发明名称 AIRFOIL COMPONENT WEAR INDICATOR
摘要 An example airfoil assembly includes an airfoil body extending between a leading edge, a trailing edge, a suction side, and a pressure side. The assembly further includes a first protective sheath, an indicator sheath, and a second protective sheath. The first protective sheath has an outer side and an inner side that forms a cavity for receiving at least a portion of the airfoil body. The inner side being bonded to the leading edge of the airfoil body. A portion of the indicator sheath is positioned forward the first sheath relative to the leading edge of the airfoil. A portion of the second protective sheath is positioned forward the indicator sheath relative to the leading edge of the airfoil.
申请公布号 US2011116906(A1) 申请公布日期 2011.05.19
申请号 US20090620537 申请日期 2009.11.17
申请人 SMITH BLAIR A;HUTH BRIAN P;CARVALHO PAUL A 发明人 SMITH BLAIR A.;HUTH BRIAN P.;CARVALHO PAUL A.
分类号 F01D9/02;F01D5/14 主分类号 F01D9/02
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