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41. 发明授权

US10492246B2 Method and communications system for speech communication 有权
公开(公告)号：US10492246B2
公开(公告)日：2019-11-26
申请号：US16177982
申请日：2018-11-01
申请人： FREQUENTIS AG
发明人： Ernst Szabo , Bernhard Haindl , Gerald Mohnl
IPC分类号： H04W76/45 , H04L29/06 , H04W4/10 , G08G5/00 , H04W84/08
CPC分类号： H04W76/45 , G08G5/0026 , G08G5/0095 , H04L65/4061 , H04W4/10 , H04M2250/74 , H04W84/08
摘要： A method and a communications system for speech communication includes a plurality of workstations and a plurality of radio transmission devices and radio receiving devices. There are control units in the signal path between the workstations and the radio transmission devices and the radio receiving devices. The control units select the speech signals of one of the workstations according to predetermined or predeterminable criteria when there is a simultaneous plurality of operating signals of a plurality of workstations, or overlap the speech signals of a plurality of workstations according to predefined criteria, and transmit the speech signal thus obtained, chosen or overlapped for sending on the radio transmission device. Further, the control units transmit a receiving signal to the workstations connected thereto when the speech signals transmitted from the radio receiving unit are present, and transfer the speech signals to said workstations.

42. 发明申请

US20180253097A1 VEHICLE SYSTEM AND METHOD FOR PROVIDING SERVICES 审中-公开
公开(公告)号：US20180253097A1
公开(公告)日：2018-09-06
申请号：US15971530
申请日：2018-05-04
申请人： SkyRyse, Inc.
发明人： Mark Groden , Mitch Adler , Nur Harell
IPC分类号： G05D1/00 , G08G5/00 , G05D1/02 , B64F5/60 , B64D45/00
CPC分类号： G05D1/0088 , A61G3/001 , A61G2220/10 , B64D45/00 , B64D45/08 , B64D2045/0085 , B64F1/18 , B64F5/60 , G05D1/0202 , G05D1/0676 , G06F19/00 , G06K9/00771 , G06Q10/047 , G06Q10/0832 , G06Q50/22 , G06Q50/30 , G07C5/008 , G08B7/06 , G08G5/0013 , G08G5/003 , G08G5/0034 , G08G5/0056 , G08G5/0091 , G08G5/0095 , G16H15/00 , G16H40/20
摘要： A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

43. 发明申请

US20180214324A1 SAFETY SYSTEM FOR AERIAL VEHICLES AND METHOD OF OPERATION 审中-公开
公开(公告)号：US20180214324A1
公开(公告)日：2018-08-02
申请号：US15903996
申请日：2018-02-23
申请人： SkyRyse, Inc.
发明人： Mark Groden , Mitch Adler
IPC分类号： A61G3/00 , G08G5/00 , B64F5/60 , G16H40/20 , B64D45/08 , B64F1/18 , G07C5/00 , G06Q50/30 , G06Q10/02 , G05D1/00 , G16H15/00 , G06K9/00 , G08B7/06
CPC分类号： A61G3/001 , A61G2220/10 , B64D17/80 , B64D45/04 , B64D45/08 , B64F1/18 , B64F5/60 , G05D1/0088 , G05D1/0808 , G06K9/00771 , G06Q10/02 , G06Q50/30 , G07C5/008 , G08B7/06 , G08G5/0013 , G08G5/003 , G08G5/0034 , G08G5/0056 , G08G5/0069 , G08G5/0095 , G16H15/00 , G16H40/20
摘要： A safety system for an aerial vehicle, preferably including: a ballistic subsystem, preferably including one or more rockets operable to adjust motion of the aerial vehicle and a mounting unit that couples the ballistic subsystem to the aerial vehicle; and/or a deployable parachute subsystem. An aerial vehicle, preferably including a safety system. A method for aerial vehicle operation, preferably including activating a safety system.

44. 发明申请

US20170267343A1 UNMANNED AERIAL VEHICLE OPERATION SYSTEMS 审中-公开
公开(公告)号：US20170267343A1
公开(公告)日：2017-09-21
申请号：US15072172
申请日：2016-03-16
申请人： FUJITSU LIMITED
发明人： Wei-Peng CHEN , Daisuke MASHIMA
IPC分类号： B64C39/02 , G06Q10/08 , G08G5/00 , H04L29/08 , B64F1/36
CPC分类号： B64C39/024 , B64C2201/042 , B64C2201/066 , B64C2201/128 , B64C2201/141 , B64C2201/182 , G06Q10/08355 , G08G5/0026 , G08G5/0034 , G08G5/0069 , G08G5/0095
摘要： A method of deploying an unmanned aerial vehicle (UAV) operation system may be provided. A method may include estimating an amount of traffic for one or more routes based on a demand of the one or more routes. The method may also include determining a required number of docking stations for each route of the one or more routes based on the estimated amount of traffic for the route, a distance of the route, and a maximum travel distance for a UAV. Further, the method may include installing the required number of docking stations for each route of the one or more routes, wherein each docking station of the required number of docking stations including at least one of a power supply, a wireless charger, a communication module, a control module, and a camera.

