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1. 发明授权

US5836545A Rotary wing model aircraft 失效
标题翻译：旋翼机型飞机
公开(公告)号：US5836545A
公开(公告)日：1998-11-17
申请号：US728929
申请日：1996-10-11
申请人： Paul E. Arlton , David J. Arlton , Paul Klusman
发明人： Paul E. Arlton , David J. Arlton , Paul Klusman
IPC分类号： A63H27/133 , B64C1/00 , B64C1/08 , B64C25/00 , B64C25/52 , B64C27/00 , B64C27/04 , B64C27/06 , B64C27/10 , B64C27/32 , B64C27/39 , B64C27/467 , B64C27/605 , B64C27/625 , B64C27/82 , B64D35/02
CPC分类号： A63H27/12
摘要： A model rotary wing aircraft is provided that includes a fuselage, a power plant, a main rotor, a tail rotor, and a drive apparatus. The power plant includes a passive cooling system to transfer heat produced by the power plant to the atmosphere. The passive cooling system consumes less than about five percent of the power produced by the power plant. The main rotor is driven by the power plant at a main rotor speed of rotation and the tail rotor is driven by the power plant at a tail rotor speed of rotation. The drive apparatus transfers power from the power plant to the main rotor and tail rotor to rotate the tail rotor at a tail rotor speed of rotation that is about three times greater than the main rotor speed of rotation to minimize the amount of power used by the tail rotor.
摘要翻译：提供了一种型号旋翼飞机，其包括机身，发电厂，主转子，尾转子和驱动装置。发电厂包括一个被动冷却系统，用于将发电厂产生的热量转移到大气中。被动冷却系统消耗的电力不到发电厂产生的功率的5％左右。主转子由发电厂以主转子旋转速度驱动，尾转子由发电厂以转子转子旋转速度驱动。驱动装置将电力从发电厂传递到主转子和尾部转子，以使转子的转子旋转速度大于主转子旋转速度的三分之一，从而将尾部转子的转速最小化，尾转子。

2. 发明申请

US20090314883A1 UAV LAUNCH AND RECOVERY SYSTEM 审中-公开
标题翻译：无人机发射和恢复系统
公开(公告)号：US20090314883A1
公开(公告)日：2009-12-24
申请号：US12119428
申请日：2008-05-12
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： B64F1/04 , B25J9/00
CPC分类号： B64C39/024 , B64C2201/027 , B64C2201/201 , B64C2201/208 , F41A9/13 , F41A23/34 , F41F7/00 , F41H7/02
摘要： An unmanned aerial vehicle (UAV) is launched and recovered using a UAV management system. The UAV is stored in a magazine and moved from the magazine during a launch operation and to the magazine during a recovery operation.
摘要翻译：使用无人机管理系统发射和恢复无人机（UAV）。 UAV被存储在杂志中，并且在发射操作期间从杂志移动并在恢复操作期间移动到杂志。

3. 发明授权

US07789341B2 Rotary wing aircraft having a non-rotating structural backbone and a rotor blade pitch controller 有权
标题翻译：旋翼机具有不旋转的结构主干和转子叶片桨距控制器
公开(公告)号：US07789341B2
公开(公告)日：2010-09-07
申请号：US11105746
申请日：2005-04-14
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： B64C27/08
CPC分类号： B64C27/10 , B64C27/22 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
摘要： A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
摘要翻译：旋转翼车辆包括具有细长管状骨架或芯体的主体结构，以及具有转子的反向旋转同轴转子系统，每个转子具有单独的电动机，以围绕公共转子旋转轴线驱动转子。转子系统用于在定向飞行中移动旋翼机。

