-
公开(公告)号：EP3106906B1
公开(公告)日：2018-04-18
申请号：EP16174600.3
申请日：2016-06-15
Applicant: Sunlight Photonics Inc.
Inventor： Bruce, Allan James , Cyrus, Michael , Frolov, Sergey
IPC: G02B6/42 , H04B10/60 , H04B10/112 , G01J1/04 , G01J1/42
CPC classification number: H04B10/1121 , G01J1/0422 , G01J1/42 , G02B6/42
Abstract: A multilayer film or skin for free space optical data transmission includes a first outer layer. The first outer layer has a first laterally extending area that transmits optical data signals received over a range of incident angle. A second layer that includes a second laterally extending area underlies the first layer. At least a portion of the optical data signals received by the second layer from the first outer layer is focused or otherwise concentrated into a substantially reduced area. An optical detector receives the concentrated optical data signals from the second layer. An electrical connection extends from the optical detector to an external receiving device. The multilayer film or skin may be used, for example, in applications involving mobile free space optical communication platforms where low profile, volume and mass and/or enhanced platforms are important.
-
公开(公告)号：EP3290334A1
公开(公告)日：2018-03-07
申请号：EP17188895.1
申请日：2017-08-31
Applicant: Sunlight Photonics Inc.
Inventor： Frolov, Sergey V. , Cyrus, Michael , Moussouris, John Peter
CPC classification number: B64D27/24 , B64C11/001 , B64C29/0025 , B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/086 , B64C2201/108 , B64C2201/128 , B64C2201/162 , B64C2201/208 , Y02T50/64
Abstract: Embodiments of the present invention provide an aircraft (200) for vertical take-off and landing. In various embodiments, an aircraft assembly includes at least one first wing portion (210) 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 (210) and at least one thruster (240) positioned inside the at least one wing opening to provide vertical thrust during a vertical flight. The aircraft assembly can further include air vents (2030) positioned inside at least one of the wing openings. The air vents can further include louvres (2040) positioned over or under the air vents (2030) 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用于垂直起飞和降落的飞行器（200）。 在各种实施例中，飞机组件包括在水平飞行期间提供升力的至少一个第一机翼部分（210），设置在至少一个第一机翼部分（210）的竖直轴线上的至少一个机翼开口以及至少一个 一个推进器（240）位于所述至少一个翼开口内以在垂直飞行期间提供垂直推力。 飞机组件还可以包括定位在至少一个翼开口内的通气孔（2030）。 通风口还可以包括位于通风口（2030）上方或下方的百叶窗（2040）以打开和关闭翼部开口。 推进器可以进一步用于为飞机提供飞行控制。
-
公开(公告)号：EP3106906A1
公开(公告)日：2016-12-21
申请号：EP16174600.3
申请日：2016-06-15
Applicant: Sunlight Photonics Inc.
Inventor： Bruce, Allan James , Cyrus, Michael , Frolov, Sergey
CPC classification number: H04B10/1121 , G01J1/0422 , G01J1/42 , G02B6/42
Abstract: A multilayer film or skin for free space optical data transmission includes a first outer layer. The first outer layer has a first laterally extending area that transmits optical data signals received over a range of incident angle. A second layer that includes a second laterally extending area underlies the first layer. At least a portion of the optical data signals received by the second layer from the first outer layer is focused or otherwise concentrated into a substantially reduced area. An optical detector receives the concentrated optical data signals from the second layer. An electrical connection extends from the optical detector to an external receiving device. The multilayer film or skin may be used, for example, in applications involving mobile free space optical communication platforms where low profile, volume and mass and/or enhanced platforms are important.
Abstract translation: 用于自由空间光学数据传输的多层膜或皮肤包括第一外层。 第一外层具有第一横向延伸的区域，其传送在入射角范围内接收的光学数据信号。 第二层，其包括在第一层下面的第二横向延伸区域。 由第二层从第一外层接收的光学数据信号的至少一部分被聚焦或以其他方式集中在基本上减小的区域中。 光学检测器从第二层接收浓缩的光学数据信号。 电连接从光学检测器延伸到外部接收装置。 多层膜或皮肤可以用于例如涉及移动自由空间光通信平台的应用，其中薄型，体积和质量和/或增强平台是重要的。
-
公开(公告)号：EP3243741B1
公开(公告)日：2019-04-17
申请号：EP17176920.1
申请日：2014-01-23
Applicant: Sunlight Photonics Inc.
Inventor： Moussouris, John Peter , Frolov, Sergey V. , Cyrus, Michael
-
公开(公告)号：EP3243741A1
公开(公告)日：2017-11-15
申请号：EP17176920.1
申请日：2014-01-23
Applicant: Sunlight Photonics Inc.
Inventor： Moussouris, John Peter , Frolov, Sergey V. , Cyrus, Michael
CPC classification number: B64C1/0009 , B64C1/34 , B64C3/46 , B64C39/024 , B64C2201/105 , B64D2211/00 , G01S3/7861 , Y02T50/14 , Y02T50/55
Abstract: Methods and apparatus for an adaptable solar airframe are provided herein. In some embodiments, an adaptable solar airframe includes a solar PV system having at least one solar tracking system and being able to follow the sun position in order to increase sunlight collection and power output; and an expandable body having an aerodynamic cross-section that minimizes parasitic air drag at any given thickness of the body, further being at least partially transparent to sunlight, further enclosing the solar PV system, and further being able to change its shape in response to changes in the positions of the solar PV system.
