Patent · US Active

Rotary wing aircraft with a shrouded tail propeller

US12037110B2 · kind B2 · utility

1Cited by
9References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 29, 2021
Grant dateJul 16, 2024
Priority date
Expiry dateMar 23, 2042

Classification

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

Abstract

The present disclosure relates to a rotary wing aircraft that extends along an associated roll axis between a nose region and an aft region. The rotary wing aircraft comprises a main rotor; a shrouded duct that is arranged in the aft region and that forms an inner air duct, wherein the shrouded duct is formed to generate sideward thrust for main rotor anti-torque in forward flight condition of the rotary wing aircraft; and a propeller that is at least configured to propel the rotary wing aircraft in the forward flight condition; wherein the propeller forms a circular propeller disc in rotation around an associated rotation axis; and wherein the propeller is rotatably mounted to the shrouded duct such that the circular propeller disc is at least essentially arranged inside of the inner air duct.

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