飞行包线
101. AUTOMATED DISTRIBUTION OF LOGON CREDENTIALS FOR ESTABLISHING WIRELESS CONNECTIVITY OF ELECTRONIC FLIGHT BAG(EFB)
申请号: EP16150505.2
申请日: 2016-01-07
公开（公告）号: EP3046305A1
公开（公告）日: 2016-07-20
发明人: HENZL, Martin; GOTTHARD, Petr
Automated distribution of wireless logon credentials for an electronic flight bag (EFB) is provided. In one embodiment, a method for secured aircraft wireless network access comprises: establishing a NFC link between an EFB and an NFC node, wherein the node is hardwired to a wireless access point coupled to EFB service applications via an aircraft network. The access point provides a plurality of wireless channels for accessing the network, each are single user wireless channels. In response to a request from the EFB, determining whether a first wireless channel is available; if the first wireless channel is available, generating a logon credential associated with the first wireless channel and transmitting the credential to the EFB with the NFC node; establishing a second link between the EFB and the wireless access point using the credential; and transferring data between the EFB and EFB server applications over the second link.
102. Aircraft in-flight entertainment system including a distributed digital radio service and associated methods
申请号: US11023728
申请日: 2004-12-28
公开（公告）号: US08776146B2
公开（公告）日: 2014-07-08
发明人: Jason Funderburk; Scott D. Easterling; Robert M. Keen
An aircraft in-flight entertainment (IFE) system includes an antenna for receiving digital satellite radio signals, and an intermediate frequency (IF) down converter is connected to the antenna for down converting the digital satellite radio signals. A plurality of seat electronic boxes (SEBs) are spaced throughout the aircraft. Each SEB includes at least one IF tuner in communications with the IF down converter.
更多103. Disc drive actuator incorporating injection molding, flying leads, and locking flanges
申请号: US622616
申请日: 1996-03-26
公开（公告）号: US5734528A
公开（公告）日: 1998-03-31
发明人: Iraj Jabbari; Brian L. Phillips; Brian T. Bonn; Chul Soo Kim; Michael A. Maiers; Mark E. Gauger
The present invention provides an improved actuator arm assembly including scalloped locking flanges with indentations for longitudinal, perpendicular, and torsional support, an injection molding for precisely locating and fixing a motor coil bobbin, motor coil wires, magnetic latch striker plate, and a crash stop to an actuator arm. Apertures on the actuator arm allow the plastic molding to pass through and lock the actuator arm to the motor coil bobbin together. The magnetic latch striker plate fixably parks the actuator arm in the disc drive assembly. Locating apertures of various shapes in the motor coil bobbin adds further stability and aids in interlocking the plastic molds around the motor coil bobbin. Furthermore, to reduce the height of the disc drive, protect the lead wires from being unduly stressed during the formation of the mold, and increase wire strength to tolerate stresses during testing and assembly, another embodiment of the invention utilizes insulating sleeves around the lead wires. Thus, after forming the lead coils from a molded coil mounted at the rear of an actuator arm, the two lead wires from either end of the coil are led out from the end of the coil, and plastic tubes are slid over the wires up to a point closely adjacent the wound coil. The wound coil is then molded, fixing its shape and holding it in place on the rear of the actuator arm.
