Federkompressionsvorrichtung

EP3263944 Art B1 22. Juni 2022

Anmelder: Hamilton Sundstrand Corporation 🇺🇸

Details

Veröffentlichungs-Nr.
EP3263944
Aktenzeichen
EP16461533
Anmeldetag
1. Juli 2016
Veröffentlichung
22. Juni 2022
Erteilung
22. Juni 2022
Rechtsraum
EP
IPC
F03G1/02F03G1/06F16F1/12B64D41/00
Offizieller Volltext

Abstract

A spring compression device (100) comprises a spring sleeve (110) configured to receive a spring (210); a spring adjustment member (130) provided on and engaged with the spring sleeve and configured to abut a spring (210) mounted on the spring sleeve, wherein the spring sleeve and spring adjustment member define an operating length (L) of the spring compression device, and the spring adjustment member is configured to be moved relative to the spring sleeve to adjust the operating length of the spring compression device; and at least one blocking component (140) for blocking movement between the spring sleeve and the spring adjustment member. The spring sleeve and spring adjustment member may be engaged with a threaded connection (120). An exterior surface of the spring sleeve and an interior surface (135) of the spring adjustment member may each have at least one recess (116, 136) which align to form a hole for receiving the blocking component. The hole may extend in a direction parallel to a longitudinal axis (R) of the spring sleeve.

Anmelder

Firma
Hamilton Sundstrand Corporation
Land
🇺🇸 USA
🇺🇸 Hamilton Sundstrand

US-amerikanisches Unternehmen der Luft- und Raumfahrtindustrie, das Flugzeugsysteme wie Umweltkontroll-, Energie- und Antriebssysteme entwickelt; heute Teil von Collins Aerospace innerhalb von RTX.

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