发明名称 Gas turbine impingement cooling structure and method of impingement cooling
摘要 An extended impingement cooling structure to cool outside an air supply plenum comprises an inner wall (102); an impingement sheet (104); a series of supports (106,106a) to maintain the inner wall (102) in spaced relation to the impingement sheet (104), and a baffle (112) supported between the inner wall (102) and the impingement sheet (104). The baffle (112) has a collector plenum area (150) that receives impingement cooling air from the air supply plenum (108) and a channel (154) in fluid communication with the collector plenum (150) and extending outside the air supply plenum with openings (156) to allow impingement cooling air to pass therethrough and having a series of lands (152) extending into the channel (154) wherein the lands (152) are located in proximity to impingement cooling air outlets (130) in the inner wall (102).
申请公布号 EP1600608(A2) 申请公布日期 2005.11.30
申请号 EP20050250046 申请日期 2005.01.07
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MAYER, ROBERT F.;STONER, CHARLES D.
分类号 F01D25/12;F02C7/18;F01D25/08;F23R3/06;(IPC1-7):F01D25/08 主分类号 F01D25/12
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