首页> 外国专利> APPARATUS AND METHODS FOR RELIEVING THERMALLY INDUCED STRESSES IN INNER AND OUTER BANDS OF THERMALLY COOLED TURBINE NOZZLE STAGES

APPARATUS AND METHODS FOR RELIEVING THERMALLY INDUCED STRESSES IN INNER AND OUTER BANDS OF THERMALLY COOLED TURBINE NOZZLE STAGES

机译:缓解热固式涡轮喷嘴阶段内外带热致应力的装置和方法

摘要

To control the temperature mismatch between the inner and outer bands (16, 18) and covers (28, 30) forming plenums (P) with the inner and outer bands on sides thereof remote from the hot gas path (20), passages (42) extend from the leading edge (44) of the covers in communication with the hot gases of combustion to the trailing edge of the covers in communication with the hot gas flowpath. A mixing chamber (48) is provided in each passage in communication with compressor discharge air for mixing the hot gases of combustion and compressor discharge air for flow through the passage, thereby heating the cover and minimizing the temperature differential between the inner and outer bands and their respective covers. The passages are particularly useful adjacent the welded or brazed joints between the covers and inner band portions. IMAGE
机译:为了控制内带和外带(16、18)与形成充气室(P)的盖(28、30)之间的温度失配,使内带和外带的侧面远离热气路径(20),设有通道(42) )从与燃烧热气体连通的盖的前缘(44)延伸到与热气体流路连通的盖的后缘。在每个通道中设置有混合室(48),其与压缩机排出空气连通以使燃烧的热气体与压缩机排出空气通过通道流动,从而加热盖并最小化内带和外带之间的温差。他们各自的封面。这些通道在盖和内带部分之间的焊接或铜焊接头附近特别有用。 <图像>

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