Entriegelungsmechanismus für eine Stauluftturbine Aktuator
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3184437
- Aktenzeichen
- EP15461586
- Anmeldetag
- 22. Dezember 2015
- Veröffentlichung
- 13. April 2022
- Erteilung
- 13. April 2022
- Rechtsraum
- EP
- IPC
- B64D41/00F15B15/26
Abstract
An unlocking mechanism (68) for an actuator (24) comprises a base (70) and an unlocking element (72) mounted to said base (70) for rotation around an axis (A) between a first, locking position and a second, unlocking position. The unlocking element (72) has an axially facing end surface (78) for engagement, in the first position, with an operating element (76), and further comprises a slot (118) extending axially thereinto from the end surface (78) for receiving the operating element (78) in the second position for permitting an unlocking movement of the operating element along the slot (118). The mechanism further comprises an unlocking actuator (74) for rotating said unlocking element (72) between said first and second positions.
Anmelder
- Firma
- Hamilton Sundstrand Corporation
- Land
- 🇺🇸 USA
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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Dehns
Dehns · London