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1. 发明申请

US20180043640A1 BOND FIXTURE FOR ROOT END LAMINATE OR ROTOR BLADE 审中-公开
公开(公告)号：US20180043640A1
公开(公告)日：2018-02-15
申请号：US15232265
申请日：2016-08-09
申请人： Sikorsky Aircraft Corporation
发明人： Sven Roy Lofstrom , Ryan Lehto
IPC分类号： B29C70/44 , B64F5/00 , B64C27/32
CPC分类号： B29C70/44 , B29L2031/082 , B64C27/32 , B64C27/46 , B64F5/10 , B64F5/40
摘要： A bond assembly includes a fixture having a first section movably coupled to a second section. The first section and the second section are disposed opposite one another. A bladder assembly is mounted to at least one of the first section and the second section. The bladder assembly is configured to apply controlled, localized pressure and heat to a component receivable between the first section and the second section.

2. 发明申请

US20170212528A1 Apparatus and Method for Autonomous Landing of an Aerial Vehicle 审中-公开
公开(公告)号：US20170212528A1
公开(公告)日：2017-07-27
申请号：US15006460
申请日：2016-01-26
申请人： Patrick A. Henderson
发明人： Patrick A. Henderson
IPC分类号： G05D1/06 , G05D1/10 , B64F1/00 , B64C39/02
CPC分类号： G05D1/0676 , B64C27/46 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/145 , B64C2201/18 , B64F1/00
摘要： An apparatus and method of autonomously landing an aerial vehicle is disclosed herein. In a non-limiting embodiment, the apparatus is a landing pad controller that includes a plurality of receiving antennae, each of which is configured to receive an instance/version of a localization signal from the aerial vehicle. A localization calculation processor determines a precise position of the aerial vehicle based upon a comparison of the localization signal received by each of the plurality of receiving antennae. The landing pad controller also includes a transmitter that sends at least one course direction adjustment to the aerial vehicle, which can be used to direct the aerial vehicle from the precise position to a target landing area.

3. 发明申请

US20150251757A1 VERTICAL SHORT TAKEOFF AND LANDING APPARATUS 审中-公开
标题翻译：垂直吊带和吊装装置
公开(公告)号：US20150251757A1
公开(公告)日：2015-09-10
申请号：US14659282
申请日：2015-03-16
申请人： RADEUS LABS, INC.
发明人： Raymond Don Hayden, III
IPC分类号： B64C39/02 , B64C27/46 , B64C29/00 , B64C27/39
CPC分类号： B64C39/024 , B64C27/20 , B64C27/39 , B64C27/46 , B64C29/00 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/12 , B64C2201/127 , B64C2201/146
摘要： Methods and apparatus for vertical or short takeoff and landing. In one embodiment, the apparatus comprises two or more counter driven rings with one or more airfoils attached. In one variant, there is an upper ring and a lower ring, each with multiple airfoils attached. In one variant, lift is generated largely via ambient air currents, allowing for long term on-station operation of the device.
摘要翻译：垂直或短时起飞和着陆的方法和装置。在一个实施例中，该装置包括两个或多个连接有一个或多个翼型件的反向驱动环。在一个变型中，存在上环和下环，每个具有多个翼型件连接。在一个变型中，电梯主要通过环境气流产生，从而允许设备的长期驻车操作。

