公开(公告)号：EP2664945A1

公开(公告)日：2013-11-20

申请号：EP12382178.7

申请日：2012-05-15

Applicant: The Boeing Company

Inventor： Scarlatti, David ,  Esteban-Campillo, David ,  Garcia, Javier

IPC: G01V1/16 ,  F42B12/36

CPC classification number: G01V1/168 ,  B64C27/51 ,  B64C27/68 ,  B64C39/02 ,  B64C2201/082 ,  B64C2201/123 ,  B64C2201/185 ,  F42B12/365 ,  G01V1/16 ,  G01V1/182

Abstract: The present invention relates to unattended ground sensors for detecting the presence of a pedestrian or vehicle in a monitored area using seismic sensors. Networks of simple and inexpensive sensors are disclosed that may be rapidly deployed from the air. Each ground sensor is provided with a rotor that slows the rate of descent of the ground sensor during deployment.

Abstract translation: 本发明涉及无人值守地面传感器，用于使用地震传感器来检测被监视区域中行人或车辆的存在。 公开了可以从空中快速部署的简单和便宜的传感器的网络。 每个地面传感器都设有一个转子，可在展开期间减慢地面传感器的下降速度。

公开(公告)号：EP1767912B1

公开(公告)日：2011-12-07

申请号：EP06126080.8

申请日：2001-12-20

Applicant: Honeywell International Inc.

Inventor： Wood, Roland, Andrew

IPC: G01J5/02 ,  G01J5/26 ,  B64C39/02 ,  H04N5/232

CPC classification number: H04N5/33 ,  B64C2201/123 ,  B64C2201/127 ,  G01J1/02 ,  G01J1/0219 ,  G01J1/04 ,  G01J1/0403 ,  G01J5/02 ,  G01J5/0205 ,  G01J5/0215 ,  G01J5/025 ,  G01J5/08 ,  G01J5/0806 ,  G01J5/522 ,  G01J2005/0048 ,  G01J2005/0077 ,  H04N5/2176 ,  H04N5/2251 ,  H04N5/361 ,  H04N5/3651

公开(公告)号：EP1799545B1

公开(公告)日：2009-07-01

申请号：EP05789189.7

申请日：2005-02-14

Applicant: RAYTHEON COMPANY

Inventor： CORDER, David, A. ,  KOESSLER, Jeffrey, H. ,  WEBB, George, R.

IPC: B64C39/02

CPC classification number: B64C3/56 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/165 ,  B64C2201/201

Abstract: An air-launched aircraft (10) includes deployable wings (16, 18), elevons (20, 22), and vertical fins (26, 28) that deploy from a fuselage (12) during flight. The aircraft may include a control system for operating the elevons, a communication system, and batteries for powering the systems. In addition, the aircraft may include a payload module (14) that mates with an interface in the fuselage. The payload module may include any of a variety of payloads, including cameras, sensors, and/or radar emitters. The aircraft may be powered or unpowered, and may be very small, for example, less than on the order of 10 kg (22 pounds). The deployable surfaces of the aircraft may be configured to deploy in a pre-determined order, allowing the aircraft automatically to enter controlled flight after being launched in a tumbling mode.

公开(公告)号：EP1713689A2

公开(公告)日：2006-10-25

申请号：EP04821333.4

申请日：2004-03-25

Applicant: The Insitu Group

Inventor： MCGEER, Brian T. ,  ROESELER, Cory ,  VON FLOTOW, Andreas

IPC: B64F1/06

CPC classification number: B64F1/06 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/084 ,  B64C2201/104 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/165

Abstract: Methods and apparatuses for launching unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft (150) can be launched from an apparatus that includes a launch carriage (120) that moves along a launch axis. A gripper (180) carried by the launch carriage can have at least one grip Portion (181) in contact with the aircraft while the launch carriage accelerates along the launch axis. The at least one grip portion can move out of contact with the fuselage of the aircraft as the launch carriage (120) decelerates, releasing the aircraft (150) for takeoff.

公开(公告)号：EP1193168B1

公开(公告)日：2006-05-10

申请号：EP01121573.8

申请日：2001-09-10

Applicant: Rafael Armament Development Authority Ltd.

Inventor： Yavnai, Arie

IPC: B62D57/032 ,  B62D57/04

CPC classification number: G05D1/0038 ,  B62D57/02 ,  B62D57/04 ,  B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165 ,  G05D1/0044

公开(公告)号：EP1384662B1

公开(公告)日：2005-06-15

申请号：EP03016348.9

申请日：2003-07-18

Applicant: C.R.F. Società Consortile per Azioni

Inventor： Perlo, Piero ,  Bollea, Denis ,  Finizio, Roberto ,  Carvignese, Cosimo ,  Balocco, Elena

IPC: B64C39/02 ,  B64C29/02

CPC classification number: B64C29/02 ,  B64C27/20 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165

公开(公告)号：EP1502852A1

公开(公告)日：2005-02-02

申请号：EP04017945.9

申请日：2004-07-29

Applicant: C.R.F. Società Consortile per Azioni

Inventor： Perlo, Pietro ,  Bollea, Denis ,  Pairetti, Bartolo ,  Alacqua, Stefano ,  Finizio, Roberto ,  Carvignese, Cosimo ,  Repetto, Piermario ,  Innocenti, Gianfranco

