Montageanordnung zum Verbinden von Flugzeugkomponenten

Details

Veröffentlichungs-Nr.

EP4714830

Anmeldetag

19. September 2025

Veröffentlichung

25. März 2026

Rechtsraum

EP

Abstract

An assembly is provided for an aircraft. This aircraft assembly includes a first mount (28), a second mount (30), a mounting assembly (20) and a fluid reservoir structure. The mounting assembly (20) connects the first mount (28) to the second mount (30) along an axis (26) while providing controlled intercomponent movement between the first mount (28) and the second mount (30) to reduce internal stress and/or wear. The mounting assembly (20) includes an outer bushing (32), an inner bushing (34) and a fastener (36). The fluid reservoir structure includes one of the first mount (28) or the second mount (30).

Anmelder

Firma

PRATT & WHITNEY CANADA CORP.

Land

🇨🇦 Kanada