4. 发明申请

US20090212157A1 MICRO-ROTORCRAFT SURVEILLANCE SYSTEM 审中-公开
标题翻译：微电机监控系统
公开(公告)号：US20090212157A1
公开(公告)日：2009-08-27
申请号：US11616201
申请日：2006-12-26
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： G05D1/00 , B64F1/04 , B64C9/00 , H02J7/00
CPC分类号： G08B13/19621 , B64C27/10 , B64C39/024 , B64C39/028 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/108 , B64C2201/121 , B64C2201/122 , B64C2201/127 , B64C2201/146 , B64C2201/201 , B64C2201/203 , B64C2201/208 , G08B13/19619 , G08B13/1963
摘要： A flying micro-rotorcraft unit is provided for remote tactical and operational missions. The unit includes an elongated body having an upper and a lower end. The body defines a vertical axis. The unit further includes a navigation module including means for determining a global position of the elongated body during flight of the unit. Rotor means of the unit is coupled to the upper end of the elongated body for generating a thrust force that acts in a direction parallel to the vertical axis to lift the elongated body into the air. The rotor means is located between the elongated body and the navigation module.
摘要翻译：提供了一个飞行的微型旋翼航空器，用于远程战术和作战任务。该单元包括具有上端和下端的细长主体。身体定义垂直轴。该单元还包括导航模块，其包括用于在单元飞行期间确定细长主体的全局位置的装置。该单元的转子装置联接到细长主体的上端，用于产生沿平行于垂直轴线的方向作用的推力，以将细长主体提升到空气中。转子装置位于细长主体和导航模块之间。

5. 发明授权

US5879131A Main rotor system for model helicopters 失效
标题翻译：模型直升机主转子系统
公开(公告)号：US5879131A
公开(公告)日：1999-03-09
申请号：US729184
申请日：1996-10-11
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： B64C27/10 , B64C27/32 , B64C27/43 , B64C27/467 , B64C27/46
CPC分类号： B64C27/467 , B64C27/10 , B64C27/32 , B64C27/43 , Y10S416/05
摘要： A main rotor is provided for use on a model helicopter. The main rotor includes rotor blades having an inboard section and an outboard section. The inboard section includes a higher camber, thin, wide airfoils, and greater pitch and camber relative to the outboard section. The outboard section includes an average chord length that is less than the chord length of the inboard section, The rotor blades also include a blade body that is semiflexible to bend during a crash landing of the model helicopter.
摘要翻译：提供主转子用于模型直升机。主转子包括具有内侧部分和外侧部分的转子叶片。内侧部分包括相对于外侧部分的更高的弯度，薄的，宽的翼型，以及更大的俯仰和弯度。外侧部分包括小于内侧部分的弦长的平均弦长。转子叶片还包括在模型直升机的碰撞着陆期间半柔性弯曲的叶片体。

6. 发明授权

US5597138A Yaw control and stabilization system for helicopters 失效
标题翻译：直升机的控制和稳定系统
公开(公告)号：US5597138A
公开(公告)日：1997-01-28
申请号：US292719
申请日：1994-08-18
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： B64C1/08 , B64C25/52 , B64C27/00 , B64C27/04 , B64C27/10 , B64C27/32 , B64C27/39 , B64C27/467 , B64C27/605 , B64C27/625 , B64C27/82 , B64C27/78
CPC分类号： B64C27/32 , A63H27/12 , B64C27/10 , B64C27/467 , B64C27/82
摘要： A device for stabilizing yaw motion is provided for use on a helicopter having a main rotor rotatable about a main rotor axis, a power source, and a tail rotor boom with a longitudinal axis. The device includes a tail rotor and a gyroscopic mechanism. The tail rotor is mounted to the tail boom of a helicopter and is rotated about a tail rotor axis by the power source to generate a thrust force transverse to the tail boom and offset from the main rotor axis. The gyroscopic mechanism automatically varies the thrust force generated by the tail rotor to oppose yaw motions. The gyroscopic mechanism includes first and second variable pitch gyro arms extending along first and second gyro arm pitch axes, respectively, a support mechanism, and a pitch adjustor linkage. The support mechanism is configured to support the variable pitch gyro arms for pivotable movement about a gyro pivot axis between a nominal orientation and a tilted orientation so that the variable pitch gyro arms pivot about the gyro pivot axis from the nominal orientation toward the tilted orientation in response to yaw motion encountered by the gyro arms during flight to vary the thrust generated by the tail rotor. The pitch adjustor linkage is appended to the first gyro arm to adjust the pitch of the first gyro arm about the first gyro arm pitch axis.
摘要翻译：提供一种用于稳定偏转运动的装置，用于具有可绕主转子轴线旋转的主转子的直升机，具有纵向轴线的动力源和尾转子悬臂。该装置包括尾部转子和陀螺仪机构。尾部转子安装在直升机的尾臂上，并通过动力源围绕尾部转子轴线旋转，以产生横向于尾臂的推力并从主转子轴线偏移。陀螺仪机构自动地改变由尾部转子产生的反作用力与偏航运动的反作用力。陀螺仪机构包括分别沿着第一和第二陀螺仪俯仰轴延伸的第一和第二可变俯仰陀螺臂，支撑机构和俯仰调节器连杆。支撑机构被配置为支撑可变俯仰陀螺臂，用于在标称方向和倾斜方向之间围绕陀螺仪枢转轴线的可枢转运动，使得可变俯仰陀螺臂围绕陀螺仪枢转轴线从标称方位向倾斜方向枢转响应于在飞行期间由陀螺仪臂遇到的偏航运动，以改变由尾部转子产生的推力。俯仰调节器联动装置附加到第一陀螺仪臂以调整第一陀螺仪臂围绕第一陀螺仪俯仰轴的俯仰。

