公开(公告)号：US20160009370A1

公开(公告)日：2016-01-14

申请号：US14636019

申请日：2015-03-02

Applicant: AEROVIRONMENT, INC.

Inventor： Tony Shuo Tao ,  Nathan Olson ,  Carlos Thomas Miralles ,  Robert Nickerson Plumb

IPC: B64C3/56 ,  B64C5/12 ,  B64C9/02 ,  B64C39/02 ,  B64C9/18

CPC classification number: B64C3/56 ,  B64C3/44 ,  B64C3/50 ,  B64C5/12 ,  B64C9/02 ,  B64C9/08 ,  B64C9/18 ,  B64C11/00 ,  B64C13/18 ,  B64C13/34 ,  B64C39/024 ,  B64C2009/005 ,  B64C2201/021 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/121 ,  B64C2201/14 ,  B64C2201/145 ,  B64C2201/146

Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.

公开(公告)号：US20150321769A1

公开(公告)日：2015-11-12

申请号：US14715236

申请日：2015-05-18

Applicant: James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

IPC: B64D45/00 ,  B64D43/00

CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

Abstract translation: 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个都位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。

公开(公告)号：US08857312B2

公开(公告)日：2014-10-14

申请号：US13664195

申请日：2012-10-30

Applicant: Alliant Techsystems Inc.

Inventor： Kent C. Nelson ,  Kenneth Nash ,  Dennis C. Philpot

IPC: B64D7/06

CPC classification number: F41A19/08 ,  B64C2201/028 ,  B64C2201/121 ,  B64D7/06 ,  F41A19/58 ,  F41A19/59 ,  F41A23/005 ,  F41A23/20 ,  F41A25/12 ,  F41A25/22 ,  F41F3/06 ,  F41F3/065

Abstract: In some embodiments, an adapter for attaching a handheld firearm to an unmanned air vehicle comprises a mounting assembly configured for attachment to said firearm and to the unmanned air vehicle, and an actuation assembly comprising an actuation device configured to actuate a trigger of the handheld firearm.

Abstract translation: 在一些实施例中，用于将手持式火器附接到无人驾驶飞行器的适配器包括配置成附接到所述枪支和无人驾驶飞行器的安装组件，以及包括致动装置的致动组件，所述致动装置被配置为致动手持式枪械 。

公开(公告)号：US20140284422A1

公开(公告)日：2014-09-25

申请号：US13848443

申请日：2013-03-21

Applicant: Itzhak Sapir

Inventor： Itzhak Sapir

IPC: B64B1/00

CPC classification number: B64B1/24 ,  B64B1/40 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/121 ,  B64C2201/123

Abstract: A hovering surveillance device. An electronic imaging device is disposed on a housing having a primary lift element, at least one compressed lighter-than-air gas element, a pitch adjustment element, and, a steering element. The compressed lighter-than-air gas is channeled to the primary lift element and the pitch adjustment element to selectively vary the altitude and angle for the housing such that scene of interest may be imaged. The lighter-than-air gas may be selected from the group of helium, hydrogen, heated air, neon, ammonia, and methane.

Abstract translation: 悬停监视装置。 电子成像装置设置在具有主提升元件的壳体上，至少一个压缩的轻质空气气体元件，俯仰调节元件和转向元件。 压缩的轻型空气气体被引导到主提升元件和俯仰调节元件以选择性地改变壳体的高度和角度，使得可以对感兴趣的场景进行成像。 轻于空气的气体可以选自氦气，氢气，加热空气，氖气，氨气和甲烷。

公开(公告)号：US20140150631A1

公开(公告)日：2014-06-05

申请号：US13664195

申请日：2012-10-30

Applicant: Alliant Techsystems Inc.

Inventor： Kent C. Nelson ,  Kenneth Nash ,  Dennis C. Philpot

IPC: F41A19/08 ,  F41A23/20 ,  B64D7/06 ,  F41A23/00

CPC classification number: F41A19/08 ,  B64C2201/028 ,  B64C2201/121 ,  B64D7/06 ,  F41A19/58 ,  F41A19/59 ,  F41A23/005 ,  F41A23/20 ,  F41A25/12 ,  F41A25/22 ,  F41F3/06 ,  F41F3/065

Abstract: In some embodiments, an adapter for attaching a handheld firearm to an unmanned air vehicle comprises a mounting assembly configured for attachment to said firearm and to the unmanned air vehicle, and an actuation assembly comprising an actuation device configured to actuate a trigger of the handheld firearm.

Abstract translation: 在一些实施例中，用于将手持式火器附接到无人驾驶飞行器的适配器包括配置成附接到所述枪支和无人驾驶飞行器的安装组件，以及包括致动装置的致动组件，所述致动装置被配置为致动手持式枪械 。

公开(公告)号：US08314374B2

公开(公告)日：2012-11-20

申请号：US11455709

申请日：2006-06-20

Applicant: Burak Uzman

Inventor： Burak Uzman

IPC: F41G7/20 ,  F41G7/24 ,  F41G7/30

CPC classification number: F42B12/365 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/122 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  F41G7/30 ,  F42B15/01 ,  F42B15/10 ,  G05D1/0038

Abstract: A lightweight, man-portable weapon delivery system includes a fuselage, and first and second wings mounted to opposing sides of the fuselage. The system includes an electric motor for driving a propeller for providing thrust to propel the system. The electric motor is mounted to the fuselage, and configured to be remotely started by a user. The system includes an imaging device mounted to the system and configured to capture images of a theater of operations of the system. The system includes a communication circuit in communication with the imaging device and configured to transmit the images from the imaging device to the user for viewing the theater of operations of the system for remotely steering the system. The communication circuit is configured to receive commands from the user for steering the system into the target. The system includes a payload configured to store the ordnance.

