公开(公告)号：KR101914305B1

公开(公告)日：2018-11-01

申请号：KR1020127009072

申请日：2010-09-09

Applicant: 에어로바이론먼트, 인크.

Inventor： 미랄레스,카로스토마스 ,  프럼브,닉 ,  타우,슈요 ,  올센,나탄

IPC: B64C9/34 ,  B64C13/18 ,  B64C13/28 ,  B64C3/44 ,  B64C3/50 ,  B64C3/56 ,  B64C39/02 ,  B64C5/12 ,  B64C9/02 ,  B64C9/00

CPC classification number: B64C13/28 ,  B64C3/44 ,  B64C3/50 ,  B64C3/56 ,  B64C5/12 ,  B64C9/02 ,  B64C9/08 ,  B64C9/18 ,  B64C11/00 ,  B64C13/18 ,  B64C39/024 ,  B64C2009/005 ,  B64C2201/021 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/121 ,  B64C2201/14 ,  B64C2201/145 ,  B64C2201/146

Abstract: 본발명은, 동체하우징편향액츄에이터혼(621, 622)을대향하는탄성장착된트레일링에지를가진에어포일(141, 142, 1345, 1346)을통해키놀이, 옆놀이, 및/또는빗놀이를제어하도록구성된항공기또는무인항공기(UAV)(100, 400, 1000, 1500)를포함하는시스템에관한것이다. 실시형태들은, 회전가능하게부착되며이펙터부재(1049, 1149, 1249, 1349)에의해작동될수 있는하나이상의방향타요소(1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546)를포함하고, 상기이펙터부재는동체하우징(1001) 내에배치되며, 하나이상의방향타요소들과맞물리도록일부신장가능하다.

公开(公告)号：KR20180040160A

公开(公告)日：2018-04-19

申请号：KR20187009629

申请日：2010-02-02

Applicant: 에어로바이론먼트, 인크.

Inventor： MIRALLES CARLOS

IPC: F41G7/00 ,  B64C13/20 ,  F41G7/22 ,  F41G9/00 ,  F42B15/01 ,  G08G5/00

CPC classification number: F41G7/2246 ,  B64C39/024 ,  B64C2201/121 ,  B64C2201/141 ,  F41G7/008 ,  F41G7/2206 ,  F41G7/2253 ,  F41G7/2293 ,  F41G9/002 ,  G05D1/0094 ,  G05D1/12 ,  G08G5/0069

Abstract: 시스템은업링크신호(451) 및/또는장면변화의자발적인결정에응답하여, 터미널호밍모드(510)로부터타겟서치모드(530)로트랜지션되도록구성된무인항공기(UAV)(100)를포함한다.

公开(公告)号：KR1020170061510A

公开(公告)日：2017-06-05

申请号：KR1020150166656

申请日：2015-11-26

Applicant: 국방과학연구소

Inventor： 한승조 ,  홍종태

IPC: F41G9/02 ,  F41G7/22 ,  F42B10/60 ,  F42B15/01 ,  B64C39/02 ,  B64D1/06 ,  B64D45/00

CPC classification number: F41G9/02 ,  B64C39/024 ,  B64C2201/121 ,  B64C2201/146 ,  B64D1/06 ,  B64D45/00 ,  F41G7/22 ,  F42B10/60 ,  F42B15/01

Abstract: 본발명은, 공중에서표적정보를획득하는무인비행체; 및상기무인비행체의내부에분리가능하게장착되는적어도하나이상의지능자탄을포함하고, 상기지능자탄은,날개와상기날개를구동하는로터를구비하는지능자탄몸체; 및분리명령에의해상기지능자탄이상기무인비행체로부터분리될때, 상기지능자탄몸체로부터방출시킨상기로터를구동시켜, 표적과기설정된거리이내까지진입되도록하는구동부를포함하는것을특징으로하는지능자탄투하시스템을제공한다.

公开(公告)号：US20230382527A1

公开(公告)日：2023-11-30

申请号：US17824592

申请日：2022-05-25

Applicant: Neil Buttermore

Inventor： Neil Buttermore

IPC: B64D1/04 ,  B64C39/02 ,  B64D5/00

CPC classification number: B64D1/04 ,  B64C39/024 ,  B64D5/00 ,  B64C2201/121

Abstract: Embodiments of a payload attachment system secure a payload to a wing or fuselage of the drone 102 (or another type of aircraft) using one or more vacuum mounting modules, wherein each vacuum mounting module comprises at least one vacuum pump controllably coupled to a microcontroller, a vacuum cup fluidly coupled to the at least one vacuum pump, and a transceiver that receives an instruction corresponding to one of a vacuum cup actuation signal or a vacuum cup release signal.

公开(公告)号：US20230141493A1

公开(公告)日：2023-05-11

申请号：US17983384

申请日：2022-11-08

Applicant: Autoflight (Kunshan) Co., Ltd.

Inventor： Yu Tian

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/121 ,  B64C2201/104

Abstract: A device for unmanned aerial vehicle to deploy a rainfall catalytic bomb deploy which comprises an unmanned aerial vehicle, a cannonball for artificial precipitation and a cylinder, wherein the unmanned aerial vehicle is connected with the cannonball for artificial precipitation through a soft lock, the cannonball for artificial precipitation are multiple and are wrapped in the cylinder, a second sensor is arranged in the cylinder wing surfaces are arranged on the other side of the cylinder, the wing surfaces are multiple and are arranged at one end of the cylinder in the long shaft direction, and one end of the soft lock is connected to the other end of the cylinder in the long shaft direction.

