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61. 发明申请

US20110168834A1 DUCTED FAN VTOL VEHICLES 有权
标题翻译：导向风扇垂直起落车
公开(公告)号：US20110168834A1
公开(公告)日：2011-07-14
申请号：US12938444
申请日：2010-11-03
申请人： Raphael YOELI
发明人： Raphael YOELI
IPC分类号： B64C3/56 , B64C29/00 , B64C25/00 , B64C15/00 , B64D35/04 , B64D35/08 , B64C3/30 , B64D11/00 , F04D29/56
CPC分类号： B64C1/1415 , B64C1/22 , B64C3/40 , B64C27/08 , B64C27/20 , B64C29/0025 , B64C29/0033 , B64D7/00 , B64D17/80 , Y02T50/14
摘要： A vehicle including a fuselage having a longitudinal axis and a transverse axis, two Ducted Fan lift-producing propellers carried by the fuselage on each side of the transverse axis, a pilot's compartment formed in the fuselage between the lift-producing propellers and substantially aligned with one side of the fuselage, a payload bay formed in the fuselage between the lift-producing propellers and opposite the pilot's compartment, and two pusher fans located at the rear of the vehicle. Many variations are described enabling the vehicle to be used not only as a VTOL vehicle, but also as a multi-function utility vehicle for performing many diverse functions including hovercraft and ATV functions. Also described is an Unmanned version of the vehicle. Also described are unique features applicable in any single or multiple ducted fans and VTOL vehicles.
摘要翻译：一种包括具有纵向轴线和横向轴线的机身的车辆，由机身在横轴的每一侧承载的两个导风扇提升产生螺旋桨，形成在提升产生螺旋桨之间的机身中并基本上与在机身的一侧，形成在机身之间的机身中的有效载荷舱在提升产生螺旋桨之间并且与飞行员舱室相对，以及位于车辆后部的两个推进器风扇。描述了许多变型，使得车辆不仅可以用作垂直起降车辆，而且可以用作执行包括气垫船和ATV功能在内的许多不同功能的多功能多用途车辆。还描述了车辆的无人版本。还描述了适用于任何单个或多个管道风扇和垂直起落架车辆的独特特征。

62. 发明申请

US20100264270A1 Airfoil wing system for inflatable airfoils 失效
标题翻译：用于充气翼型的翼型翼系统
公开(公告)号：US20100264270A1
公开(公告)日：2010-10-21
申请号：US12583901
申请日：2009-08-27
申请人： Tony W. Mears
发明人： Tony W. Mears
IPC分类号： B64C3/30
CPC分类号： B64D17/025
摘要： An airfoil wing system for releasing air from an airfoil wing for an inflatable airfoil is provided. The airfoil wing is secured to the inflatable airfoil. The airfoil wing system comprises at least two wing panels connected together and an opening formed between the two wing panels wherein the opening automatically moves from a closed position to an open position to release air from beneath the airfoil wing thereby allowing takedown of the inflatable airfoil.
摘要翻译：提供了一种用于从用于可充气翼型的翼型翼释放空气的翼型翼系统。翼型翼固定到可充气翼面上。翼型翼系统包括连接在一起的至少两个翼板和形成在两个翼板之间的开口，其中开口自动地从关闭位置移动到打开位置，以从翼型翼下方释放空气，从而允许可充气翼片的移除。

