发明名称 Wide chord fan blade
摘要 <p>A laminated airfoil (10) for use in a high bypass engine. The airfoil (10) preferably has a large tip chord and is comprised of alternating layers of thin metallic foil (28) and elastomeric layers (30). The exterior surfaces of the airfoil (10) are comprised of a thin, metallic foil. The airfoil also has a metal sheath (20) secured to the leading edge (16). High strength metal members (26) extend through the dovetail root sections (14). <IMAGE></p>
申请公布号 EP0496550(B1) 申请公布日期 1997.09.17
申请号 EP19920300454 申请日期 1992.01.20
申请人 GENERAL ELECTRIC COMPANY 发明人 MURPHY, GUY CLIFF;DUHRMANN, BARRETT JOSEPH
分类号 F01D5/14;B29C43/18;B32B15/06;F01D5/28;F02K3/04;(IPC1-7):F01D5/28 主分类号 F01D5/14
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