公开(公告)号：EP2354000A1

公开(公告)日：2011-08-10

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: - Système d'emport de charge pour avion de transport.
- Le système (1) comporte un conteneur externe (15) qui est fixé, directement et complètement, dans la soute de l'avion de transport (AC), et dans lequel est agencé un conteneur interne (4) qui peut être déplacé longitudinalement et être amené d'une première position d'emport, dans laquelle il est entièrement situé à l'intérieur dudit conteneur externe (15), à une seconde position (P2) de déchargement, dans laquelle il est décalé longitudinalement vers l'arrière de l'aéronef (AC) de sorte qu'une partie (7) dudit conteneur interne (4) est alors située à l'extérieur de l'avion de transport (AC).

Abstract translation: 系统（1）固定在运输飞机（AC）的货舱中的外部容器（15）。 内部容器（4）布置在外部容器中，以使内部容器从内部容器完全位于外部容器内部的位置到另一个位置（P2），其中内部容器朝向后部侧 飞机相对于前一位置使得内部容器的释放部分（7）通过在隔室的后侧处的开口（8）位于飞机外部。

公开(公告)号：EP2329213A1

公开(公告)日：2011-06-08

申请号：EP09792723.0

申请日：2009-09-18

Applicant: Raytheon Company

Inventor： SAMPSON, Ray ,  BOSSERT, David E. ,  ZERBE, Jeffrey N.

IPC: F41F3/07 ,  B63G8/30

CPC classification number: F41F3/07 ,  B63B22/003 ,  B63B22/24 ,  B63G6/00 ,  B63G8/30 ,  B64C2201/201 ,  B64C2201/205

Abstract: Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be launched from a marine vehicle and rise to the surface. Assets, such as an unmanned aerial vehicle, may be deployed from the surfaced floatable housing.

公开(公告)号：EP2190743A2

公开(公告)日：2010-06-02

申请号：EP08862123.0

申请日：2008-09-18

Applicant: Raytheon Company

Inventor： BOSSERT, David ,  ZERBE, Jeff ,  SAMPSON, Ray

IPC: B64F1/04

CPC classification number: F41F3/07 ,  B64C2201/201 ,  B64C2201/205 ,  F42B15/20

Abstract: Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be launched from a marine vehicle and rise to the surface. Assets, such as an unmanned aerial vehicle, may be deployed from the surfaced floatable housing.

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：EP1827972B8

公开(公告)日：2008-10-22

申请号：EP05813078.2

申请日：2005-11-30

Applicant: Israel Aerospace 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.

Abstract translation: 提供了一种用于着陆固定翼飞机的方法，其中执行反转操纵，使得飞机的背面朝向地面，并且飞机的底面背离地面。 在开始或完成这种机动之后，引起深度失速，并且飞机几乎垂直下降以落在其上侧，从而最小化撞击载荷或其下侧的损坏。 在构造成用于执行该方法的特定空气动力学布置中，可以在正常飞行期间收起的襟翼（24）以诸如在空气动力学上引起飞行器上的负俯仰力矩和深度失速的方式展开。

公开(公告)号：EP1884463A1

公开(公告)日：2008-02-06

申请号：EP07106798.7

申请日：2007-04-24

Applicant: HONEYWELL INC.

Inventor： Goossen, Emray R ,  Mantych, Glen A. ,  Campbell, William T.

IPC: B64C39/02 ,  B64F1/04

CPC classification number: B64C39/028 ,  B64C2201/027 ,  B64C2201/044 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/201

Abstract: A Micro Air-Vehicle (MAV) starting system that provides the combined functions of: packing protection of sensitive vehicle components, a mechanical starting assembly, and a launch pad. The preferred embodiment comprises a container (110) and a container lid (101) with the MAV (200) clamped to the lid. Also disposed on the container lid is a starting assembly (111). The lid (101) which doubles as a launching pad with the attached MAV (200) is removed from the container (110), placed on the ground, the MAV (200) is started with the starling mechanism and launched. The arrangement minimizes the physical risk to the operator, minimizes weight of the total MAV system, consumes minimum space in the operators transport system, and eliminates dependence on supply lines for battery replacement or charging.

Abstract translation: 微型飞行器（MAV）启动系统，提供组合功能：敏感车辆部件的包装保护，机械启动组件和发射台。 优选实施例包括容器（110）和容纳盖（101），其中MAV（200）夹在盖子上。 还设置在容器盖上的是起动组件（111）。 将具有连接的MAV（200）的作为发射台的盖（101）从容器（110）中取出，放置在地面上，MAV（200）以起落机构启动并启动。 这种安排可最大限度地减少操作者的身体风险，最大限度地减少总体MAV系统的重量，消耗操作员运输系统的最小空间，并消除对电池更换或充电的供电线路的依赖。

公开(公告)号：EP1590238A2

公开(公告)日：2005-11-02

申请号：EP04775727.3

申请日：2004-01-17

Applicant: The Insitu Group

Inventor： DENNIS, Bryan, D. ,  JACKSON, Clifford ,  MCGEER, Brian, T. ,  ROESELER, Cory ,  VONFLOTOW, Andreas, H.

IPC: B64B1/00

CPC classification number: B64F1/02 ,  B63B27/26 ,  B64C25/68 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/201 ,  B64F1/04 ,  B64F1/06

Abstract: Methods and apparatuses for assembling, launching, recovering, disassembling, capturing, and storing unmanned aircraft (140) and other flight devices or projectiles are described. In one embodiment, the aircraft (140) can be assembled from a container (111) with little or no manual engagement by an operator. The container (111) can include a guide structure to control motion of the aircraft components. The aircraft (140) can be launched from an apparatus that includes an extendable boom (103). The boom (103) can be extended to deploy a recovery line (853) to capture the aircraft (140) in flight. The aircraft (140) can then be returned to its launch platform, disassembled, and stored in the container (111), again with little or no direct manual contact between the operator and the aircraft (140).

公开(公告)号：EP0141895B1

公开(公告)日：1988-03-09

申请号：EP84103991.0

申请日：1984-04-10

Applicant: Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung

Inventor： Höppner, Hans-Jochen ,  Krämer, Ulrich ,  Sölter, Michael

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C3/56 ,  B64C2201/046 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  F42B10/16

公开(公告)号：EP0141895A3

公开(公告)日：1986-03-05

申请号：EP84103991

申请日：1984-04-10

Applicant: Messerschmitt-Bölkow-Blohm GmbH

Inventor： Höppner, Hans-Jochen ,  Krämer, Ulrich ,  Sölter, Michael

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C3/56 ,  B64C2201/046 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  F42B10/16

公开(公告)号：EP0141895A2

公开(公告)日：1985-05-22

申请号：EP84103991.0

申请日：1984-04-10

Applicant: Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung

Inventor： Höppner, Hans-Jochen ,  Krämer, Ulrich ,  Sölter, Michael

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C3/56 ,  B64C2201/046 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  F42B10/16

Abstract: Die Erfindung bezieht sich auf ein Luftfahrzeug mit faltbaren und/oder schwenkbaren Tragflügeln. Eine zwischen den Flügelteilen und/oder dem Rumpf angreifende Gasdruckfeder mit starker Enddämpfung sorgt für eine schnelle und automatische Entfaltung bzw. Schwenkung der Tragflügel.

Abstract translation: 本发明涉及一种具有可折叠和/或旋转翼的飞机。 机翼部分和/或机身气弹簧之间的作用力与强烈的末端阻尼确保了机翼的快速和自动展开或倾斜。