Turbine engine and component parts to be used in it

A turbine engine that includes an engine housing comprising a pressurized fluid supply chamber, a cooperating surface, a nozzle feed channel, and a cavity flow channel that both extend between a pressurized fluid supply chamber and a cooperating surface. The turbine engine further comprises a turbin...

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Main Authors TRALEWSKI ADAM, RZESZUTEK LESZEK MAREK, KACZMAREK GRZEGORZ MACIEJ, OLCZAK DARIUSZ, BULSIEWICZ TOMASZ JAN, STANCZYK MACIEJ
Format Patent
LanguageChinese
English
Published 23.10.2018
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Summary:A turbine engine that includes an engine housing comprising a pressurized fluid supply chamber, a cooperating surface, a nozzle feed channel, and a cavity flow channel that both extend between a pressurized fluid supply chamber and a cooperating surface. The turbine engine further comprises a turbine nozzle assembly including a cooperating band. The cooperating band includes an inlet connection influid connection with the nozzle feed channel. There is an interface between the cooperating band and the first part of the interacting surface, and there is a niche of the band between the cooperating band and the second part of the cooperating surface. The cavity flow channel connects the compressed fluid supply chamber in fluid communication with the wristband recess. 种涡轮发动机,其包括发动机壳体,该发动机壳体包括流体供应增压室、配合表面以及均在流体供应增压室与配合表面之间延伸的喷嘴供应通道和腔体流动通道。涡轮发动机还包括涡轮喷嘴组件,该涡轮喷嘴组件包括配合带。配合带包括与喷嘴供应通道流动连通的进气口。在配合带和配合表面的第部分之间限定了界面,并且在配合带和配合表面的第二部分之间限定了带腔体。腔体流动通道将流体供应增压室与带腔体流动连通地联接。
Bibliography:Application Number: CN201810304772