4. 发明申请

US20140369850A1 CROSS-LINKABLE COATING COMPOSITION AND METHOD OF PRODUCING THE SAME 有权
标题翻译：交联涂料组合物及其制造方法
公开(公告)号：US20140369850A1
公开(公告)日：2014-12-18
申请号：US13920341
申请日：2013-06-18
申请人： ROHM AND HAAS COMPANY , DOW GLOBAL TECHNOLOGIES LLC
发明人： Paul J. Popa , Ben W. Schaefer , John N. Argyropoulos , Kenneth E. Wohltmann , Sandra Hofmann , Daniel Haile , Paul Foley , YanXiang Li
IPC分类号： C09D133/08 , F03D1/06 , B64C27/46 , F01D5/28
CPC分类号： B64C27/46 , C08G12/46 , C08K5/07 , C09D133/10 , C09D161/20 , F01D5/288 , F05B2280/6011 , F05D2300/43 , Y02E10/721 , Y02T50/672 , C09D133/14 , C08F2220/1825 , C08F220/20 , C08F2220/1858 , C08F220/14 , C08F2220/1875 , C08F220/06
摘要： The instant invention provides cross-linkable coating compositions, process for producing the same, and substrates coated therewith. The cross-linkable coating composition comprises: (a) polyaldehyde, or acetal or hemiacetal thereof; (b) an acid catalyst having pKa of less than 6; (c) a liquid media; (d) an acrylic polycarbamate comprising at least an average of 2.0 carbamate functional groups, wherein said polycarbamate has a glass transition (Tg) of less than 25° C.; and (e) one or more fillers having a pH in the range of equal to or less than 9 and/or one or more pigments having a pH in the range of equal to or less than 9, and/or one or more additives having a pH in the range of equal to or less than 9, wherein said composition has a curing temperature in the range of less than 70° C.
摘要翻译：本发明提供了可交联的涂料组合物，其制备方法和用其涂布的基材。可交联涂料组合物包含：（a）多醛，或其缩醛或半缩醛; （b）pKa小于6的酸催化剂; （c）液体介质; （d）包含至少平均2.0个氨基甲酸酯官能团的丙烯酸聚氨酯，其中所述聚氨酯具有小于25℃的玻璃化转变温度（Tg）。和（e）一种或多种pH值在等于或小于9的范围内的一种或多种填料和/或一种或多种pH值在等于或小于9的范围内的颜料，和/或一种或多种添加剂具有 pH在等于或小于9的范围内，其中所述组合物的固化温度在小于70℃的范围内。

5. 发明授权

US08459948B2 Retractable composite rotor blade assembly 有权
标题翻译：伸缩复合转子叶片组件
公开(公告)号：US08459948B2
公开(公告)日：2013-06-11
申请号：US12582889
申请日：2009-10-21
申请人： Esteban A. Caraballoso , Ali M. Sadegh
发明人： Esteban A. Caraballoso , Ali M. Sadegh
IPC分类号： B64C11/28
CPC分类号： B64C27/50 , B64C11/28 , B64C27/46 , B64C27/473 , B64C27/51 , B64C2027/4736 , F05D2250/90
摘要： A retractable rotor blade for a flying vehicle includes an interlink assembly having interconnected link base subassemblies, a helical ribbon assembly reinforcing the interlink assembly, and a flexible and elastic sleeve that covers the interlink and helical ribbon assemblies in extended and retracted states of the rotor blade. Each link base subassembly has a damper for dampening movement of the interlink assembly during extension and retraction of the rotor blade, a pair of retractable links by which the link base subassembly is interconnected with another of the link base subassemblies, a link hub, and a pair of locking arms housed in the link hub for locking the rotor blade in the extended state. The helical ribbon assembly has sequentially overlapped ribbons helically wound around the interlink assembly. The flexible and elastic sleeve has a flexible and elastic skin and elastic ribs for imparting rigidity to the flexible and elastic skin.
摘要翻译：用于飞行车辆的可伸缩转子叶片包括具有相互连接的基座子组件的互连组件，加强相互连接组件的螺旋形带组件以及在转子叶片的延伸和缩回状态下覆盖互连和螺旋形带组件的柔性和弹性套筒。每个链接底座组件具有阻尼器，用于在转子叶片的延伸和缩回期间阻尼互连组件的运动，一对可缩回的连杆，链节基部组件通过该可伸缩的连杆与另一个连杆底座组件相连，一对锁定臂容纳在连接毂中，用于将转子叶片锁定在伸出状态。螺旋带组件具有螺旋缠绕在互连组件周围的顺序重叠的带。柔性和弹性套筒具有弹性和弹性的皮肤和弹性肋，用于赋予柔性和弹性皮肤刚性。