IPC: B64C27/20 ,  A63H29/22 ,  B64C39/02

CPC classification number: B64C39/024 ,  A63H27/12 ,  A63H29/22 ,  B64C27/20 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/146

Abstract: The flying machine (1) comprises

a supporting structure (2) including a central rotational support (3) having a vertical axis connected to an essentially horizontal, preferably annular, peripheral support part (4), coaxial with the central support (3),
at least one upper rotor (6) including a central hub (7) rotatable about the axis of the central support (3) of the supporting structure (2), an outer channel-section ring (8) supported by the peripheral part (4) of the supporting structure (2) by contactless suspension means (23-27), preferably magnetic suspension means, and a plurality of blades (9) which extend from the hub (7) to the channel-section ring (8) and which are inclined with respect to the horizontal plane; and
motor devices (40-43; 50-53) carried at least partially by the peripheral part (4) of the supporting structure (2) and operable to cause rotation of the rotor (6) with respect to this structure (2) in a predetermined direction.

Abstract translation: 飞行器（1）包括支撑结构（2），其包括中心旋转支撑件（3），该中心旋转支撑件具有连接到与中心支撑件（3）同轴的基本上水平的，优选环形的外围支撑部分（4）的垂直轴线， 至少一个上转子（6），包括可围绕所述支撑结构（2）的中心支撑件（3）的轴线旋转的中心毂（7），由所述周边部分（4）支撑的外通道部分环 ）由非接触式悬挂装置（23-27），优选磁悬浮装置和从轮毂（7）延伸到通道截面环（8）的多个叶片（9）支撑结构（2），并且 相对于水平面倾斜; 以及至少部分地由所述支撑结构（2）的周边部分（4）承载并可操作以使转子（6）相对于该结构（2）旋转的马达装置（40-43; 50-53） 预定的方向。

公开(公告)号：EP1384662A1

公开(公告)日：2004-01-28

申请号：EP03016348.9

申请日：2003-07-18

Applicant: C.R.F. Società Consortile per Azioni

Inventor： Perlo, Piero ,  Bollea, Denis ,  Finizio, Roberto ,  Carvignese, Cosimo ,  Balocco, Elena

IPC: B64C39/02 ,  B64C29/02

CPC classification number: B64C29/02 ,  B64C27/20 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165

Abstract: VTOL micro-aircraft comprising a first and a second ducted rotor (1, 2) mutually aligned and distanced according to a common axis and whose propellers (4, 6) are driven in rotation in mutually opposite directions. Between the two ducted rotors (1, 2) are positioned a fuselage (3) and a wing system (13) formed by wing profiles (10, 11) forming an X or an H configuration and provided with control flaps (16).

Abstract translation: 该VTOL微型飞机包括第一和第二管道转子（1,2），所述第一和第二管道转子（1,2）根据公共轴线相互对准和隔开，并且其螺旋桨（4,6）在相反方向上被驱动旋转。 在两个管道转子（1,2）之间定位有机翼（3）和由翼型材（10,11）形成的翼型系统（13），所述翼型型材形成X或H形并且设有控制翼片（16）。

公开(公告)号：PE13932017A1

公开(公告)日：2017-09-20

申请号：PE0013302017

申请日：2016-02-12

Applicant: ESCO CORP

Inventor： CARPENTER CRISTOPHER M ,  ZUENDEL KARSTEN D ,  HYDE STEVEN D ,  LANDER JAVIER ,  BETOURNAY JASON W

IPC: E02F3/00 ,  E02F9/26 ,  G08B23/00

CPC classification number: E02F9/26 ,  B64C39/024 ,  B64C2201/123 ,  E02F9/267 ,  E02F9/2825 ,  E02F9/2833 ,  E02F9/2841

Abstract: Un producto y sistema para identificar y monitorear una caracteristica que incluye la ID de la pieza, la presencia, la condicion, el uso y/o el funcionamiento de los productos de acondicionamiento del terreno usados en varios tipos de equipos de trabajo de movimiento de tierra.

公开(公告)号：KR102230107B1

公开(公告)日：2021-03-18

申请号：KR1020200104840A

申请日：2020-08-20

Applicant: 우대원

Inventor： 우대원

IPC: E01D22/00 ,  B64C39/02 ,  B66F3/24 ,  B66F3/46 ,  E01D19/04 ,  G01B11/00 ,  G01B11/02 ,  G01C11/02 ,  G01C11/36

CPC classification number: E01D22/00 ,  B64C39/024 ,  B66F3/24 ,  B66F3/46 ,  E01D19/04 ,  G01B11/002 ,  G01B11/022 ,  G01C11/02 ,  B64C2201/123 ,  G01C2011/36

Abstract: 본 발명은 수평 수직 변위 제어 교량 인상 방법 에 관한 것으로서, 더욱 상세하게는, 인상잭에 의해 교량 상부구조의 인상을 수행하면서 수평변위구속장치에 의해 교량 상부구조의 수평 이동을 제한하고, 드론 측량을 통해 교량 상부구조의 인상 시 변위를 측정하며, 측정된 상부구조의 변위에 따라 상부구조수평이동장치를 통해 교량 상부구조의 수평 이동을 수행하는 수평 수직 변위 제어 교량 인상 방법에 관한 것이다.