Fixation d'un train d'atterrissage d'un hélicoptère

Befestigung eines Hubschrauberfahrwerks

Attachment of a helicopter landing gear

Abstract

The invention is related to a bracket (24) for connecting a traverse (20) of a landing gear to a cabin of a helicopter. A landing gear retainer (5) is fixed around the traverse (20) coaxially to the longitudinal direction of the traverse (20) and at least one cabin clamp mount (7) is fixed to the cabin. The landing gear retainer (5) is in between the cabin and upper and lower pendulum bolts (12, 13) and upper and lower pendulum bearings (18, 19). A pendulum (9) is in longitudinal direction of the traverse (20) hinged to the landing gear retainer (5). The invention is further related to an application of such brackets (24).

Claims

Description

Topics

Download Full PDF Version (Non-Commercial Use)

Patent Citations (3)

    Publication numberPublication dateAssigneeTitle
    US-4270711-AJune 02, 1981Textron, Inc.Helicopter landing gear with crosstube pivot
    US-6244538-B1June 12, 2001Bell Helicopter Textron Inc.Stiffness de-coupled skid landing gear
    WO-2009097192-A2August 06, 2009Bell Helicopter Textron Inc.Split pivot fitting for helicopter landing gear

NO-Patent Citations (0)

    Title

Cited By (0)

    Publication numberPublication dateAssigneeTitle