更多104. 飛球方向とフェースの開き具合を示すラインとスウィング軌道を示すラインをフェース上に印したアプローチウエッジ
申请号: JP2016018389
申请日: 2016-01-15
公开（公告）号: JP2016105808A
公开（公告）日: 2016-06-16
发明人: 水戸 貞夫
【課題】飛球方向より約20°でカット打ちにできるようテイクバックの目印となるガイドラインをフェース面上に印したアプローチウエッジを提供する。
【解決手段】フェース面の一番下のスコアラインの溝を刻んで加工した部分とフェース面上のトゥ側の加工していないクラウン部分を含む部分との境目の線を0°としてトゥ側に約10°の線を印し、その線がフェースを約10°開くガイドラインでもあり、飛球方向を示すラインになるものであり、また飛球方向を示すラインを基本線としてクラウン部分より最下部のスコアライン方向へ、フェース面のスコアラインの数本ある溝を斜め方向へ横切る約20°のラインを印し、再下部のスコアラインの左右の中心より少し外側にガイドラインがいくようにしてシャンクを押さえる役目を果たせ、スタンスも約20°開くのでカット打ちする感覚を持つことなくスタンスと平行にスウィングできるように導いてくれるようにしたもの。
【選択図】図1
105. Automated distribution of logon credentials for establishing wireless connectivity of electronic flight bag (EFB)
申请号: US14599198
申请日: 2015-01-16
公开（公告）号: US09402182B1
公开（公告）日: 2016-07-26
发明人: Martin Henzl; Petr Gotthard
Automated distribution of wireless logon credentials for an electronic flight bag (EFB) is provided. In one embodiment, a method for secured aircraft wireless network access comprises: establishing a NFC link between an EFB and an NFC node, wherein the node is hardwired to a wireless access point coupled to EFB service applications via an aircraft network. The access point provides a plurality of wireless channels for accessing the network, each are single user wireless channels. In response to a request from the EFB, determining whether a first wireless channel is available; if the first wireless channel is available, generating a logon credential associated with the first wireless channel and transmitting the credential to the EFB with the NFC node; establishing a second link between the EFB and the wireless access point using the credential; and transferring data between the EFB and EFB server applications over the second link.
更多106. AUTOMATED DISTRIBUTION OF LOGON CREDENTIALS FOR ESTABLISHING WIRELESS CONNECTIVITY OF ELECTRONIC FLIGHT BAG (EFB)
申请号: US14599198
申请日: 2015-01-16
公开（公告）号: US20160212618A1
公开（公告）日: 2016-07-21
发明人: Martin Henzl; Petr Gotthard
Automated distribution of wireless logon credentials for an electronic flight bag (EFB) is provided. In one embodiment, a method for secured aircraft wireless network access comprises: establishing a NFC link between an EFB and an NFC node, wherein the node is hardwired to a wireless access point coupled to EFB service applications via an aircraft network. The access point provides a plurality of wireless channels for accessing the network, each are single user wireless channels. In response to a request from the EFB, determining whether a first wireless channel is available; if the first wireless channel is available, generating a logon credential associated with the first wireless channel and transmitting the credential to the EFB with the NFC node; establishing a second link between the EFB and the wireless access point using the credential; and transferring data between the EFB and EFB server applications over the second link.
更多107. Aircraft in-flight entertainment system including a distributed digital radio service and associated methods
申请号: US11023728
申请日: 2004-12-28
公开（公告）号: US20060143661A1
公开（公告）日: 2006-06-29
发明人: Jason Funderburk; Scott Easterling; Robert Keen
An aircraft in-flight entertainment (IFE) system includes an antenna for receiving digital satellite radio signals, and an intermediate frequency (IF) down converter is connected to the antenna for down converting the digital satellite radio signals. A plurality of seat electronic boxes (SEBs) are spaced throughout the aircraft. Each SEB includes at least one IF tuner in communications with the IF down converter.
更多108. Aircraft front portion including a concave bulkhead separating a non-pressurized radome area and a pressurized area
申请号: US12686761
申请日: 2010-01-13
公开（公告）号: US08434717B2
公开（公告）日: 2013-05-07
发明人: Cédric Meyer; Bernard Guering
An aircraft front portion includes a sealed bulkhead separating a non pressurized radome area from a pressurized area. The sealed bulkhead is delimited by two surfaces opposite to each other, one being substantially concave when seen from the radome area and the other being substantially convex when seen from the pressurized area.
