公开(公告)号：WO2016085769A1

公开(公告)日：2016-06-02

申请号：PCT/US2015/061706

申请日：2015-11-19

Applicant: SIKORSKY AIRCRAFT CORPORATION

Inventor： DERENICK, Jason C. ,  WANG, Hongcheng ,  STATHIS, Christopher ,  CHEREPINSKY, Igor

IPC: G01C21/20 ,  G06K9/00 ,  G01C21/00 ,  G05D1/00 ,  G01C23/00

CPC classification number: B64D45/08 ,  B63B35/50 ,  B64C39/024 ,  G01C21/00 ,  G01C21/20 ,  G01C23/00 ,  G05D1/0088 ,  G05D1/0684

Abstract: An electronic landing platform state module is configured to generate a state estimation of a platform surface at sea includes a plurality of electronic platform state process modules configured to receive an output from a respective spectral sensor. The plurality of electronic platform state process modules are further configured to output a monitored spectral platform state signal in response to applying a spectral process on a respective output. Each spectral process corresponds to a particular spectral modality of the respective spectral sensor. The electronic landing platform state module further includes an electronic platform state estimator module configured to determine a corrected dynamic state of the platform in response to fusing together the individual monitored spectral platform state signals.

Abstract translation: 电子着陆平台状态模块被配置为生成海上平台表面的状态估计包括多个电子平台状态处理模块，其被配置为从相应的光谱传感器接收输出。 多个电子平台状态处理模块还被配置为响应于对相应输出应用频谱处理而输出被监视的频谱平台状态信号。 每个光谱过程对应于相应光谱传感器的特定光谱模态。 电子着陆平台状态模块还包括电子平台状态估计器模块，其被配置为响应于将各个监视的频谱平台状态信号融合在一起来确定平台的校正的动态状态。

公开(公告)号：WO2014059785A1

公开(公告)日：2014-04-24

申请号：PCT/CN2013/075138

申请日：2013-05-03

Applicant: 大连理工大学

Inventor： 黄一 ,  王文华 ,  姚宇鑫 ,  刘刚 ,  张琦 ,  李红霞 ,  陈景杰 ,  翟刚军

IPC: B63B35/44 ,  B63B21/50

CPC classification number: B63B35/4413 ,  B63B1/04 ,  B63B1/041 ,  B63B3/20 ,  B63B21/50 ,  B63B29/02 ,  B63B35/50

Abstract: 一种对接八棱台式浮式生产储油系统，其浮体具有一个为八棱台的上部结构体（2）和一个为正八棱台的下部结构体（3）；组合状态下，所述上部结构体面积较小的底面与所述下部结构体面积较小的底面固定连接，形成连接面；所述上部结构体与下部结构体的轴位于同一直线上，上部结构物面积较大的底为浮式结构物的上甲板，下部结构物面积较大的底为浮式结构物处于水下的下底；所述连接面为浮式结构物的满载水线面（1）。并且在此基础上配有系泊定位、油气生产、储存和外输等功能模块以构成新型浮式生产储油系统。所述浮体具有类似沙漏的外形特点，可以弥补传统浮式生产储油系统在耐波性能、强度疲劳和管线布置等方面的不足，扩展其功能。

公开(公告)号：WO2013077742A1

公开(公告)日：2013-05-30

申请号：PCT/NO2012/050230

申请日：2012-11-21

Applicant: MARINE ALUMINIUM AS

Inventor： RØD, Karl Johan

IPC: B64F1/12 ,  B63B35/50 ,  E01F3/00 ,  E04H6/44

CPC classification number: B64F1/125 ,  B63B35/50 ,  E01F3/00

Abstract: Anchoring device (1) in a helicopter deck (2), where a housing (11) that is provided with an open top (111) and lowered into the helicopter deck (2), contains a fastener (12) which is vertically displaceable between a withdrawn, inactive position and an active position where an upper fastener portion (121) extends at least partly up from the helicopter deck (2) and where the upper fastener portion (121) is arranged to be detachably connected to an anchoring means (3); and the housing (11) is provided with a detachable lid (13) arranged to be able to close tightly against the housing (11).

