including an outer liner having a forward end and an aft end, an inner liner having a forward end and an aft end, a first dome formed upstream of the outer liner forward end so as to define a first combustion zone radially oriented to the longitudinal axis, and a dome plate having an outer portion connected to an upstream end of the first dome and an inner portion connected to the inner liner forward end, wherein a second combustion zone is defined by the dome plate, the outer liner, and the inner liner substantially perpendicular to the first combustion zone.
대표청구항
▼
A combustor for a gas turbine engine having a longitudinal axis therethrough, including an outer liner having a forward end and an aft end, an inner liner having a forward end and an aft end, a first dome formed upstream of the outer liner forward end so as to define a first combustion zone radially
A combustor for a gas turbine engine having a longitudinal axis therethrough, including an outer liner having a forward end and an aft end, an inner liner having a forward end and an aft end, a first dome formed upstream of the outer liner forward end so as to define a first combustion zone radially oriented to the longitudinal axis, and a dome plate having an outer portion connected to an upstream end of the first dome and an inner portion connected to the inner liner forward end, wherein a second combustion zone is defined by the dome plate, the outer liner, and the inner liner substantially perpendicular to the first combustion zone. S-5452574, 19950900, Cowell et al., 060/723; US-5511375, 19960400, Joshi et al., 060/737; US-5660045, 19970800, Ito et al., 060/737; US-5685157, 19971100, Pandalia et al., 060/725; US-5899074, 19990500, Komatsu et al., 060/737; US-5901555, 19990500, Mandai et al., 060/747; US-6026645, 20000200, Stokes et al., 060/737; US-6038861, 20000300, Amos et al., 060/737; US-6047551, 20000400, Ishiguro et al., 060/740; US-6070411, 20000600, Iwai et al., 060/737; US-6082111, 20000700, Stokes, 060/737; US-6109038, 20000800, Sharifi et al.; US-6122916, 20000900, Amos et al., 060/747
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