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公开(公告)号：US10450077B2
公开(公告)日：2019-10-22
申请号：US15149019
申请日：2016-05-06
申请人： THE BOEING COMPANY
发明人： Eduardo Gabriel Ferreyra , Enrique Emilio Serrot , Jose Luis Lemus , Jose Antonio Blanco , Nieves Lapena
摘要： The present disclosure refers to a method and a related system of flight termination for air vehicles. The method and the system of flight termination for air vehicles involve deploying a parachute for flight termination of an air vehicle. A flight termination system, which in turn comprises at least one microcontroller unit that is connected to at least one parachute deployment system for deploying an air vehicle's parachute when a major emergency is determined during an air vehicle's flight.
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公开(公告)号：US09868548B2
公开(公告)日：2018-01-16
申请号：US14955945
申请日：2015-12-01
申请人： The Boeing Company
发明人： Enrique Emilio Serrot Hauke , Eduardo Gabriel Ferreyra , Jose Luis Lemus , Jose Antonio Blanco Del Alamo , Nieves Lapena Rey
CPC分类号： B64F1/08 , B64C39/024 , B64C2201/08
摘要： An unmanned aerial vehicles take-off system may include at least one winch, at least one towline, at least one dolly on which at least one aircraft is mounted, and at least one battery of the at least one winch. At least one micro-controller unit is connected to the at least one winch, wherein the at least one microcontroller unit is configured to control the activation/deactivation of the at least one winch. An unmanned aerial vehicle take-off method is also disclosed that includes operating the at least one winch by means of at least one microcontroller unit connected to said at least one winch.
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公开(公告)号：US20160340049A1
公开(公告)日：2016-11-24
申请号：US15149019
申请日：2016-05-06
申请人： THE BOEING COMPANY
发明人： Eduardo Gabriel Ferreyra , Enrique Emilio Serrot , Jose Luis Lemus , Jose Antonio Blanco , Nieves Lapena
摘要： The present disclosure refers to a method and a related system of flight termination for air vehicles. The method and the system of flight termination for air vehicles involve deploying a parachute for flight termination of an air vehicle. A flight termination system, which in turn comprises at least one microcontroller unit that is connected to at least one parachute deployment system for deploying an air vehicle's parachute when a major emergency is determined during an air vehicle's flight.
摘要翻译： 本公开涉及一种用于飞行器的飞行终止的方法和相关系统。 飞行器的飞行终止方法和系统涉及部署飞行终止飞机的降落伞。 飞行终端系统，其又包括至少一个微控制器单元，其连接到至少一个降落伞部署系统，以在空中飞行器飞行期间确定主要紧急情况时部署空中飞行器的降落伞。
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公开(公告)号：US20180175400A1
公开(公告)日：2018-06-21
申请号：US15837915
申请日：2017-12-11
申请人： The Boeing Company
发明人： Eduardo Gabriel Ferreyra , Enrique Emilio Serrot Hauke , Jose Luis Lemus , Jose Antonio Blanco , Nieves Lapeña-Rey
IPC分类号： H01M8/0202 , H01M16/00 , H01M8/04858 , H01M8/2465
CPC分类号： H01M8/0202 , H01M8/04559 , H01M8/0488 , H01M8/2432 , H01M8/2465 , H01M8/249 , H01M16/006 , H01M2250/20 , Y02T90/32
摘要： A fuel cell stack for enhanced hybrid power systems, comprising first (2) and second (3) conductive end plates with contact terminals (4); a plurality of fuel cells (7) configured to be connected in series and stacked between the conductive end plates (2, 3); at least one conductive middle plate (6, 6′) with at least one contact terminal (11, 11′), each conductive middle plate (6, 6′) being configured to be stacked between adjacent fuel cells (7). The contact terminals (11, 11′) may comprise conductive tabs (11) protruding from the fuel cell stack (1).The invention also refers to a hybrid power system comprising a battery (50), a fuel cell stack (1) and a control unit (70) configured to select an operating voltage of the fuel cell stack (1) when the hybrid power system (90) is feeding a load (60). The operating voltage is obtained from the contact terminals (4, 11, 11′) of the conductive middle plate (6, 6′) and conductive end plates (2, 3) depending on the values of the voltages (V1, V2, V3) at the contact terminals (4, 11, 11′) of the fuel cell stack (1).
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公开(公告)号：US20170159883A1
公开(公告)日：2017-06-08
申请号：US15360928
申请日：2016-11-23
申请人： The Boeing Company
发明人： Nieves Lapeña Rey , Jose Antonio Blanco , Jose Luis Lemus , Enrique Emilio Serrot Hauke , Eduardo Gabriel Ferreyra
CPC分类号： F17C13/001 , F17C3/08 , F17C2201/0109 , F17C2201/0119 , F17C2201/0161 , F17C2201/0166 , F17C2201/0171 , F17C2201/035 , F17C2201/056 , F17C2203/0391 , F17C2203/0629 , F17C2203/0646 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2260/016 , F17C2260/033 , F17C2270/0168 , F17C2270/0186 , F17C2270/0189 , Y02E60/321
摘要： Method and apparatus for storing cryogenic liquids. A cryogenic tank comprising an inner storage volume within a first wall and a plurality of chambers defined by a plurality of chamber walls within the inner storage volume. The chamber walls extending the length of the inner storage volume, and the chambers disposed along the first wall and that at least one of the chambers of the plurality of chambers is defined by a plurality of chamber walls and a portion of the first wall.
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公开(公告)号：US20160167804A1
公开(公告)日：2016-06-16
申请号：US14955945
申请日：2015-12-01
申请人： The Boeing Company
发明人： Enrique Emilio Serrot Hauke , Eduardo Gabriel Ferreyra , Jose Luis Lemus , Jose Antonio Blanco Del Alamo , Nieves Lapena Rey
CPC分类号： B64F1/08 , B64C39/024 , B64C2201/08
摘要： An unmanned aerial vehicles take-off system may include at least one winch, at least one towline, at least one dolly on which at least one aircraft is mounted, and at least one battery of the at least one winch. At least one micro-controller unit is connected to the at least one winch, wherein the at least one microcontroller unit is configured to control the activation/deactivation of the at least one winch. An unmanned aerial vehicle take-off method is also disclosed that includes operating the at least one winch by means of at least one microcontroller unit connected to said at least one winch.
摘要翻译： 无人飞行器起飞系统可以包括至少一个绞盘，至少一个拖链，至少一个安装有至少一架飞机的小车以及至少一个绞盘的至少一个电池。 至少一个微控制器单元连接到所述至少一个绞盘，其中所述至少一个微控制器单元被配置为控制所述至少一个绞盘的激活/去激活。 还公开了一种无人飞行器起飞方法，其包括通过连接到所述至少一个绞盘的至少一个微控制器单元来操作所述至少一个绞盘。
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