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    Performing corrective action on unmanned aerial vehicle using one axis of three-axis magnetometer
    72.
    发明专利
    Performing corrective action on unmanned aerial vehicle using one axis of three-axis magnetometer 审中-公开
    使用三轴磁力计的一个轴进行无人驾驶车辆的正确行为

    公开(公告)号：JP2010241409A

    公开(公告)日：2010-10-28

    申请号：JP2010013993

    申请日：2010-01-26

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： FITZPATRICK DAVID

    IPC: B64C17/00 ,  B64C29/00 ,  B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/044 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/141 ,  G01R33/0206 ,  G05D1/0858

    Abstract: PROBLEM TO BE SOLVED: To provide a means for preventing uncontrolled flight or tip-over of an unmanned aerial vehicle (UAV) during take-off.
    SOLUTION: The UAV includes: a step 302 for receiving a measurement representative of a posture of the UAV from the magnetometer, wherein the measurement is of only one axis of the three-axis magnetometer; a step 304 fpr comparing the measurement to an allowable range of posture; a step 306 for determining that the measurement is not within the allowable range of posture; and a step 308 for performing at least one corrective action for the UAV.
    COPYRIGHT: (C)2011,JPO&INPIT

    Abstract translation: 要解决的问题：提供一种在起飞期间防止无人驾驶飞行器（UAV）的不受控飞行或翻倒的手段。 解决方案：UAV包括：步骤302，用于从磁力计接收代表UAV的姿势的测量，其中测量仅为三轴磁力计的一个轴; 将测量与允许的姿势范围进行比较的步骤304fpr; 用于确定测量不在允许的姿势范围内的步骤306; 以及用于对UAV执行至少一个校正动作的步骤308。 版权所有（C）2011，JPO＆INPIT

    Ducted fan core used for unmanned aircraft
    73.
    发明专利
    Ducted fan core used for unmanned aircraft 有权
    用于不定期飞机的导向风扇芯

    公开(公告)号：JP2010030585A

    公开(公告)日：2010-02-12

    申请号：JP2009125187

    申请日：2009-05-25

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： COLLETTE DANIEL ROSS

    IPC: B64C29/00 ,  B64C39/02

    CPC classification number: B64C39/024 ,  B64C27/20 ,  B64C2201/027 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/162

    Abstract: PROBLEM TO BE SOLVED: To provide a ducted fan core for housing a wide variety of payloads for an unmanned aircraft.
    SOLUTION: A ducted fan core 100 includes a frame 110 attached to an engine 120, a gearbox assembly, a fan 140, and a plurality of control vanes 130. A first surface 112 on the frame includes a plurality of connecting sections or electrical traces. The plurality of connecting sections are used for removably attaching a variety of pods holding various payloads. Thus, the wide variety of payloads can be conveyed by using the same unmanned aircraft, simply by removing pods from the fixed core of the aircraft and attaching different pods thereto. These pods are shaped so as to form part of the exterior of the aircraft, and when the pods are attached to the frame, they enhance the characteristics of aerodynamics of the aircraft.
    COPYRIGHT: (C)2010,JPO&INPIT

    Abstract translation: 要解决的问题：提供一种用于无人驾驶飞机的用于容纳各种有效载荷的管道风扇芯。 管道风扇芯100包括附接到发动机120的框架110，齿轮箱组件，风扇140和多个控制叶片130.框架上的第一表面112包括多个连接部分或 电痕迹。 多个连接部分用于可拆卸地连接保持各种有效载荷的各种荚。 因此，可以通过使用相同的无人驾驶飞机来简单地通过从飞行器的固定核中移除舱架并且将不同舱架附接到其上来传送各种有效载荷。 这些荚形成为形成飞行器外部的一部分，并且当荚附接到框架时，它们增强了飞行器的空气动力学的特性。 版权所有（C）2010，JPO＆INPIT

    Method for vertical takeoff from and landing on inclined surfaces
    74.
    发明专利
    Method for vertical takeoff from and landing on inclined surfaces 审中-公开
    在垂直表面上垂直剥离和着陆的方法

    公开(公告)号：JP2008290704A

    公开(公告)日：2008-12-04

    申请号：JP2008042051

    申请日：2008-02-22

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： HURSIG DAVID C ,  MARTINEZ STEVEN D

    IPC: B64C25/32 ,  B64C29/00

    CPC classification number: B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/162 ,  B64D45/04 ,  G05D1/0653 ,  G05D1/0858

    Abstract: PROBLEM TO BE SOLVED: To provide an unmanned air vehicle capable of performing vertical takeoff from and landing on inclined surfaces.
    SOLUTION: Takeoff and landing modes are added to a flight control system of a Vertical Take-Off and Landing (VTOL) Unmanned Air Vehicle (UAV). The takeoff and landing modes use data available to the flight control system and the VTOL UAV's existing control surfaces and throttle control. As a result, the VTOL UAV can takeoff from and land on inclined surfaces without the use of landing gear mechanisms designed to level the UAV on the inclined surfaces.
    COPYRIGHT: (C)2009,JPO&INPIT

