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    MANNED UNMANNED TEAMING (MUM-T) SYSTEM TO TRANSFORM IMAGE DATA BASED ON GEOGRAPHIC ORIENTATION
    83.
    发明申请
    MANNED UNMANNED TEAMING (MUM-T) SYSTEM TO TRANSFORM IMAGE DATA BASED ON GEOGRAPHIC ORIENTATION 审中-公开
    基于地理位置转换图像数据的曼德曼（MUM-T）系统

    公开(公告)号：US20170076159A1

    公开(公告)日：2017-03-16

    申请号：US15266886

    申请日：2016-09-15

    申请人： Sikorsky Aircraft Corporation

    发明人： Robert Pupalaikis ,  James S. Magson

    IPC分类号： G06K9/00 ,  G06T3/20 ,  G06T11/60 ,  G05D1/00 ,  H04N5/38 ,  B64C39/02 ,  B64D47/08 ,  G06T7/00 ,  G06K9/62

    CPC分类号： G06K9/00791 ,  B64C27/06 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/123 ,  B64C2201/146 ,  B64D47/08 ,  G05D1/0011 ,  G05D1/0094 ,  G05D1/104 ,  G06K9/0063 ,  G06K9/4671 ,  G06K9/6201 ,  G06K2009/4666 ,  G06T3/0006 ,  G06T11/60

    摘要： A manned unmanned teaming (MUM-T) image system includes an unmanned vehicle (UV) configured to travel in a first heading and includes at least one sensor configured to capture at least one image having a first visual orientation pursuant to the first heading. The MUM-T image system generates image data indicative of the at least one image. A manually operated vehicle (MOV) in signal communication with the UV is configured to travel in a second heading. The MOV comprises an electronic image transformation module configured to receive the image data and to transform the image data into a second orientation different from the first orientation based on the second heading. An electronic display unit is configured to receive the transformed image data and to display the at least one image according to the second orientation.

    摘要翻译： 载人无人机组合（MUM-T）图像系统包括被配置为在第一航标中行进的无人驾驶车辆（UV），并且包括至少一个传感器，所述至少一个传感器被配置为捕获依照第一航标具有第一视觉定向的至少一个图像。 MUM-T图像系统产生指示至少一个图像的图像数据。 与UV信号通信的手动车辆（MOV）配置为在第二个航向运行。 MOV包括电子图像变换模块，被配置为接收图像数据并且基于第二标题将图像数据变换成与第一取向不同的第二取向。 电子显示单元被配置为接收变换的图像数据并根据第二取向显示至少一个图像。

    METHOD OF REGULATING A THREE-ENGINED POWER PLANT FOR A ROTARY WING AIRCRAFT
    84.
    发明申请
    METHOD OF REGULATING A THREE-ENGINED POWER PLANT FOR A ROTARY WING AIRCRAFT 审中-公开
    调整用于旋转式飞机的三座发电厂的方法

    公开(公告)号：US20170066541A1

    公开(公告)日：2017-03-09

    申请号：US15175269

    申请日：2016-06-07

    申请人： AIRBUS HELICOPTERS

    发明人： Regis ROSSOTTO

    IPC分类号： B64D31/06 ,  B64D35/08 ,  B64C27/06

    CPC分类号： B64D31/06 ,  B64C27/06 ,  B64C27/12 ,  B64D35/08 ,  F02C6/206 ,  F02C9/42 ,  F05D2220/329 ,  Y02T50/671

    摘要： A power plant comprising two engine groups and a main power transmission gearbox. Each engine group drives the main gearbox mechanically in order to rotate a main rotor of an aircraft at a frequency of rotation NR. A first engine group comprising two main engines is regulated on a first setpoint NR* for the frequency of rotation NR, while a second engine group comprising a secondary engine is regulated on a second setpoint W2* for power. The second setpoint W2* for power is determined so that each secondary engine operates only when a flight power Wvol necessary for the flight of the aircraft is greater than the sum of the main maximum powers WMax1 from each main engine.

