发明授权
US09169009B1 Hub-mounted auxilliary systems for tipjets in a reaction drive rotor system 有权
枢轴安装的辅助系统用于反应驱动转子系统中的尖端

Hub-mounted auxilliary systems for tipjets in a reaction drive rotor system
摘要:
A rotor system is disclosed for a reactive drive rotary wing aircraft. Apparatus and methods are disclosed for mounting to the rotor hub certain controls, both electrical and mechanical, as well as fuel delivery for tipjets mounted to rotor blades. Air passively or actively drawn through rotor may feed the tipjets directly through the blades, while fuel and control is delivered along the blade to the tip thereof.
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