    Abstract translation: 要解决的问题：提供能够在倾斜表面上执行垂直起飞和着陆的无人驾驶飞行器。

    解决方案：起飞和着陆模式被添加到垂直起飞和着陆（VTOL）无人机（UAV）的飞行控制系统。 起飞和着陆模式使用可用于飞行控制系统和VTOL无人机现有控制面和节气门控制的数据。 因此，VTOL无人机可以在倾斜的表面上起飞和着陆，而不需要使用设计成在倾斜表面上对无人机进行平坦化的起落架机构。 版权所有（C）2009，JPO＆INPIT

    착륙이 용이한 무인비행체
    76.
    发明授权
    착륙이 용이한 무인비행체 有权
    用于轻松登陆的无人驾驶的空中客车

    公开(公告)号：KR101287624B1

    公开(公告)日：2013-07-23

    申请号：KR1020130020070

    申请日：2013-02-25

    Applicant: 주식회사 네스앤텍

    Inventor： 이기성

    IPC: B64C29/02 ,  B64C13/20 ,  B64C3/38

    CPC classification number: B64C27/28 ,  B64C3/38 ,  B64C3/58 ,  B64C9/323 ,  B64C39/024 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/185 ,  B64C2201/187

    Abstract: PURPOSE: An unmanned aerial vehicle for easy landing is provided to enable easy landing without a parachute or airbag by switching the direction of a propeller upward and controlling the descending velocity thereof. CONSTITUTION: An unmanned aerial vehicle for easy landing comprises a propeller (100), a propeller tower (200), a body (300), main wings (400), auxiliary wings (500), and an actuator. The propeller tower supports the propeller. The body is connected to the propeller tower. The main wings are symmetrical with respect to the horizontal shaft of the body and have a pair of through holes (410). The auxiliary wings are located inside the through holes. The actuator is connected to a reference shaft fixed to the main wings through the auxiliary wings and controls the inclination of the auxiliary wings.

    Abstract translation: 目的：提供一种易于着陆的无人驾驶飞行器，通过向上切换螺旋桨的方向并控制其下降速度，轻松着陆，无需降落伞或气囊。 构成：易于着陆的无人驾驶飞行器包括螺旋桨（100），螺旋桨塔（200），主体（300），主翼（400），辅助翼（500）和致动器。 螺旋桨塔支撑螺旋桨。 车身连接到螺旋桨塔。 主翼相对于主体的水平轴对称，并具有一对通孔（410）。 辅助翼位于通孔内。 致动器通过辅助翼连接到固定到主翼的基准轴，并控制辅助翼的倾斜。

    무선조정 다목적 항공기의 수직 착륙장치 및 이를 이용한착륙방법
    78.
    发明公开
    무선조정 다목적 항공기의 수직 착륙장치 및 이를 이용한착륙방법 失效
    用于无线电遥控多功能飞机的垂直起落设备及其方法

    公开(公告)号：KR1020070059748A

    公开(公告)日：2007-06-12

    申请号：KR1020050118972

    申请日：2005-12-07

    Applicant: 김주은

    Inventor： 김주은 ,  문상도 ,  노항배

    IPC: B64C29/00

    CPC classification number: B64C39/024 ,  A63H27/02 ,  A63H30/04 ,  A63H33/20 ,  B64C2201/021 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/126 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/185

    Abstract: A vertical landing apparatus for a radio control multipurpose aircraft and a landing method using the same are provided to safely land the aircraft at a goal spot without damaging the aircraft. A radio control multipurpose aircraft includes a body section(100), wing sections(200), and a landing unit(300). The landing unit includes a parachute. The parachute and the body section are connected to each other by including at least one pair of highly flexible guide cords and at least one pair of non-flexible guide cords. The highly flexible guide cord includes a first guide cord and a second guide cord. The first and second guide cords are connected to an engine cover and a front main blade connecting rod. The non-flexible guide cord is connected to a rear main blade connecting rod.

    Abstract translation: 提供用于无线电控制多用途飞行器的垂直着陆装置和使用其的着陆方法，以便在不损害飞行器的情况下将飞机安全着陆在目标位置。 无线电控制多功能飞机包括主体部分（100），机翼部分（200）和着陆单元（300）。 着陆单元包括降落伞。 降落伞和主体部分通过包括至少一对高度柔性的引导线和至少一对非柔性引导线彼此连接。 高度柔性的导绳包括第一导绳和第二导绳。 第一和第二引导线连接到发动机盖和前主叶片连接杆。 非柔性引导线连接到后主刀连接杆。

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