7. 发明申请

US20170166305A1 ROTARY WING VEHICLE 审中-公开
公开(公告)号：US20170166305A1
公开(公告)日：2017-06-15
申请号：US15175161
申请日：2016-06-07
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： B64C27/605 , B64C39/02 , B64C27/14 , B64C27/10
CPC分类号： B64C27/605 , B64C7/00 , B64C27/10 , B64C27/14 , B64C39/024 , B64C2027/8236 , B64C2027/8281 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
摘要： A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.

8. 发明授权

US08042763B2 Rotary wing vehicle 有权
标题翻译：旋翼车
公开(公告)号：US08042763B2
公开(公告)日：2011-10-25
申请号：US12872622
申请日：2010-08-31
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： B64C27/08
CPC分类号： B64C27/10 , B64C27/22 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
摘要： A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
摘要翻译：旋转翼车辆包括具有细长管状骨架或芯体的主体结构，以及具有转子的反向旋转同轴转子系统，每个转子具有单独的电动机，以围绕公共转子旋转轴线驱动转子。转子系统用于在定向飞行中移动旋翼机。

9. 发明申请

US20110006166A1 ROTARY WING VEHICLE 有权
标题翻译：旋转翼车
公开(公告)号：US20110006166A1
公开(公告)日：2011-01-13
申请号：US12872622
申请日：2010-08-31
申请人： Paul E. ARLTON , David J. Arlton
发明人： Paul E. ARLTON , David J. Arlton
IPC分类号： B64C27/22 , B64C27/08 , G05D1/00 , B64C27/00 , B64C13/04 , B64D1/02 , B64C13/50 , B64C39/00
CPC分类号： B64C27/10 , B64C27/22 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
摘要： A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
摘要翻译：旋转翼车辆包括具有细长管状骨架或芯体的主体结构，以及具有转子的反向旋转同轴转子系统，每个转子具有单独的电动机，以围绕公共转子旋转轴线驱动转子。转子系统用于在定向飞行中移动旋翼机。

10. 发明申请

US20080245924A1 ROTARYCRAFT POWER AND PROPULSION SYSTEM 有权
标题翻译：旋转动力和推进系统
公开(公告)号：US20080245924A1
公开(公告)日：2008-10-09
申请号：US12016821
申请日：2008-01-18
申请人： Paul E. Arlton , David J. Arlton
发明人： Paul E. Arlton , David J. Arlton
IPC分类号： B64C27/57 , B64C27/08
CPC分类号： B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/108 , B64C2201/127 , B64C2201/201
摘要： A rotary wing vehicle includes a body structure having an elongated tubular backbone or core and a counter-rotating coaxial rotor system having rotors. The rotor system is used to move the rotary wing vehicle in directional flight.
摘要翻译：旋转翼车辆包括具有细长管状骨架或芯体的主体结构和具有转子的反向旋转同轴转子系统。转子系统用于在定向飞行中移动旋翼机。

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