Abstract translation: 在直升机甲板（2）中的锚定装置（1），其中设置有开口顶部（111）并且下降到直升机甲板（2）中的壳体（11）包含紧固件（12），所述紧固件 撤回的非活动位置和主动位置，其中上紧固件部分（121）至少部分地从直升机甲板（2）延伸，并且其中上紧固件部分（121）布置成可拆卸地连接到锚固装置（3） ）; 并且所述壳体（11）设置有能够紧密地紧靠所述壳体（11）紧密地关闭的可拆卸盖（13）。

公开(公告)号：WO2011135605A2

公开(公告)日：2011-11-03

申请号：PCT/IT2011/000132

申请日：2011-04-28

Applicant: B. FINANCIAL S.r.l. ,  BESENZONI, Giovanni

Inventor： BESENZONI, Giovanni

IPC: B63B35/50 ,  B64F1/36 ,  E01F3/00

CPC classification number: B64F1/36 ,  B63B3/48 ,  B63B35/50 ,  B63B2017/0072 ,  B64F1/007 ,  B64F1/02 ,  E01F3/00

Abstract: A reduced dimensions platform (1) for the landing of an aircraft on an access facility (B) comprising a support base (2), suitable to be fixed on a reference surface (P) belonging to said access facility (B), and a landing footboard (3), superiorly connected with said support base (2) and suitable to receive said aircraft. Specifically, the landing footboard (3) includes a central body (4), coupled with support base (2), and a plurality of peripheral panels (5), operatively connected with drive means (6) which move the peripheral panels (5) from/to a rest position, in which said peripheral panels (5) are contained within the dimensions of the central body (4), to/from an operating position, in which the peripheral panels (5) projects laterally from the central body (4) and are combined and side-by- side each other so as to be coplanar with each other and the central body (4) itself and make the landing footboard (3) ready to receive said aircraft.

Abstract translation: 一种用于飞机在进入设施（B）上着陆的减小尺寸的平台（1），其包括适于固定在属于所述参考表面（P）的支撑基座（2） （B）和登陆脚踏板（3），所述登陆脚踏板优先与所述支撑基座（2）连接并适于接收所述飞机。 具体地，登陆脚踏板3包括与支撑基座2联接的中央主体4以及与驱动装置6可操作地连接的多个外围面板5，所述驱动装置6移动外围面板5， 其中所述外围面板（5）被容纳在所述中心体（4）的尺寸内的休息位置到达/来自工作位置，在所述工作位置中，所述外围面板（5）从所述中心体侧向地突出 4）并且并排并且彼此并排以彼此共面以及中央主体（4）本身并且使得着陆踏板（3）准备好接收所述飞机。

公开(公告)号：WO2010113030A3

公开(公告)日：2011-05-12

申请号：PCT/IB2010000886

申请日：2010-03-10

Applicant: WANG LIFENG

Inventor： WANG LIFENG

IPC: B64F1/10 ,  B63B35/50 ,  B63G11/00 ,  B64D1/00 ,  B64F1/04 ,  B64F1/06 ,  B64F1/08

CPC classification number: B64F1/04 ,  B63B35/50 ,  B63G11/00 ,  B64F1/10

Abstract: The present invention provides a carrier-borne aircraft takeoff/landing system comprising a takeoff auxiliary mechanism and/or an integrated runway which are/is positioned on the aircraft carrier. The takeoff auxiliary mechanism can be a sliding vehicle or a simple pendulum type projectile mechanism, the integrated runway is a carrier-borne aircraft runway which can be extended out of the aircraft carrier. The carrier-borne aircraft takeoff/landing system of the present invention concentrates the advantages of current ways of catapult launch and ski-jump takeoff and abandons the faults existed, which can reduce the difficulties and risks involved during the traditional landing. The takeoff/landing system which is outstanding for its simple structure, significantly reduced research cost and energy consumption, with improved efficiency, easy operation and maintenance, high reliability, which are applicable to various carrier-borne aircraft for take off and/or landing.

Abstract translation: 本发明提供一种载体飞行器起飞/着陆系统，其包括位于航空母舰上的起飞辅助机构和/或集成跑道。 起飞辅助机构可以是滑动车辆或简单的摆锤式抛射机构，综合跑道是可以延伸出航空母舰的载体飞机跑道。 本发明的载波飞机起飞/着陆系统集中了当前弹射发射和滑雪起飞方式的优点，放弃了存在的故障，可以减少传统降落过程中的困难和风险。 起飞/着陆系统结构简单，大大降低了研究成本和能耗，提高了效率，操作维护方便，可靠性高，适用于起飞和/或降落的各种载体飞机。

公开(公告)号：WO2016137877A1

公开(公告)日：2016-09-01

申请号：PCT/US2016/018901

申请日：2016-02-22

Applicant: ADVANCED AEROSPACE TECHNOLOGIES, INC.

