公开(公告)号：US20160280369A1

公开(公告)日：2016-09-29

申请号：US15033788

申请日：2014-10-31

Applicant: THE UNIVERSITY OF QUEENSLAND

Inventor： Paul Edward Ian POUNDS

IPC: B64C27/82 ,  G05D1/08 ,  B64C27/43 ,  B64C39/02 ,  B64C27/08

CPC classification number: B64C27/82 ,  A63H27/00 ,  B64C27/08 ,  B64C27/43 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  G05D1/0816

Abstract: A rotorcraft having a body and a propulsion system wherein the propulsion system includes a main thrust rotor and multiple control rotors, wherein the main thrust rotor is coupled to the body, whereby the main thrust rotor is driven by a main thrust drive shaft having an axis of rotation maintained in a fixed orientation to the body of the rotorcraft and wherein the multiple control rotors are arranged to control roll, pitch and yaw of the rotorcraft and are driven by respective control drive shafts offset to the axis of rotation of the main thrust drive shaft.

Abstract translation: 具有主体和推进系统的旋翼飞机，其中推进系统包括主推力转子和多个控制转子，其中主推力转子联接到主体，由此主推力转子由具有轴线的主推力驱动轴驱动 的旋转保持在与旋翼航空器的主体固定的方向上，并且其中所述多个控制转子被布置成控制所述旋翼航空器的滚动，俯仰和偏航，并且由相应的控制驱动轴驱动，所述控制驱动轴偏移到所述主推力驱动器的旋转轴线 轴。

公开(公告)号：US20160272310A1

公开(公告)日：2016-09-22

申请号：US14560606

申请日：2014-12-04

Applicant: Elwha LLC

Inventor： ALISTAIR K. CHAN ,  JESSE R. CHEATHAM, III ,  HON WAH CHIN ,  WILLIAM DAVID DUNCAN ,  RODERICK A. HYDE ,  MURIEL Y. ISHIKAWA ,  JORDIN T. KARE ,  TONY S. PAN ,  ROBERT C. PETROSKI ,  CLARENCE T. TEGREENE ,  DAVID B. TUCKERMAN ,  THOMAS ALLAN WEAVER ,  LOWELL L. WOOD, JR.

IPC: B64C27/08 ,  B64C39/02 ,  B64D1/00 ,  B64C13/02 ,  B64C27/54

CPC classification number: B64C27/08 ,  B64C13/02 ,  B64C27/37 ,  B64C27/54 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/128 ,  B64C2201/165 ,  B64D1/00 ,  B64D45/00

Abstract: A reconfigurable unmanned aircraft system is disclosed. A system and method for configuring a reconfigurable unmanned aircraft and system and method for operation and management of a reconfigurable unmanned aircraft in an airspace are also disclosed. The aircraft is selectively reconfigurable to modify flight characteristics. The aircraft comprises a set of rotors. The position of at least one rotor relative to the base can be modified by at least one of translation of the rotor relative to the boom, pivoting of the boom relative to the base, and translation of the boom relative to the base; so that flight characteristics can be modified by configuration of position of at least one rotor relative to the base. A method of configuring an aircraft having a set of rotors on a mission to carry a payload comprises the steps of determining properties of the payload including at least mass properties, determining the manner in which the payload will be coupled to the aircraft, determining configuration for each of the rotors in the set of rotors at least partially in consideration of the properties of the payload, and positioning the set of rotors in the configuration for the aircraft to perform the mission.

公开(公告)号：US09442496B1

公开(公告)日：2016-09-13

申请号：US14858270

申请日：2015-09-18

Applicant: Amazon Technologies, Inc.

