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公开(公告)号:US08484962B2
公开(公告)日:2013-07-16
申请号:US12443760
申请日:2008-06-19
申请人: Robert Behr , Jurgen Laude , Rolf Gossing , Sebastian Lauckner
发明人: Robert Behr , Jurgen Laude , Rolf Gossing , Sebastian Lauckner
CPC分类号: B64C13/40 , F15B21/042 , Y10T137/7737
摘要: The invention relates to a system for regulating a temperature of hydraulic fluid in at least one hydraulic circuit of an aircraft, wherein, in a periphery of the aircraft, additional hydraulic consumption units are each provided with at least one controllable valve for heating the hydraulic fluid above an adjustable minimum temperature limit value (Tmin), wherein the controllable valve is closed during a maneuver of the aircraft, wherein the controllable valves of the additional hydraulic consumption units are closed when the temperature of the hydraulic fluid exceeds an adjustable theoretical temperature value (Tsoll), and wherein a temperature control system is connected to a temperature sensor for adjusting the controllable valve on the basis of a local temperature of the hydraulic fluid, the temperature sensor being near the hydraulic consumption units which are arranged in wings and tail of the aircraft.
摘要翻译: 本发明涉及一种用于调节飞行器的至少一个液压回路中的液压流体的温度的系统,其中,在飞行器的周边中,附加的液压消耗单元分别设置有至少一个用于加热液压流体的可控阀 高于可调节的最小温度极限值(Tmin),其中在飞行器的操纵期间可控阀关闭,其中当液压流体的温度超过可调节的理论温度值时,额外的液压消耗单元的可控阀被关闭 Tsoll),并且其中温度控制系统连接到温度传感器,用于基于液压流体的局部温度来调节可控阀,所述温度传感器靠近布置在机翼和尾部的液压消耗单元 飞机。
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公开(公告)号:US20100170238A1
公开(公告)日:2010-07-08
申请号:US12443760
申请日:2008-06-19
申请人: Robert Behr , Jurgen Laude , Rolf Grossing , Sebastian Lauckner
发明人: Robert Behr , Jurgen Laude , Rolf Grossing , Sebastian Lauckner
CPC分类号: B64C13/40 , F15B21/042 , Y10T137/7737
摘要: The present invention provides a device and a method for regulating a temperature (T) of hydraulic fluid in at least one hydraulic circuit (2) of an aircraft (1). In this case the temperature (T) of the hydraulic fluid is regulated so that it is above an adjustable minimum temperature limit value {Tmin) of approximately 20° C., for example, at all times.
摘要翻译: 本发明提供一种用于调节飞机(1)的至少一个液压回路(2)中的液压流体的温度(T)的装置和方法。 在这种情况下,液压流体的温度(T)被调节为使其高于约20℃的可调节的最小温度极限值(Tmin),例如始终是。
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公开(公告)号:US07578548B2
公开(公告)日:2009-08-25
申请号:US10540194
申请日:2003-12-02
申请人: Robert Behr , Martin Gruenbaum , Dieter Lange
发明人: Robert Behr , Martin Gruenbaum , Dieter Lange
IPC分类号: B60J11/00
CPC分类号: B60R21/34 , B60R2021/343 , B62D25/105
摘要: An engine hood for motor vehicles has a deformable head impact zone to protect pedestrians in the event of a collision with the motor vehicle. The engine hood comprises an outer shell, which is formed by the body paneling, and an inner shell which is arranged below the outer shell and is connected to the outer shell. The inner shell is provided with a vault-structured stiffening region in the region of the head impact zone.
摘要翻译: 机动车辆的发动机罩具有可变形的头部撞击区域,以在与机动车辆碰撞的情况下保护行人。 发动机罩包括由车身镶板形成的外壳和布置在外壳下方并连接到外壳的内壳。 内壳在头部撞击区域的区域中设置有拱顶结构的加强区域。
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公开(公告)号:US20060220418A1
公开(公告)日:2006-10-05
申请号:US10540194
申请日:2003-12-02
申请人: Robert Behr , Martin Gruenbaum , Dieter Lange
发明人: Robert Behr , Martin Gruenbaum , Dieter Lange
IPC分类号: B60R27/00
CPC分类号: B60R21/34 , B60R2021/343 , B62D25/105
摘要: An engine hood for motor vehicles has a deformable head impact zone to protect pedestrians in the event of a collision with the motor vehicle. The engine hood comprises an outer shell, which is formed by the body paneling, and an inner shell which is arranged below the outer shell and is connected to the outer shell. The inner shell is provided with a vault-structured stiffening region in the region of the head impact zone.
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