发明名称 TURBINE ENGINE EXHAUST NOZZLE FLAP
摘要 An exhaust nozzle flap for a turbine engine may include an exhaust nozzle flap linkage, an exhaust nozzle flap panel and a mounting pin. The linkage may include a first linkage segment that extends longitudinally from a linkage end to a second linkage segment, and a mounting aperture that extends transversely through the second linkage segment. The panel may include a first panel segment that extends longitudinally from a panel end to a second panel segment. The first panel segment may be pivotally engaged with the first linkage segment. The mounting pin may extend through and move transversely within the mounting aperture, and may be connected to the second panel segment.
申请公布号 WO2014011279(A3) 申请公布日期 2014.03.06
申请号 WO2013US36194 申请日期 2013.04.11
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MOON, FRANCIS R.;BARNETT, JR., CLAUDE;JACQUES, JEFFREY M.
分类号 F02K1/06;F02C7/00;F02K9/86 主分类号 F02K1/06
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