Patent · US Active

Rotary wing aircraft with a tail shroud

US9475578B2 · kind B2 · utility

0Cited by
7References
9Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 8, 2014
Grant dateOct 25, 2016
Priority date
Expiry dateApr 18, 2036

Classification

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

Abstract

A rotary wing aircraft with a tail rotor in a rotor duct of a shroud. A bumper projects from a lower transition region of said shroud, said lower transition region having a left hand and a right hand lower transition edge between respectively the left hand and the right hand annular surface around the rotor duct and the bumper. Upper leading edges of a vertical fin and of said shroud are provided with left hand and right hand trailing edges. A projection of the upper transition edge to an upright longitudinal plane is defined by a spline curve through points Pi (i=1 . . . 5) and a projection of the lower transition edge to the plane is defined by a spline curve through points Pi (i=6 . . . 10) defined by their respective coordinates (xi, zi) relative to a centre of the shrouded tail rotor.

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