公开(公告)号：EP3124381A1

公开(公告)日：2017-02-01

申请号：EP16190021.2

申请日：2014-12-11

Applicant: Korea Aerospace Research Institute

Inventor： LEE, Sang-Cherl ,  KIM, Hae-Dong ,  GONG, Hyeon-Cheol ,  CHOI, Gi-Hyuk ,  HWANG, In-Hee ,  SUK, Byong-Suk

IPC: B64C39/02 ,  B64F1/12 ,  B64F1/22

CPC classification number: B60L11/1824 ,  B60L2200/10 ,  B60L2230/10 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/182 ,  B64C2201/201 ,  B64D45/08 ,  B64F1/00 ,  B64F1/005 ,  B64F1/12 ,  B64F1/222 ,  F21S8/086 ,  F21V33/00 ,  F21W2131/103 ,  F21Y2115/10

Abstract: An apparatus for containing and charging an unmanned VTOL aircraft 300, comprising a post 200 placed on a ground and at least one lateral fastening hole 210 formed in a side of the post, and configured such that a pole 340 of the unmanned VTOL aircraft is inserted and fastened into the lateral fastening hole, wherein an entrance of the lateral fastening hole is formed in a cone shape, and thus the pole of the unmanned VTOL aircraft is easily inserted into the lateral fastening hole during fastening of the unmanned VTOL aircraft. The lateral fastening hole is further configured such that target- and cross-shaped LED/IR lights are lit in order to guide the unmanned VTOL aircraft through automatic insertion via vision of the unmanned VTOL aircraft.

Abstract translation: 得到的装置用于容纳和无人驾驶垂直起落飞机300的充电，其包括一个柱200放置在地面和在所述柱的侧面的至少一个侧面的固定210形成，并且配置的搜索做了无人驾驶垂直起落飞机的极340被插入 紧固并进入横向紧固孔，worin在横向紧固孔的入口的圆锥形状是形成，因此无人垂直起落飞机的极无人驾驶垂直起落飞机的紧固过程中容易地插入到所述横向紧固孔。 横向紧固孔被构造进一步调查做靶和交叉形的LED / IR灯，以便经由无人垂直起落飞机的视力通过自动插入引导无人驾驶垂直起落飞机点亮。

公开(公告)号：EP2974958A3

公开(公告)日：2016-04-13

申请号：EP14197368.5

申请日：2014-12-11

Applicant: Korea Aerospace Research Institute

Inventor： Lee, Sang-Cherl ,  Kim, Hae-Dong ,  Gong, Hyeon-Cheol ,  Choi, Gi-Hyuk ,  Hwang, In-Hee ,  Suk, Byong-Suk

IPC: B64C39/02 ,  B64F1/12 ,  B64F1/22

CPC classification number: B60L11/1824 ,  B60L2200/10 ,  B60L2230/10 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/182 ,  B64C2201/201 ,  B64D45/08 ,  B64F1/00 ,  B64F1/005 ,  B64F1/12 ,  B64F1/222 ,  F21S8/086 ,  F21V33/00 ,  F21W2131/103 ,  F21Y2115/10

Abstract: An apparatus and method for containing and charging an unmanned VTOL aircraft are disclosed. The apparatus for containing and charging an unmanned VTOL aircraft includes a post 110, an extended member 120, a cover 130, a fastening unit 140, and a charging unit 150. The post is placed on a ground. The extended member is connected to the post. The cover is provided on the extended member, and is configured to be opened or closed in order to contain and protect the unmanned VTOL aircraft. The fastening unit is provided in the cover, and is configured to fasten the unmanned VTOL aircraft. The charging unit is provided in the fastening unit, and is configured to charge the unmanned VTOL aircraft.

Abstract translation: 用于容纳和无人垂直起落飞机的充电的装置和方法是游离缺失盘。 用于容纳和无人垂直起落飞机的充电的装置，包括：延伸件120上的柱110，一个盖130，紧固单元140和所述柱在地面上放置的充电单元150。 延伸件连接到所述后，提供所述延伸件上的盖，并且被配置以容纳和保护无人垂直起落飞机，以被打开或关闭。 所述紧固单元设置在所述盖中设置，并且被配置来紧固无人驾驶垂直起落飞机。 充电单元设置在所述紧固单元中提供，并且被配置为充电无人垂直起落飞机。

公开(公告)号：EP2766260A4

公开(公告)日：2015-07-01

申请号：EP11874051

申请日：2011-10-12

Applicant: SAAB AB

Inventor： DANIELSSON TORKEL

IPC: B64F1/02 ,  B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/084 ,  B64C2201/182 ,  B64C2201/201

公开(公告)号：EP2799332A2

公开(公告)日：2014-11-05

申请号：EP14002518.0

申请日：2005-04-14

Applicant: Arlton, Paul E. ,  Arlton, David J.

Inventor： Arlton, Paul E. ,  Arlton, David J.

IPC: B64C27/10 ,  B64C27/22 ,  B64C39/02

CPC classification number: B64C27/10 ,  B64C27/22 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2201/205

Abstract: A rotary wing vehicle (1) includes a body structure having an elongated tubular backbone or core (40), and a counter-rotating coaxial rotor system (3, 5) having rotors with each rotor having a separate motor (54, 61) to drive the rotors about a common rotor axis of rotation (7), The rotor system is used to move the rotary wing vehicle (1) in directional flight.

