Patent · US Active

Dual rotor, rotary wing aircraft

US10822076B2 · kind B2 · utility

6Cited by
161References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 30, 2015
Grant dateNov 3, 2020
Priority date
Expiry dateSep 19, 2036

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2027/8281
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A main rotor blade assembly for a rotary wing aircraft is provided including a main rotor blade root region, a main rotor blade inboard region arranged outboard of said main rotor blade root region, a main rotor blade main region arranged outboard of said main rotor blade inboard region, and a main rotor blade tip region arranged outboard of said main rotor blade main region. At least one of chord, twist, sweep, airfoil shape, and thickness/chord of the main rotor blade assembly has been optimized to achieve balanced high speed forward flight and hover relative to both efficiency and high thrust capability.

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