发明名称 Augmentor liner construction
摘要 The cooling air for the nozzle of an augmentor of a gas turbine engine is maintained uniformly around the circumference to assure the prevention of hot streaks that would be occasioned by the liner "sagging". A separate end piece having judiciously located gaps for directing air over the nozzles, flaps and seals attached to the end of the augmentor duct maintains concentricity during augmentor operation, and affords support to the liner of the duct.
申请公布号 US4718230(A) 申请公布日期 1988.01.12
申请号 US19860929542 申请日期 1986.11.10
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HONEYCUTT, JR., FRED L.;MCLEAN, HOWARD J.
分类号 F02K1/82;(IPC1-7):F02K3/10 主分类号 F02K1/82
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