发明授权
US5118257A Boot attachment for composite turbine blade, turbine blade and method of making turbine blade 失效
复合涡轮叶片,涡轮叶片和制造涡轮叶片的引导附件

Boot attachment for composite turbine blade, turbine blade and method of
making turbine blade
摘要:
A root attachment for a turbine blade is integrally molded with a composite turbine blade for a ram air turbine. The root attachment includes an insert at the one end of the root attachment for integrally molding within the blade and a hub connector at an opposite end for connecting the blade to a rotor hub. The insert has a geometry and surface area 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 which resists failure in bearing. Each of the adhesive bond and the mechanical locking is designed to fail above an ultimate design load.
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