6. 发明申请

US20120219417A1 DISC ROTOR RETRACTION SYSTEM 有权
标题翻译：光盘转子回缩系统
公开(公告)号：US20120219417A1
公开(公告)日：2012-08-30
申请号：US13037205
申请日：2011-02-28
申请人： Daniel M. Podgurski
发明人： Daniel M. Podgurski
IPC分类号： F04D29/36 , F04D19/00
CPC分类号： B64C27/32 , B64C11/003 , B64C27/00 , B64C27/30 , B64C27/46 , B64C27/467 , B64C27/473
摘要： A disc rotor blade retraction system includes a main blade spar incorporating a hydraulic cylinder and having a screw thread, A ball screw is concentrically carried within the main blade spar and is operably connected to a ball nut which has an outboard end connected to an intermediate spar with a hydraulic piston received for reciprocation in the hydraulic cylinder. A first geared actuator engages the ball screw and a second geared actuator engages the main blade spar screw thread. A hydraulic fluid accumulator providing pressurized hydraulic fluid is connected to an outboard end of the hydraulic cylinder and a controller actuates the first and second geared actuators.
摘要翻译：圆盘转子叶片回缩系统包括一个包括液压缸并具有螺纹的主叶片翼梁。一个滚珠丝杠同心地承载在主叶片翼梁内，并且可操作地连接到一个滚珠螺母，该滚珠螺母具有连接到中间翼梁的外侧端液压活塞被接收用于在液压缸中往复运动。第一个齿轮传动执行机构接合滚珠丝杠，第二个齿轮传动部件接合主叶片翼梁螺纹。提供加压液压流体的液压流体蓄能器连接到液压缸的外侧端，并且控制器致动第一和第二齿轮传动的致动器。

7. 发明授权

US07475847B2 Retractable lifting blades for aircraft 有权
标题翻译：用于飞机的伸缩式提升叶片
公开(公告)号：US07475847B2
公开(公告)日：2009-01-13
申请号：US11317855
申请日：2005-12-22
申请人： Allen J. Gerbino
发明人： Allen J. Gerbino
IPC分类号： B64C27/52
CPC分类号： B64C27/022 , B64C27/26 , B64C27/30 , B64C27/32 , B64C27/46 , B64C27/605
摘要： A rotor blade assembly for providing vertical lift to an aircraft, having a rotor head and a plurality of blades, with each blade attached to a mechanism such as a cam surface, whereby movement of the mechanism causes the radial distance between the distal tip of the attached blade and the center of the rotor head to alter, decreasing or increasing the length of the lifting surface. The blades are moved from a fully extended position providing maximum lift, to a retracted position in which the blades are removed from the airstream. The pitch of the blades may be controlled by a pitch controller to achieve full helicopter responsiveness. A plurality of bladeletts may be positioned near the outer periphery of the rotor head. When they are moved into the airstream, passing air impacts the bladeletts exerting a pressure, causing rotational movement of the rotor blade assembly.
摘要翻译：一种用于向航空器提供垂直升降机的转子叶片组件，其具有转子头部和多个叶片，每个叶片附接到诸如凸轮表面的机构，由此机构的运动导致所述机翼的远端之间的径向距离连接的叶片和转子头的中心以改变，减小或增加提升表面的长度。叶片从提供最大提升的完全延伸位置移动到叶片从气流中移除的缩回位置。叶片的桨距可由桨距控制器控制，以实现全直升机响应。多个叶片可以位于转子头的外周边附近。当它们移入气流中时，通过的空气冲击施加压力的叶片，引起转子叶片组件的旋转运动。

