Rutschfahrwerk für ein Drehflügelflugzeug

Details

Veröffentlichungs-Nr.

EP4711270

Anmeldetag

11. September 2024

Veröffentlichung

18. März 2026

Rechtsraum

EP

IPC

B64C25/52, B64C25/32(MA YONGZHENG et al.)(COLLINS BOBBY A et al.)

Abstract

The invention relates to a skid-type landing gear (10) for a rotorcraft (1), which comprises at least two skids (11) which are connected to each other via at least two cross tubes (13). Each cross tube (14) is connected to the skids (12) via connecting components (17), each comprising a pressure plate (17b). The pressure plates (17b) are respectively attached to the skids (12) by means of vertical attachments (29) via a predetermined number of fasteners (22). The vertical attachments (29) are configured to enable load transfer from the cross tubes (14) to the skids (12) by tension in the predetermined number of fasteners (22) and by pressure between the pressure plates (17b) and skids (11).

Anmelder

Firma

AIRBUS HELICOPTERS DEUTSCHLAND GmbH

Land

🇩🇪 Deutschland