The invention provides an engine flight attack angle electric adjusting mechanism of an electric culvert vertical lifting co-rotating wing aircraft, which comprises a movable sleeve connected with an engine, and a co-rotating beam and a fixed sleeve which are connected with each other, and the movable sleeve and the fixed sleeve are coaxially arranged and rotationally sleeved with each other; a first slideway forming a certain included angle with the axial direction of the movable sleeve is arranged on the side wall of the movable sleeve; a second slideway parallel to the axial direction of the fixed sleeve is arranged on the side wall of the fixed sleeve; a sliding rod is arranged between the first sliding way and the second sliding way in a penetrating mode and is in linkage with an electric telescopic mechanism. According to the engine flight attack angle electric adjusting mechanism of the electric culvert vertical lifting co-rotor aircraft, a wider optimal cruise speed range can be obtained, the comprehensive energy consumption of flight is lower, and more energy is saved.
本发明提出了一种电涵垂升共转翼飞机的发动机飞行攻角电动调节机构,包括用于与发动机连接的动套筒、相连接的共转梁和定套筒,动套筒和定套筒同轴线布置且相互转动套接;动套筒侧壁上设有与其轴向呈一定夹角的第一滑道,定套筒侧壁上设有与其轴向相平行的第二滑道;第一滑道和第二滑道之间穿设有滑杆,滑杆联动有电动伸缩机构。本发明提供的电涵垂升共转翼飞机的发动机飞行攻角电动调节机构,不仅能获得更广的最佳巡航速度范围,而且飞行综合能耗更低,更节能。
Engine flight attack angle electric adjusting mechanism of electric culvert vertical lifting co-rotor aircraft
电涵垂升共转翼飞机的发动机飞行攻角电动调节机构
2023-06-02
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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