Abstract translation: 轻便的便携式武器传送系统包括机身，以及安装在机身相对两侧的第一和第二翼。 该系统包括用于驱动螺旋桨以提供推力以推动系统的电动马达。 电动机安装在机身上，并被配置为由用户远程启动。 该系统包括安装到系统并被配置为捕获系统的操作剧场的图像的成像装置。 该系统包括与成像装置通信的通信电路，并且被配置为将图像从成像装置传输到用户，以观看用于远程转向系统的系统的操作剧场。 通信电路被配置为从用户接收命令以将系统转向目标。 系统包括配置为存储军械的有效载荷。

公开(公告)号：US08297172B2

公开(公告)日：2012-10-30

申请号：US12269731

申请日：2008-11-12

Applicant: Kent C. Nelson ,  Kenneth Nash ,  Dennis C. Philpot

Inventor： Kent C. Nelson ,  Kenneth Nash ,  Dennis C. Philpot

IPC: B64D7/06

CPC classification number: F41A19/08 ,  B64C2201/028 ,  B64C2201/121 ,  B64D7/06 ,  F41A19/58 ,  F41A19/59 ,  F41A23/005 ,  F41A23/20 ,  F41A25/12 ,  F41A25/22 ,  F41F3/06 ,  F41F3/065

Abstract: In some embodiments, an adapter for attaching a handheld firearm to an unmanned air vehicle comprises a mounting assembly configured for attachment to said firearm and to the unmanned air vehicle, and an actuation assembly comprising an actuation device configured to actuate a trigger of the handheld firearm.

Abstract translation: 在一些实施例中，用于将手持式火器附接到无人驾驶飞行器的适配器包括配置成附接到所述枪支和无人驾驶飞行器的安装组件，以及包括致动装置的致动组件，所述致动装置被配置为致动手持式枪械 。

公开(公告)号：US20090212157A1

公开(公告)日：2009-08-27

申请号：US11616201

申请日：2006-12-26

Applicant: Paul E. Arlton ,  David J. Arlton

Inventor： Paul E. Arlton ,  David J. Arlton

IPC: G05D1/00 ,  B64F1/04 ,  B64C9/00 ,  H02J7/00

CPC classification number: 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

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20070023570A1

公开(公告)日：2007-02-01

申请号：US11192171

申请日：2005-07-29

Applicant: Charles Bernard

Inventor： Charles Bernard

IPC: B64C13/00

CPC classification number: B64C13/20 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/121 ,  B64C2201/128 ,  B64C2201/145 ,  B64C2201/146 ,  B64C2201/167 ,  B64D39/00 ,  G05D1/0027

Abstract: An aircraft attack interdiction system using an unmanned interdiction aircraft piloted using a remote control system. In-flight refueling system, weapons launcher systems and intelligence gathering equipment are mounted on the interdiction aircraft. A remote flight control operator to remotely fly the interdiction aircraft can be based on a remote flight control commander aircraft that can be flown at safe distances from targets that are attacked by the interdiction aircraft.

Abstract translation: 使用遥控系统驾驶的无人拦截飞机的飞机攻击拦截系统。 飞机上的加油系统，武器发射系统和情报搜集设备都安装在拦截飞机上。 远程飞行拦截飞机的远程飞行控制操作员可以基于远程飞行控制指挥员飞机，该飞机可以在距离被拦截飞机攻击的目标的安全距离处飞行。

公开(公告)号：US20050051667A1

公开(公告)日：2005-03-10

申请号：US10499530

申请日：2002-12-19

Applicant: Paul Arlton ,  David Arlton

Inventor： Paul Arlton ,  David Arlton

IPC: B64C27/10 ,  B64C39/02 ,  B64C27/00

CPC classification number: 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

Abstract: A flying micro-rotorcraft unit (18, 24, 310, 330, 370) is provided for remote tactical and operational missions. The unit (18, 24, 310, 330, 370) includes an elongated body (52) having an upper and a lower end. The body (52) defines a vertical axis (60). The unit (18, 24, 310, 330, 370) further includes a navigation module (54) including means for determining a global position of the elongated body (52) during flight of the unit (18, 24, 310, 330, 370). Rotor means of the unit (18, 24, 310, 330, 370) is coupled to the upper end of the elongated body (52) for generating a thrust force that acts in a direction parallel to the vertical axis (60) to lift the elongated body (52) into the air. The rotor means is located between the elongated body (52) and the navigation module (54).

Abstract translation: 飞行的微型旋翼航空器（18,24,310,330,370）用于远程战术和作战任务。 单元（18,24,310,330,370）包括具有上端和下端的细长主体（52）。 主体（52）限定垂直轴线（60）。 该单元（18,24,310,330,370）还包括导航模块（54），该导航模块（54）包括用于在单元（18,24,310,330,370）的飞行期间确定细长主体（52）的全局位置的装置 ）。 单元（18,24,310,330,370）的转子装置联接到细长主体（52）的上端，用于产生沿平行于垂直轴线（60）的方向作用的推力，以提升 细长的主体（52）进入空气。 转子装置位于细长主体（52）和导航模块（54）之间。