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    PARACHUTE DEVICE
    131.
    发明公开
    PARACHUTE DEVICE 审中-公开
    PARACHUTE设备

    公开(公告)号：EP3309074A1

    公开(公告)日：2018-04-18

    申请号：EP17195810.1

    申请日：2017-10-10

    Applicant: Ravennadron di Andrea Antonioli

    Inventor： ANTONIOLI, Andrea

    IPC: B64D17/72

    CPC classification number: B64D17/72 ,  B64C2201/185

    Abstract: Parachute device (100), especially for remotely controlled aircraft (200) such as drones or the like, wherein a canopy (160) can be alternatively switched between a closing condition and an opening condition, wherein, when the canopy (160) is in opening condition, the device allows the aircraft (200) to fall in a controlled way, the device comprising a support and switching structure (150) for the canopy (160), the support and switching structure (150) being switchable between an idle condition and an operating condition - also called use condition-, wherein the switching of the support and switching structure (150) between the idle condition and the use condition results in the switching of the canopy (160) between the opening condition and the closing condition respectively; wherein the support and switching structure (150) can be alternatively inflated and deflated, and the inflating and deflating of the support and switching structure (150) result in the switching of the support and switching structure (150) into the use condition and the idle condition respectively and, thus, into the switching of the canopy (160) into the opening condition and the closing condition respectively.

    Abstract translation: 特别是对于诸如无人机等的遥控飞机（200）的降落伞装置（100），其中顶篷（160）可以可选地在闭合状态和打开状态之间切换，其中，当顶篷（160）处于 所述装置允许所述飞机（200）以受控方式下落，所述装置包括用于所述顶篷（160）的支撑和开关结构（150），所述支撑和开关结构（150）可在怠速状态 和操作条件 - 也称为使用条件 - ，其中支撑和开关结构（150）在空闲状态和使用状态之间的切换导致遮篷（160）分别在打开状态和闭合状态之间切换 ; 其中支撑和开关结构（150）可以交替地充气和放气，并且支撑和开关结构（150）的膨胀和放气导致支撑和开关结构（150）切换到使用状态，并且空闲 条件，并且因此分别将遮篷160切换到打开状态和关闭状态。

    DRONE ET ÉQUIPEMENT D'INTERVENTION AÉROPORTÉE ASSOCIÉ
    134.
    发明公开
    DRONE ET ÉQUIPEMENT D'INTERVENTION AÉROPORTÉE ASSOCIÉ 有权
    DRONE ETÉQUIPEMENTD'INTERVENTIONAÉROPORTÉEASSOCIÉ

    公开(公告)号：EP3233632A1

    公开(公告)日：2017-10-25

    申请号：EP15816171.1

    申请日：2015-12-18

    Applicant: DAE

    Inventor： DEMONFORT, Thierry

    IPC: B64C39/02 ,  B64D5/00

    CPC classification number: B64C39/026 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/185 ,  B64D5/00

    Abstract: The present invention relates; - to a drone comprising a fuselage (1) provided with carrying means (11, 12) capable of allowing a belly-to-ground flight position and an inverted flight position, at least one propulsion means (2), autonomous navigation instruments and an axial compartment (10) forming a recess incorporated into an upper part of the fuselage in order to receive a parachutist (h) in the lying position, avionics provided with programmable control means coupled to the autonomous navigation instruments and means for releasing said parachutist controlled by said avionics, characterised in that said release means are designed and intended to ensure the release of said parachutist in the inverted flight position, and, - to a piece of airborne intervention equipment.

