| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | AUTOMATED DISTRIBUTION OF LOGON CREDENTIALS FOR ESTABLISHING WIRELESS CONNECTIVITY OF ELECTRONIC FLIGHT BAG (EFB) | US14599198 | 2015-01-16 | US20160212618A1 | 2016-07-21 | 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. | ||||||
| 102 | Electronic flight bag systems and methods for verifying correct takeoff performance data entry | US13751831 | 2013-01-28 | US09061770B2 | 2015-06-23 | Steve Johnson; Yasuo Ishihara; Kevin J. Conner; Robert A. Champion |
| Systems and methods for verifying that the flight crew has not made an error in entering takeoff flight performance data into the flight management system (FMS) using the electronic flight bag (EFB). The EFB includes a user interface that receives basic flight plan information and a processor. The processor automatically receives calculated takeoff performance data based on a previously entered basic flight plan, automatically receives user-entered takeoff performance data from a flight management system (FMS) located on a host aircraft, automatically compares the calculated takeoff performance data to the received takeoff performance data, and generates an entry error indication, if the comparison indicates that at least a portion of the entered takeoff performance data does not match the calculated takeoff performance data. An output device outputs the generated entry error indication. | ||||||
| 103 | AIRCRAFT COMPUTER SYSTEM FOR EXECUTING INFLIGHT ENTERTAINMENT AND ELECTRONIC FLIGHT BAG APPLICATIONS | US13679044 | 2012-11-16 | US20130132548A1 | 2013-05-23 | Ralf Cabos |
| An aircraft computer system comprises an electronic flight bag computer and at least two server computers which are linked via a databus in a network configuration. The electronic flight bag computer and the at least two server computers are linked via respective control lines. At least one of the server computers is configured to change between an electronic flight bag mode and an in-flight entertainment mode in response to receiving a pre-determined signal via the control line. At least one of the server computers comprises at least two network switches and is configured to activate one of the at least two network switches and to deactivate the other one of the at least two network switches in response to the pre-determined signal via the control line. | ||||||
| 104 | ELECTRONIC FLIGHT BAG SYSTEMS AND METHODS FOR VERIFYING CORRECT TAKEOFF PERFORMANCE DATA ENTRY | US13751831 | 2013-01-28 | US20140214246A1 | 2014-07-31 | Steve Johnson; Yasuo Ishihara; Kevin J. Conner; Robert A. Champion |
| Systems and methods for verifying that the flight crew has not made an error in entering takeoff flight performance data into the flight management system (FMS) using the electronic flight bag (EFB). The EFB includes a user interface that receives basic flight plan information and a processor. The processor automatically receives calculated takeoff performance data based on a previously entered basic flight plan, automatically receives user-entered takeoff performance data from a flight management system (FMS) located on a host aircraft, automatically compares the calculated takeoff performance data to the received takeoff performance data, and generates an entry error indication, if the comparison indicates that at least a portion of the entered takeoff performance data does not match the calculated takeoff performance data. An output device outputs the generated entry error indication. | ||||||
| 105 | Method and apparatus for remote e-Enabled aircraft solution management using an electronic flight bag (EFB) | US13676885 | 2012-11-14 | US09087419B2 | 2015-07-21 | Robert Lewis Lentz |
