公开(公告)号：US20140157783A1

公开(公告)日：2014-06-12

申请号：US13710395

申请日：2012-12-10

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Kyle Lee Kidder ,  Jerome D. Brown

IPC: F23R3/00

CPC classification number: F23R3/002 ,  F23R3/005 ,  F23R3/007 ,  F23R3/06 ,  F23R2900/00019 ,  F23R2900/03041 ,  F23R2900/03042 ,  Y02T50/675 ,  Y02T50/6765

Abstract: In a first embodiment a system, including a gas turbine combustor, including an inner wall disposed about a combustion chamber, and an outer wall disposed about the inner wall, wherein a coolant flow path extends between the inner and outer walls, wherein the inner wall comprises a material blocking a plurality of openings, and the plurality of openings are configured to open after the material is consumed or depleted to define a plurality of coolant passages through the inner wall.

Abstract translation: 在第一实施例中，包括燃气轮机燃烧器的系统，包括围绕燃烧室设置的内壁，以及围绕内壁设置的外壁，其中冷却剂流动路径在内壁和外壁之间延伸，其中内壁 包括阻挡多个开口的材料，并且多个开口构造成在材料消耗或耗尽之后打开以限定穿过内壁的多个冷却剂通道。