Abstract translation: 旋翼机（1）包括具有细长管状骨架或芯（40）的本体结构和具有转子的反向旋转同轴转子系统（3,5），每个转子具有单独的电机（54,61） 驱动转子围绕共同的转子旋转轴（7）。转子系统用于在定向飞行中移动旋翼机（1）。

公开(公告)号：EP2354000B1

公开(公告)日：2012-07-04

申请号：EP11290030.3

申请日：2011-01-19

Applicant: MBDA France

Inventor： Jaurand, Benoît

IPC: B64D1/10 ,  B64D1/12 ,  B64D1/02

CPC classification number: B64D1/02 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/201 ,  B64C2201/206

Abstract: The system (1) an external container (15) fixed in a cargo compartment of a transport aircraft (AC). An internal container (4) is arranged in the external container to bring the internal container from a position in which the internal container is entirely located inside the external container to another position (P2) in which the internal container is shifted toward a rear side of the aircraft with respect to the former position such that a release part (7) of the internal container is located outside the aircraft through an opening (8) at a rear side of the compartment.

公开(公告)号：EP1594736A4

公开(公告)日：2010-02-24

申请号：EP04809283

申请日：2004-02-19

Applicant: AAI CORP

Inventor： MILLER STEPHEN W ,  VELAZQUEZ MATTHEW T

IPC: B64B20060101 ,  B64B1/00 ,  B64C3/56 ,  B64C39/02 ,  B64F1/04 ,  B64F1/06

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64F1/06

公开(公告)号：EP2103518A2

公开(公告)日：2009-09-23

申请号：EP09153384.4

申请日：2009-02-21

Applicant: Honeywell International Inc.

Inventor： Goossen, Emray R. ,  Sheoran, Yogendra Y.

IPC: B64F1/04

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/088 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/205 ,  B64C2201/208 ,  B64F1/04

Abstract: A launch and capture system for capturing a vertical take-off and landing (VTOL) vehicle having a thruster (104) and a duct (106) configured to direct airflow generated by the thruster includes a capture plate (120) and an extension (122). The capture plate is configured to alter the airflow and generate a force attracting the duct to the capture plate. The extension is coupled to the capture plate, and is configured to at least facilitate holding the VTOL vehicle against the capture plate.

Abstract translation: 用于捕获具有推进器（104）和构造成引导由推进器产生的气流的管道（106）的垂直起飞和着陆（VTOL）车辆的发射和捕获系统包括捕获板（120）和延伸部（122） ）。 捕获板被配置为改变气流并产生吸引到捕获板的管道的力。 延伸部联接到捕获板，并且被构造成至少有利于将VTOL车辆保持抵靠捕获板。

公开(公告)号：EP1827972B1

公开(公告)日：2008-09-10

申请号：EP05813078.2

申请日：2005-11-30

Applicant: ISRAEL AIRCRAFT INDUSTRIES, LTD.

Inventor： SIRKIS, Omri

IPC: B64C9/18 ,  B64C39/02

CPC classification number: B64C39/024 ,  B64C9/18 ,  B64C2201/021 ,  B64C2201/028 ,  B64C2201/084 ,  B64C2201/104 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/185 ,  B64C2201/187 ,  B64C2201/201

Abstract: A method for landing a fixed wing aircraft is provided in which an inversion maneuver is performed so that the aircraft's back is facing the ground, and the aircraft's underside is facing away from the ground. After initiation or completion of this maneuver, deep stall is induced, and the aircraft descends almost vertically to land on its upper side, thus minimizing impact loads or damage on its underside. In a particular aerodynamic arrangement configured for carrying out the method, a flap (24), which may be stowed during normal flight, is deployed in a manner such as to aerodynamically induce a negative pitching moment on the aircraft and deep stall.

公开(公告)号：EP1687200A2

公开(公告)日：2006-08-09

申请号：EP04810203.2

申请日：2004-11-01

Applicant: The Insitu Group, Inc.

Inventor： SLIWA, Steven, M. ,  VON FLOTOW, Andreas, H. ,  DENNIS, Brian, D.

IPC: B63H1/00

CPC classification number: B64C11/003 ,  A63H27/02 ,  B64C11/04 ,  B64C11/14 ,  B64C11/28 ,  B64C39/024 ,  B64C2201/044 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/206 ,  B64D41/007 ,  F02K5/023 ,  F05D2260/85 ,  Y02T50/44 ,  Y02T50/672

Abstract: Methods and systems for starting propeller driven aircraft and other devices are disclosed. A system in accordance with one embodiment of the invention includes a removable fixture that is coupled to the propeller and has at least one portion exposed to a flowstream to rotate the propeller during engine start-up. The fixture is configured to separate from the propeller after the engine begins to turn over (e.g., after the engine starts and/or rotates above a threshold rate). Accordingly, the system can include a releasable link between the fixture and the propeller.

公开(公告)号：EP0148968B1

公开(公告)日：1988-01-13

申请号：EP84100428.6

申请日：1984-01-17

Applicant: DORNIER GMBH

Inventor： Frühauf, Werner, Ing. grad.

IPC: B64C39/02 ,  B64D37/00

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/044 ,  B64C2201/165 ,  B64C2201/201 ,  B64D37/00