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公开(公告)号：US11618956B2
公开(公告)日：2023-04-04
申请号：US16689526
申请日：2019-11-20
发明人： Thomas Eck , Walter Jehle , Winfried Lohmiller
IPC分类号： H01M8/0258 , C25B9/75 , H01M8/0267 , H01M8/04029 , H01M8/04007 , C25B11/036
摘要： A bipolar plate for use in an electrochemical device is proposed, in which a flow duct runs between two outer boundary surfaces and extends from a peripheral fluid inlet to a peripheral fluid outlet. As a result, very good cooling of electrochemical cells via a bipolar plate which is in surface contact therewith can be achieved.
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公开(公告)号：US09851724B2
公开(公告)日：2017-12-26
申请号：US14940353
申请日：2015-11-13
CPC分类号： G05D1/101 , B64C39/024 , B64D47/08 , G01S19/48 , G05D1/0653 , G08G5/0021 , G08G5/0065 , G08G5/0069 , G08G5/025
摘要： An automatic take-off and landing control device for an aircraft is provided. The control device comprises at least two of at least one local tracking device adapted for receiving at least one local signal from at least one local ground station and for determining a position of the aircraft based on the local signals, at least one GNSS tracking device adapted for receiving a GNSS signal and for determining a position of the aircraft based on the GNSS signal; and at least one camera device adapted for observing an environment of the aircraft and for determining a position of the aircraft based on the camera signal.
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13.发明申请METHOD FOR AUTONOMOUS CONTROLLING OF AN AERIAL VEHICLE AND CORRESPONDING SYSTEM 审中-公开用于自动控制汽车和相应系统的方法公开(公告)号：US20160240091A1
公开(公告)日：2016-08-18
申请号：US15023962
申请日：2014-09-23
CPC分类号： G08G5/045 , B64C39/02 , B64C2201/141 , G05D1/042 , G05D1/101 , G08G5/0013 , G08G5/0021 , G08G5/0056 , G08G5/0065 , G08G5/0069 , G08G5/0091 , G08G5/025
摘要： A method for autonomous controlling of an aerial vehicle, wherein a flight operator commands the aerial vehicle, comprising the steps of: measuring flight and/or system data of the aerial vehicle; performing an evaluation of a flight condition of the aerial vehicle based on the measured data and based on at least one decision criterion; and, issuing at least one autonomous controlling command, if, as a result of the evaluation of the flight condition, the aerial vehicle is in danger.
摘要翻译： 一种用于自主控制飞行器的方法，其中飞行操作员命令所述飞行器，包括以下步骤：测量所述飞行器的飞行和/或系统数据; 基于测量数据并基于至少一个决策标准对飞行器的飞行状况进行评估; 并且发出至少一个自主控制命令，如果作为对飞行条件的评估的结果，飞行器处于危险中。
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公开(公告)号：US11493171B2
公开(公告)日：2022-11-08
申请号：US16684235
申请日：2019-11-14
发明人： Michael Stamm , Clemens Brand , Winfried Lohmiller
IPC分类号： F17C1/06 , H01M8/04 , H01M8/06 , B64D37/02 , H01M8/04082 , H01M8/0656
摘要： A device for carrying fuel in aircraft and spacecraft includes a carrier element having a longitudinal axis, and a fuel tank with a side wall and a chamber at least partially delimited by the side wall. The tank is arranged in the carrier element. The chamber and the side wall extend in a direction along the longitudinal axis. The side wall has a pressure-receiving component that converts a pressure from the chamber on the side wall into a contraction force acting on the side wall along the longitudinal axis. The contraction force compensates for an expansion force, resulting from the pressure from the chamber and acting on the side wall along the longitudinal axis. This provides an improved device for carrying fuel in aircraft and spacecraft, wherein the aircraft and spacecraft has constant flight mechanical properties because of the device.
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公开(公告)号：US11186380B2
公开(公告)日：2021-11-30
申请号：US16864277
申请日：2020-05-01
IPC分类号： B64D31/00 , H01M8/04858 , H01M16/00 , H02J4/00
摘要： An energy management system for an aircraft, wherein the energy management system comprises a fuel cell configured to convert chemical energy into electric energy, at least one energy source configured to provide electric energy, at least one electrical load, an electric bus electrically coupled to the fuel cell, the at least one energy source, and the at least one electrical load, and a controller configured to control the at least one electrical load in such a manner that a minimum load to the fuel cell is ensured. Furthermore, an aircraft comprises such energy management system. A method for managing energy in a system comprises electrically coupling a fuel cell, at least one energy source, and at least one electrical load by an electric bus, and controlling at least one electrical load in such a manner that a minimum load to the fuel cell is ensured.