| A method for using an Electronic Flight Bag (EFB) located on an aircraft to communicate with a remote aircraft system data communications unit concerning aircraft systems problems and malfunctions, is disclosed. The method may include receiving aircraft systems data from one or more aircraft systems, identifying any problems or malfunctions in the aircraft systems, automatically communicating any identified problems or malfunctions in the aircraft systems to the remote aircraft system data communications unit, receiving information concerning a solution to the identified problems or malfunctions in the aircraft systems from the remote aircraft system data communications unit, and implementing the solution to the identified problems or malfunctions in the aircraft systems. | ||||||
| 106 | METHOD AND APPARATUS FOR REMOTE E-ENABLED AIRCRAFT SOLUTION MANAGEMENT USING AN ELECTRONIC FLIGHT BAG (EFB) | US13676885 | 2012-11-14 | US20130124034A1 | 2013-05-16 | Robert Lewis LENTZ |
| A method for using an Electronic Flight Bag (EFB) located on an aircraft to communicate with a remote aircraft system data communications unit concerning aircraft systems problems and malfunctions, is disclosed. The method may include receiving aircraft systems data from one or more aircraft systems, identifying any problems or malfunctions in the aircraft systems, automatically communicating any identified problems or malfunctions in the aircraft systems to the remote aircraft system data communications unit, receiving information concerning a solution to the identified problems or malfunctions in the aircraft systems from the remote aircraft system data communications unit, and implementing the solution to the identified problems or malfunctions in the aircraft systems. | ||||||
| 107 | Shielding device for optical and/or electronic apparatuses, and space vehicle comprising such device | US12512177 | 2009-07-30 | US08083407B2 | 2011-12-27 | Primo Attina; Enrico Domenico Bertuccio; Luciana Bonino |
| A shielding device (20) for optical and/or electronic apparatuses (16) is described, wherein said apparatuses may cooperate with incident electromagnetic radiation (X1, X2), in particular for space telescopes, the shielding device including: at least a filter (24, 26) provided for interacting with said incident electromagnetic radiation (X1, X2), for selectively filtering said radiation; and a support structure (22) for the filter. The support structure (22) is an inflatable structure, which is able to achieve an operating stand-by configuration, in which it is substantially folded together, and an active operating configuration, in which it extends along the longitudinal extension axis (ZZ), and is essentially completely unfolded. Furthermore, the filter (24, 26) includes a filter body, which is provided in order to be transversely positioned with respect to said longitudinal extension axis, when the support structure reaches its active operating configuration. | ||||||
| 108 | Shielding Device for Optical and/or Electronic Apparatuses, and Space Vehicle Comprising Such Device | US12512177 | 2009-07-30 | US20100034358A1 | 2010-02-11 | Primo Attina; Enrico Domenico Bertuccio; Luciana Bonino |
| A shielding device (20) for optical and/or electronic apparatuses (16) is described, wherein said apparatuses may cooperate with incident electromagnetic radiation (X1, X2), in particular for space telescopes, the shielding device including: at least a filter (24, 26) provided for interacting with said incident electromagnetic radiation (X1, X2), for selectively filtering said radiation; and a support structure (22) for the filter. The support structure (22) is an inflatable structure, which is able to achieve an operating stand-by configuration, in which it is substantially folded together, and an active operating configuration, in which it extends along the longitudinal extension axis (ZZ), and is essentially completely unfolded. Furthermore, the filter (24, 26) includes a filter body, which is provided in order to be transversely positioned with respect to said longitudinal extension axis, when the support structure reaches its active operating configuration. | ||||||
| 109 | Avionics system for assisting implementation of security measures onboard an aircraft, aircraft comprising such a system, and associated method | US15497916 | 2017-04-26 | US20170313425A1 | 2017-11-02 | Mathieu SENET |
