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11. 发明公开

EP3390224A1 AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING AND ITS OPERATING PROCESS 有权转让
公开(公告)号：EP3390224A1
公开(公告)日：2018-10-24
申请号：EP16831647.9
申请日：2016-12-16
申请人： IOSIF, Taposu , RAZVAN, Sabie
发明人： RAZVAN, Sabie
IPC分类号： B64C39/00
CPC分类号： B64C39/001 , B64C2201/027 , B64C2201/14 , B64C2201/162 , B64C2201/167 , B64C2201/185
摘要： The invention relates to an aircraft with vertical takeoff and landing and its operation method. Aircraft with vertical takeoff and landing of aerodyne type according to the invention comprises a circular symmetrical aerodynamic body (1) having an internal stiffening platform (2) located on the chord of the aerodynamic profile and which supports the components of the aircraft, at least four vertical ducted propellers (3a), (3b), (3c), (3d) arranged symmetrically to the central vertical axis of the carrier body (1), but also to the predetemined flight axis and to the transverse axis of the carrier body (1), propellers (3a) and (3c) having the same rotational direction opposite to that of propellers (3b) and (3d) at least two horizontal ducted propellers (4) with opposite rotation directions located inside the carrier body or outside of it, placed parallel symmetrical with the predetermined flight axis and on both sides of it, vector nozzles (5), one for each horizontal propeller (4), which provides vector orientation to jets of the horizontal ducted propellers (4), the means of power supply (6), which are designed to provide electricity necessary to operate all engines and all electrical and electronic devices on board, an electronic control and management flight module (7) and a landing gear (9), which aims to promote contact between the aircraft and the ground.

12. 发明公开

EP2879954A4 UNMANNED AERIAL SYSTEMS 审中-公开
标题翻译：无人航空系统
公开(公告)号：EP2879954A4
公开(公告)日：2016-07-27
申请号：EP13845941
申请日：2013-07-25
申请人： BYE UAS INC
发明人： BYE GEORGE , BICKEL MATT
IPC分类号： B64C39/02
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/08 , B64C2201/086 , B64C2201/104 , B64C2201/126 , B64C2201/165 , B64C2201/167 , B64C2201/185 , B64C2211/00

13. 发明公开

EP2879954A2 UNMANNED AERIAL SYSTEMS 审中-公开
标题翻译：无人航空系统
公开(公告)号：EP2879954A2
公开(公告)日：2015-06-10
申请号：EP13845941.7
申请日：2013-07-25
申请人： Bye UAS Inc.
发明人： BYE, George , BICKEL, Matt
IPC分类号： B64C39/02
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/08 , B64C2201/086 , B64C2201/104 , B64C2201/126 , B64C2201/165 , B64C2201/167 , B64C2201/185 , B64C2211/00
摘要： 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.

14. 发明公开

EP1833721A2 CARGO AIRCRAFT 失效转让
标题翻译： FRACHTFLUGZEUG
公开(公告)号：EP1833721A2
公开(公告)日：2007-09-19
申请号：EP05857018.5
申请日：2005-11-22
申请人： Helou, Elie Jr.
发明人： Helou, Elie Jr.
IPC分类号： B64C1/22
CPC分类号： B64C1/10 , B64C1/00 , B64C1/061 , B64C1/065 , B64C39/02 , B64C39/024 , B64C2001/0072 , B64C2201/021 , B64C2201/048 , B64C2201/086 , B64C2201/104 , B64C2201/128 , B64C2201/162 , B64C2201/167 , B64C2211/00 , Y02T50/43
摘要： In one embodiment, an aircraft for transporting at least one cargo container is disclosed. The aircraft comprises a forward fuselage, an empennage, a beam structure, and mounts to detachably and structurally engage the at least one cargo container with the beam structure. The beam structure is disposed between the forward fuselage and the empennage and the beam structure configured to receive the at least one cargo container. The beam structure and structurally engaged cargo container provide sufficient structural rigidity to support the aircraft in flight.
摘要翻译：在一个实施例中，公开了一种运送至少一个货物集装箱的飞机。飞行器包括前机身，尾翼，梁结构，以及可拆卸地和结构地接合具有梁结构的至少一个货物集装箱的安装件。梁结构设置在前机身和尾翼之间，梁结构构造成接收至少一个货物集装箱。梁结构和结构上接合的货物集装箱提供足够的结构刚度以支持飞行中的飞机。

