Patent · US Active

Skid-type landing gear for a helicopter

US8561945B2 · kind B2 · utility

4Cited by
7References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 24, 2011
Grant dateOct 22, 2013
Priority date
Expiry dateMay 9, 2032

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2025/325
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

The invention relates to a skid-type landing gear (1) for a helicopter (2) comprising bow shaped crosstubes (10-13) directed symmetrically towards a left- and a right-hand side of a longitudinal mid axis (9) of the helicopter (2) with respective skids (14, 15) at outboard ends thereof and main beams (5-8) in a fuselage (4), the crosstubes (10-13) being connected to the main beams (5-8) via supports (16-23) fixed to the main beams (5-8). The skid-type landing gear (1) is retractable. A method for operating such a skid-type landing gear (1) for a helicopter (2) is provided.

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