Inventor： Brian C. Beckman ,  Gur Kimchi

IPC: G05D19/02 ,  B64C39/02 ,  G10K11/178

CPC classification number: G10K11/178 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2220/00 ,  G01S19/13 ,  G05D1/101 ,  G05D19/02 ,  G05D27/02 ,  G06N99/005 ,  G10K11/17823 ,  G10K11/17853 ,  G10K11/17873 ,  G10K2210/1281 ,  G10K2210/30231 ,  G10K2210/30351 ,  G10K2210/3038 ,  G10K2210/3045

Abstract: Noises that are to be emitted by an aerial vehicle during operations may be predicted using one or more machine learning systems, algorithms or techniques. Anti-noises having equal or similar intensities and equal but out-of-phase frequencies may be identified and generated based on the predicted noises, thereby reducing or eliminating the net effect of the noises. The machine learning systems, algorithms or techniques used to predict such noises may be trained using emitted sound pressure levels observed during prior operations of aerial vehicles, as well as environmental conditions, operational characteristics of the aerial vehicles or locations of the aerial vehicles during such prior operations. Anti-noises may be identified and generated based on an overall sound profile of the aerial vehicle, or on individual sounds emitted by the aerial vehicle by discrete sources.

Abstract translation: 可以使用一个或多个机器学习系统，算法或技术来预测在操作期间由飞行器发射的噪声。 可以基于预测的噪声来识别和产生具有相同或相似的强度和等于或相同的频率的抗噪声，从而减少或消除噪声的净效应。 可以使用用于预测这种噪声的机器学习系统，算法或技术来使用在先前的飞行器操作期间观察到的发射声压级，以及环境条件，飞行器的操作特性或飞行器的位置 操作。 可以基于飞行器的整体声音轮廓或者由离散源发出的飞行器发出的各种声音来识别和产生抗噪声。

公开(公告)号：US09440736B2

公开(公告)日：2016-09-13

申请号：US13480431

申请日：2012-05-24

Applicant: Pete Bitar

Inventor： Pete Bitar

IPC: B64C27/10 ,  B64C27/12 ,  B64C39/02 ,  B64D27/24

CPC classification number: B64C27/10 ,  B64C27/12 ,  B64C39/026 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64D27/24 ,  Y02T50/62

Abstract: Disclosed is a Personal Electric Helicopter device with an integral wind turbine recharging capability. The device is a relatively small, lighter weight powered aircraft capable of vertical take-offs and propulsion across various terrain at low altitudes. The device is uniquely capable of re-charging its power source by connection to an electrical grid or by using its uplift components as a wind turbine for re-charging. The preferred embodiment is comprised of a rechargeable uplift and propulsion power system with components and features; a frame structure to carry an operator and/or payload; a means to connect the structure to the power system; and a means to control the uplift and propulsion system wherein the vehicle may be used to elevate and propel a payload at low altitudes across various terrains and may be positioned to reverse power the wind turbine to recharge the batteries.

Abstract translation: 公开了具有整体风力涡轮机充电能力的个人电动直升机装置。 该装置是一种相对较小，重量更轻的动力飞机，能够在低海拔地区的各种地形垂直起飞和推进。 该装置独特地能够通过连接到电网或通过使用其提升部件作为风力涡轮机来重新充电其电源来进行再充电。 优选实施例包括具有部件和特征的可再充电提升和推进动力系统; 携带操作者和/或有效载荷的帧结构; 将结构连接到电力系统的手段; 以及用于控制升降和推进系统的手段，其中车辆可用于在不同的地形上提升和推进低海拔地区的有效载荷，并且可被定位成使风力涡轮机反向动力以对电池再充电。

公开(公告)号：US20160257423A1

公开(公告)日：2016-09-08

申请号：US14481456

申请日：2014-09-09

Applicant: Joseph Martin

Inventor： Joseph Martin

IPC: B64F1/00 ,  B64D1/10 ,  G05D1/10 ,  B64C39/02

CPC classification number: B64F1/00 ,  A47G29/14 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/128

Abstract: An unmanned aerial vehicle delivery system utilizes an unmanned aerial vehicle (UAV) to deliver packages between an initiation point and multiple delivery points at a raised elevation. The UAV flies between points in an organized manner, using logistical, maintenance and safety software, commands from a delivery organization, and guidance tools to coordinate deliveries. One advantage of the system is that the UAV engages the delivery points at a raised elevation, rather than the ground level. The UAV docks through an elevated structure at the delivery point for delivering the package and replenishing a power source. The package is conveyed from a docking end and through a central shaft of the elevated structure by means of an elevator. The package then travels to a lower structure, such as a house or office, for pickup. After completion of the delivery, the UAV replenishes its power source and/or continues on the delivery route.