45. 发明授权

US09741254B2 System and method for defining and predicting aircraft trajectories 有权
公开(公告)号：US09741254B2
公开(公告)日：2017-08-22
申请号：US15109319
申请日：2014-11-24
申请人： The Boeing Company
发明人： Francisco Navarro , Ernesto Hernandez Valls , Miguel Vilaplana , Piero Chessa , Carlos Querejeta Massaveu
IPC分类号： G05D1/00 , G08G5/00 , G01C21/20 , G06Q10/04 , G06Q50/30
CPC分类号： G08G5/0052 , G01C21/20 , G06Q10/047 , G06Q50/30 , G08G5/0034 , G08G5/0091 , G08G5/0095
摘要： The method of the present invention comprises acquiring input data of both aircraft performance characteristics and atmospheric data, and defining trajectory parameters to which the aircraft trajectory must be subjected, the method further comprising defining aircraft trajectory parameters; acquiring a plurality of atmospheric forecast ensembles; calculating a predicted trajectory from each atmospheric forecast of an atmospheric forecast ensemble, said predicted trajectory having associated information regarding a certain figure of merit of the aircraft trajectory, wherein an ensemble of predicted trajectories is obtained from each atmospheric forecast ensemble, each predicted trajectory of the ensemble of predicted trajectories having an associated probability derived from the probability of each atmospheric forecast within an atmospheric forecast ensemble; the system of the present disclosure comprising all the necessary equipment to carry out the method of the present disclosure.

46. 发明申请

US20160343258A1 System and Method for Defining and Predicting Aircraft Trajectories 有权
标题翻译：定义和预测飞机轨迹的系统和方法
公开(公告)号：US20160343258A1
公开(公告)日：2016-11-24
申请号：US15109319
申请日：2014-11-24
申请人： THE BOEING COMPANY
发明人： Francisco Navarro , Ernesto Hernandez Valls , Miguel Vilaplana , Piero Chessa , Carlos Querejeta Massaveu
IPC分类号： G08G5/00
CPC分类号： G08G5/0052 , G01C21/20 , G06Q10/047 , G06Q50/30 , G08G5/0034 , G08G5/0091 , G08G5/0095
摘要： The method of the present invention comprises acquiring input data of both aircraft performance characteristics and atmospheric data, and defining trajectory parameters to which the aircraft trajectory must be subjected, the method further comprising defining aircraft trajectory parameters; acquiring a plurality of atmospheric forecast ensembles; calculating a predicted trajectory from each atmospheric forecast of an atmospheric forecast ensemble, said predicted trajectory having associated information regarding a certain figure of merit of the aircraft trajectory, wherein an ensemble of predicted trajectories is obtained from each atmospheric forecast ensemble, each predicted trajectory of the ensemble of predicted trajectories having an associated probability derived from the probability of each atmospheric forecast within an atmospheric forecast ensemble; the system of the present disclosure comprising all the necessary equipment to carry out the method of the present disclosure.
摘要翻译：本发明的方法包括获取飞机性能特征和大气数据两者的输入数据，以及定义飞机轨迹必须经受的轨迹参数，该方法还包括定义飞机轨迹参数; 获取多个大气预报组合; 计算大气预报集合的每个大气预报的预测轨迹，所述预测轨迹具有关于飞机轨迹的某个品质因数的相关信息，其中从每个大气预报集合获得每个预测轨迹的集合，每个预测轨迹具有相关概率的预测轨迹的集合从大气预报集合内的每个大气预报的概率导出; 本公开的系统包括执行本公开的方法的所有必要设备。

47. 发明授权

US09218742B2 System and method for airport noise monitoring 有权
标题翻译：机场噪声监测系统及方法
公开(公告)号：US09218742B2
公开(公告)日：2015-12-22
申请号：US11686172
申请日：2007-03-14
申请人： James Barry , Renee Johns Alter , Ron Dunsky
发明人： James Barry , Renee Johns Alter , Ron Dunsky
IPC分类号： G08B21/00 , G08G5/00 , G08G1/01
CPC分类号： G08G5/0095 , G08G1/0104 , G08G5/0013 , G08G5/0026 , G08G5/0082
摘要： Described are a system and a method for airport noise monitoring. The system may include (a) a data receiving arrangement receiving, from a data source, information corresponding to an airport; (b) a data comparing arrangement comparing the received information to noise rules; and (c) an alert generating arrangement generating a noise alert based on the comparison of the received information to the noise rules.
摘要翻译：描述了一种用于机场噪声监测的系统和方法。该系统可以包括（a）数据接收装置，从数据源接收对应于机场的信息; （b）将接收的信息与噪声规则进行比较的数据比较装置; 和（c）警报生成装置，其基于所接收的信息与噪声规则的比较来产生噪声警报。

