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公开(公告)号：US20170267371A1
公开(公告)日：2017-09-21
申请号：US15075097
申请日：2016-03-18
CPC分类号： B64D43/02 , B64D43/00 , G01F1/32 , G01F1/46 , G01F1/68 , G01P5/00 , G01P5/165 , G01P13/025 , G05D1/104
摘要： Embodiments of methods and apparatus for close formation flight are provided herein. In some embodiments, a method of sensing three dimensional (3D) airflow by an aircraft includes: collecting measurements characterizing airflow near the aircraft; analyzing the collected measurements; creating, by a processor, a computer model predicting one or more 3D airflow patterns parameter values based on the analyzing; obtaining one or more additional measurements characterizing airflow near an aircraft of the plurality of aircraft, and evaluating an error between an airflow parameter value predicted by the computer model and the one or more additional measurement.
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2.发明申请DISTRIBUTED SOLAR POWER PLANT AND A METHOD OF ITS CONNECTION TO THE EXISTING POWER GRID 有权分布式太阳能发电厂及其与现有电力网连接的方法公开(公告)号：US20130342021A1
公开(公告)日：2013-12-26
申请号：US14015372
申请日：2013-08-30
发明人： MICHAEL CYRUS , SERGEY V. FROLOV
IPC分类号： H02J3/00
CPC分类号： H02J3/00 , H02J3/382 , H02J3/383 , H02J3/386 , Y02E10/563 , Y02E10/763 , Y10T307/615 , Y10T307/642 , Y10T307/658 , Y10T307/718
摘要： Methods and apparatus are provided for using a renewable source of energy such as solar, wind, or geothermal energy. In some embodiments, the method may include generating electric energy from a renewable form of energy at a plurality of locations at which reside an electric power line associated with an electric power grid. The electric energy generated at each location may be transferred to the electric power line to thereby supply electric energy to the electric power grid.
摘要翻译： 提供了使用可再生能源（如太阳能，风能或地热能）的方法和装置。 在一些实施例中，该方法可以包括在驻留在与电网相关联的电力线的多个位置处从可再生形式的能量产生电能。 在每个位置处产生的电能可以传送到电力线，从而向电力网提供电能。
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公开(公告)号：US20180281984A1
公开(公告)日：2018-10-04
申请号：US16007293
申请日：2018-06-13
IPC分类号： B64D43/02 , G01F1/32 , G01F1/46 , G05D1/10 , B64D43/00 , G01F1/68 , G01P5/165 , G01P13/02 , G01P5/00
摘要： Embodiments of methods and apparatus for close formation flight are provided herein. In some embodiments, a method of sensing three dimensional (3D) airflow by an aircraft includes: collecting measurements characterizing airflow near the aircraft; analyzing the collected measurements; creating, by a processor, a computer model predicting one or more 3D airflow patterns parameter values based on the analyzing; obtaining one or more additional measurements characterizing airflow near an aircraft of the plurality of aircraft, and evaluating an error between an airflow parameter value predicted by the computer model and the one or more additional measurement.
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公开(公告)号：US20160363938A1
公开(公告)日：2016-12-15
申请号：US14737814
申请日：2015-06-12
CPC分类号： G05D1/104 , B64C3/56 , B64C29/0016 , B64C37/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/102 , B64C2201/128 , B64C2201/143 , B64C2201/145 , B64D1/02 , G05D1/0022 , G05D1/0027 , G05D1/005 , G05D1/0212 , G05D1/0669 , G05D1/102 , G08G5/0008 , G08G5/0013 , G08G5/0017 , G08G5/0021 , G08G5/003 , G08G5/0065 , G08G5/0069 , G08G5/025 , G08G5/045 , G08G7/02 , Y02T50/14
摘要： Embodiments of the present invention provide an alternative distributed airborne transportation system. In some embodiments, a method for distributed airborne transportation includes: providing an airborne vehicle with a wing and a wing span, having capacity to carry one or more of passengers or cargo; landing of the airborne vehicle near one or more of passengers or cargo and loading at least one of passengers or cargo; taking-off and determining a flight direction for the airborne vehicle; locating at least one other airborne vehicle, which has substantially the same flight direction; and joining at least one other airborne vehicle in flight formation and forming a fleet, in which airborne vehicles fly with the same speed and direction and in which adjacent airborne vehicles are separated by distance of less than 100 wing spans.
