首页> 外国专利> A coaxial transmission/center hub subassembly for the rotor assembly of an unmanned aerial vehicle having ducted, coaxial counter-rotating rotors

A coaxial transmission/center hub subassembly for the rotor assembly of an unmanned aerial vehicle having ducted, coaxial counter-rotating rotors

机译:同轴传输/中心轮毂子组件,用于无人驾驶飞机的转子组件,具有导管式同轴反向旋转转子

摘要

A coaxial transmission/center hub subassembly (110) for a rotor assembly (100) of an unmanned aerial vehicle (10) having ducted, coaxial counter-rotating rotors (200, 202) defining a rotational axis (12) for the unmanned aerial vehicle (10), the unmanned aerial vehicle (10) having a toroidal fuselage (20) with a plurality of inwardly extending support struts (24) and including a powerplant subsystem (50), the rotor assembly (100) including upper and lower swashplate subassemblies (80), comprising: center hub support structure means (160, 146) intermediate said counter-rotating rotors (200, 202) for mounting said coaxial transmission/center hub (110) assembly in fixed coaxial relation to the toroidal fuselage (20) utilizing the plurality of inwardly extending support struts (24); a multi-member transmission housing (140); and a single stage transmission subsystem (120); characterized in that said multi-member transmission housing (140) includes upper and lower standpipe housings (142, 144) secured in combination with said center hub support structure means (160, 146) in opposed relation along the rotational axis (12) of the unmanned aerial vehicle (10), said upper and lower standpipe housings (142, 144) having external surfaces (142E, 144E) that function as sliding surfaces for the upper and lower swashplate subassemblies (80), respectively; and said single stage transmission subsystem (120) includes an upper bevel gear (128) that includes an upper rotor shaft (128R) rotatably mounted in combination with said upper standpipe housing (142), a lower bevel gear (130) that includes a lower rotor shaft (130R) rotatably mounted in combination with said lower standpipe housing (144), said upper and lower rotor shafts (128R, 130R) providing means for mounting the counter-rotating rotors (200, 202) in combination with said coaxial transmission/center hub subassembly (110), and an input gear (122) rotatably mounted in said center hub support structure means (160, 146) and being mechanically coupled in combination with said upper and lower bevel gears (128, 130) and the powerplant subsystem (50) to couple torque to the counter-rotating rotors (200, 202). IMAGE
机译:用于无人机(10)的转子组件(100)的同轴传动/中心轮毂子组件(110),其具有导管式同轴反向旋转转子(200、202),该同轴,同轴反向转子(200、202)限定了无人机的旋转轴(12) (10),具有环形机身(20)的无人飞行器(10),所述环形机身(20)具有多个向内延伸的支撑支柱(24),并且包括动力装置子系统(50),转子组件(100)包括上部和下部旋转斜盘组件(80),包括:中心轮毂支撑结构装置(160、146),位于所述反向旋转转子(200、202)的中间,用于将所述同轴传动/中心轮毂(110)组件以与同轴机身(20)固定同轴的关系安装。利用多个向内延伸的支撑杆(24);多部件变速器壳体(140);单级传输子系统(120);其特征在于,所述多件式变速器壳体(140)包括沿着所述轮毂的旋转轴(12)以相对关系与所述中心轮毂支撑结构装置(160、146)组合固定的上,下竖管壳体(142、144)。一种无人飞行器(10),所述上,下竖管壳体(142、144)具有外表面(142E,144E),所述外表面分别用作上斜盘组件和下斜盘组件(80)的滑动表面;所述单级传动子系统(120)包括上锥齿轮(128)和下锥齿轮(130),所述上锥齿轮包括与所述上竖管壳体(142)可旋转地安装的上转子轴(128R)。转子轴(130R)与所述下部立管壳体(144)组合旋转安装,所述上部和下部转子轴(128R,130R)提供了与所述同轴传动装置组合安装反向旋转转子(200、202)的装置。中心轮毂组件(110)和可旋转地安装在所述中心轮毂支撑结构装置(160、146)中并与所述上,下锥齿轮(128、130)以及动力装置子系统机械耦合的输入齿轮(122) (50)将扭矩耦合到反向旋转的转子(200、202)。 <图像>

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号