48. 发明申请

US20150364044A1 AIRCRAFT DISPLAY SYSTEMS AND METHODS FOR PROVIDING AN AIRCRAFT DISPLAY FOR USE WITH AIRPORT DEPARTURE AND ARRIVAL PROCEDURES 有权
标题翻译：飞机展示系统和提供航空器显示的方法，用于机场出发和到达程序
公开(公告)号：US20150364044A1
公开(公告)日：2015-12-17
申请号：US14302649
申请日：2014-06-12
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Rajanikanth Nagaraj Kashi , Divakara Rao Vadada , Cercuncesao Fernandes
IPC分类号： G08G5/00
CPC分类号： G08G5/0021 , G01C23/005 , G08G5/0013 , G08G5/0065 , G08G5/0078 , G08G5/0095 , G08G5/025 , G08G5/045
摘要： A method for generating a flight display in an aircraft includes the steps of receiving an indication of an arrival or a departure procedure for the aircraft to follow, receiving an indication of a current position and altitude of the aircraft, and receiving a voice communication or information by digital data link regarding the arrival or departure procedure. The method further includes the steps of recognizing speech in the voice communication and transforming the speech to a restriction regarding the arrival or departure procedure and providing a flight display comprising a visual depiction of the arrival or departure procedure, the current position and altitude of the aircraft, and the restriction regarding the arrival or departure procedure. The method also provides improved situational awareness to pilots by providing appropriate alerts and indications in the context of these restrictions and the implications that these may have on the ownship with reference to the surrounding traffic and the emergent conditions.
摘要翻译：一种用于在飞行器中产生飞行显示的方法包括以下步骤：接收飞行器的到达或离开程序的指示，接收飞行器的当前位置和高度的指示，以及接收语音通信或信息通过关于到达或离开程序的数字数据链接。该方法还包括以下步骤：识别语音通信中的语音并将语音转换为关于到达或离开过程的限制，并提供飞行显示，其包括到达或离开过程的视觉描述，飞行器的当前位置和高度以及关于到达或离开程序的限制。该方法还通过在这些限制的背景下提供适当的警报和指示以及这些可能对自身的影响，参考周围的交通和紧急情况，为飞行员提供了更好的情境意识。

49. 发明申请

US20150293225A1 AERIAL POSITIONING SYSTEMS AND METHODS 有权
标题翻译：空气定位系统和方法
公开(公告)号：US20150293225A1
公开(公告)日：2015-10-15
申请号：US14543493
申请日：2014-11-17
申请人： THE BOEING COMPANY
发明人： David Ray Riley , John N. Sanders-Reed
IPC分类号： G01S17/06 , G01S17/93
CPC分类号： G01S17/06 , B64D39/00 , G01S17/42 , G01S17/74 , G01S17/88 , G01S17/933 , G05D1/0684 , G05D1/104 , G08G5/0021 , G08G5/0069 , G08G5/0095 , G08G5/025
摘要： Aerial positioning systems and methods include a Light Detection and Ranging (LIDAR) device mounted to a hub and one or more reflectors attached to a portion of an aircraft and configured to encode information scanable by the LIDAR device. The LIDAR device is configured to scan a field of view to identify the one or more reflectors and reflector encoded information to determine reflector position data.
摘要翻译：空中定位系统和方法包括安装到集线器的光检测和测距（LIDAR）装置，以及附接到飞行器的一部分的一个或多个反射器，并配置为编码由激光雷达装置扫描的信息。 LIDAR设备被配置为扫描视场以识别一个或多个反射器和反射器编码信息以确定反射器位置数据。

50. 发明申请

US20150262490A1 Flight management method and system 有权
标题翻译：飞行管理方法和系统
公开(公告)号：US20150262490A1
公开(公告)日：2015-09-17
申请号：US14627645
申请日：2015-02-20
申请人： THALES
发明人： Guy DEKER , Michel ROGER , Bruno AYMERIC
IPC分类号： G08G5/00
CPC分类号： G08G5/0039 , G05D1/101 , G08G5/0013 , G08G5/0021 , G08G5/0047 , G08G5/0052 , G08G5/0095
摘要： A method and system, for flight management of an aircraft flying on a trajectory shifted with respect to a flight plan comprising a plurality of constrained waypoints, comprises a step of determining and displaying at least one point of the trajectory, termed decision point, beyond which the aircraft can no longer rejoin a constrained waypoint of the flight plan by determining a point of intersection between the trajectory and a rejoining trajectory steering towards the selected constrained waypoint, the rejoining trajectory complying with at least one predefined criterion.
摘要翻译：一种用于对在相对于包括多个受限航路点的飞行计划移动的轨迹上飞行的飞行器的飞行管理的方法和系统包括确定和显示所述轨迹的至少一个点（被称为决策点）的步骤，超过该点飞行器不能再通过确定轨迹与朝向选定的受限航路点转向的重合轨迹之间的交点，重新加入飞行计划的约束航点，该重合轨迹符合至少一个预定准则。

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