    Abstract translation: 本发明涉及; - 包括机身（1）的无人机，所述机身（1）设置有能够允许腹部至地面飞行位置和倒飞位置的携带装置（11,12），至少一个推进装置（2），自主导航仪器和 （10）形成结合到机身上部中的凹部以便接纳躺卧位置的伞兵（h），配备有耦合到自主导航仪器的可编程控制装置的航空电子设备以及用于释放由所述控制装置控制的所述伞兵的装置 所述航空电子设备的特征在于，所述释放装置被设计并且旨在确保所述伞兵在所述倒转飞行位置中的释放，以及 - 至一件空中传播设备。

    EMERGENCY EQUIPMENT FOR UNMANNED AERIAL VEHICLES
    135.
    发明公开
    EMERGENCY EQUIPMENT FOR UNMANNED AERIAL VEHICLES 有权
    NOTAUSRÜSTUNGFÜRUNBEMANNTE LUFTFAHRZEUGE

    公开(公告)号：EP3050805A1

    公开(公告)日：2016-08-03

    申请号：EP16152684.3

    申请日：2016-01-26

    Applicant: Vysoke Uceni Technicke V Brne ,  Babovka, Milan

    Inventor： Popela, Robert ,  Daniel, Milos ,  Pejchar, Jan ,  Babovka, Milan ,  Nemcak, Ondrej

    IPC: B64D17/50 ,  B64D17/52 ,  B64D17/72 ,  B64D17/80 ,  B64C39/02 ,  B64D17/42

    CPC classification number: B64D17/725 ,  B64C39/024 ,  B64C2201/185 ,  B64D17/42 ,  B64D17/80

    Abstract: Emergency equipment for unmanned aerial vehicles comprising
    - a container (1) having an opening,
    - a parachute (8), comprising a parachute canopy (80), suspension lines and a harness (81), wherein the parachute (8) is foldable into the container (1),
    - a plug (3) for dividing the inner space of the container (1) into a combustion chamber (12) and a storage chamber (13) for storing the parachute (8), the storage chamber (13) being arranged between the plug (3) and the opening of the container (1), and the plug (3) being adapted such that it may be ejected out of the container (1) through the opening, and
    - at least one pyrotechnic gas generator (7) arranged in the combustion chamber (12) and being connectable to an activation line (4).

    Abstract translation: 用于无人驾驶飞行器的应急设备包括 - 具有开口的容器（1）， - 降落伞（8），包括降落伞（80），悬挂线和吊带（81），其中降落伞（8）可折叠成 容器（1）， - 用于将容器（1）的内部空间分成燃烧室（12）的塞子（3）和用于储存降落伞（8）的储存室（13），储存室 ）设置在插头（3）和容器（1）的开口之间，并且插头（3）适于使其可以通过开口从容器（1）中排出，并且 - 至少一个烟火 气体发生器（7），其布置在燃烧室（12）中并且可连接到激活线（4）。

    PARACHUTE RELEASE DEVICE AND METHODS
    136.
    发明公开
    PARACHUTE RELEASE DEVICE AND METHODS 审中-公开
    降落伞释放设备和方法

    公开(公告)号：EP1945508A1

    公开(公告)日：2008-07-23

    申请号：EP05812878.6

    申请日：2005-11-30

    Applicant: BlueBird Aero Systems Ltd.

    Inventor： NADIR, Ronen

    IPC: B64D17/00

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/084 ,  B64C2201/104 ,  B64C2201/146 ,  B64C2201/185 ,  B64D17/80

    Abstract: The disclosure provides a parachute release device which may include a connecting element capable of connecting to an aircraft and to a parachute and a locking mechanism capable of releasing the connecting element from the aircraft upon being actuated by an actuator, wherein the parachute may be connected to the connecting element by a multiplicity of points, wherein the locking mechanism is adapted to inhibit a force from being applied to the actuator and wherein the device may be suitable for use in small weights aircrafts due to its small size and weight . The disclosure further provides a method for releasing a parachute from an aircraft, the method may include activating an actuator capable of releasing a locking mechanism, wherein the locking mechanism is adapted to release a connecting element from an aircraft upon being actuated, wherein the connecting element is adapted to connect a parachute and wherein the locking mechanism is adapted to inhibit a force from being applied to the actuator.