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公开(公告)号：US20200184834A1
公开(公告)日：2020-06-11
申请号：US16668164
申请日：2019-10-30
发明人： Winfried Lohmiller , Jörg Meyer , Thomas Heuer
摘要： A method for operating an at least temporarily unmanned aircraft, wherein a flight is performed according to a prior flight plan in an airspace controlled by a control instance. A flight direction is determined during the flight via a control device influenced via a data connection by a control instance. The data connection is temporarily unavailable, and a hazardous or emergency situation requiring deviation from the flight plan, is identified by the control device based on first sensor data. An avoidance route is determined by the control device based on a second sensor data, the avoidance route including a avoidance manoeuvre avoiding the hazardous or emergency situation, the avoidance route is used in the meantime to fly towards a destination area with the least possible volume of air traffic; and the necessary avoidance manoeuvre(s) are performed based on the second data by the control device in an autonomous staggering procedure.
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17.发明授权公开(公告)号：US10650685B2
公开(公告)日：2020-05-12
申请号：US15023983
申请日：2014-09-23
摘要： A method for autonomous controlling of a remote controlled aerial vehicle, wherein a flight operator commands the aerial vehicle, comprising the steps of: initializing a data link between the aerial vehicle and a ground segment; determining an operation condition of the data link during use of the data link; and issuing at least one autonomous controlling command, if, as a result of the determining, a loss of the data link is determined.
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公开(公告)号：US10109207B2
公开(公告)日：2018-10-23
申请号：US15084917
申请日：2016-03-30
摘要： A method for an aircraft for handling potential collisions in air traffic includes providing by a collision avoidance system a collision avoidance maneuver to avoid a collision with one or more intruders. The collision avoidance system is configured to obtain information about these intruders. The method includes further providing flight management constraints from an onboard flight system. Further, the method includes providing flight situation data from a navigation system. The method includes generating a modified collision avoidance maneuver based on the collision avoidance maneuver provided by the collision avoidance system, the flight situation data and the flight management constraints.
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公开(公告)号：US09753143B2
公开(公告)日：2017-09-05
申请号：US15035819
申请日：2014-11-10
CPC分类号： G01S19/32 , G01S19/18 , G01S19/21 , G05D1/0022 , G05D1/0077 , G08G5/0004
摘要： An aircraft navigation system and navigation method. The system comprises a civil-certified GPS-receiver for determining first position information based on C/A-GPS-signals, and a military-type GPS-receiver for determining a second position information based on P(Y)-GPS-signals. A monitoring unit detects a first abnormal condition during jamming conditions within the C/A-GPS-signals. The unit compares the first position information with the second position information and detects a second abnormal condition when a difference between these position information is larger than a threshold value for more than a threshold duration. Upon detecting an abnormal condition, an alert procedure is initiated. In remotely piloted aircraft, Command & Control link-loss is also monitored and during link-loss, a transponder code automatically indicates communication failure. When in such situation an abnormal condition is additionally detected, a transponder code indicates airborne emergency and, subsequently, the aircraft navigation system is switched to navigating based on position information from the military-type GPS-receiver.
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公开(公告)号：US09573682B2
公开(公告)日：2017-02-21
申请号：US14668408
申请日：2015-03-25
发明人： Hugo Heusinger , Winfried Lohmiller , Reinhard Reischl , Gregor Jarasch , Rosa Maria Delgado Romero
CPC分类号： B64C39/024 , B64C15/00 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/0077
摘要： A control and/or management system for a vehicle includes at least one of: (A) at least two redundant vehicle management computers configured to generate system control commands for each maneuvering actuators and for each system actor based on the data acquired by the sensors; (B) at least two redundant remote interface units for interconnecting a sensor or a system actor with a vehicle management computer; (C) at least two redundant actuator control computers configured to generate control commands for each maneuvering actuator based on received maneuvering commands; and (D) a common interface for connecting an external computer, the common interface being directly connected to at least two redundant computers.
摘要翻译： 一种用于车辆的控制和/或管理系统包括以下至少一个：（A）至少两个冗余车辆管理计算机，其被配置为基于由所述传感器获取的数据为每个操纵致动器和每个系统执行器生成系统控制命令; （B）至少两个用于将传感器或系统主体与车辆管理计算机互连的冗余远程接口单元; （C）至少两个冗余致动器控制计算机，其被配置为基于接收到的操纵命令来为每个操纵致动器生成控制命令; 和（D）用于连接外部计算机的通用接口，所述公共接口直接连接到至少两个冗余计算机。
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