发明名称 DUCTED COWL SUPPORT FOR GAS TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To provide a ducted cowl support which provides structural support and a fluid bypass flowpath.SOLUTION: A ducted cowl support (54) comprises an annular structure configured to be mounted on an annular turbine engine frame (46) and including one or more bypass ducts (62) integrally formed in the annular structure. The bypass ducts (62) may comprise projecting bulges that can mate with openings (47) formed in a turbine engine frame (46) to cooperatively define flow passages.SELECTED DRAWING: Figure 1
申请公布号 JP2016125495(A) 申请公布日期 2016.07.11
申请号 JP20150250814 申请日期 2015.12.24
申请人 GENERAL ELECTRIC CO <GE> 发明人 HASTING WILLIAM HOWARD;JARED MATTHEW WOLFE;DAVID EDWARD DALE
分类号 F02C7/20;F02C7/00;F02C7/18 主分类号 F02C7/20
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