发明名称 Detuned vane airfoil assembly
摘要 A vane assembly comprises circumferentially adjacent airfoils formed of composite materials. The airfoils have matching exterior geometries defined by pressure and suction surfaces extending axially from a leading edge to a trailing edge and radially from a root section to a tip section. An inner platform is attached to each of the circumferentially adjacent airfoils at the root section, and an outer platform is attached at the tip section. The composite materials are selected to define a vibration mode with different vibration frequencies in the circumferentially adjacent airfoils, where the different vibration frequencies are separated by more than a full width of the vibration mode at half maximum.
申请公布号 US8834098(B2) 申请公布日期 2014.09.16
申请号 US201113310228 申请日期 2011.12.02
申请人 United Technologies Corporation 发明人 Glaspey James
分类号 F01D5/14;F01D5/16 主分类号 F01D5/14
代理机构 Kinney & Lange, P.A. 代理人 Kinney & Lange, P.A.
主权项 1. A vane assembly comprising: circumferentially adjacent airfoils formed of composite materials, the circumferentially adjacent airfoils having matching exterior geometries defined by pressure and suction surfaces extending axially from a leading edge to a trailing edge and radially from a root section to a tip section; an inner platform attached to each of the circumferentially adjacent airfoils at the root section; and an outer platform attached to each of circumferentially adjacent airfoils at the tip section; wherein the composite materials are selected to define a vibration mode with different vibration frequencies in the circumferentially adjacent airfoils, the different vibration frequencies separated by more than a full width of the vibration mode at half maximum.
地址 Hartford CT US