公开(公告)号：WO2008108813A2

公开(公告)日：2008-09-12

申请号：PCT/US2007/020470

申请日：2007-09-21

Applicant: SOLAR TURBINES INCORPORATED ,  LOCKYER, John, F. ,  GREENWOOD, Stuart, A. ,  DUTTA, Partha, X. ,  GROOCOCK, Ted, E. ,  FOX, Michael, D.

Inventor： LOCKYER, John, F. ,  GREENWOOD, Stuart, A. ,  DUTTA, Partha, X. ,  GROOCOCK, Ted, E. ,  FOX, Michael, D.

CPC classification number: F23R3/04 ,  F23R3/002 ,  F23R2900/03044 ,  Y02T50/675

Abstract: A combustor liner assembly (46) includes a liner assembly (56), including a hot dome (82), a hot wall (78, 80), and an impingement shield (76, 96). The liner assembly further includes a convector assembly (58). The combustor liner assembly further includes an impingement dome assembly (60), including a ring-shaped portion (104) defining a plurality of apertures (106) configured to receive a plurality of fuel injectors, and a face (126). The ring- shaped portion and the face define an annular passage (128), and the face defines a plurality of apertures and a plurality of orifices (130). The convector assembly and the impingement dome assembly are operably coupled to one another, and the plurality of orifices of the face are configured such that the hot dome is exposed to air flowing in the annular passage of the impingement dome assembly. The combustor liner assembly is configured to provide flow communication between the annular passage of the impingement dome assembly and the plurality of fuel injectors.

Abstract translation: 燃烧器衬套组件（46）包括衬套组件（56），其包括热穹顶（82），热壁（78,80）和冲击屏蔽件（76,96）。 衬套组件还包括对流式组件（58）。 燃烧器衬套组件还包括冲击圆顶组件（60），其包括限定被配置为容纳多个燃料喷射器的多个孔（106）的环形部分（104）和面部（126）。 所述环形部分和所述面限定环形通道（128），并且所述面限定多个孔和多个孔（130）。 对流器组件和冲击圆顶组件可操作地彼此联接，并且面的多个孔被构造成使得热的圆顶暴露于在冲击圆顶组件的环形通道中流动的空气。 燃烧器衬套组件构造成提供冲击圆顶组件的环形通道与多个燃料喷射器之间的流动连通。

公开(公告)号：WO2008108813A3

公开(公告)日：2008-11-06

申请号：PCT/US2007020470

申请日：2007-09-21

Applicant: SOLAR TURBINES INC ,  LOCKYER JOHN F ,  GREENWOOD STUART A ,  DUTTA PARTHA X ,  GROOCOCK TED E ,  FOX MICHAEL D

Inventor： LOCKYER JOHN F ,  GREENWOOD STUART A ,  DUTTA PARTHA X ,  GROOCOCK TED E ,  FOX MICHAEL D

IPC: F23R3/00

CPC classification number: F23R3/04 ,  F23R3/002 ,  F23R2900/03044 ,  Y02T50/675

Abstract: A combustor liner assembly (46) includes a liner assembly (56), including a hot dome (82), a hot wall (78, 80), and an impingement shield (76, 96). The liner assembly further includes a convector assembly (58). The combustor liner assembly further includes an impingement dome assembly (60), including a ring-shaped portion (104) defining a plurality of apertures (106) configured to receive a plurality of fuel injectors, and a face (126). The ring- shaped portion and the face define an annular passage (128), and the face defines a plurality of apertures and a plurality of orifices (130). The convector assembly and the impingement dome assembly are operably coupled to one another, and the plurality of orifices of the face are configured such that the hot dome is exposed to air flowing in the annular passage of the impingement dome assembly. The combustor liner assembly is configured to provide flow communication between the annular passage of the impingement dome assembly and the plurality of fuel injectors.

Abstract translation: 燃烧器衬里组件（46）包括衬里组件（56），衬里组件包括热圆顶（82），热壁（78,80）和冲击护罩（76,96）。 衬套组件还包括对流器组件（58）。 燃烧器衬里组件进一步包括冲击圆顶组件（60），该冲击圆顶组件包括限定被构造成接收多个燃料喷射器的多个孔（106）的环形部分（104）和面（126）。 环形部分和面限定环形通道（128），并且该面限定多个孔和多个孔（130）。 对流器组件和冲击圆顶组件可操作地彼此联接，并且面的多个孔构造成使得热圆顶暴露于在冲击圆顶组件的环形通道中流动的空气。 燃烧器衬里组件构造成提供冲击圆顶组件的环形通道与多个燃料喷射器之间的流动连通。