    摘要翻译： 一个发电厂，包括两个发动机组和一个主动力传动齿轮箱。 每个发动机组以机械方式驱动主变速箱，以便以旋转频率NR旋转飞行器的主转子。 包括两个主发动机的第一发动机组在第一设定点NR *上针对旋转频率NR进行调节，而包括二次发动机的第二发动机组被调节在第二设定点W2 *上用于动力。 确定功率的第二设定点W2 *，使得每个次级发动机仅在飞行器飞行所需的飞行功率Wvol大于来自每个主发动机的主最大功率WMax1的总和时才起作用。

    ROTOR WIRELESS LOAD AND MOTION MONITORING SENSOR NETWORK
    85.
    发明申请
    ROTOR WIRELESS LOAD AND MOTION MONITORING SENSOR NETWORK 审中-公开
    转子无线负载和运动监控传感器网络

    公开(公告)号：US20170050745A1

    公开(公告)日：2017-02-23

    申请号：US15301104

    申请日：2015-03-26

    申请人： Sikorsky Aircraft Corporation

    发明人： Sanjay Bajekal ,  Brian Dean Bouquillon ,  Cagatay Tokgoz

    IPC分类号： B64D45/00 ,  B64C27/06 ,  G07C5/08

    CPC分类号： B64D45/0005 ,  B64C27/008 ,  B64C27/06 ,  B64D2045/0085 ,  G07C5/0841 ,  H04Q9/00 ,  H04Q2209/40

    摘要： A method of data collection from a rotor system of an aircraft includes positioning a plurality of sensors at a plurality of locations of a rotating portion of the rotor system. One or more antennae are located at one or more rotationally fixed locations of the aircraft. Rotor system data is collected via the sensors and is wirelessly transmitted from the sensors to the antennae and is transferred from the antennae to a gateway where it is normalized and synchronized. In another embodiment, a data collection system for a rotor includes a plurality of sensors located at rotating locations of the rotor, the sensors configured to collect and wirelessly transmit rotor data. Antennae are located at a fixed location of the aircraft. The antennae are configured to send and receive data from the sensors. A gateway is connected to the antennae to normalize and synchronize the rotor data.

    摘要翻译： 从飞行器的转子系统收集数据的方法包括在转子系统的旋转部分的多个位置处定位多个传感器。 一个或多个天线位于飞机的一个或多个旋转固定位置。 转子系统数据通过传感器收集，并从传感器无线传输到天线，并从天线传送到网关，在那里它被归一化和同步。 在另一个实施例中，用于转子的数据收集系统包括位于转子旋转位置处的多个传感器，该传感器配置成收集和无线传送转子数据。 天线位于飞机的固定位置。 天线被配置为从传感器发送和接收数据。 网关连接到天线以使转子数据归一化和同步。

    Coaxial counter-rotating rotor system
    88.
    发明授权
    Coaxial counter-rotating rotor system 有权
    同轴反转转子系统

    公开(公告)号：US09169012B2

    公开(公告)日：2015-10-27

    申请号：US13401110

    申请日：2012-02-21

    申请人： John Corrigan ,  Frank Bradley Stamps

    发明人： John Corrigan ,  Frank Bradley Stamps

    IPC分类号： B64C27/08 ,  B64C27/52 ,  B64C27/10

    CPC分类号： B64C27/82 ,  B64C27/06 ,  B64C27/10 ,  B64C27/14 ,  B64C27/32 ,  B64C27/52 ,  B64C27/57 ,  B64C27/64 ,  B64C2027/8227

    摘要： A system and method to tilt coaxial counter-rotating rotor hub assemblies relative to a fuselage. The system includes a first rotor hub assembly and a second rotor hub assembly spaced apart from the first hub assembly and carried by the fuselage. The method includes pivotally attaching the first rotor hub assembly and the second rotor hub assembly to a pivot joint and thereafter tilting the first rotor hub assembly and the second rotor hub assembly about the pivot joint with a driver.

    摘要翻译： 相对于机身倾斜同轴反转转子毂组件的系统和方法。 该系统包括第一转子轮毂组件和与第一轮毂组件间隔开并由机身承载的第二转子轮毂组件。 该方法包括将第一转子轮毂组件和第二转子轮毂组件枢转地连接到枢转接头，然后使用驱动器使第一转子轮毂组件和第二转子轮毂组件围绕枢转接头倾斜。

    VEHICLE
    89.
    发明申请
    VEHICLE 有权
    车辆

    公开(公告)号：US20140291440A1

    公开(公告)日：2014-10-02

    申请号：US14357075

    申请日：2012-11-09

    申请人： PAL-V EUROPE, N.V.