8. 发明申请

US20080145219A1 VORTEX GENERATORS ON ROTOR BLADES TO DELAY AN ONSET OF LARGE OSCILLATORY PITCHING MOMENTS AND INCREASE MAXIMUM LIFT 有权
标题翻译：转子叶片上的VORTEX发生器延迟了大量的振荡器摆动，并增加了最大的提升
公开(公告)号：US20080145219A1
公开(公告)日：2008-06-19
申请号：US11610317
申请日：2006-12-13
申请人： Michael A. McVeigh , Robert F. Maciolek
发明人： Michael A. McVeigh , Robert F. Maciolek
IPC分类号： F01D5/14
CPC分类号： F03D1/0675 , B64C23/06 , B64C27/46 , F05B2240/32 , F05B2250/61 , F05D2240/31 , F05D2250/61 , Y02E10/721 , Y02T50/162 , Y02T50/673
摘要： An airborne mobile platform generally includes a plurality of rotating rotor blades operating in an airflow that forms a boundary layer on each of the rotor blades. At least one of the rotor blades includes a section that encounters the airflow that includes an unsteady subsonic airflow having at least a varying angle of attack. At least one of the rotor blades also includes one or more vortex generators on the at least one of the rotor blades that generate a vortex that interacts with the boundary layer to at least delay an onset of separation of the boundary layer, to increase a value of an unsteady maximum lift coefficient and to reduce a value of an unsteady pitching moment coefficient for the section.
摘要翻译：机载移动平台通常包括在形成每个转子叶片上的边界层的气流中操作的多个旋转转子叶片。至少一个转子叶片包括遇到气流的部分，该部分包括具有至少不同的迎角的不稳定的亚音速气流。转子叶片中的至少一个还包括在至少一个转子叶片上的一个或多个涡流发生器，其产生与边界层相互作用的至少延迟边界层分离开始的涡流，以增加值的不稳定的最大升力系数，并减小该段的不稳定俯仰力矩系数的值。

9. 发明授权

US07326435B2 Method of illuminating a rotary blade by application of a photoluminescent paint 失效
标题翻译：通过应用光致发光涂料照射旋转刀片的方法
公开(公告)号：US07326435B2
公开(公告)日：2008-02-05
申请号：US10623186
申请日：2003-07-21
申请人： Thomas Martin Buckingham , Wallace Michael Elger
发明人： Thomas Martin Buckingham , Wallace Michael Elger
IPC分类号： B05D5/00 , B05D1/00
CPC分类号： C09D5/22 , B64C11/16 , B64C27/46
摘要： Low light level illumination is applied to rotary blades of vehicles to increase visibility to minimize ground injuries. Either photoluminescent paint or photoluminescent film may be affixed to rotary blades in use to help deter accidents. An electro-luminescent film may be integrated into future rotary blades to provide greater visibility without making the vehicle vulnerable to detection.
摘要翻译：车辆的旋转叶片应用低光照度以提高可见度，以减少地面伤害。光致发光涂料或光致发光膜可以在使用中固定到旋转刀片上以帮助阻止事故。电致发光膜可以集成到未来的旋转叶片中以提供更大的可视性而不使车辆易于检测。

10. 发明申请

US20050207895A1 Aerofoils 有权
标题翻译：机动航空
公开(公告)号：US20050207895A1
公开(公告)日：2005-09-22
申请号：US10958589
申请日：2004-10-06
申请人： Shaun Dunn
发明人： Shaun Dunn
IPC分类号： B64C27/467 , B64C21/02 , B64C21/04 , B64C23/06 , B64C27/46 , B63H1/26
CPC分类号： B64C27/46 , B64C2230/04 , B64C2230/20 , B64C2230/22 , B64C2230/28 , Y02T50/166
摘要： An aerofoil has a body, and at least one flow control device, the flow control device including a passage within the body of the aerofoil, and a passage outlet at an upper aerofoil surface of the aerofoil, whereby in use, air from the passage passes through the passage outlet to affect airflow over the upper surface of the aerofoil over at least a range of incidence angles, wherein the passage outlet is provided by an outlet fitting which is secured relative to the upper surface of the aerofoil, the outlet fitting including a surface part which lies contiguously with the surrounding upper aerofoil surface so there is no or only a minimal discontinuity where the surface part and the surrounding upper aerofoil surface interface, the surface part of the fitting further including an opening which communicates with the passage within the body of the aerofoil.
摘要翻译：机翼具有主体和至少一个流量控制装置，该流量控制装置包括在机翼的主体内的通道和在机翼的上部机翼表面处的通道出口，由此在使用中，来自通道的空气通过通过通道出口在至少一个入射角范围内影响机翼上表面上的气流，其中通道出口由相对于机翼的上表面固定的出口接头提供，出口接头包括一个表面部分与周围的上机翼表面相邻，因此没有或只有最小的不连续性，其中表面部分和周围的上翼面接合，配件的表面部分还包括与体内的通道连通的开口的机翼。

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