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公开(公告)号:US10693567B2
公开(公告)日:2020-06-23
申请号:US15636907
申请日:2017-06-29
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
Abstract: A spacecraft including a frame including a joint coupling a first frame portion to a second frame portion, and an acoustic communication system configured to transfer acoustic data signals across the joint between the first frame portion and the second frame portion.
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公开(公告)号:US20190315479A1
公开(公告)日:2019-10-17
申请号:US15951855
申请日:2018-04-12
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
Abstract: Systems and methods for transferring electric power to an aircraft during flight. Power transfer to the receiver aircraft is effected by means of a donor aircraft using a wired electrical connection. The method for transferring electric power includes: establishing an electrical connection between a receiver aircraft and a donor aircraft during flight; and transferring electric power from the donor aircraft to the receiver aircraft via the electrical connection. In one embodiment, electric power is transferred by way of a power cable deployed by the donor aircraft, a drogue attached to a trailing end of the power cable, and a probe mounted to the fuselage of the receiver aircraft, The probe and drogue are configured to form an electrical connection when fully engaged.
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公开(公告)号:US10435125B2
公开(公告)日:2019-10-08
申请号:US15289622
申请日:2016-10-10
Applicant: THE BOEING COMPANY
Inventor: Brian J. Tillotson
Abstract: A methane transportation system is provided. The system may include a methane source configured to dispense methane at a first location, and an underwater vehicle. The underwater vehicle may include a propulsion system configured to transport the underwater vehicle underwater from the first location to a second location and a vessel defining a storage chamber configured to receive water and the methane from the methane source. The storage chamber of the vessel may have a pressure exceeding one atmosphere and a temperature during transport from the first location to the second location sufficient to form methane clathrate in the storage chamber. The system may further include a methane receiver configured to receive the methane released from the storage chamber at the second location. Related methods are also provided.
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公开(公告)号:US20190252887A1
公开(公告)日:2019-08-15
申请号:US16394887
申请日:2019-04-25
Applicant: The Boeing Company
Inventor: Brian J. Tillotson , Peng Zeng
CPC classification number: H02J5/005 , G01B7/30 , G01R19/04 , H01F38/14 , H01F2005/027 , H02J50/10 , H02J50/70 , H02J50/80 , H02J50/90 , H04B5/0037 , H04B5/0087
Abstract: Systems and methods for mitigating constraints associated with wireless power transmission in applications where the position and orientation of the desired magnetic field changes over time, for example, because the position and orientation of the receiver being powered changes over time or because different receivers having different positions and orientations are being powered at different times. In accordance with some embodiments, the system employs a plurality of wireless power transmitters in a defined space, each transmitter consisting of individual coils oriented orthogonally relative to each other. Using field interference amongst these individual coils as well as amongst the transmitters they form, one can actively control the wireless power field intensity and orientation at any given point in the defined space. This allows for methods to steer the power transmission towards a specific target at a specific angle.
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公开(公告)号:US20190237999A1
公开(公告)日:2019-08-01
申请号:US15886362
申请日:2018-02-01
Applicant: The Boeing Company
Inventor: Brian J. Tillotson , Teiyuri Aoshima
Abstract: Systems and methods for recharging the battery onboard an aircraft (hereinafter “receiving aircraft”) via resonant inductive coupling. In accordance with some embodiments, wireless power transfer to the receiving aircraft is effected by means of a second aircraft (hereinafter “transmitting aircraft”). The receiving and transmitting aircraft are both equipped with respective LC circuits. The aircraft fly in a formation such that transmit coils onboard the transmitting aircraft and receive coils onboard the receiving aircraft are separated by a distance within a resonant inductive coupling range. During the recharge procedure, each transmit coil is driven by an alternating current source having a frequency equal to the resonant frequency of the LC circuit onboard the receiving aircraft. The receive coils then feed the induced alternating current to a rectifier for supplying direct current to the onboard battery charger.
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公开(公告)号:US09948866B2
公开(公告)日:2018-04-17
申请号:US15011727
申请日:2016-02-01
Applicant: The Boeing Company
Inventor: Brian J. Tillotson , Kathryn M. Neville
CPC classification number: H04N5/2353 , G01S7/4804 , G01S7/495 , G02B5/10 , G02B17/06 , G02B17/061 , G02B23/06 , G02B23/08 , G02B23/12 , G02B26/04 , G02F1/01
Abstract: Systems and methods for preventing high-radiant-flux light, such as laser light or a nuclear flash, from causing harm to imaging devices, such as a camera or telescope. In response to detection of high-radiant-flux light, the proposed systems have the feature in common that a shutter is closed sufficiently fast that light from the source will be blocked from reaching the image sensor of the imaging device. Some of the proposed systems include a folded optical path to increase the allowable reaction time to close the shutter.
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公开(公告)号:US09929569B2
公开(公告)日:2018-03-27
申请号:US14535383
申请日:2014-11-07
Applicant: The Boeing Company
Inventor: Brian J. Tillotson , Peng Zeng
IPC: H02J5/00 , H01F38/14 , H04B5/00 , H02J50/10 , H02J50/90 , G01B7/30 , G01R19/04 , H02J50/70 , H02J50/80 , H01F5/02
CPC classification number: H02J5/005 , G01B7/30 , G01R19/04 , H01F38/14 , H01F2005/027 , H02J50/10 , H02J50/70 , H02J50/80 , H02J50/90 , H04B5/0037 , H04B5/0087
Abstract: Systems and methods for mitigating constraints associated with wireless power transmission in applications where the position and orientation of the desired magnetic field changes over time, for example, because the position and orientation of the receiver being powered changes over time or because different receivers having different positions and orientations are being powered at different times. In accordance with some embodiments, the system employs a plurality of wireless power transmitters in a defined space, each transmitter consisting of individual coils oriented orthogonally relative to each other. Using field interference amongst these individual coils as well as amongst the transmitters they form, one can actively control the wireless power field intensity and orientation at any given point in the defined space. This allows for methods to steer the power transmission towards a specific target at a specific angle.
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公开(公告)号:US09918050B2
公开(公告)日:2018-03-13
申请号:US15397540
申请日:2017-01-03
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
IPC: H04N5/335 , H04N9/07 , G06K9/46 , H04N5/232 , G02B5/20 , G02B5/28 , G01J3/00 , G01J3/28 , H04N17/00 , B64C39/02 , B64D47/08 , G06K9/00 , G01J3/12
CPC classification number: H04N9/07 , B64C39/024 , B64D47/08 , G01J3/00 , G01J3/2823 , G01J2003/1213 , G01J2003/1226 , G02B5/201 , G02B5/28 , G06K9/4652 , G06K2009/00644 , H04N5/23229 , H04N17/002
Abstract: A method for capturing hyperspectral images using a regular color camera. In the method, the camera takes multiple images of a scene, with the camera oriented differently for each image. For a camera carried by an aircraft or spacecraft, this allows hyperspectral imaging without the cost or weight of a hyperspectral camera.
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公开(公告)号:US09576216B2
公开(公告)日:2017-02-21
申请号:US14535485
申请日:2014-11-07
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
CPC classification number: H04N9/07 , B64C39/024 , B64D47/08 , G01J3/00 , G01J3/2823 , G01J2003/1213 , G01J2003/1226 , G02B5/201 , G02B5/28 , G06K9/4652 , G06K2009/00644 , H04N5/23229 , H04N17/002
Abstract: A method for capturing hyperspectral images using a regular color camera. In the method, the camera takes multiple images of a scene, with the camera oriented differently for each image. For a camera carried by an aircraft or spacecraft, this allows hyperspectral imaging without the cost or weight of a hyperspectral camera.
Abstract translation: 使用常规彩色相机捕获高光谱图像的方法。 在该方法中,相机拍摄场景的多个图像,其中相机以每个图像的方向不同。 对于由飞机或航天器携带的相机,这允许高光谱成像,而不需要高光谱相机的成本或重量。
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公开(公告)号:US09503696B2
公开(公告)日:2016-11-22
申请号:US14081356
申请日:2013-11-15
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
IPC: H04N7/18 , B64D47/08 , B64D45/00 , G01N21/21 , G01N21/41 , G01N21/59 , G01N15/06 , G08G5/00 , G01N21/17 , G01N15/00
CPC classification number: H04N7/183 , B64D45/00 , G01N15/06 , G01N21/21 , G01N21/41 , G01N21/59 , G01N2015/0046 , G01N2015/0693 , G01N2021/1793 , G01N2021/4106 , G01N2201/0214 , G08G5/0021 , G08G5/0052 , G08G5/0091
Abstract: A system for detecting volcanic plumes using a camera on an aircraft, a distant point-like source of light, and a computerized method of processing images acquired by the camera to detect phenomena indicative of the presence of volcanic plumes in a volume of space intersected by light from the light source. A computer system is programmed to determine whether the image data from the camera has characteristics indicating that the imaged light had passed through a volcanic plume or not. In response to detection of a volcanic plume in the flight path of an aircraft, the computer system outputs an alert activation signal to an alert device that produces a visible or audible alert.
Abstract translation: 一种用于使用飞机上的照相机,遥远的点状光源来检测火山灰的系统,以及一种处理由照相机获取的图像的计算机化方法,以检测指示在与空间相交的空间体积中的火山羽状物的存在的现象 来自光源的光。 计算机系统被编程以确定来自相机的图像数据是否具有指示成像的光已经通过火山羽流的特征。 响应于飞行器的飞行路径中的火山羽毛的检测,计算机系统向警报装置输出警报激活信号,该警报装置产生可见或可听见的警报。
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