| Avionics system for assisting implementation of security measures onboard an aircraft, aircraft comprising such a system, and associated method are provided. The avionics system is intended to assist the occupants of an aircraft in implementing security measures onboard the aircraft. It includes a parameter collector for collecting at least one avionics parameter of the aircraft, a context finder to determine a context from the or each avionics parameter collected by the collector, an instruction identifier to identify at least one relevant security instruction based on the context determined by the context finder, and at least one instruction submitter to submit the or each relevant security instruction to a passenger of the aircraft. | ||||||
| 110 | Method and apparatus for converting dirty electrical power to a clean electrical power suitable for a portable electronic flight bag in an aircraft | US13224111 | 2011-09-01 | US08581546B2 | 2013-11-12 | Richard Luke Ribich |
| Provided is an apparatus. The apparatus includes a power conditioning module. The power conditioning module includes an input that is operable to receive a first power from an aircraft. The power conditioning module includes electronic circuitry that is operable to transform the first power to a second power. The second power is different from the first power and is suitable for charging a portable electronic device. The power conditioning module includes a status indication mechanism that is operable to indicate a status of the power conditioning module. | ||||||
| 111 | Power supply system with at least a primary power source and an auxiliary power source for powering an electronic flight bag depending on an whether an aircraft is in a flight condition | US13176637 | 2011-07-05 | US09347790B2 | 2016-05-24 | Michael Haukom; Thomas Horsager; Brett Willenbring |
| A control system for providing electrical power to an electronic flight bag device on an aircraft. The control system including a power switching component coupled to a plurality of power sources and at least one electronic flight bag device. The power switching component is operative and configured to selectively apply electrical power from at least one of the plurality of power sources to the at least one electronic flight bag device based upon a condition of the aircraft. | ||||||
| 112 | METHOD AND APPARATUS FOR A PASSIVE AVIONICS DATA TRANSFER DEVICE FOR USE WITH COTS TABLET EQUIPMENT DEPLOYED AS CLASS I OR II ELECTRONIC FLIGHT BAG SYSTEMS | US13791249 | 2013-03-08 | US20140222254A1 | 2014-08-07 | Richard Luke Ribich |
| The present disclosure provides an aerospace grade data conversion apparatus. The data conversion apparatus includes an avionics interface module for: collecting data outputs from a plurality of analog and digital avionics and electrical data sources; aligning digital data respectively output from the plurality of digital data sources; and commingling the digital data in order to generate a data sequence interpreted by a receiving device, the receiving device including an electronic tablet. The present disclosure also provides a software developer's kit. The software developer's kit includes a library configured to allow application software developers to utilize digital data output from an avionics interface module. The present disclosure further includes a mounting system. The mounting system includes one or more assemblies for securing an electronic flight bag device to an aircraft, wherein the electronic flight bag includes an electronic tablet. | ||||||
| 113 | Method and apparatus for a passive avionics data transfer device for use with cots tablet equipment deployed as class I or II electronic flight bag systems | US13791249 | 2013-03-08 | US09335796B2 | 2016-05-10 | Richard Luke Ribich |
