发明名称 Quad Rotor Aircraft With Fixed Wing And Variable Tail Surfaces
摘要 An aircraft with four rotors, a fixed wing, and an adjustable v-tail to allow for both vertical take-off and landing and the capability to fly in straight and level flight. The angle of each rotor and engine, with respect to the airfoil surfaces to which they are attached, is adjustable, allowing for thrust to be directed either downwards, allowing the craft to hover, or backwards, allowing the aircraft to travel horizontally while lift is provided and controlled by the wing and v-tail.
申请公布号 US2017113795(A1) 申请公布日期 2017.04.27
申请号 US201615210664 申请日期 2016.07.14
申请人 Duque Jeremy 发明人 Duque Jeremy
分类号 B64C29/00;B64C27/08;B64C39/02;B64C27/52 主分类号 B64C29/00
代理机构 代理人
主权项 1. An aircraft comprising: a wing attached to a fuselage; an empennage having two tail surfaces; a forward source of thrust mounted to the wing; and a rear source of thrust mounted to at least one of the two tail surfaces.
地址 Boise ID US