发明名称 GAS TURBINE ENGINE EXHAUST COMPONENT AND MANUFACTURING METHOD OF SAME
摘要 A gas turbine exhaust component, such as an exhaust nozzle, is provided that includes circumferential ribs arranged along a longitudinal axis. Longitudinal strakes are supported by the circumferential ribs and arranged about the longitudinal axis. Fastening elements are used to secure the longitudinal strakes to one another to provide a desired exhaust component contour. In one example, fastening elements are used to secure the longitudinal strakes to the circumferential ribs using a bracket. The longitudinal strakes are preformed into the desired exhaust component contour, using low cost forming methods. The longitudinal strakes are formed to fit the circumferential ribs and provide the desired exhaust component contour. The longitudinal strakes are secured to one another to maintain the desired exhaust component contour. The longitudinal strakes may be provided by a low cost steel, in one example.
申请公布号 US2009313825(A1) 申请公布日期 2009.12.24
申请号 US20080132157 申请日期 2008.06.03
申请人 HARRIS ANDREW H;KONIKOWSKI RAYMOND E 发明人 HARRIS ANDREW H.;KONIKOWSKI RAYMOND E.
分类号 B21D53/00 主分类号 B21D53/00
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