Kompressionsstab für Triebwerksgondel

EP4779143 22. Juli 2026

Anmelder: Rohr, Inc. 🇺🇸

Details

Veröffentlichungs-Nr.
EP4779143
Anmeldetag
14. Januar 2026
Veröffentlichung
22. Juli 2026
Rechtsraum
EP
IPC
F02K1/72, F02K1/76
Offizieller Volltext

Abstract

A nacelle compression rod is provided that includes a central member (78) and first and second rod extensions (80, 82). The central member (78) extends axially between first and second end surfaces (86A, 86B). The first rod extension (80), FRE, extends between an FRE spring end surface and an FRE tip surface. The second rod extension (SRE) extends between an SRE spring end surface and an SRE tip surface. The central member (78) includes a first end bore (92) extending axially into the central member (78) from the first end surface (86A), and a second end bore (94) extending axially into the central member (78) from the second end surface. The first rod extension (80) is partially disposed within the first end bore (92), and is linearly translatable. The second rod extension (82) is partially disposed within the second end bore (94), and is linearly translatable. The first end rod extension is biased axially outward and the second end rod extension is biased axially outward.

Anmelder

Firma
Rohr, Inc.
Land
🇺🇸 USA
🇺🇸 Rohr

US-amerikanisches Unternehmen, das Triebwerksverkleidungen und weitere Strukturkomponenten für Flugzeugtriebwerke entwickelt und herstellt.

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