15. 发明专利

JP2018020761A 展開可能な送信/受信モジュール装置を有するラムジェット付き無人航空ビークル审中-公开
公开(公告)号：JP2018020761A
公开(公告)日：2018-02-08
申请号：JP2017100925
申请日：2017-05-22
申请人：ザ・ボーイング・カンパニー , The Boeing Company
发明人：キム, イニョンダニエル , ウィルソン, ライアンエス.
IPC分类号： B64C39/02 , B64D47/00 , B64D27/16 , F41G7/30 , G01S13/46 , G01S7/02 , H01Q21/06 , H01Q3/02 , H01Q1/28 , B64C30/00
CPC分类号： G01S7/021 , B64C3/38 , B64C9/326 , B64C30/00 , B64C39/024 , B64C2201/021 , B64C2201/082 , B64C2201/12 , B64C2201/122 , B64C2201/167 , B64D5/00 , B64D7/00 , B64D47/02 , F02K7/10 , F05D2220/10 , F42B10/48 , G01S7/003 , G01S13/003 , G01S13/87 , G05D1/0011 , G05D1/0088 , H01Q1/287
摘要：【課題】超音速無人航空ビークルを用いたバイスタティック戦術レーダーの用途に関し、具体的には、格納された超音速巡航ポジションから、拡張された三角形状へと展開可能な送信/受信用アンテナを有する小型無人航空ビークル(UAV)を用いたシステムをする。【解決手段】超音速巡航のためのラムジェットエンジンを有する無人航空ビークル(UAV)14を用いる。展開可能アンテナアームは、超音速巡航用の第1の格納ポジションを有し、エアブレーキとして機能し且つレーダー受信器のボアサイトアライメントを提供する、第2の拡張位置へと展開可能なように適合している。母機10は、レーダーパルスを送信するレーダー送信器を有し、通信データリンクが、UAVと戦術母機を操作可能に相互接続し、反射レーダーパルスをUAVレーダーアンテナでバイスタティック受信することによって生成されたデータを、母機に向けて送信する。【選択図】図1

16. 发明专利

JPWO2003004352A1 飛行船システム审中-公开
公开(公告)号：JPWO2003004352A1
公开(公告)日：2004-10-21
申请号：JP2003510336
申请日：2002-06-17
申请人：セイコーエプソン株式会社
发明人：赤堀　豊 , 豊赤堀
IPC分类号： G05D1/00 , B64B1/00 , B64B1/06 , B64C39/02 , B64F1/18 , G01S5/20 , G01S5/22 , G05D1/02 , G08G5/00
CPC分类号： G08G5/0052 , B64B1/06 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/048 , B64C2201/101 , B64C2201/122 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/167 , B64F1/18 , G01S5/20 , G01S5/22 , G05D1/0202 , G08G5/00 , G08G5/0013
摘要：本発明の飛行船システムは、飛行船(110)と、基地局120と、少なくとも3つの測定点とを有する。基地局(120)からの指令を受けた飛行船(110)が超音波を発信すると、測定点ユニット(S1〜S3)にて超音波を受信することにより、これら3つの測定点までの距離を測定し、基地局(120)内に内蔵されたMPUが飛行船(110)の位置を算出する。この位置に応じて基地局(120)は飛行船(110)に対して航行指令を送信し、飛行船(110)の航路を制御する。これにより、オペレータの操船を不要にすることができるとともに、飛行船の搭載重量及び消費電力の低減が可能な飛行船システムを提供することができる。

17. 发明申请

US20170343645A1 UNMANNED AERIAL VEHICLE WITH DEPLOYABLE TRANSMIT/RECEIVE MODULE APPARATUS WITH RAMJET 审中-公开
公开(公告)号：US20170343645A1
公开(公告)日：2017-11-30
申请号：US15165663
申请日：2016-05-26
申请人： The Boeing Company
发明人： Inyoung Daniel Kim , Ryan S. Wilson
IPC分类号： G01S7/02 , G01S7/00 , B64C39/02 , F02K7/10 , B64D5/00 , G05D1/00 , B64C30/00
CPC分类号： G01S7/021 , B64C3/38 , B64C9/326 , B64C30/00 , B64C39/024 , B64C2201/021 , B64C2201/082 , B64C2201/12 , B64C2201/122 , B64C2201/167 , B64D5/00 , B64D7/00 , B64D47/02 , F02K7/10 , F05D2220/10 , F42B10/48 , G01S7/003 , G01S13/003 , G01S13/87 , G05D1/0011 , G05D1/0088 , H01Q1/287
摘要： A system for bistatic radar target detection employs an unmanned aerial vehicle (UAV) having a ramjet providing supersonic cruise of the UAV. Deployable antenna arms support a passive radar receiver for bistatic reception of reflected radar pulses. The UAV operates with a UAV flight profile in airspace beyond a radar range limit. The deployable antenna arms have a first retracted position for supersonic cruise and are adapted for deployment to a second extended position acting as an airbrake and providing boresight alignment of the radar receiver. A mothership aircraft has a radar transmitter for transmitting radar pulses and operates with an aircraft flight profile outside the radar range limit. A communications data link operably interconnects the UAV and the tactical mothership aircraft, transmitting data produced by the bistatic reception of reflected radar pulses in the UAV radar antenna to the mothership aircraft.

