公开(公告)号：WO2007120185A2

公开(公告)日：2007-10-25

申请号：PCT/US2006/041108

申请日：2006-10-20

Applicant: ROLLS-ROYCE CANADA, LTD. ,  SCARINCI, Thomas

Inventor： SCARINCI, Thomas

IPC: F02C7/26

CPC classification number: F02C7/26 ,  F02C7/222 ,  F05D2240/127 ,  F23D2207/00 ,  F23R3/14 ,  F23R3/286

Abstract: A combustion chamber device having a field static pressure gradient adapted to expel a flame kernel or hot spot from a fuel-air mixing duct. The swirling flow passing through an annular mixing duct is turned from a radial direction to an axial direction before entering the combustion chamber. An ignition source located within the fuel-air mixing duct can then be used to start the combustion process in the gas turbine.

Abstract translation: 具有适于从燃料 - 空气混合管道排出火焰核或热点的场静压力梯度的燃烧室装置。 通过环形混合管道的旋流在进入燃烧室之前从径向转向轴向。 然后可以使用位于燃料 - 空气混合管道内的点燃源来启动燃气轮机中的燃烧过程。

公开(公告)号：WO2007033306A2

公开(公告)日：2007-03-22

申请号：PCT/US2006/035785

申请日：2006-09-13

Applicant: ROLLS-ROYCE CORPORATION, LTD. ,  SCARINCI, Thomas ,  MORAN, Anthony, John ,  STEWARD, Lynn, Ivor, Thomas ,  JONES, Bryn

Inventor： SCARINCI, Thomas ,  MORAN, Anthony, John ,  STEWARD, Lynn, Ivor, Thomas ,  JONES, Bryn

IPC: F02C1/00

CPC classification number: F02C3/14 ,  F23R3/14 ,  F23R3/286 ,  F23R3/346 ,  F23R3/44 ,  F23R3/50

Abstract: One embodiment is a unique gas turbine engine combustion chamber including primary and secondary burning zones. Other embodiments include unique gas turbine engine apparatuses, systems, methods, and combinations.

Abstract translation: 一个实施例是独特的燃气涡轮发动机燃烧室，其包括主燃烧区和次燃烧区。 其他实施例包括独特的燃气涡轮发动机装置，系统，方法和组合。