更多109. AGENCEMENT DE COUSSIN DE SECURITE GONFLABLE DANS UNE PLANCHE DE BORD COMPORTANT UN VOLET RELIE A LA PLANCHE DE BORD PAR UN LIEN LINEAIRE
申请号: PCT/EP2011/001444
申请日: 2011-03-23
公开（公告）号: WO2011116950A1
公开（公告）日: 2011-09-29
发明人: ORY, Daniel
L'invention concerne un agencement (1) de coussin de sécurité gonflable, comprenant un corps de planche de bord (2) présentant une fenêtre (3), un volet (10) fermant cette fenêtre (3) en étant articulé sur un bord d'articulation transversal de cette fenêtre, un canal de tir (4) fixé en face inférieure du corps de planche de bord (2). Au moins un lien (18) est fixé au volet (10) et au canal de tir (4) pour former une charnière et/ou pour limiter l'ouverture du volet (10), et le canal de tir (4) comporte au moins une ouverture (28, 29, 42) mettant en communication une face interne et une face externe d'un bord (8, 9, 6) du canal de tir (4). Le lien (18) traverse cette ouverture (28, 29, 42) pour être fixé en étant retenu fermement au niveau d'une face externe du canal de tir (4) lors de l'ouverture du volet (10).
更多110. RADIATION DETECTOR OF VERY HIGH PERFORMANCE AND PLANISPHERICAL PARALLAX-FREE X-RAY IMAGER COMPRISING SUCH A RADIATION DETECTOR
申请号: PCT/EP1998/006569
申请日: 1998-10-16
公开（公告）号: WO99021211A1
公开（公告）日: 1999-04-29
发明人:
A radiation detector in which primary electrons are released into a gas by ionizing radiations and drifted through an electric field (E) to a collecting electrode (CE) for detection. It further includes a gas electron multiplier (10, 11, 12) formed by one or several matrices of electric field condensing areas (1i) which are distributed within a solid surface perpendicular to the electric field. Each electric field condensing area consists of a tiny hole passing through the solid surface that forms a dipole adapted to produce a local electric field amplitude enhancement proper to generate an electron avalanche from one primary electron. The gas electron multiplier operates thus as an amplifier or a preamplifier within a host radiation detector.
更多111. 在與無人機耦合的使用者設備和陸地無線通訊用戶網路的元件之間交換包括飛行中狀態指示符的訊息
申请号: TW107115055
申请日: 2018-05-03
公开（公告）号: TW201844017A
公开（公告）日: 2018-12-16
发明人: 福雅爾 烏梅許; PHUYAL, UMESH; 瑞可亞瓦利諾 艾柏多; RICO ALVARINO, ALBERTO; 斯西摩波羅斯 哈利斯; ZISIMOPOULOS, HARIS; 北添真人; KITAZOE, MASATO
在實施例中，與無人機耦合的UE決定與無人機耦合的UE是否參與飛行狀態，以及向陸地無線通訊用戶網路的網路元件傳輸指示決定的結果的訊息。網路元件從與無人機耦合的UE接收訊息。在一實施例中，陸地無線通訊用戶網路的網路元件基於來自與無人機耦合的UE的訊息，決定與無人機耦合的UE是否參與飛行狀態。隨後，網路元件基於決定來應用協定。
更多112. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated mehtods
申请号: US11284113
申请日: 2005-11-21
公开（公告）号: US20070114328A1
公开（公告）日: 2007-05-24
发明人: Douglas Lacy; Jan Kordel; John Dovey; Michael Balzer; Seiya Sakurai; Neal Huynh
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
更多113. Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
申请号: US10703564
申请日: 2003-11-10
公开（公告）号: US20050021193A1
公开（公告）日: 2005-01-27
发明人: Nathalie Raimbault; Jean-Pierre Gautier; Alain Sagansan; Pierre Fabre
Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system. According to the invention, provision is made for the pivotings of said control (2) to be damped by controllable damping means (15, 16) controlled by means (7) detecting oscillations corresponding to pilot induced oscillations.
