The invention relates to a lockset system (30) for a turbine engine nacelle, the lockset system comprising:-a support (41) to support a hooked member (42); -a three-point lock (51) comprising a support (52), a yoke (53), and a three-point mechanism (54) hingedly connected to the points of the support; -an actuation handle (60) for actuating the mechanism (54) between a locked position and an unlocked position, characterized in that the actuation handle comprises a first end (60A) connected to the three-point mechanism and a locking bushing (70) fixed to a second end (60B), the locking bushing is mounted to pivot relative to the support of the three-point lockset between a first end position in which the three-point mechanism is locked and a second end position in which the three-point mechanism is unlocked, the lockset system comprising a blocking tool (80) for blocking the three-point mechanism from the locking bushing. A blocking tool is adapted to cooperate with the locking bushing and is configured to move the locking bushing between a blocking position and an unblocking position when the bushing is in the first end position, and to prevent movement of the actuation handle when the bushing is in the blocking position.
本发明涉及一种用于涡轮发动机机舱的锁具系统(30),锁具系统包括:‑支撑件(41),支撑件对被钩状件(42)进行支撑;‑三点式锁具(51),三点式锁具包括支撑件(52)、轭部(53)、以及铰接地连接到支撑件的点的三点式机构(54);‑致动手柄(60),致动手柄用于在锁定位置和解锁位置之间致动机构(54),其特征在于,致动手柄包括连接到三点式机构的第一端部(60A)和固定到第二端部(60B)的锁定衬套(70),锁定衬套被安装成相对于三点式锁具的支撑件在第一端部位置和第二端部位置之间枢转,在第一端部位置,三点式机构被锁定,在第二端部位置,三点式机构被解锁,锁具系统包括阻挡工具(80),阻挡工具适于与锁定衬套协作并且被构造成当衬套处于第一端部位置时使锁定衬套在阻挡位置和未阻挡位置之间移动,并且当衬套处于阻挡位置时防止致动手柄移动。
Lock system for nacelle of turbine engine and nacelle comprising such lock system
用于涡轮发动机机舱的锁具系统和包括该锁具系统的机舱
16.05.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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