发明名称 |
Root attachment for composite turbine blade |
摘要 |
A root attachment 2 (which may be of titanium or stainless steel) includes an insert 3 at one end thereof for integrally molding within a ram air turbine blade and has a hub connector 7 for connecting the blade to a rotor hub. The insert geometry (tapering width and flaring thickness) and surface area are such that a dual load carrying capability is achieved during molding by the formation of an adhesive bond between the material of the blade and the insert and also a mechanical locking. Both the adhesive bond and the mechanical locking are designed to fail above a predetermined load. The blade may be made from preformed sheets and molded in a compression mold. Details of materials used are disclosed. <IMAGE> |
申请公布号 |
GB2247285(A) |
申请公布日期 |
1992.02.26 |
申请号 |
GB19910011185 |
申请日期 |
1991.05.23 |
申请人 |
* SUNDSTRAND CORPORATION |
发明人 |
ANTHONY * BLAKELEY;GREGORY E * HORIHAN;TIMOTHY S * KONICEK;PATRICK J * O'CALLAGHAN;MARTIN W * CARRINGTON;JEFFREY A * BROWN |
分类号 |
B64C11/04;F01D5/30 |
主分类号 |
B64C11/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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