摘要翻译： 本发明的实施例提供了一种替代的分布式机载运输系统。 在一些实施例中，一种用于分布式机载运输的方法包括：向机载车辆提供机翼和机翼跨度，具有携带乘客或货物中的一个或多个的能力; 机载车辆靠近一个或多个乘客或货物并装载至少一个乘客或货物; 起飞和确定机载飞行方向; 至少定位一个具有大致相同的飞行方向的其他机载车辆; 并将至少一架其他机载车辆接入飞行形成并形成一个舰队，其中机载车辆以相同的速度和方向飞行，并且相邻的机载车辆以小于100个翼跨的距离分开。
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5.发明申请公开(公告)号：US20160046387A1
公开(公告)日：2016-02-18
申请号：US14462152
申请日：2014-08-18
IPC分类号： B64D47/00 , B64D35/02 , B64C19/00 , B64D31/00 , H04B7/185 , B64B1/00 , G08G5/00 , G05D1/10 , G08G5/04 , B64D33/00 , B64C39/02
CPC分类号： B64D47/00 , B64B1/00 , B64C19/00 , B64C39/02 , B64C2201/022 , B64C2201/042 , B64C2201/06 , B64C2201/122 , B64C2201/143 , B64D31/00 , B64D33/00 , B64D35/02 , G05D1/104 , G08G5/0069 , H04B7/18508
摘要： Embodiments of methods and apparatus for providing distributed airborne wireless communications are provided herein. In some embodiments, a communication fleet includes: an airborne communication payload subdivided into multiple payload sections; and a plurality of airborne platforms each including a payload section, wherein each airborne platform comprises an airframe, a propulsion system, a power system, and flight control electronics, wherein the propulsion system is configured to provide propulsion power and thrust to maintain level flight, ascend, descend and maneuver the airborne platform, wherein the power system provides electrical power to the propulsion system, the flight control electronics, and the payload section, and wherein the flight control electronics provide capability to control a position, speed, and flight pattern of the airborne platform.
摘要翻译： 本文提供了用于提供分布式机载无线通信的方法和装置的实施例。 在一些实施例中，通信车队包括：被分为多个有效载荷部分的机载通信有效载荷; 以及多个机载平台，每个机载平台各自包括有效载荷部分，其中每个机载平台包括机体，推进系统，电力系统和飞行控制电子设备，其中所述推进系统被配置为提供推进力和推力以维持水平飞行， 上升，下降和操纵机载平台，其中电力系统向推进系统，飞行控制电子装置和有效载荷部分提供电力，并且其中飞行控制电子装置提供控制位置，速度和飞行模式的能力 机载平台。
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公开(公告)号：US20140203139A1
公开(公告)日：2014-07-24
申请号：US14091969
申请日：2013-11-27
CPC分类号： B64C1/0009 , B64C1/34 , B64C3/46 , B64C39/024 , B64C2201/105 , B64D2211/00 , G01S3/7861 , Y02T50/14
摘要： Methods and apparatus for an adaptable solar airframe are provided herein. In some embodiments, an adaptable solar airframe includes an expandable body having an aerodynamic cross-section that reduces parasitic air drag at any given thickness of the body, further being able to change its shape in flight in response to changes in the relative position of the sun; and a flexible solar PV system attached to the surface of the expandable body.
摘要翻译： 本文提供了适用于太阳能机身的方法和装置。 在一些实施例中，可适应的太阳能机身包括具有空气动力学横截面的可膨胀体，该横截面减小了任何给定厚度的身体的寄生空气阻力，并且还能够响应于相对位置的变化而改变其在飞行中的形状 太阳; 以及附接到可膨胀体表面的柔性太阳能光伏系统。
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公开(公告)号：US20180346118A1
公开(公告)日：2018-12-06
申请号：US16056794
申请日：2018-08-07
发明人： SERGEY V. FROLOV , MICHAEL CYRUS , ALLAN J. BRUCE
摘要： Methods and apparatus to harvest renewable energy are provided herein. In some embodiments, a wind-powered aircraft includes an airframe suitable for untethered flight in an open airspace; and an airborne kinetic energy conversion system attached to the airframe, the airborne kinetic energy conversion system comprising a turbine, a generator connected to the turbine, and an energy storage means connected to the generator.
