A throttle lever suitable for controlling the magnitude and direction of thrust of one or more aircraft engines is described. The throttle lever includes a frame, a trigger mechanism, a connection element, a cam engagement mechanism, a biasing device, a cam, and a handle adapted to be grasped by a user when the throttle lever is in use. The cam includes a slot having first and second slot portions and a stop portion. A stop portion extends between and connects the first slot portion and the second slot portion. The cam engagement mechanism includes a cam lever pivotally attached to the frame via a cam lever pivot and a slot engagement element attached to the cam lever. The trigger mechanism includes a trigger lever pivotally attached to the frame via a trigger pivot and a trigger. A trigger extends through the handle. A connecting element is attached to the trigger lever and the cam lever. A biasing device biases the cam lever to rotate in a first direction about the cam lever pivot.
描述了一种适用于控制一个或多个飞行器发动机的推力的大小和方向的节流控制杆。节流控制杆包括框架、触发机构、连接元件、凸轮接合机构、偏置装置、凸轮以及适用于在节流控制杆使用时由使用者抓握的把手。凸轮包括具有第一狭槽部分和第二狭槽部分以及止动部分的狭槽。止动部分在第一狭槽部分和第二狭槽部分之间延伸并连接第一狭槽部分和第二狭槽部分。凸轮接合机构包括凸轮杆和狭槽接合元件,凸轮杆经由凸轮杆枢轴枢转地附接到框架,并且狭槽接合元件附接到凸轮杆。触发机构包括触发杆和触发器,触发杆经由触发枢轴枢转地附接到框架。触发器延伸穿过把手。连接元件附接到触发杆和凸轮杆。偏置装置偏置凸轮杆以围绕凸轮杆枢轴在第一方向上旋转。
Throttle control rod
节流控制杆
2023-11-14
Patent
Electronic Resource
Chinese
Tema Archive | 1991
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