发明名称 Tip Turbine Engine Composite Tailcone
摘要 A non-metallic tailcone ( 202 ) in a tip turbine engine includes a tapered wall structure disposed ( 208 ) about a central axis. The non-metallic tailcone is fastened to a structural frame ( 44 ) in the aft portion of the tip turbine engine. The tip turbine engine produces a first temperature gas stream from a first output source and a second temperature gas stream from a second output source. The second temperature gas stream is a lower temperature than the first temperature gas stream. The second temperature gas stream is discharged at an inner diameter of the tip turbine engine over an outer surface of the tailcone. Discharging the cooler second temperature gas stream at the inner diameter allows a non-metallic to be used to form the tailcone.
申请公布号 US2008092514(A1) 申请公布日期 2008.04.24
申请号 US20040720463 申请日期 2004.12.01
申请人 SUCIU GABRIEL L;NORRIS JAMES W;MERRY BRIAN 发明人 SUCIU GABRIEL L.;NORRIS JAMES W.;MERRY BRIAN
分类号 F02K1/04 主分类号 F02K1/04
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