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公开(公告)号：US10399692B2
公开(公告)日：2019-09-03
申请号：US15101786
申请日：2014-11-27
发明人： Enrique Soriano , Sven Kopp , Winfried Lohmiller , Christian Thiele , Sergio Fernandez , Pablo Blazques
摘要： An aircraft fuel system comprises a fuselage tank and wing fuel tanks each connected to the fuselage fuel tank by a respective fuel line. A first fuel line connects the fuselage fuel tank to a collector fuel tank, which is connected by second fuel lines to aircraft engines in use of the system. Unspent fuel output from the aircraft engines is returned to the collector fuel tank via third fuel lines. A fuel line arrangement is arranged to draw fuel from, and return that fuel to, the wing fuel tanks. Fuel within the third fuel lines is thermally coupled to fuel within the fuel line arrangement by a heat exchanger. Heat energy within unspent fuel output from the aircraft engines is transferred to the wing fuel tanks, reducing the likelihood of fuel freezing within these tanks during extended flying in cold environments.
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公开(公告)号：US10049590B2
公开(公告)日：2018-08-14
申请号：US15023962
申请日：2014-09-23
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.
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3.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：US09944398B2
公开(公告)日：2018-04-17
申请号：US15035716
申请日：2014-11-10
发明人： Christian Thiele , Emil Cernko
CPC分类号： B64D13/08 , B64D2013/0614 , B64D2013/0629 , B64D2013/064 , B64D2013/0674 , F24F2005/0039 , F25D3/10 , Y02T50/56
摘要： A cooling system for an interior space of a vehicle comprises a main cooling system coupled with an air inlet for receiving air and coupled with the interior space for providing cooled air to the interior space, at least one air duct arranged between the air inlet and the interior space, a reservoir for liquid nitrogen having a nitrogen outlet and a valve arranged between the outlet and an injection port of the at least one air duct. The reservoir is couplable with the injection port of the at least one air duct via the valve on demand for evaporating nitrogen in the at least one air duct. With the injection of liquid nitrogen the main cooling system is supported in case it is not able to provide a sufficient cooling power.
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5.发明申请METHOD FOR AUTONOMOUS CONTROLLING OF A REMOTE CONTROLLED AERIAL VEHICLE AND CORRESPONDING SYSTEM 审中-公开远程控制车辆和相应系统的自动控制方法公开(公告)号：US20160232795A1
公开(公告)日：2016-08-11
申请号：US15023983
申请日：2014-09-23
CPC分类号： G08G5/0069 , B64C39/024 , B64C2201/141 , B64C2201/146 , G05D1/0022 , G05D1/0088 , G08G5/0013 , G08G5/0056 , G08G5/045
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.
摘要翻译： 一种用于自主控制遥控飞行器的方法，其中飞行操作者命令所述飞行器，包括以下步骤：初始化所述空中飞行器与地面段之间的数据链路; 在数据链路的使用期间确定数据链路的操作条件; 以及发出至少一个自主控制命令，如果作为确定的结果确定了数据链路的丢失。
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公开(公告)号：US20160257411A1
公开(公告)日：2016-09-08
申请号：US15035716
申请日：2014-11-10
发明人： Christian Thiele , Emil Cernko
CPC分类号： B64D13/08 , B64D2013/0614 , B64D2013/0629 , B64D2013/064 , B64D2013/0674 , F24F2005/0039 , F25D3/10 , Y02T50/56
摘要： A cooling system for an interior space of a vehicle comprises a main cooling system coupled with an air inlet for receiving air and coupled with the interior space for providing cooled air to the interior space, at least one air duct arranged between the air inlet and the interior space, a reservoir for liquid nitrogen having a nitrogen outlet and a valve arranged between the outlet and an injection port of the at least one air duct. The reservoir is couplable with the injection port of the at least one air duct via the valve on demand for evaporating nitrogen in the at least one air duct. With the injection of liquid nitrogen the main cooling system is supported in case it is not able to provide a sufficient cooling power.
摘要翻译： 一种用于车辆内部空间的冷却系统，包括与用于接收空气的空气入口耦合的主冷却系统，并与内部空间相连，用于向内部空间提供冷却的空气，至少一个空气管道，其布置在空气入口和 内部空间，具有氮气出口的液氮的储存器和布置在所述出口与所述至少一个空气管道的注入口之间的阀。 储存器可随着至少一个空气管道的注入口经由阀根据要求与至少一个空气管道中的氮气蒸发相联。 在注入液氮的情况下，主冷却系统不能提供足够的冷却功率。
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7.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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