Abstract translation: 无人驾驶飞行器运输系统利用无人驾驶飞行器（UAV）在升起的高度在起始点和多个输送点之间输送包装。 无人机以有组织的方式飞行，使用后勤，维护和安全软件，来自交付组织的命令，以及指导工具来协调交付。 该系统的一个优点是无人机以升高的高度而不是地平面接合输送点。 无人机在交付点通过升高的结构进行码头，用于交付包装并补充电源。 包装通过电梯从对接端传送并且通过升高结构的中心轴传送。 包装然后行进到较低的结构，例如房屋或办公室，以便拾取。 交付完成后，无人机将在其交付路线上补充电源和/或继续运行。

公开(公告)号：US20160236777A1

公开(公告)日：2016-08-18

申请号：US14752465

申请日：2015-06-26

Applicant: HON HAI PRECISION INDUSTRY CO., LTD.

Inventor： PEI-CHONG TANG

IPC: B64C39/02 ,  B64C25/52 ,  B64C27/08

CPC classification number: B64C39/024 ,  B64C25/52 ,  B64C2201/027 ,  B64C2201/042

Abstract: An aerial vehicle includes a body including a bottom portion, a plurality of rotors coupled to the body for driving the aerial vehicle to fly, and a landing gear coupled to the bottom portion of the body. The landing gear can include a first touchdown bar and a second touchdown bar. The first touchdown bar has a distal end for contacting a horizontal plane. The second touchdown bar has a distal end for contacting the horizontal plane. The distal end of the first touchdown bar and the distal end of the second touchdown bar cooperatively define a plane. When the aerial vehicle is in flight, the plane is at an angle relative to the horizontal plane. When the aerial vehicle is landing at the horizontal plane, the plane is parallel to the horizontal plane, the body is angled relative to the horizontal plane.

Abstract translation: 一种飞行器包括主体，该主体包括底部，多个转子，其联接到主体以驱动飞行器飞行;以及起落架，联接到主体的底部。 起落架可以包括第一接触杆和第二接触杆。 第一个触地条具有用于接触水平面的远端。 第二接触杆具有用于接触水平面的远端。 第一接触杆的远端和第二触下杆的远端协作地限定一个平面。 当飞行器飞行时，平面相对于水平面成一定角度。 当飞行器在水平面上着陆时，平面平行于水平面，主体相对于水平面成角度。

公开(公告)号：US20160236772A1

公开(公告)日：2016-08-18

申请号：US14751893

申请日：2015-06-26

Applicant: HON HAI PRECISION INDUSTRY CO., LTD.

Inventor： PEI-CHONG TANG

IPC: B64C25/52 ,  B64C27/08 ,  B64C39/02

CPC classification number: B64C25/52 ,  B64C39/024 ,  B64C2025/325 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/128

Abstract: An aerial vehicle includes a body including a bottom portion, a plurality of rotors coupled to the body for driving the aerial vehicle to fly, and a landing gear coupled to the bottom portion of the body. The landing gear can include a first touchdown bar and a second touchdown bar. The first touchdown bar has a bottom face for contacting a horizontal plane. The second touchdown bar has a bottom face for contacting the horizontal plane. The bottom face of the first touchdown bar and the bottom face of the second touchdown bar cooperatively define a plane. When the aerial vehicle is in flight, the plane is at an angle relative to the horizontal plane. When the aerial vehicle is landing at the horizontal plane, the plane is parallel to the horizontal plane, the body is angled relative to the horizontal plane.

Abstract translation: 一种飞行器包括主体，该主体包括底部，多个转子，其联接到主体以驱动飞行器飞行;以及起落架，联接到主体的底部。 起落架可以包括第一接触杆和第二接触杆。 第一个触地板具有用于接触水平面的底面。 第二触地板具有用于接触水平面的底面。 第一触地板的底面和第二触地板的底面协调地限定一个平面。 当飞行器飞行时，平面相对于水平面成一定角度。 当飞行器在水平面上着陆时，平面平行于水平面，主体相对于水平面成角度。

公开(公告)号：US20160236346A1

公开(公告)日：2016-08-18

申请号：US14923442

申请日：2015-10-27

Applicant: Seoul National University R&DB Foundation

Inventor： DONG JUN LEE ,  HAI NGUYEN NGUYEN ,  SANGYUL PARK

IPC: B25J9/10 ,  B64C39/02 ,  B25J9/16

CPC classification number: B25J9/10 ,  B25J5/007 ,  B25J9/0087 ,  B25J9/162 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/128 ,  B64C2201/146

