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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
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , JOHN PETER MOUSSOURIS , MICHAEL CYRUS
CPC classification number: 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
Abstract: 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.
Abstract translation: 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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2.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
Applicant: Sunlight Photonics Inc.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , ALLAN J. BRUCE , JOHN PETER MOUSSOURIS
IPC: B64D47/00 , B64D35/02 , B64C19/00 , B64D31/00 , H04B7/185 , B64B1/00 , G08G5/00 , G05D1/10 , G08G5/04 , B64D33/00 , B64C39/02
CPC classification number: 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
Abstract: 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.
Abstract translation: 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
Applicant: SunLight Photonics Inc.
Inventor： JOHN PETER MOUSSOURIS , SERGEY V. FROLOV , MICHAEL CYRUS
CPC classification number: B64C1/0009 , B64C1/34 , B64C3/46 , B64C39/024 , B64C2201/105 , B64D2211/00 , G01S3/7861 , Y02T50/14
Abstract: 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.
Abstract translation: 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：US20170274996A1
公开(公告)日：2017-09-28
申请号：US15620178
申请日：2017-06-12
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , JOHN PETER MOUSSOURIS
IPC: 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 classification number: 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
Abstract: 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
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , JOHN PETER MOUSSOURIS , MICHAEL CYRUS
CPC classification number: 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
Abstract: 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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Patent Agency Ranking
公开(公告)号：US20160156406A1
公开(公告)日：2016-06-02
申请号：US14462167
申请日：2014-08-18
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , ALLAN J. BRUCE , JOHN PETER MOUSSOURIS
CPC classification number: H04B7/18504 , H04W16/28
Abstract: 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.
Abstract translation: 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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公开(公告)号：US20180354617A1
公开(公告)日：2018-12-13
申请号：US16052938
申请日：2018-08-02
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , JOHN PETER MOUSSOURIS
Abstract: An aircraft for vertical take-off and landing includes an aircraft frame having an open frame portion, at least one vertical thruster, a pod, separable from the aircraft and including a cabin to contain at least one of cargo and passengers, where the pod, when mounted to the aircraft, defines at least a portion of the aircraft frame, and a mounting system including at least one attachment member configured to attach the pod to the open frame portion. Such aircraft is capable of flight with and without the pod.
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公开(公告)号：US20180123678A1
公开(公告)日：2018-05-03
申请号：US15457988
申请日：2017-03-13
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , ALLAN J. BRUCE , JOHN PETER MOUSSOURIS
IPC: H04B7/185
CPC classification number: H04B7/18506 , H04B7/18504
Abstract: Embodiments of methods for providing distributed airborne wireless communications are provided herein. In some embodiments, a method of providing wireless communication services includes: receiving a radio frequency (RF) signal from a first area by a distributed airborne communication payload, wherein the distributed airborne communication payload is comprised of sections located on respective ones of a plurality of airborne platforms; relaying the RF signal along the sections located on different airborne platforms; and transmitting the RF signal to a second area.
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公开(公告)号：US20160368600A1
公开(公告)日：2016-12-22
申请号：US15252297
申请日：2016-08-31
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , JOHN PETER MOUSSOURIS
CPC classification number: 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
Abstract: 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.
Abstract translation: 本发明的实施例提供一种用于垂直起飞和着陆的飞行器。 在各种实施例中，飞行器组件包括至少一个在水平飞行期间提供提升力的第一翼部分，至少一个翼开口，设置在至少一个第一翼部分的垂直轴线上，以及至少一个推进器， 至少一个翼开口在垂直飞行期间提供垂直推力。 飞行器组件还可以包括定位在至少一个机翼开口内的通风口。 通风口还可以包括位于空气通风口上方或下方的百叶窗，以打开和关闭机翼开口。 推进器还可用于为飞机提供飞行控制。
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公开(公告)号：US20160050012A1
公开(公告)日：2016-02-18
申请号：US14462421
申请日：2014-08-18
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , ALLAN J. BRUCE , JOHN PETER MOUSSOURIS
IPC: H04B7/185
CPC classification number: H04B7/18506 , H04B7/18504
Abstract: Embodiments of methods for providing distributed airborne wireless communications are provided herein. In some embodiments, a method of providing wireless communication services includes: receiving a radio frequency (RF) signal from a first area by a distributed airborne communication payload, wherein the distributed airborne communication payload is comprised of sections located on respective ones of a plurality of airborne platforms; relaying the RF signal along the sections located on different airborne platforms; and transmitting the RF signal to a second area.
Abstract translation: 本文提供了用于提供分布式机载无线通信的方法的实施例。 在一些实施例中，提供无线通信服务的方法包括：通过分布式机载通信有效载荷从第一区域接收射频（RF）信号，其中分布式机载通信有效载荷包括位于多个 机载平台; 沿着位于不同机载平台的部分中继射频信号; 以及将RF信号发送到第二区域。
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