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公开(公告)号：US20170274996A1
公开(公告)日：2017-09-28
申请号：US15620178
申请日：2017-06-12
IPC分类号： B64C39/02 , B64C11/00 , B64C29/00 , B64C3/56 , B64C37/02 , B64C39/10 , G05D1/00 , G05D1/02 , G05D1/06 , G05D1/10 , G08G5/00 , G08G5/02 , G08G7/02 , G08G5/04
CPC分类号： B64C39/024 , B64C29/0025 , B64C37/02 , B64C39/10 , B64C2201/021 , B64C2201/088 , B64C2201/128 , B64C2201/143 , B64C2211/00 , B64D9/00 , G05D1/0022 , G05D1/0027 , G05D1/005 , G05D1/0212 , G05D1/0669 , G05D1/102 , G05D1/104 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0065 , G08G5/0069 , G08G5/025 , G08G5/045 , G08G7/02 , Y02T50/12
摘要： Embodiments of the present invention provide an aircraft for vertical take-off and landing. In various embodiments, an aircraft assembly includes at least one first wing portion providing a lift force during a horizontal flight, at least one wing opening disposed on a vertical axis of the at least one first wing portion and at least one thruster positioned inside the at least one wing opening to provide vertical thrust during a vertical flight. The aircraft assembly can further include air vents positioned inside at least one of the wing openings. The air vents can further include louvres positioned over or under the air vents to open and close the wing openings. The thruster can further be used to provide flight control for the aircraft.
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公开(公告)号：US20170115668A1
公开(公告)日：2017-04-27
申请号：US15401893
申请日：2017-01-09
CPC分类号： G05D1/104 , B64C3/56 , B64C29/0016 , B64C37/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/102 , B64C2201/128 , B64C2201/143 , B64C2201/145 , B64D1/02 , G05D1/0022 , G05D1/0027 , G05D1/005 , G05D1/0212 , G05D1/0669 , G05D1/102 , G08G5/0008 , G08G5/0013 , G08G5/0017 , G08G5/0021 , G08G5/003 , G08G5/0065 , G08G5/0069 , G08G5/025 , G08G5/045 , G08G7/02 , Y02T50/14
摘要： Embodiments of the present invention provide an alternative distributed airborne transportation system. In some embodiments, a method for distributed airborne transportation includes: providing an airborne vehicle with a wing and a wing span, having capacity to carry one or more of passengers or cargo; landing of the airborne vehicle near one or more of passengers or cargo and loading at least one of passengers or cargo; taking-off and determining a flight direction for the airborne vehicle; locating at least one other airborne vehicle, which has substantially the same flight direction; and joining at least one other airborne vehicle in flight formation and forming a fleet, in which airborne vehicles fly with the same speed and direction and in which adjacent airborne vehicles are separated by distance of less than 100 wing spans.
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公开(公告)号：US20160156406A1
公开(公告)日：2016-06-02
申请号：US14462167
申请日：2014-08-18
CPC分类号： H04B7/18504 , H04W16/28
摘要： Embodiments of methods and apparatus for providing distributed airborne wireless communications are provided herein. In some embodiments, an airborne wireless service area includes: an airborne fleet, comprised of a plurality of aircraft, wherein the airborne fleet is configured to transmit a plurality of first beams at a first radio frequency (RF), wherein the plurality of first beams are characterized by corresponding first frequency band, channel, bandwidth, transmission format, uneven angular field intensity distribution, and boundaries, wherein neighboring first beams have an overlap region, and wherein at least one of the following characteristics is different between the neighboring first beams: frequency band, channel, or transmission format; and a plurality of first communication cells defined by respective boundaries of the plurality of first beams, wherein each of the first communication cells are characterized by their size, shape, and position.
摘要翻译： 本文提供了用于提供分布式机载无线通信的方法和装置的实施例。 在一些实施例中，机载无线服务区域包括：由多个飞行器组成的空中机队，其中所述机载舰队被配置为以第一射频（RF）发射多个第一波束，其中所述多个第一波束 其特征在于相应的第一频带，信道，带宽，传输格式，不均匀角场强度分布和边界，其中相邻的第一光束具有重叠区域，并且其中以下特征中的至少一个在相邻的第一光束之间是不同的： 频段，频道或传输格式; 以及由所述多个第一光束的相应边界限定的多个第一通信单元，其中所述第一通信单元中的每一个的特征在于其大小，形状和位置。
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