Patent · US Active

Nose landing gear arrangements and methods for making the same

US9290263B2 · kind B2 · utility

4Cited by
8References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 7, 2014
Grant dateMar 22, 2016
Priority date
Expiry dateJul 18, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/4984
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Nose landing gear arrangements including a folding follow-up door for reducing airflow noise for aircrafts, aircrafts including such nose landing gear arrangements, and methods for making such nose landing gear arrangements are provided herein. In one example, a nose landing gear arrangement includes a wheel assembly and a main strut. The main strut is operatively coupled to the wheel assembly and is configured to extend outside of the fuselage substantially along a generally vertical plane. A folding follow-up door is pivotally coupled to the main strut and extends to the fuselage. The folding follow-up door includes a first door section and a second door section that extend outwardly in directions away from each other to define an unfolded position. The folding follow-up door is foldable to move the first and second door sections towards each other about the generally vertical plane to define a folded position.

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