Patent · US Active

Rotor blade tip planform

US7513750B2 · kind B2 · utility

18Cited by
9References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 8, 2006
Grant dateApr 7, 2009
Priority date
Expiry dateApr 10, 2027

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/463
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A main rotor blade incorporating a rotor blade tip region having a tip chord and a tip taper such that the ratio of the main rotor blade chord to the tip chord is approximately 0.30. The tip taper ratio preferably providing an approximately 28% area of reduction in said outer 10% of said blade span. The tip region preferably further including a hover optimized high lift airfoil and a tip sweep that reaches a constant value of approximately 30 degrees along the quarter chord line.

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