Inventor： MCDONNELL, William Randall

IPC: B64G5/00 ,  B64F1/02 ,  B63B35/52 ,  B63B1/10 ,  B63B15/00 ,  B63B17/00

CPC classification number: B64F1/02 ,  B63B1/121 ,  B63B17/00 ,  B63B35/50 ,  B63B35/52 ,  B64G5/00

Abstract: A generally vertical rocket (2) flies generally horizontally into recovery line, cable or chain (3) suspended between towers (5, 7) of a catamaran landing ship (9). High speed winches (11, 13), preferably located near or at the tops of the towers (5, 7) can rapidly reel in or out the recovery line (3) to effectively raise or lower the recovery line (3). The fixture engages a capture device on the rocket located usually above the rocket center of gravity. This invention provides a more reliable means of landing a rocket and also eliminates rocket weight, cost and complexity associated with previous means of landing a rocket.

Abstract translation: 大体上垂直的火箭（2）大致水平地飞往回收线，悬挂在双体船着陆船（9）的塔架（5,7）之间的电缆或链条（3）。 优选位于塔（5,7）顶部附近或顶部的高速绞盘（11,13）可以快速地卷入或退出回收管线（3）以有效地升高或降低回收管线（3）。 固定装置与通常位于火箭重心上方的火箭上的捕获装置接合。 本发明提供了一种更可靠的降落火箭的手段，并且还消除了火箭的重量，成本和与先前的火箭登陆手段相关的复杂性。

公开(公告)号：WO2016059555A1

公开(公告)日：2016-04-21

申请号：PCT/IB2015/057837

申请日：2015-10-13

Applicant: SYSTEMS ENGINEERING ASSOCIATES CORPORATION

Inventor： LUSSIER, David ,  DELISLE, Andrew ,  CHARPENTIER, Brian

IPC: B64F1/00 ,  B64F1/04 ,  B64F1/22 ,  B64C39/02 ,  B64C29/00 ,  B64C27/08 ,  B63B35/50 ,  H02J7/00

CPC classification number: B64F1/222 ,  B60L11/1833 ,  B63B35/50 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/201 ,  B64C2201/206 ,  B64C2201/208 ,  B64D47/08 ,  B64F1/00 ,  B64F1/007 ,  B64F1/22 ,  E04H12/003 ,  E04H12/18 ,  G01S19/03 ,  H02J7/355 ,  Y02E10/766

Abstract: An unmanned aerial vehicle (UAV) system provides for UAV deployment and remote, unattended operation with reduced logistics requirements. The system includes a launcher that can include one or more containers, or hangars, configured to house vertical take-off and landing (VTOL) UAVs. The system can further include a VTOL UAV orientation and charging module configured to mechanically position a UAV within a container and facilitate electrical mating and charging of a battery in the UAV. These operations, and others, can be performed by remote command that can initiate a series of pre-programmed steps. The UAV system can further include a power generation and storage subsystem, a security subsystem, a command and control subsystem and a communications subsystem. Command, control and communications can be provided between a remote station and the UAV.

Abstract translation: 无人飞行器（UAV）系统提供无人机部署和远程无人值守操作，物流需求减少。 该系统包括可以包括一个或多个容器或机库的发射器，其被配置为容纳垂直起飞和着陆（VTOL）无人机。 该系统还可以包括一个VTOL UAV取向和充电模块，其被配置为将UAV机械地定位在容器内并且促进UAV中的电池的电配合和充电。 这些操作和其他操作可以通过可以启动一系列预编程步骤的远程命令执行。 UAV系统还可以包括发电和存储子系统，安全子系统，命令和控制子系统以及通信子系统。 可以在远程站和无人机之间提供命令，控制和通信。

公开(公告)号：WO2016043371A1

公开(公告)日：2016-03-24

申请号：PCT/KR2014/010165

申请日：2014-10-28

Applicant: 울산대학교 산학협력단

Inventor： 신현경 ,  김동주 ,  최준서

IPC: B63B35/00 ,  B63B39/06 ,  F03B13/14 ,  B63B35/50

CPC classification number: B63B39/06 ,  B63B1/041 ,  B63B35/44 ,  B63B35/50 ,  B63B2001/044 ,  B63B2035/4466 ,  B63B2039/063 ,  B63B2039/067 ,  B63B2039/068 ,  F03B13/14 ,  Y02E10/38

Abstract: 본 발명은, 해상에 부유하도록 부력을 가지는 메인부유체, 메인부유체의 상부에 설치되어, 항공기의 이착륙이 이루어지는 활주로, 메인부유체에 연결 설치되어, 메인부유체의 위치를 제어하는 위치제어수단, 메인부유체에 연결 설치되어, 해상의 파랑을 흡수하여 메인부유체를 평형상태로 유지시키는 동요억제수단을 포함하는 부유식 해상공항을 제공한다. 이와 같이, 부유식 해상공항은, 활주로를 메인부유체 상에 설치한 상태에서 해상에서 발생되는 파도는 위치제어수단과 더불어 동요억제수단에 의해 발생되는 상하방향으로의 왕복 운동에너지에 의해 흡수되는 바, 메인부유체가 파도의 영향을 받아 요동되는 것을 방지하면서 평형상태를 유지할 수 있게 되어 활주로 상에서 항공기의 안정적인 이착륙을 가능하게 한다.