    GYROPTERE A SECURITE RENFORCEE
    137.
    发明公开
    GYROPTERE A SECURITE RENFORCEE 审中-公开
    具有增强的安全GYROPTER

    公开(公告)号：EP1656294A1

    公开(公告)日：2006-05-17

    申请号：EP04767383.5

    申请日：2004-06-18

    Applicant: GUILHOT-GAUDEFFROY, Michel

    Inventor： GUILHOT-GAUDEFFROY, Michel

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

    CPC classification number: B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/185

    Abstract: The invention relates to a gyropter having coaxial contrarotating rotating aerofoils, in particular, one having two crown rotors (2,1) that rotate in opposite directions about a pod (6) either provided in the form of a drone or of a manned pod with a machine piloting process involving the control of the angle of attack of the blades by control rings. The safety is advantageously increased by adapted structures, by a multifunctional protective envelop (27), and by a lift system between the crowns (2,1) and the pod (6) with regard to both the radial forces as well as the axial forces, assisting in the optimized control of stresses. The gyropter also comprises electronic controls that are adapted to both model making and drones as well as to manned and/or piloted aircraft.

    착륙이 용이한 무인비행체
    138.
    发明申请
    착륙이 용이한 무인비행체 审中-公开
    轻松登陆

    公开(公告)号：WO2014129761A1

    公开(公告)日：2014-08-28

    申请号：PCT/KR2014/001001

    申请日：2014-02-06

    Applicant: 주식회사 네스앤텍

    Inventor： 이기성

    IPC: B64C29/02 ,  B64C13/20 ,  B64C3/38

    CPC classification number: B64C27/28 ,  B64C3/38 ,  B64C3/58 ,  B64C9/323 ,  B64C39/024 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/185 ,  B64C2201/187

    Abstract: 착륙이 용이한 무인비행체가 제공되며, 무인비행체는 방향을 전환하는 프로펠러, 상기 프로펠러를 지지하는 프로펠러 타워, 상기 프로펠러 타워에 연결되어 있는 동체, 상기 동체의 수평축을 기준으로 좌우가 대칭이며, 상기 동체의 무게중심부에 한 쌍의 통공을 포함하는 주날개, 상기 한 쌍의 통공 내부에 각각 위치하는 한 쌍의 보조날개, 그리고 상기 한 쌍의 보조날개를 관통하며 상기 주날개에 고정되어 있는 기준축에 연결되어 있으며, 상기 한 쌍의 보조날개의 경사각도를 제어하는 액츄에이터(actuator)를 포함한다.

    Abstract translation: 披露了一个简单的降落无人机，包括：改变方向的螺旋桨; 用于支撑螺旋桨的螺旋桨塔; 连接到螺旋桨塔的主体; 相对于主体的水平轴线对称地设置有两侧的主翼，在主体的主体的重心处形成有一对开口部， 一对辅助翼分别布置在该对开口中; 以及通过所述一对辅助翼连接到固定到主翼的基准轴的致动器，用于控制所述一对辅助翼的倾斜角。

    UNMANNED AERIAL SYSTEMS
    139.
    发明申请
    UNMANNED AERIAL SYSTEMS 审中-公开
    无人机系统

    公开(公告)号：WO2014058510A2

    公开(公告)日：2014-04-17

    申请号：PCT/US2013/051959

    申请日：2013-07-25

    Applicant: BYE UAS, INC. ,  BYE, George ,  BICKEL, Matt

    Inventor： BYE, George ,  BICKEL, Matt

    IPC: B64C19/02

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/126 ,  B64C2201/165 ,  B64C2201/167 ,  B64C2201/185 ,  B64C2211/00

    Abstract: The present invention provides an Unmanned Aircraft System, including an integrated unmanned aerial vehicle and all related components and subsystems that can be packaged and transported as a kit, and customized to fit desired mission profiles, and easily repaired by replacement of damaged components or subsystems. The present invention further provides unmanned aircraft system components and subsystems that facilitate low power and low noise operation, and extended flight times.

    Abstract translation: 本发明提供了一种无人驾驶飞机系统，其包括集成的无人驾驶飞行器以及可以作为套件来包装和运输的所有相关部件和子系统，并且定制以适应期望的任务轮廓并且易于修理 通过更换损坏的部件或子系统。 本发明还提供了有助于低功率和低噪音操作以及延长飞行时间的无人驾驶飞机系统部件和子系统。

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