    发明人： Michael Alwin William Stekelenburg ,  Christiaan Cornelis Klok ,  Louis Petrus Valentijn Marie Van Rijn ,  Wouter Adriaan Soethoudt ,  Robert Christiaan Wegerif

    IPC分类号： B60F5/02 ,  B64C27/50 ,  B64C1/30

    CPC分类号： B60F5/02 ,  B64C1/063 ,  B64C1/26 ,  B64C1/30 ,  B64C27/02 ,  B64C27/06 ,  B64C27/50 ,  B64C37/00

    摘要： The present invention discloses a vehicle (1) capable of being converted between a flying condition and an automotive riding condition. The vehicle has a telescopically extendable tail (10) comprising a first tubular tail segment (11) and a second tail segment (12) disposed axially slideable within the first tubular tail segment. The tail is provided with at least two form-closing coupling members (21, 35; 31, 36) located at an axial distance (LI) from each other for providing a force-transferring coupling between the second tail segment (12) and the first tubular tail segment (11) in the extended state of the second tail segment (12), each of said form-closing coupling members (21, 35; 31, 36) capable of transferring torque and transverse forces, and each of said form-closing coupling members (21, 35; 31, 36) coming into engagement by axial displacement of the second tail segment (12) in the outward direction.

    摘要翻译： 本发明公开了一种能够在飞行状态和汽车行驶状态之间进行转换的车辆（1）。 车辆具有可伸缩地延伸的尾部（10），其包括第一管状尾部段（11）和第二尾部段（12），所述第二尾部段（12）可在第一管状尾部段内轴向滑动设置。 尾部设有至少两个位于彼此轴向距离（LI）处的形成 - 闭合联接构件（21,35; 31,36），用于在第二尾段（12）和 在第二尾段（12）的延伸状态下的第一管状尾部段（11），能够传递扭矩和横向力的每个所述成形 - 闭合联接构件（21,35; 31,36），以及每个所述形式 闭合联接构件（21,35; 31,36）通过第二尾段（12）沿向外的方向的轴向位移而接合。

    ASYMMETRICAL SINGLE MAIN ROTOR UNMANNED AERIAL VEHICLE
    90.
    发明申请
    ASYMMETRICAL SINGLE MAIN ROTOR UNMANNED AERIAL VEHICLE 有权
    不对称单主转子无人驾驶车

    公开(公告)号：US20140008486A1

    公开(公告)日：2014-01-09

    申请号：US13532212

    申请日：2012-06-25

    申请人： Mark R. Alber ,  Jessica Newman

    发明人： Mark R. Alber ,  Jessica Newman

    IPC分类号： B64C27/12 ,  B64C27/82 ,  B64C27/06

    CPC分类号： B64C27/12 ,  B64C27/06 ,  B64C27/82 ,  B64C39/024 ,  B64C2027/8218 ,  B64C2201/024

    摘要： A single engine rotary wing aircraft is provided including a fuselage having a longitudinal first axis. A main rotor assembly is mounted to the fuselage for rotation about a second axis, perpendicular to the first axis. A tailboom is connected to an empennage. The tailboom is mounted to an end of the fuselage such that the tailboom is laterally offset from the first axis in a first direction. The rotary wing aircraft also includes a propulsion system. The single engine of the propulsion system is laterally offset from the first axis in a second direction opposite the first direction.

    摘要翻译： 提供了包括具有纵向第一轴线的机身的单个发动机旋翼飞行器。 主转子组件安装到机身上以围绕垂直于第一轴线的第二轴线旋转。 尾巴连接到一个尾翼。 尾杆安装到机身的一端，使得尾杆在第一方向上从第一轴线横向偏移。 旋翼飞机还包括推进系统。 推进系统的单个发动机在与第一方向相反的第二方向上与第一轴线横向偏移。