Abstract translation: 本文提供了用于可适应的太阳能机身的方法和设备。 在一些实施例中，可适应的太阳能机身包括太阳能PV系统，其具有至少一个太阳能跟踪系统并且能够跟随太阳位置以增加太阳光收集和功率输出; 以及具有空气动力学横截面的可膨胀体，其使得在任何给定的身体厚度下的寄生空气阻力最小化，进一步对太阳光至少部分透明，进一步包围太阳能PV系统，并且还能够响应于 太阳能光伏系统位置的变化。
-
Patent Agency Ranking
公开(公告)号：EP2660151B1
公开(公告)日：2016-04-27
申请号：EP13166020.1
申请日：2013-04-30
Applicant: Sunlight Photonics Inc.
Inventor： Frolov, Sergey V. , Cyrus, Michael , Bruce, Allan J.
IPC: B64C31/036
CPC classification number: B64C39/024 , B64C2201/02 , B64C2201/042 , B64C2201/06 , B64C2201/165 , B64D27/24 , B64D2211/00 , H01L31/048 , H02S20/00 , Y02E10/50 , Y02T50/64
-
公开(公告)号：EP2660151A1
公开(公告)日：2013-11-06
申请号：EP13166020.1
申请日：2013-04-30
Applicant: Sunlight Photonics Inc.
Inventor： Frolov, Sergey V. , Cyrus, Michael , Bruce, Allan J.
IPC: B64C31/036
CPC classification number: B64C39/024 , B64C2201/02 , B64C2201/042 , B64C2201/06 , B64C2201/165 , B64D27/24 , B64D2211/00 , H01L31/048 , H02S20/00 , Y02E10/50 , Y02T50/64
Abstract: An unmanned solar-powered aircraft (300) comprises a lightweight solar wing (310) comprising an airfoil profile, a top surface, a bottom surface, a leading edge, a trailing edge, wing tips, and at least one photovoltaic cell, wherein the surfaces and edges follow an arched bow shape across a span of the wing. The unmanned solar-powered aircraft includes a fuselage (330) and a propeller (340), wherein the fuselage is placed below the solar wing and contains an electric motor, battery, and electronics.
Abstract translation: 无人太阳能飞机（300）包括轻型太阳能翼（310），其包括翼型轮廓，顶表面，底表面，前缘，后缘，翼尖和至少一个光伏电池，其中， 表面和边缘沿着机翼跨度的弓形弓形。 无人太阳能飞机包括机身（330）和螺旋桨（340），其中机身放置在太阳能飞轮下方并且包含电动机，电池和电子设备。
-
公开(公告)号：EP2759469B1
公开(公告)日：2017-06-21
申请号：EP14152285.4
申请日：2014-01-23
Applicant: Sunlight Photonics Inc.
Inventor： Moussouris, John Peter , Frolov, Sergey V. , Cyrus, Michael
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 a solar PV system having at least one solar tracking system and being able to follow the sun position in order to increase sunlight collection and power output; and an expandable body having an aerodynamic cross-section that minimizes parasitic air drag at any given thickness of the body, further being at least partially transparent to sunlight, further enclosing the solar PV system, and further being able to change its shape in response to changes in the positions of the solar PV system.
Abstract translation: 本文提供了用于可适应的太阳能机身的方法和设备。 在一些实施例中，可适应的太阳能机身包括太阳能PV系统，其具有至少一个太阳能跟踪系统并且能够跟随太阳位置以增加太阳光收集和功率输出; 以及具有空气动力学横截面的可膨胀体，其使得在任何给定的身体厚度下的寄生空气阻力最小化，进一步对太阳光至少部分透明，进一步包围太阳能PV系统，并且还能够响应于 太阳能光伏系统位置的变化。
-
公开(公告)号：EP2503589B1
公开(公告)日：2017-01-11
申请号：EP12002005.2
申请日：2012-03-21
Applicant: Sunlight Photonics Inc.
Inventor： Frolov, Sergey , Bruce, Allan, James , Cyrus, Michael
IPC: H01L21/36 , H01L31/0248 , H01L31/032
CPC classification number: H01L21/02568 , H01L21/02562 , H01L21/02614 , H01L31/0322 , Y02E10/541
-
公开(公告)号：EP3106906B8
公开(公告)日：2018-06-06
申请号：EP16174600.3
申请日：2016-06-15
Applicant: Sunlight Photonics Inc.
Inventor： Bruce, Allan James , Cyrus, Michael , Frolov, Sergey
IPC: G02B6/42 , H04B10/60 , H04B10/112 , G01J1/04 , G01J1/42
CPC classification number: H04B10/1121 , G01J1/0422 , G01J1/42 , G02B6/42
Abstract: A multilayer film or skin for free space optical data transmission includes a first outer layer. The first outer layer has a first laterally extending area that transmits optical data signals received over a range of incident angle. A second layer that includes a second laterally extending area underlies the first layer. At least a portion of the optical data signals received by the second layer from the first outer layer is focused or otherwise concentrated into a substantially reduced area. An optical detector receives the concentrated optical data signals from the second layer. An electrical connection extends from the optical detector to an external receiving device. The multilayer film or skin may be used, for example, in applications involving mobile free space optical communication platforms where low profile, volume and mass and/or enhanced platforms are important.
-
-
-
-
-
-
-
-
-
Search Results
13
records
(took 0.049 seconds)