63. 发明申请

US20050056731A1 Fiber matrix for a geometric morphing wing 有权
标题翻译：用于几何变形翼的纤维矩阵
公开(公告)号：US20050056731A1
公开(公告)日：2005-03-17
申请号：US10357022
申请日：2003-02-03
申请人： Brian Hamilton , Stephen Guymon , Gregory Dockter , Ahmed Hassan
发明人： Brian Hamilton , Stephen Guymon , Gregory Dockter , Ahmed Hassan
IPC分类号： B64C3/30 , B64C3/38 , B64C3/46 , B64C3/54 , B64C5/10 , B64C27/473 , B64C3/44
CPC分类号： B64C3/54 , B64C3/30 , B64C3/38 , B64C3/46 , B64C5/10 , B64C27/473 , B64C2003/445 , Y02T50/14
摘要： An airfoil member (14) includes a geometric morphing device (18). The geometric morphing device (18) has an inflatable member (30). The inflatable member (30) has an exterior wall (32) and multiple inflated states. The exterior wall (32) includes a layer with one or more fibers embedded therein. The exterior wall (32) controls size, shape, and expansion ability of the geometric morphing device (18).
摘要翻译：机翼构件（14）包括几何变形装置（18）。几何变形装置（18）具有可充气构件（30）。可膨胀构件（30）具有外壁（32）和多个充气状态。外壁（32）包括具有嵌入其中的一个或多个纤维的层。外壁（32）控制几何变形装置（18）的尺寸，形状和膨胀能力。

64. 发明授权

US5697579A Aircraft having inflatable tubular support structure 失效
标题翻译：飞机具有可充气的管状支撑结构
公开(公告)号：US5697579A
公开(公告)日：1997-12-16
申请号：US642984
申请日：1996-05-06
申请人： Masahiko Hayashi
发明人： Masahiko Hayashi
IPC分类号： B64B1/40 , B64B1/58 , B64C3/30 , B64C31/028 , B64D17/02
CPC分类号： B64B1/58 , B64B1/40 , B64C3/30 , B64C31/028 , B64D17/025
摘要： An airship has a flexible gas storage tube which forms a frame that maintains an inflated condition of an envelope of the airship permitting the envelope to be charged with hot air. A pump and valve are provided for supplying gas such as air, helium, and hydrogen to the gas storage tube.
摘要翻译：飞艇具有柔性储气管，其形成框架，其保持飞艇的信封的充气状态，允许信封充满热空气。提供泵和阀，用于将气体例如空气，氦气和氢气供应到储气管。

65. 发明授权

US5433404A Airfoil with variable geometry expansion surface 失效
标题翻译：具有可变几何膨胀表面的翼型
公开(公告)号：US5433404A
公开(公告)日：1995-07-18
申请号：US190052
申请日：1994-05-25
申请人： Patrick R. Ashill , John L. Fulker
发明人： Patrick R. Ashill , John L. Fulker
IPC分类号： B64C3/30 , B64C3/44 , B64C3/48 , B64C23/00
CPC分类号： B64C23/00 , B64C3/44 , B64C3/48 , Y02T50/145
摘要： A wing, or similar article of airfoil section, has a variable geometry surface for the active control of shock strength and transonic wave drag. In one embodiment, the wing has a region of distensible skin (4) aft of the line of maximum section, which extends along the span of the wing in those areas that experience drag. Pressure means (10, 20, 30) within the wing outwardly deflect the distensible region and produce a local bulge in the expansion surface. This bulge induces pre-shock compression and reduces the effect of the shock. The bulge is retracted by the natural elasticity of the skin material (which can be a conventional aluminum alloy) upon removal of the applied pressure. In another embodiment, the wing has a ramp portion (14) which is outwardly deflectable for the same purpose. The invention is applicable to supercritical and natural laminar flow wings.
摘要翻译： PCT No.PCT / GB92 / 01396 Sec。 371日期：1994年5月25日 102（e）日期1994年5月25日PCT提交1992年7月28日PCT公布。出版物WO93 / 02915 日期：1993年2月18日。翼或类似的翼型部件，具有可变的几何表面，用于主动控制冲击强度和跨音波阻力。在一个实施例中，机翼具有最大截面线后面的可膨胀皮肤（4）的区域，其在经历阻力的那些区域中沿翼的跨度延伸。翼内的压力装置（10,20,30）向外偏转可膨胀区域，并在膨胀表面产生局部凸起。这种凸起引起预冲击压缩并减少冲击的影响。在去除施加的压力时，凸起由于表皮材料（其可以是常规铝合金）的自然弹性而缩回。在另一个实施例中，机翼具有用于相同目的向外偏转的斜坡部分（14）。本发明适用于超临界和天然层流翅膀。

