公开(公告)号：US20080087019A1

公开(公告)日：2008-04-17

申请号：US11806366

申请日：2007-05-31

申请人： Michael Macquisten ,  Anthony Moran ,  Michael Whiteman ,  Jonathan Carrotte ,  Ashley Barker

发明人： Michael Macquisten ,  Anthony Moran ,  Michael Whiteman ,  Jonathan Carrotte ,  Ashley Barker

IPC分类号： F02C7/24

CPC分类号： F23R3/002 ,  F23M20/005 ,  F23R2900/00014

摘要： A combustion chamber for a gas turbine engine comprising at least one Helmholtz resonator having a resonator cavity and a resonator neck in flow communication with the interior of the combustion chamber. The cavity extends around at least part of the neck and is spaced apart therefrom to define a cooling chamber therebetween. The cooling chamber allows the neck and the cavity to be cooled with a flow of cooling air. The sunken neck allows the resonator to be located within enclosures with minimal volume without compromising on the damping properties afforded.

摘要翻译： 一种用于燃气涡轮发动机的燃烧室，包括至少一个具有谐振腔的亥姆霍兹共振器和与燃烧室内部流动连通的谐振器颈部。 空腔围绕颈部的至少一部分延伸并且与其间隔开以在其间限定冷却室。 冷却室允许颈部和空腔以冷却空气流冷却。 凹陷的颈部允许谐振器以最小的体积位于外壳内，而不会影响所提供的阻尼性能。

公开(公告)号：US20060123791A1

公开(公告)日：2006-06-15

申请号：US11280429

申请日：2005-11-17

申请人： Michael Macquisten ,  Anthony Moran ,  Michael Whiteman ,  Jonathon Carrotte ,  Ashley Barker ,  Martin Goodwin

发明人： Michael Macquisten ,  Anthony Moran ,  Michael Whiteman ,  Jonathon Carrotte ,  Ashley Barker ,  Martin Goodwin

IPC分类号： F02C7/24

CPC分类号： F23M20/005 ,  F23R3/50 ,  F23R2900/00014

摘要： A combustion chamber suitable for a gas turbine engine is provided with at least one Helmholtz resonator having a resonator cavity and a resonator neck in flow communication with the chamber interior. The resonator neck is provided with at least cooling holes extending through its wall for improved damping and cooling, at least one of the holes is directed towards the resonator cavity.

摘要翻译： 适合于燃气涡轮发动机的燃烧室设置有至少一个具有谐振腔和与室内流体连通的谐振器颈部的亥姆霍兹共振器。 谐振器颈部设置有至少冷却孔，其延伸穿过其壁以改善阻尼和冷却，至少一个孔指向谐振器腔。