公开(公告)号：US20180186453A1

公开(公告)日：2018-07-05

申请号：US15395193

申请日：2016-12-30

Applicant: Critical Solutions International, Inc.

Inventor： Arnis Mangolds ,  Benjamin Harris ,  Scott Ogle ,  Tyler Sammis

IPC: B64D1/06 ,  B64C39/02 ,  F42B3/093

CPC classification number: B64D1/06 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/121 ,  F42B3/093

Abstract: An unmanned aerial vehicle line charge deployment system includes an unmanned aerial vehicle, a payload bay mounted beneath the unmanned aerial vehicle, and a line charge release subsystem coupled to the payload bay. A first line charge release mechanism releasably secures a first portion of a line charge to the unmanned aerial vehicle payload bay and a second line charge release mechanism, independent from the first line charge release mechanism, releasably secures a second portion of the line charge to the unmanned aerial vehicle payload bay.

公开(公告)号：US09983581B1

公开(公告)日：2018-05-29

申请号：US15705027

申请日：2017-09-14

Applicant: SparkCognition, Inc.

Inventor： Syed Mohammad Amir Husain ,  John Rutherford Allen

IPC: G05D1/00 ,  B64C39/02 ,  H04N7/18

CPC classification number: G05D1/0038 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/121 ,  B64C2201/141 ,  B64C2201/146 ,  G05D1/0027 ,  G05D1/0088 ,  H04N7/18 ,  H04N7/181

Abstract: A method and system comprises a plurality of electronically controlled distributed devices and a supervisory node. The supervisory node comprises a communications interface, a processor, and a display. The supervisory node is configured to communicate with the plurality of electronically controlled distributed devices via the communications interface. The supervisory node is adapted to receive sensor information, to receive functionality information and device status information, to determine useful life prognostics from the functionality information, to obtain human defined policy and strategy directives, to assess the useful life prognostics and device status information based on the human defined policy and strategy directives to provide device assessments, to construct device commands for the plurality of electronically controlled distributed devices based on the device assessments using the processor, and to communicate the device commands to the plurality of electronically controlled distributed via the communications interface.

公开(公告)号：US09844990B2

公开(公告)日：2017-12-19

申请号：US15422252

申请日：2017-02-01

Applicant: National Technology & Engineering Solutions of Sandia, LLC

Inventor： Clinton G. Hobart ,  William D. Morse ,  Robert James Bickerstaff

IPC: B64C39/02 ,  B60F5/02 ,  B60F3/00 ,  B60F5/00 ,  B63G8/00 ,  B63G8/08 ,  B64C37/00 ,  B64D47/08

CPC classification number: B60F5/02 ,  B60F3/0007 ,  B60F3/003 ,  B60F5/006 ,  B63G8/001 ,  B63G8/08 ,  B63G2008/004 ,  B64C37/00 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/021 ,  B64C2201/028 ,  B64C2201/082 ,  B64C2201/121 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2211/00 ,  B64D47/08

Abstract: A MEUV that is able to navigate aerial, aquatic, and terrestrial environments through the use of different mission mobility attachments is disclosed. The attachments allow the MEUV to be deployed from the air or through the water prior to any terrestrial navigation. The mobility attachments can be removed or detached by and from the vehicle during a mission.

公开(公告)号：US09751597B1

公开(公告)日：2017-09-05

申请号：US14700958

申请日：2015-04-30

Applicant: Lockheed Martin Corporation

Inventor： Nathan E. Low ,  Peter J. Demas

IPC: B63B35/00 ,  B63B25/00 ,  B64C39/02

CPC classification number: B63B25/002 ,  B63B35/00 ,  B63H11/00 ,  B63H2011/006 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/121

Abstract: A water-propelled or water-powered unmanned aerial vehicle including a base configured to carry a payload, and at least one nozzle attached thereto. The at least one nozzle is configured to selectively receive pressurized fluid from a source located remotely from the vehicle. The vehicle includes a control system configured to alter or otherwise selectively dictate the flow of fluid through the at least one nozzle and/or the orientation of the at least one nozzle with respect to the base in response to a received control signal for providing controlled unmanned vehicle flight.

公开(公告)号：US20170139416A1

公开(公告)日：2017-05-18

申请号：US15355014

申请日：2016-11-17

Applicant: AeroVironment, Inc.

Inventor： William J. Nicoloff ,  Eric M. Sornborger ,  Lars B. Cremean

IPC: G05D1/00 ,  B64D47/08 ,  B64C9/00 ,  B64C39/02

CPC classification number: G05D1/0094 ,  B64C9/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/14 ,  B64D47/08 ,  F41G7/2253 ,  F41G7/2293 ,  F41G7/30

Abstract: An aircraft including a wing system, a plurality of control surfaces, a camera mounted on a camera pod, and a control system. The camera pod is configured to vary the orientation of the camera field of view only in yaw, relative to the aircraft, between a directly forward-looking orientation and a side-looking orientation. The control system controls the control surfaces such that they induce a significant aircraft yaw causing an identified target to be within the field of view of the camera with the camera in the directly forward-looking orientation.