66. 发明授权

US4930724A Powered airfoil canopy aircraft 失效
标题翻译：动力翼型飞机
公开(公告)号：US4930724A
公开(公告)日：1990-06-05
申请号：US487221
申请日：1983-03-11
申请人： Stephen L. Snyder
发明人： Stephen L. Snyder
IPC分类号： B64C3/38 , B64C3/30 , B64C31/02 , B64C31/036 , B64C39/00 , B64D17/34
CPC分类号： B64C31/036 , Y10S244/902 , Y10S244/903
摘要： Load lines connect chordwise spaced portions of a ram air inflated, airfoil canopy to spaced anchors connected to a pilot supporting vehicle frame on which a forward thrust producing unit is removably mounted. The geometry of the assembled aircraft enhances take-off inflation of the canopy, establishes a stable flight frame when airborne, and enables simple engine throttle control of the thrust producing unit to regulate climb, descent and level flight. Common control is applied for both ground steering of the vehicle frame and airborne steering of the canopy.
摘要翻译：负载线将冲压空气充气的翼型罩的弦向间隔开的部分连接到连接到先导支撑车架的间隔的锚定件，前推力产生单元可拆卸地安装在导向支撑车架上。组装飞机的几何形状增强了机舱的起飞通风，在机载时建立了稳定的飞行框架，实现了推力发动机组的简单的发动机节气门控制，以调节爬升，降落和水平飞行。共同的控制适用于车架的地面转向和机舱的机载转向。

67. 发明授权

US3486719A Airship 失效
公开(公告)号：US3486719A
公开(公告)日：1969-12-30
申请号：US3486719D
申请日：1967-12-04
申请人： AEREON CORP
发明人： FITZPATRICK JOHN R , BOCK JUERGEN K
IPC分类号： B64B1/00 , B64B1/20 , B64C3/30 , B64C39/10 , B64D9/00 , B64B1/30
CPC分类号： B64D9/00 , B64B1/00 , B64B1/20 , B64C3/30 , B64C39/10 , Y02T50/46

68. 发明授权

US2969211A Inflatable-wing rocopter 失效
标题翻译：充气翼型龙头直升机
公开(公告)号：US2969211A
公开(公告)日：1961-01-24
申请号：US84483459
申请日：1959-10-06
申请人： VON SAURMA FRIEDRICH G
发明人： VON SAURMA FRIEDRICH G
IPC分类号： B64C3/30 , B64C27/02
CPC分类号： B64C27/022 , B64C3/30

69. 发明授权

US2967573A Pneumatic airfoil 失效
标题翻译：气动翼型
公开(公告)号：US2967573A
公开(公告)日：1961-01-10
申请号：US46233054
申请日：1954-10-14
申请人： GOODYEAR AIRCRAFT CORP
发明人： JOHNSON JR WILLIAM C
IPC分类号： B64C3/30
CPC分类号： B64C3/30

70. 发明授权

US11618548B2 Shear hardening material to suppress flutter in inflatable wings 有权
公开(公告)号：US11618548B2
公开(公告)日：2023-04-04
申请号：US17165186
申请日：2021-02-02
申请人： Toyota Motor Engineering & Manufacturing North America, Inc.
发明人： Umesh N. Gandhi , Ryohei Tsuruta
IPC分类号： B64C3/30 , B64C23/00 , B64C37/00
摘要： A reinforced, foldable component for an aircraft is provided, configured to stabilize a high frequency aeroelastic fluttering movement. The reinforced component may include a frame structure defining at least one air chamber, and a plurality of sealed compartments. A shear thickening fluid is disposed in at least one of the sealed compartments, exhibiting a decreasing viscosity responsive to an impact force. The frame structure may define one of an inflatable wing structure, a fairing structure, an aileron structure, and a stabilizer structure, and the like. The foldable component may include an exterior layer with an exterior surface exposed to an external environment and an interior layer adjacent the at least one air chamber, wherein the plurality of sealed compartments are disposed between the exterior layer and the interior layer. The exterior layer or the interior layer may include an impact-resistant fabric layer including a shear thickening material.

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