| The present disclosure provides an aerospace grade data conversion apparatus. The data conversion apparatus includes an avionics interface module for: collecting data outputs from a plurality of analog and digital avionics and electrical data sources; aligning digital data respectively output from the plurality of digital data sources; and commingling the digital data in order to generate a data sequence interpreted by a receiving device, the receiving device including an electronic tablet. The present disclosure also provides a software developer's kit. The software developer's kit includes a library configured to allow application software developers to utilize digital data output from an avionics interface module. The present disclosure further includes a mounting system. The mounting system includes one or more assemblies for securing an electronic flight bag device to an aircraft, wherein the electronic flight bag includes an electronic tablet. | ||||||
| 114 | Avionics calculator with integrated routing module, related communication network and communication installation, and aircraft comprising such a communication installation | US15262772 | 2016-09-12 | US20170078142A1 | 2017-03-16 | Martial MONTRICHARD; Benoit PIERSON; Marc FUMEY |
| This avionic calculator, intended to be loaded on board an aircraft, the avionic calculator includes a protective casing and at least one module from among an information processing module able to execute at least one software application, an input/output management module and an electric power supply management module, each module being positioned inside the casing. The avionic calculator further includes a routing module positioned inside the casing, the routing module including several communication ports and being configured for transmitting at least one message from an input communication port to an output communication port. | ||||||
| 115 | 飞行器的飞行控制方法、装置、存储介质及电子设备 | PCT/CN2018/108839 | 2018-09-29 | WO2020019517A1 | 2020-01-30 | 王传松 |
一种飞行器的飞行控制方法、飞行器的飞行控制装置、计算机可读存储介质及电子设备。该飞行控制方法包括：获取飞行器飞行的目标航向；获取当前时刻的太阳方位；获取阳光照射于遮阳指针上产生的投影位置；根据太阳方位和投影位置调整飞行器的当前航向，以使飞行器沿目标航向飞行。该方法在失去GPS导航的情况下也可以依据遮阳指针的投影位置和当前时刻的太阳方位为飞行器进行应急导航，提高了飞行器执行飞行任务的效率，避免了飞行器失去导航便只能原地盘旋等待而无法继续飞行的问题。 |
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| 116 | 控制方法、飞行器控制系统和旋翼飞行器 | PCT/CN2017/079976 | 2017-04-10 | WO2018187918A1 | 2018-10-18 | 刘怀宇; 吴一凡 |
一种控制方法、飞行器控制系统(100)和一种旋翼飞行器(10)，控制方法用于控制旋翼飞行器(10)，旋翼飞行器(10)包括旋翼电机(12)和云台(14)，旋翼飞行器(10)用于与穿戴式电子设备(20)通信，穿戴式电子设备(20)包括运动状态检测单元(22)，运动状态检测单元(22)用于获取用户的身体部位的运动状态。控制方法包括步骤：(S2)控制旋翼飞行器(10)向前飞行；(S4)在旋翼飞行器(10)向前飞行时，根据运动状态控制旋翼电机(12)以控制旋翼飞行器(10)的飞行方向；和/或(S6)根据运动状态控制云台(14)的转动方向。 |
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| 117 | 控制方法、控制装置及电子装置 | PCT/CN2016/105770 | 2016-11-14 | WO2018086129A1 | 2018-05-17 | 徐普; 苏冠华; 邹成; 朱成伟; 吴迪 |
一种控制方法、控制装置（110）及电子装置（100），其中，控制方法用于控制电子装置（100），电子装置（100）能够与飞行器（200）通信。控制方法包括：接收飞行器（200）的状态信息（S1）；根据状态信息获取飞行器（200）的飞行轨迹（S2）；及显示与飞行轨迹对应的三维动态图标（101）（S3）。 |
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| 118 | 电子设备 | PCT/CN2020/139211 | 2020-12-25 | WO2021129778A1 | 2021-07-01 | 成东村; 王微; 朱丽君; 罗政军; 张小南 |
本发明公开一种电子设备，其包括设备壳体和飞行拍摄器，设备壳体具有开口与内腔，开口与内腔连通，飞行拍摄器可移动地设置于设备壳体，飞行拍摄器可通过开口伸出至设备壳体之外或回缩至设备壳体之内，在飞行拍摄器位于设备壳体之外的情况下，飞行拍摄器可与设备壳体分离。 |
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| 119 | 飞行器的控制方法及装置 | PCT/CN2019/107777 | 2019-09-25 | WO2020063655A1 | 2020-04-02 | 孙满利; 葛翠丽; 杨艳梅; 马景旺 |
一种飞行器的控制方法及装置，属于通信技术领域。该方法包括：AMF网元获取飞行器的禁飞区域的信息（301）；当该飞行器与该禁飞区域之间的最短距离小于或等于第一预设值时，该AMF网元向控制装置发送参考信息（302）；其中，参考信息包括：第一指示信息和飞行器的位置信息中的至少一种信息，该第一指示信息用于指示该飞行器与该禁飞区域之间的最短距离小于或等于第一预设值。解决了为了阻止飞行器在禁飞区域飞行的效率较低，预先的准备过程较复杂，且耗时较长的问题，避免了在禁飞区域的边缘安装电子围栏，从而简化了预先的准备过程。用于飞行器的控制。 |
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| 120 | 飞行器及其控制方法、装置和电子设备 | PCT/CN2016/105356 | 2016-11-10 | WO2018086042A1 | 2018-05-17 | 骆磊 |
一种飞行器及其控制方法、装置和电子设备。其中飞行器（100）包括飞行器本体（110）；以及设置在所述飞行器本体（110）上的通信中继装置（120）；所述通信中继装置（120）适于使飞行器（100）作为通信中继节点实现至少两个待通信设备之间的通信。通过将飞行器（100）作为待通信设备之间通信网络的通信中继，可以通过飞行器（100）组建两点或多点间的通信网络，飞行器（100）的位置便于调整，满足了通信点间有障碍物或者无法架设实体线缆时的组网需求，且组网成本相比卫星通信较低。 |
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