发明名称 MODULAR CHEVRON EXHAUST NOZZLE
摘要 An exhaust nozzle for a gas turbine engine includes a modular chevron. The chevron includes dual skins fixedly joined together at a base flange, and at a rim extending along the trailing edge of the chevron between the base and apex thereof.
申请公布号 US2009019857(A1) 申请公布日期 2009.01.22
申请号 US20070779518 申请日期 2007.07.18
申请人 TISDALE RUDOLPH MORRIS;UHLER GREGORY ALLEN;JOHNSON MICHAEL ROBERT;NYE CHRISTOPHER JOSEPH 发明人 TISDALE RUDOLPH MORRIS;UHLER GREGORY ALLEN;JOHNSON MICHAEL ROBERT;NYE CHRISTOPHER JOSEPH
分类号 F02K1/00 主分类号 F02K1/00
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