首页> 外国专利> Aircraft folding airscrew operating mechanism - has linkage to fold glider auxiliary blades into streamlined recess

Aircraft folding airscrew operating mechanism - has linkage to fold glider auxiliary blades into streamlined recess

机译:飞机折叠式螺旋桨操作机构-具有将滑翔机辅助叶片折叠成流线型凹槽的联动装置

摘要

The blades are folded longitudinally along the airscrew driving shaft at rest. The airscrew is used with starting or flying auxiliary engines in gliders, and reduces air resistance on gliding. The two blades are hinged on an adjusting mechanism which can be operated by the pilot. The blades are swung back into pockets which can be subsequently covered. Engine cooling air inlets can be used as stowing pockets for the blades. The blade actuating mechanism consists of a toggle lever system for each blade, and is connected to a sprung actuating lever in the pilot cabin.
机译:叶片在静止时沿着螺杆驱动轴纵向折叠。螺旋桨与滑翔机中的启动或飞行辅助发动机一起使用,可减少滑行时的空气阻力。两个叶片铰接在可由飞行员操作的调节机构上。刀片被摆回口袋中,随后可以将其覆盖。发动机冷却空气入口可用作叶片的存放袋。桨叶致动机构由每个桨叶的肘杆系统组成,并连接到驾驶室内的弹簧致动杆。

著录项

  • 公开/公告号DE2421627A1

    专利类型

  • 公开/公告日1975-11-13

    原文格式PDF

  • 申请/专利权人 DIRKS WILHELM 7520 BRUCHSAL;

    申请/专利号DE19742421627

  • 发明设计人 DIRKS WILHELM 7520 BRUCHSAL;

    申请日1974-05-04

  • 分类号B64C11/28;

  • 国家 DE

  • 入库时间 2022-08-23 02:06:37

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