Patent · US Active

Helicopter skid landing gear

US10858091B2 · kind B2 · utility

0Cited by
20References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 27, 2018
Grant dateDec 8, 2020
Priority date
Expiry dateMay 16, 2039

Classification

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

Abstract

In a first aspect, there is a helicopter skid landing gear assembly including a front cross tube configured to interconnect two skid tubes; and a rear cross tube configured to interconnect two skid tubes; wherein at least one of the cross tubes comprises a monolithic metallic tube having a cross-section with a round exterior shape and an elliptical hollow portion therein. In a second aspect, there is a method for retrofitting a helicopter with a landing gear assembly; the method including providing a front cross tube and a rear cross tube, at least one of the front cross tube and the rear cross tube comprises a monolithic metallic tube having a cross-section with a substantially round exterior shape and an elliptical hollow portion therein; and connecting the front cross tube and rear cross tube to a fuselage.

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