18. 发明申请

US20170057635A1 DRONE LAUNCH SYSTEMS AND METHODS 有权
标题翻译：推动系统和方法
公开(公告)号：US20170057635A1
公开(公告)日：2017-03-02
申请号：US14843329
申请日：2015-09-02
申请人： THE BOEING COMPANY
发明人： James David Strayer
IPC分类号： B64C39/02 , B64C5/06 , B64D1/02
CPC分类号： B64C39/024 , B63G3/04 , B63G2008/004 , B63G2008/008 , B64C2201/027 , B64C2201/088 , B64C2201/108 , B64C2201/167 , B64C2201/201 , B64C2201/205
摘要： A drone launch system includes a canister defining an internal cavity, and a drone positioned within the internal cavity in a stowed state. The drone is configured to be ejected from the canister and transition from the stowed state into a deployed state outside of the canister. A method for launching a drone, the method includes positioning the drone in a stowed state in an internal cavity of a canister, ejecting the drone from the canister, and transitioning the drone into a deployed state after the ejecting operation.
摘要翻译：无人机发射系统包括限定内部空腔的罐和位于收纳状态的内部空腔内的无人机。无人机被配置为从罐排出并从收起状态转换到罐外部的展开状态。一种用于发射无人机的方法，该方法包括将无人机处于收起状态，将其从罐中排出，将喷射器从罐排出，并且在喷射操作之后将无人机转换成展开状态。

19. 发明授权

US08492692B2 Unmanned aerial vehicle based sonar buoy 有权
标题翻译：无人机基于声纳浮标
公开(公告)号：US08492692B2
公开(公告)日：2013-07-23
申请号：US13097394
申请日：2011-04-29
申请人： Jeremy F. Fisher
发明人： Jeremy F. Fisher
IPC分类号： F42B12/56 , F42B15/01 , F42B15/08 , H04B1/59 , F42B15/00 , H04B1/00
CPC分类号： F42B15/10 , B64C39/024 , B64C2201/021 , B64C2201/084 , B64C2201/102 , B64C2201/122 , B64C2201/165 , B64C2201/167 , B64C2201/201 , B64C2201/205 , F41F1/08 , F41F3/042
摘要： A sonar buoy includes a fuselage having a tube-like shape, one or more wings coupled to the fuselage, an engine coupled to the fuselage and operable to propel the sonar buoy through flight, and a guidance computer operable to direct the sonar buoy to a predetermined location. The sonar buoy further includes a sonar detachably coupled to the fuselage and forming at least a part of the fuselage, and a rocket motor detachably coupled to the fuselage. The one or more wings are operable to be folded into a position to allow the sonar buoy to be disposed within a launch tube coupled to a vehicle and to automatically deploy to an appropriate position for flight after the sonar buoy is launched from the launch tube. The rocket motor propels the sonar buoy from the launch tube and detaches from the fuselage after launch.
摘要翻译：声纳浮标包括具有管状形状的机身，耦合到机身的一个或多个翼，耦合到机身的发动机，并且可操作以通过飞行推进声纳浮标;以及引导计算机，其可操作以将声纳浮标引导到预定位置。声纳浮标还包括可拆卸地联接到机身并形成机身的至少一部分的声纳和可拆卸地联接到机身的火箭发动机。一个或多个翼可操作以折叠到允许声纳浮标布置在联接到车辆的发射管内并且在从发射管发射声纳浮标之后自动部署到适当位置用于飞行的位置。火箭发动机从发射管推进声纳浮标，并在发射后从机身分离。

20. 发明申请

US20070023570A1 System and method for remote control of interdiction aircraft 审中-公开
标题翻译：拦截飞机遥控系统及方法
公开(公告)号：US20070023570A1
公开(公告)日：2007-02-01
申请号：US11192171
申请日：2005-07-29
申请人： Charles Bernard
发明人： Charles Bernard
IPC分类号： B64C13/00
CPC分类号： B64C13/20 , B64C39/024 , B64C2201/021 , B64C2201/044 , B64C2201/048 , B64C2201/082 , B64C2201/104 , B64C2201/121 , B64C2201/128 , B64C2201/145 , B64C2201/146 , B64C2201/167 , B64D39/00 , G05D1/0027
摘要： An aircraft attack interdiction system using an unmanned interdiction aircraft piloted using a remote control system. In-flight refueling system, weapons launcher systems and intelligence gathering equipment are mounted on the interdiction aircraft. A remote flight control operator to remotely fly the interdiction aircraft can be based on a remote flight control commander aircraft that can be flown at safe distances from targets that are attacked by the interdiction aircraft.
摘要翻译：使用遥控系统驾驶的无人拦截飞机的飞机攻击拦截系统。飞机上的加油系统，武器发射系统和情报搜集设备都安装在拦截飞机上。远程飞行拦截飞机的远程飞行控制操作员可以基于远程飞行控制指挥员飞机，该飞机可以在距离被拦截飞机攻击的目标的安全距离处飞行。

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