Patent · US Active

Front electric rotor helicopter

US8596569B2 · kind B2 · utility

2Cited by
3References
1Claims
0Family size

Inventor

Key dates

Filing dateSep 26, 2011
Grant dateDec 3, 2013
Priority date
Expiry dateJun 1, 2032

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2027/8254
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

My invention is a helicopter having a front electric anti-torque rotor for the purpose of having a mechanically driven pusher propeller at the rear for increasing forward speed. Speed has been a limiting factor in vertical flight. Various designs have been conceived by people around the world to make helicopters go faster. My design is a high speed single rotor helicopter design that uses a gas-electric hybrid front electric anti-torque rotor system to allow for a mechanically driven pusher propeller at the rear. As the helicopter goes forward, the front electric anti-torque gives control and the mechanically driven pusher propeller at the rear gives increased forward speed. The intent of the design is to make a high speed single rotor helicopter design.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.