Abstract: A multi-link type working apparatus moved by a thrust generating device is provided. The multi-link type working apparatus performs a work by moving a link apparatus, in which a plurality of links are connected by at least one joint, by using the thrust generating device. The multi-link type working apparatus moved by a thrust generating device may variously expand lengths of links, the number of links, and the freedom of movement by using the thrust generating device as an actuator for moving the links, compared to a general multi-link type working apparatus that uses a motor or a hydraulic cylinder as an actuator.

Abstract translation: 提供了一种由推力发生装置移动的多连杆式作业装置。 多连杆式工作装置通过使用推力发生装置移动其中多个连杆通过至少一个接头连接的连杆装置进行工作。 通过推力发生装置移动的多连杆式加工装置可以通过使用推力发生装置作为用于移动连杆的致动器来不同地扩展连杆的长度，连杆数量和移动自由度， 使用电动机或液压缸作为致动器的连杆式工作装置。

公开(公告)号：US09415869B1

公开(公告)日：2016-08-16

申请号：US14670279

申请日：2015-03-26

Applicant: Amazon Technologies, Inc.

Inventor： Danny Chan ,  Eswarappa Channabasappa ,  Namhoon Kim ,  Tzung-I (Ian) Lee ,  Ulf Jan Ove Mattsson ,  Joseph Christopher Modro ,  Ming Zheng

IPC: B64C39/02 ,  G05D1/10 ,  G08G5/00 ,  G01S5/00

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2201/143 ,  G05D1/104 ,  G08G5/0052 ,  G08G5/0069

Abstract: A plurality of UAVs may be operated in a fleet, each of the UAVs in the fleet being configured to work collectively to achieve one or more functions, such as to create a display or implement an antenna array. The fleet of UAVs may operate individually and/or may be coupled to one another to operate as a collective unit. In some embodiments, one or more UAVs in the fleet may operate individually, while two or more UAVs in the fleet may be connected to one another. In such embodiments, the individual UAVs and the connected UAVs may together comprise the fleet.

Abstract translation: 多个UAV可以在车队中操作，车队中的每个UAV被配置为共同工作以实现一个或多个功能，例如创建显示器或实现天线阵列。 无人机的舰队可以单独操作和/或可以彼此耦合以作为集体单元操作。 在一些实施例中，车队中的一个或多个UAV可以单独操作，而车队中的两个或更多UAV可以彼此连接。 在这样的实施例中，各个UAV和连接的无人机可以在一起构成车队。

公开(公告)号：US09409645B1

公开(公告)日：2016-08-09

申请号：US14635492

申请日：2015-03-02

Applicant: GOOGLE INC.

Inventor： Clark Sopper ,  Adam Woodworth ,  Clayton Woodward Bavor, Jr.

IPC: B64C39/02 ,  H04L29/08

CPC classification number: B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/127 ,  H04L67/10 ,  H04N5/2222 ,  H04N7/142

Abstract: A mobile telepresence system may include a frame, a propulsion system operably coupled to the frame to propel the frame through a designated space, a screen movably coupled to the frame, and an image output device coupled to the frame. The frame may include a central body defining a longitudinal axis of the frame, a first arm at a first end portion of the central body, and a second arm at a second end portion of the central body, opposite the first end portion of the central body. The propulsion system may include rotors at opposite end portions of the first and second arms which propel the frame in response to an external command. The image output device may project an image onto the screen in response to an external command.

Abstract translation: 移动远程呈现系统可以包括帧，可操作地耦合到帧以推动帧通过指定空间的推进系统，可移动地耦合到帧的屏幕以及耦合到帧的图像输出设备。 框架可以包括限定框架的纵向轴线的中心体，位于中心体的第一端部处的第一臂和在中心体的第二端部处的第二臂，与第二臂相对的中心体的第一端部 身体。 推进系统可以包括在第一和第二臂的相对端部处的转子，其响应于外部命令推动框架。 图像输出装置可以响应于外部命令将图像投影到屏幕上。