Abstract translation: 提供一个浮动的离岸机场，包括：浮力浮在海上的主浮力体; 设在主浮体上方的飞机和飞机起飞/着陆的跑道; 位置控制装置，连接到主浮体并控制主浮体的位置; 以及振动抑制装置，其连接到主浮力体，并且通过吸收海上的波浪使得主浮力体能够保持在平衡状态。 具有设置在主浮体顶部的跑道的浮式离岸机场能够借助于通过振荡抑制装置产生的垂直往复运动能量以及位置控制装置来吸收海浪，以便 防止主浮体受到波浪和震动的影响，从而可以保持主浮力体的平衡状态，从而使飞机从跑道/跑道上稳定起飞/降落。

公开(公告)号：WO2014031074A1

公开(公告)日：2014-02-27

申请号：PCT/SG2012/000299

申请日：2012-08-23

Applicant: KEPPEL OFFSHORE & MARINE LTD ,  MERCHANT, Aziz, Amirali ,  NAH, Hock Choon, Edwin ,  HUANG, Xu Wen

Inventor： MERCHANT, Aziz, Amirali ,  NAH, Hock Choon, Edwin ,  HUANG, Xu Wen

IPC: B63B35/44 ,  B63B35/00 ,  B63B35/34 ,  E02B3/06 ,  B63B22/02

CPC classification number: B63B1/107 ,  B63B21/00 ,  B63B29/02 ,  B63B35/38 ,  B63B35/44 ,  B63B35/4413 ,  B63B35/50 ,  B63B39/005 ,  B63B2001/128 ,  B63B2035/4473

Abstract: A semi-submersible platform that is suitable to serve as a logistic hub at a remote offshore location. The semi-submersible platform is configured in a V-shape to reduce motion of the semi-submersible platform caused by rough sea conditions. The semi-submersible platform has a vessel docking area within the platform and a balancing unit to balance the unsymmetrical load of the platform that protects a vessel in the docking area from rough sea conditions.

Abstract translation: 一种半潜式平台，适用于远程离岸位置的物流枢纽。 半潜式平台被构造成V形，以减少由于海洋条件恶劣导致的半潜式平台的运动。 该半潜式平台在该平台内具有一个容器对接区域，以及一个平衡单元，用于平衡平台的不对称载荷，从而保护对接区域内的船只不受海洋环境的干扰。

公开(公告)号：WO2009091315A1

公开(公告)日：2009-07-23

申请号：PCT/SE2009/000010

申请日：2009-01-14

Applicant: CYBAERO AB ,  MÄRTENSSON, Johan ,  SEGERSTRÖM, Torbjörn ,  SETHSON, Magnus ,  GISING, Andreas

Inventor： MÄRTENSSON, Johan ,  SEGERSTRÖM, Torbjörn ,  SETHSON, Magnus ,  GISING, Andreas

IPC: B63B35/50 ,  B63G11/00 ,  B64F1/00

CPC classification number: B63B35/50 ,  G05D1/0684 ,  G05D1/0858

Abstract: A system for automatic or auto pilot controlled landing of air vehicle (2) with an undercarriage (10) with a substantially plane lower side, at a stationary or mobile landing place is described. The system is primarily characterized in that the landing plate is settable after two axes in roll and pitch, by a set mean controlled in relationship to the air vehicle and the horizontal plane. The air vehicle (2) and the landing plate (3) are provided with transmitter and receiver which define and communicate the mutual distance and the relative angles between the landing plate (3) and the undercarriage (10). Said set means is arranged to set said two axes such that the landing plate (3) will be substantially parallel to the lower side of the undercarriage (10).

Abstract translation: 描述了一种用于在静止或移动着陆点处的具有基本上平面的下侧的起落架（10）的空中车辆（2）的自动或自动驾驶员控制着陆的系统。 该系统的主要特征在于，着陆板可以在滚动和俯仰两个轴之后通过与空中车辆和水平面相关的设定平均值来设定。 机动车辆（2）和着陆板（3）设置有发射器和接收器，其限定和连通着陆板（3）和起落架（10）之间的相互距离和相对角度。 所述设置装置被布置成设置所述两个轴使得所述着陆板（3）将基本上平行于所述起落架（10）的下侧。