更多114. Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
申请号: US12765713
申请日: 2010-04-22
公开（公告）号: US08473121B2
公开（公告）日: 2013-06-25
发明人: Nathalie Raimbault; Jean-Pierre Gautier; Alain Sagansan; Pierre Fabre
A fly-by-wire control system for an aircraft including detection of pilot induced oscillations and a mobile control unit for such a system. According to the invention, provision is made for the pivotings of the mobile control unit to be damped by a controllable damper controlled by a detector that detects oscillations corresponding to pilot induced oscillations.
更多115. Device for angular positioning of an incidence probe on a wall, of the type comprising of a weather vane that can move about an axis, particularly on a wall of an aircraft
申请号: US10168867
申请日: 2000-12-28
公开（公告）号: US06845658B2
公开（公告）日: 2005-01-25
发明人: Philippe Roberge; Bernard Christin; Alain Subtil
A device for the in situ angular positioning of an incidence probe, e.g., of the weather vane type, equipped with a vane and mounted, e.g., on an airplane. According to the device, the axis of rotation of the probe is used directly as a positioning reference. The angular-positioning device include a fixed structure secured to the wall of the airplane, of annular shape and including a circular track for a moving slider. The vane is immobilized in an enveloping structure. A coupling member coupling the slider and the enveloping structure is fixed to the enveloping structure. Coupling is afforded by a flat spring leaf including a stud at its end. The stud is slipped into a slit of the slider, which allows the vane to be driven about its axis of rotation. The position is measured using a digital inclinometer.
更多116. 无人机的安全航线生成方法、装置、控制终端和无人机
申请号: PCT/CN2020/122478
申请日: 2020-10-21
公开（公告）号: WO2021073654A1
公开（公告）日: 2021-04-22
发明人: 冯银华
一种无人机的安全航线生成方法、装置、控制终端和无人机，安全航线生成方法包括：获取路线特征点集和属性参数，其中，路线特征点集包含至少一个路线规划关键点，属性参数至少包含飞行高度（101）；根据路线特征点集、属性参数及预设路线生成策略生成飞行路线（41）（102）；根据高程数据文件调整飞行路线（41），以生成航线（103）。通过在飞行路线（41）制定中考虑高程数据，避免飞行控制过程中出现飞行障碍，可提高无人机飞行的安全性。
更多117. 无人飞行器的限高方法、装置、无人飞行器及存储介质
申请号: PCT/CN2020/092370
申请日: 2020-05-26
公开（公告）号: WO2021237462A1
公开（公告）日: 2021-12-02
发明人: 贾向华; 闫光; 王璐
无人飞行器的限高方法、装置、无人飞行器及存储介质，其中，该方法包括：获取飞行航线数据，飞行航线数据包括多个航点的航点高度；根据多个航点的航点高度确定无人飞行器在根据飞行航线数据执行飞行航线任务时的限飞高度，其中，限飞高度是相对于限飞参考点的高度。该方法可以根据飞行航线数据中多个航点的航点高度，动态确定无人飞行器的限飞高度，既能实现无人飞行器在执行飞行航线任务时的安全高度需求，又能避免因触发限高导致的飞行航线任务失败，从而提高无人飞行器在执行飞行航线任务时的作业效率。
更多118. 一种无人飞行器的控制方法和终端
申请号: PCT/CN2018/106539
申请日: 2018-09-19
公开（公告）号: WO2019091226A1
公开（公告）日: 2019-05-16
发明人: 冯银华
一种无人飞行器的控制方法和终端，该方法包括：当终端检测到与无人飞行器断开连接时，终端保存无人飞行器的飞行航线的航线信息（101）；当终端重新与无人飞行器建立连接后，终端根据航线信息判断无人飞行器是否未完成飞行航线（102）；若为是，终端将航线信息发送至无人飞行器，以控制无人飞行器根据航线信息完成飞行航线中的剩余航线（103）。本方法能够提升无人飞行器获取飞行航线的效率，简化用户操作；并能够降低无人飞行器未飞行期间的功耗。
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