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11.
公开(公告)号:US09522727B2
公开(公告)日:2016-12-20
申请号:US14628218
申请日:2015-02-21
Applicant: The Boeing Company
Inventor: William Pflug , Brian J. Tillotson
IPC: B64C23/04 , B64C30/00 , B64D27/18 , B64D29/02 , B64D7/00 , B64C3/00 , F42B10/38 , B64C3/10 , B64C5/00 , B64D1/02 , B64C1/26 , B64C7/02
CPC classification number: B64C23/04 , B64C1/26 , B64C3/00 , B64C3/10 , B64C5/00 , B64C7/02 , B64C30/00 , B64D1/02 , B64D7/00 , B64D27/18 , B64D29/02 , F42B10/38
Abstract: An air vehicle may include a body having forwardly-swept fixed wings or unswept fixed wings. The body may have a longitudinal axis continuously oriented parallel to a forward flight direction when the air vehicle is in flight. The air vehicle may include at least one of the following components being mounted on opposite sides of the body: longitudinally offset engine nacelles, asymmetrically lengthened engine nacelles, and longitudinally offset protruding aerodynamic surfaces comprising at least one of stabilizers, canards, empennage control surfaces, external stores, and high aspect ratio wings.
Abstract translation: 机动车辆可以包括具有向前扫掠的固定翼或未固定翼的主体。 当飞行器飞行时,主体可以具有平行于向前飞行方向连续定向的纵向轴线。 空中交通工具可以包括安装在主体的相对侧上的以下部件中的至少一个:纵向偏置发动机机舱,不对称延长的发动机机舱以及纵向偏移的突出空气动力表面,包括稳定器,卡车,尾翼控制面, 外部商店和高宽比机翼。
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公开(公告)号:US09423538B2
公开(公告)日:2016-08-23
申请号:US13900066
申请日:2013-05-22
Applicant: The Boeing Company
Inventor: Brian J. Tillotson , Zach J. Harris
CPC classification number: G02B5/136 , E04B1/90 , E04B2001/7691 , E04B2001/8414 , G02B5/124
Abstract: An apparatus for directing thermal infrared energy toward or away from a target is disclosed. The apparatus comprises a covering having a plurality of retroreflective elements. The plurality of retroreflective elements are configured to retroreflect electromagnetic beams primarily at thermal infrared wavelengths, receive the electromagnetic beams from the target along beam reception paths, and reflect the electromagnetic beams back toward the target along beam reflection paths. The beam reflection paths have substantially the same elevation angle and/or azimuth angle as their respective beam reception paths.
Abstract translation: 公开了一种用于将热红外能量朝向或远离目标引导的装置。 该装置包括具有多个回射元件的覆盖物。 多个逆反射元件被配置为主要以热红外波长回射电磁波束,沿着光束接收路径接收来自目标的电磁波束,并且沿着光束反射路径将电磁波反射回目标物。 光束反射路径具有与它们各自的光束接收路径基本相同的仰角和/或方位角。
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公开(公告)号:US20150138355A1
公开(公告)日:2015-05-21
申请号:US14081356
申请日:2013-11-15
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
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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公开(公告)号:US20140077969A1
公开(公告)日:2014-03-20
申请号:US13708543
申请日:2012-12-07
Applicant: The Boeing Company
Inventor: John Lyle Vian , Charles B. Spinelli , Brian J. Tillotson , George Michael Roe , Joshua Przybylko
IPC: G08C17/02
CPC classification number: G08C17/02 , H04Q9/00 , H04Q2209/40 , H04Q2209/50 , H04Q2209/80 , H04Q2209/886
Abstract: A method and apparatus for managing a location. Soil sensor units are deployed in the location in a forest from a group of aerial vehicles. Information is generated about a number of soil conditions in the location in the forest using the soil sensor units in the location. The information is transmitted from the soil sensor units to a remote location for analysis.
Abstract translation: 一种用于管理位置的方法和装置。 土壤传感器单元部署在森林中从一组飞行器的位置。 使用位置中的土壤传感器单元产生关于森林中位置的多个土壤条件的信息。 信息从土壤传感器单元传输到远程位置进行分析。
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公开(公告)号:US11964773B2
公开(公告)日:2024-04-23
申请号:US17408780
申请日:2021-08-23
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
CPC classification number: B64D41/00 , G01S5/0231 , G06T7/97 , H02G11/02 , H02J7/342 , B64D2221/00
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:US11876388B2
公开(公告)日:2024-01-16
申请号:US16677096
申请日:2019-11-07
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
Abstract: A transmitter for providing energy to a beam-powered aircraft includes an energy source that outputs an energy beam having an elongated cross-section, and a mount. The mount is operable to vary an azimuth and an elevation of the energy beam, and operable to rotate the energy beam about a central axis of the energy beam.
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公开(公告)号:US20220244190A1
公开(公告)日:2022-08-04
申请号:US17725767
申请日:2022-04-21
Applicant: The Boeing Company
Inventor: Brian J. Tillotson , Robert Paul Higgins , Andrej Martin Savol
IPC: G01N21/88 , G01N21/952 , G06T7/00
Abstract: A system for inspecting a wire segment includes an inspection apparatus and a visual imaging device. The apparatus includes an array of mirrors positioned about a centerline of the apparatus, wherein each mirror in the array is oriented such that a reflection of a first inspection zone of the wire segment in the array of mirrors forms a circumferential view of the first inspection zone of the wire segment, and the reflection from each mirror is within a field of view from a single vantage point. The visual imaging device is positioned at the single vantage point and oriented towards the wire segment such that the reflection from each mirror of the array of mirrors is within a field of view of the visual imaging device, the visual imaging device configured to capture at least one image of the reflection of the wire segment from the array of mirrors.
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公开(公告)号:US10908618B2
公开(公告)日:2021-02-02
申请号:US16188938
申请日:2018-11-13
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
IPC: G05D1/08 , G05D1/00 , B64D31/06 , B64C27/00 , G06K9/00 , G08G5/04 , H02P5/56 , G06T7/62 , B64C39/02 , G06T7/20
Abstract: Methods and systems according to one or more examples are provided for controlling a multi-rotor vehicle. In one example, a multi-rotor vehicle comprises an airframe and a plurality of rotors coupled to the airframe. The multi-rotor vehicle further comprises a controller, coupled to the airframe, configured to determine a rotational speed of each of the plurality of rotors, and adjust the rotational speed of each of the plurality of rotors such that the rotors do not dwell within a no-dwell zone comprising rotational speeds associated with one or more frequency aspects of the airframe.
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19.
公开(公告)号:US20200180791A1
公开(公告)日:2020-06-11
申请号:US16216765
申请日:2018-12-11
Applicant: The Boeing Company
Inventor: Gregory A. Kimberly , Brian J. Tillotson
Abstract: Pre-flight and episodic aircraft inspections to ensure operational safety and effectiveness are made faster, less costly and more effective by utilizing mobile model and data-driven sensor platforms inspecting known-state target vehicles. For autonomous aircraft, an inspection unmanned aerial vehicle (I-UAV) containing sensors inspects a utility unmanned aerial vehicle (U-UAV). Failure and system models of the U-UAV and the flight history of the U-UAV carried in the sensor data captured by the U-UAV's aircraft health management system are combined to guide the I-UAV to appropriately attend to the systems of the U-UAV and to drive the U-UAV systems into target states that will reveal otherwise hidden or latent failures.
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公开(公告)号:US10652441B1
公开(公告)日:2020-05-12
申请号:US16409395
申请日:2019-05-10
Applicant: The Boeing Company
Inventor: Brian J. Tillotson
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. The optical components of the imaging device have first and second foci. The second focus forms an image on an array of photodetectors and occurs at a large f-number. The first focus occurs at a small f-number in a gas that is dense enough to dissipate most of a femtosecond laser pulse of potentially damaging intensity and conditioned to easily undergo dielectric breakdown when exposed to high-radiant-flux light that is less intense than a femtosecond laser pulse. Dielectric breakdown forms a conductive arc that dissipates or scatters light, blocking high-radiant-flux light from reaching the array of photodetectors. Several methods may be used for conditioning the gas to break down quickly when exposed to laser attack.
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