侧向倾转机构和飞行器
By employing a linkage transmission structure consisting of a rocker arm, a tie rod, and a drive arm in the aircraft, the problem of drive source damage due to torque overload is solved, torque transmission is reduced, and the stability and maneuverability of the aircraft are improved.
CN224511453UActive Publication Date: 2026-07-17SHENYANG WOOZOOM TECH CO LTD
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- SHENYANG WOOZOOM TECH CO LTD
- Filing Date
- 2026-06-15
- Publication Date
- 2026-07-17
AI Technical Summary
Technical Problem
The aircraft's lateral tilting motion is directly driven by the drive source, which makes the output shaft of the drive source prone to damage due to torque overload after long-term use.
Method used
The linkage transmission structure is adopted. By setting up a rocker arm, a tie rod and a drive arm to form a linkage transmission structure with a reduction ratio greater than one, the torque transmitted from the tilting seat to the drive source is reduced, and the load torque of the drive source is reduced.
Benefits of technology
It effectively reduces the probability of damage to the drive source due to torque overload, and improves the lateral stability and maneuverability of the aircraft.
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Figure CN224511453U_ABST
Abstract
本申请公开了一种侧向倾转机构和飞行器，属于飞行器倾转机构技术领域，主要目的是通过减速比大于一的连杆传动结构降低驱动源承受的负载扭矩。本申请的主要技术方案为：该侧向倾转机构包括固定座、倾转座、拉杆和驱动臂；所述固定座设置于机臂远离机身的一端；所述倾转座可转动地连接于所述固定座，所述倾转座用于承载动力组件，所述倾转座的倾转轴线垂直于所述机臂，所述倾转座与所述固定座的转动连接点位于所述倾转轴线上；所述倾转座上设置有摇臂，所述拉杆的一端与所述摇臂相铰接，另一端与所述驱动臂相铰接，所述驱动臂的长度小于所述摇臂的长度。
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