Befestigung zur Befestigung eines Flugzeugantriebssystems an einer Pylonstruktur

Details

Veröffentlichungs-Nr.

EP4759717

Anmeldetag

15. Dezember 2025

Veröffentlichung

17. Juni 2026

Rechtsraum

EP

IPC

B64D27/40, F02C7/20

Abstract

An aircraft system includes a turbine engine case and an attachment that is configured to mount the turbine engine case (64) to a pylon structure (88) and transfer one or more loads between the turbine engine case (64) and the pylon structure (88). The attachment includes a bracket (100), a first link (102A) and a second link (102B). The bracket is configured to mount to the pylon structure (88) through a bracket-pylon pin connection (160) such that the attachment (98) is operable to pivot about the bracket-pylon pin connection (160) and move relative to the pylon structure (88). The bracket is mounted to the first link (102A) through a bracket-first link pin connection (144A). The bracket is mounted to the second link (102B) through a bracket-second link pin connection (144B). The first link (102A) is mounted to the turbine engine case (64) through a first link-case pin connection (146A). The second link (102B) is mounted to the turbine engine case (64) through a second link-case pin connection (146B).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA