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1.发明授权公开(公告)号：US09828107B1
公开(公告)日：2017-11-28
申请号：US14835567
申请日：2015-08-25
IPC分类号： B64D31/06 , B64C29/00 , A62C37/10 , B64B1/06 , A62C3/02 , B64B1/00 , B64C13/00 , B64B1/34 , B64B1/08 , A62C19/00 , G05D1/04 , B64C27/52 , G05D1/08 , B64C27/20 , B64B1/10 , B64B1/12 , B64C27/00 , B64C13/04 , B64C13/20 , G06F7/00 , B64B1/36 , G06N5/00
CPC分类号： B64D31/06 , A62C3/02 , A62C19/00 , A62C37/10 , B64B1/00 , B64B1/06 , B64B1/08 , B64B1/10 , B64B1/12 , B64B1/34 , B64B1/36 , B64C13/00 , B64C13/04 , B64C13/20 , B64C27/00 , B64C27/20 , B64C27/52 , B64C29/00 , B64C29/0033 , G05D1/0077 , G05D1/04 , G05D1/08 , G06F7/00 , G06N5/00
摘要： The present invention provides a vehicle with redundant systems to increase the overall safety of the vehicle. In other aspects, the present invention provides a method for learning control of non-linear motion systems through combined learning of state value and action-value functions.
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公开(公告)号：US20160332714A1
公开(公告)日：2016-11-17
申请号：US15222704
申请日：2016-07-28
CPC分类号： B64B1/02 , B64B1/10 , B64B1/12 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/32 , B64B1/34 , B64B1/58 , B64B2201/00 , B64D27/24 , B64D2211/00 , G05D1/0011
摘要： An air vehicle comprises a vehicle body and a propulsion assembly. The vehicle body has the shape of a wing airfoil so that the vehicle body generates lift when air flows over the vehicle body. The vehicle body has a body longitudinal axis, and includes a first hull and a second hull that are secured together side-by-side, the hulls having longitudinal axes that are substantially parallel to the body longitudinal axis. Each hull defines a separate fluid chamber that is filled with a fluid that is at least partially buoyant. The propulsion assembly is secured to the vehicle body. The propulsion assembly generates thrust and includes a port front engine, a port rear engine, a starboard front engine, and a starboard rear engine, wherein at least two of the engines have independently controlled thrust vectors.
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公开(公告)号：US20140339356A1
公开(公告)日：2014-11-20
申请号：US14324306
申请日：2014-07-07
申请人： Athene Works Limited
CPC分类号： B64B1/02 , B64B1/08 , B64B1/10 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/38 , B64B1/64 , B64B2201/00 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/101 , B64C2201/122 , B64C2201/127 , B64C2201/165 , B64C2201/167 , H01Q1/36 , H01Q9/27
摘要： An aerial vehicle comprises an elongate envelope within which are at least one first compartment for holding a lighter than air gas and at least one second compartment for holding atmospheric air and said at least one second compartment having an inlet and an outlet and at least one pair of wings extending laterally from the envelope; said wings being planar units with a leading and trailing edge, the width of the wings from their leading edges to their trailing edges being substantially less than the length of the envelope with airfoil portions fitted between the leading and trailing edges of the wing: the top and bottom of the wings are mirror images of one another; in which forward motion of the vehicle is obtainable without trust through alternate diving and climbing motion.
摘要翻译： 一种空中飞行器包括一个细长的外壳，其中至少有一个用于保持比空气气体轻的第一隔间和至少一个用于保持大气空气的第二隔室，并且所述至少一个第二隔室具有入口和出口以及至少一对 的翼从信封横向延伸; 所述翼是具有前缘和后缘的平面单元，翼从其前缘到其后缘的宽度基本上小于具有机翼部分装配在翼的前缘和后缘之间的封套的长度：顶部 翅膀的底部是彼此的镜像; 其中车辆的向前运动通过交替的潜水和爬坡运动而不被信任地获得。
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4.发明申请公开(公告)号：US20130175382A1
公开(公告)日：2013-07-11
申请号：US13716281
申请日：2012-12-17
申请人： Rinaldo Brutoco
发明人： Rinaldo Brutoco
CPC分类号： B64B1/62 , B64B1/00 , B64B1/06 , B64B1/12 , B64B1/20 , B64B1/32 , B64B1/66 , B64F1/02 , F42B15/00 , Y10T137/6906
摘要： A hydrogen airship for efficiently transporting hydrogen from where it can be economically made to where it is most needed using specially designed airships. Hydrogen can be delivered from the place where it is produced to the place where it is needed using an airship in which the hydrogen gas can also be used for generating lift, providing propulsion energy and serving ancillary needs. A unique docking system can use a remotely piloted unmanned aircraft flown from the mother craft to carry a guide line into a receiving attachment point.
摘要翻译： 氢气飞艇能够从经济上高效运输氢气到特别设计的飞艇最需要的地方。 氢气可以从生产地点运送到需要的地方，使用其中氢气也可以用于产生升降机的飞艇，提供推进能量和服务辅助需求。 独特的对接系统可以使用从母机飞行的遥控无人驾驶飞机将引导线运送到接收附件点。
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公开(公告)号：US3598631A
公开(公告)日：1971-08-10
申请号：US3598631D
申请日：1969-03-19
申请人： HERMANN E R PAPST
发明人： PAPST HERMANN E R
摘要： A LOW-FRICTION FLOW SURFACE FOR AIRSHIP ENVELOPES OR OUTER SURFACES OF AIRPLANES, FLOW SURFACES OF WIND-TUNNELS AND THE LIKE AND THE PROCESS FOR MANUFACTURING SUCH LOWFRICTION FLOW SURFACES WHEREIN A METAL FOIL IS HEATED AND, AT THE SAME TIME, DE-GASSED IMMEDIATELY AFTER WHICH A HYDROPHOBE LAYER IS APPLIED TO THE HEATED FOIL IN A VACUUM OR A PROTECTIVE GAS WITH SAID HYDROPHOBE LAYER BEING APPLIED BY SQUEEZING AND SUBSEQUENTLY EVEN-MELTING THE MATERIAL OF THE HYDROPHOBE LAYER ONTO THE FOIL.
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公开(公告)号：US09969481B2
公开(公告)日：2018-05-15
申请号：US15160874
申请日：2016-05-20
IPC分类号： B64B1/12 , G08G5/00 , B64B1/10 , B64B1/14 , B64B1/22 , B64B1/24 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/02 , G09F21/04 , G09F21/06 , B64B1/00 , B64B1/18 , G05D1/00 , B64B1/36 , G05D1/10
CPC分类号： B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
摘要： An intelligence, surveillance, and reconnaissance system is disclosed including a ground station and one or more aerial vehicles. The aerial vehicles are autonomous systems capable of communicating intelligence data to the ground station and be used as part of a missile delivery package. A plurality of aerial vehicles can be configured to cast a wide net of reconnaissance over a large area on the ground including smaller overlapping reconnaissance areas provided by each of the plurality of the aerial vehicles.
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公开(公告)号：US20160375976A1
公开(公告)日：2016-12-29
申请号：US15160874
申请日：2016-05-20
CPC分类号： B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
摘要： An intelligence, surveillance, and reconnaissance system is disclosed including a ground station and one or more aerial vehicles. The aerial vehicles are autonomous systems capable of communicating intelligence data to the ground station and be used as part of a missile delivery package. A plurality of aerial vehicles can be configured to cast a wide net of reconnaissance over a large area on the ground including smaller overlapping reconnaissance areas provided by each of the plurality of the aerial vehicles.
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8.发明申请LIFTING ENTRY/ATMOSPHERIC FLIGHT (LEAF) UNIFIED PLATFORM FOR ULTRA-LOW BALLISTIC COEFFICIENT ATMOSPHERIC ENTRY AND MANEUVERABLE ATMOSPHERIC FLIGHT AT SOLAR SYSTEM BODIES 审中-公开提升进入/大气飞行（LEAF）统一的平台，用于超低温度系统大气入口和可转换的太阳系系统大气层飞行公开(公告)号：US20150210407A1
公开(公告)日：2015-07-30
申请号：US14297370
申请日：2014-06-05
发明人： KRISTEN S. GRIFFIN , JON CARPENTER , GREGORY J. LEE , AMY LO , RONALD POLIDAN , DANIEL SOKOL , BARNABY WAINFAN , WARREN JAMES , DENNIS POULOS
CPC分类号： B64G1/62 , B64B1/12 , B64B1/20 , B64B1/24 , B64B2201/00 , B64D2211/00 , B64G1/007 , B64G1/242 , B64G2001/1064 , B64G2001/224 , Y02T50/55
摘要： An aerial vehicle including a collapsible and inflatable vehicle body capable of being filled with a lighter than air gas so as to make the vehicle semi-buoyant or 100% buoyant at a predetermined altitude in an atmosphere above a solar system body. The vehicle body has a shape suitable to provide aerodynamic lift. The vehicle may include a propulsion device coupled to and extending from the vehicle body, where the device provides power to aerodynamically lift the vehicle above the 100% buoyant altitude to a higher altitude where the vehicle can maintain that altitude through the aerodynamic lift and vehicle buoyancy. The vehicle is configured to be deployed/inflated from a collapsed and stowed configuration to a deployed/inflated configuration in an orbit above the atmosphere of the solar system body, and is configured to enter the atmosphere in the inflated configuration and descend without propulsion.
摘要翻译： 一种飞行器，其包括可折叠且可充气的车身，其能够充满比空气更轻的车辆，以使得车辆在太阳系体上方的气氛中在预定高度上半浮力或100％浮力。 车体具有适于提供气动升力的形状。 车辆可以包括联接到车身并从车身延伸的推进装置，其中该装置提供动力以将车辆空气动力地提升到高于100％浮力高度的高度，其中车辆可以通过空气动力升力和车辆浮力保持高度 。 车辆被构造成从塌陷和收起的构造展开/充气到位于太阳系体内的空气上方的轨道上的展开/膨胀构造，并且被构造成以膨胀构型进入大气并且不推动下降。
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公开(公告)号：US20150076279A1
公开(公告)日：2015-03-19
申请号：US14485685
申请日：2014-09-13
CPC分类号： B64B1/02 , B64B1/10 , B64B1/12 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/32 , B64B1/34 , B64B1/58 , B64B2201/00 , B64D27/24 , B64D2211/00 , G05D1/0011
摘要： An air vehicle comprises a vehicle body and a propulsion assembly. The vehicle body has the shape of a wing airfoil so that the vehicle body generates lift when air flows over the vehicle body. The vehicle body has a body longitudinal axis, and includes a first hull and a second hull that are secured together side-by-side, the hulls having longitudinal axes that are substantially parallel to the body longitudinal axis. Each hull defines a separate fluid chamber that is filled with a fluid that is at least partially buoyant. The propulsion assembly is secured to the vehicle body. The propulsion assembly generates thrust and includes a port front engine, a port rear engine, a starboard front engine, and a starboard rear engine, wherein at least two of the engines have independently controlled thrust vectors.
摘要翻译： 一种机动车辆包括车体和推进组件。 车身具有翼型件的形状，使得当空气流过车体时车身产生升力。 车体具有主体纵向轴线，并且包括并排固定在一起的第一船体和第二船体，所述船体具有基本上平行于主体纵向轴线的纵向轴线。 每个船体限定了一个单独的流体室，其中填充有至少部分浮力的流体。 推进组件固定在车体上。 推进组件产生推力并且包括端口前置发动机，端口后部发动机，右舷前置发动机和右舷后部发动机，其中至少两个发动机具有独立控制的推力矢量。
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公开(公告)号：US20120248241A1
公开(公告)日：2012-10-04
申请号：US13430010
申请日：2012-03-26
申请人： John Goelet
发明人： John Goelet
CPC分类号： B64B1/68 , B64B1/00 , B64B1/06 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/34 , B64B1/58 , B64B1/60 , B64B2201/00 , B64C25/32 , B64C25/56 , B64D2211/00
摘要： An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship.
摘要翻译： 提供飞艇。 飞艇包括构造成容纳气体的船体，耦合到船体的至少一个推进组件，并且包括推进装置，以及包括多个整流罩结构（包括一个或多个板条）的至少一个空气动力部件，其中所述至少一个空气动力学 组件与船体相关联，并且被配置为引导飞艇周围的气流。
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