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公开(公告)号：US09233759B2
公开(公告)日：2016-01-12
申请号：US13703497
申请日：2011-06-06
摘要： An aircraft electrical supply circuit including: a power distribution network, onboard the aircraft, for electrical devices located in an engine of the aircraft or near the engine; and a power supply generator built into the engine of the aircraft to supply AC voltage power to a deicing or anti-icing system. The power supply generator is connected to a thrust reverser electromechanical actuator by a rectifier for supplying DC voltage power to the actuator.
摘要翻译： 一种飞机供电电路，包括：飞机上的配电网，位于飞机发动机或发动机附近的电气设备; 以及内置于飞行器发动机中的电源发生器，以向除冰或防冰系统提供交流电压。 电源发生器通过用于向致动器提供直流电压电力的整流器连接到推力反向器机电致动器。
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2.发明授权Regulating the flow rate of fuel taken from a fuel circuit of an aircraft propelled by an engine 有权调节从发动机推进的飞行器的燃料回路中获取的燃料的流量公开(公告)号：US08484977B2
公开(公告)日：2013-07-16
申请号：US12499391
申请日：2009-07-08
IPC分类号： F02C9/00
CPC分类号： F02C7/236 , F02C7/32 , F02C7/36 , F02C9/30 , F02C9/56 , F05D2220/323 , F05D2270/304 , F05D2270/31 , Y02T50/671
摘要： The invention relates to a device for regulating the flow rate of fuel taken from a fuel circuit of an aircraft propelled by an engine. The device comprises: a positive displacement pump receiving fuel from a fuel circuit of the aircraft and delivering fuel at a flow rate that is proportional to its speed of rotation; a differential gear having a predefined transmission ratio, a first inlet mechanically coupled to the aircraft engine, a second inlet mechanically coupled to an electric motor/generator, and an outlet mechanically coupled to the positive displacement pump to drive it in rotation; and an electronic control system for regulating the speed of rotation of the electric motor/generator as a function of a setpoint value for the flow rate of fuel to be injected.
摘要翻译： 本发明涉及一种用于调节从由发动机推进的飞行器的燃料回路获取的燃料的流量的装置。 该装置包括：容积式泵，其从飞行器的燃料回路接收燃料并以与其旋转速度成比例的流量输送燃料; 具有预定传动比的差速齿轮，机械联接到飞行器发动机的第一入口，机械耦合到电动机/发电机的第二入口，以及机械联接到所述正排量泵以驱动其旋转的出口; 以及用于根据要喷射的燃料的流量的设定点值来调节电动机/发电机的转速的电子控制系统。
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3.发明申请REGULATING THE FLOW RATE OF FUEL TAKEN FROM A FUEL CIRCUIT OF AN AIRCRAFT PROPELLED BY AN ENGINE 有权从发动机推出的飞机的燃油电路调节燃油流量公开(公告)号：US20100018182A1
公开(公告)日：2010-01-28
申请号：US12499391
申请日：2009-07-08
CPC分类号： F02C7/236 , F02C7/32 , F02C7/36 , F02C9/30 , F02C9/56 , F05D2220/323 , F05D2270/304 , F05D2270/31 , Y02T50/671
摘要： The invention relates to a device for regulating the flow rate of fuel taken from a fuel circuit of an aircraft propelled by an engine. The device comprises: a positive displacement pump receiving fuel from a fuel circuit of the aircraft and delivering fuel at a flow rate that is proportional to its speed of rotation; a differential gear having a predefined transmission ratio, a first inlet mechanically coupled to the aircraft engine, a second inlet mechanically coupled to an electric motor/generator, and an outlet mechanically coupled to the positive displacement pump to drive it in rotation; and an electronic control system for regulating the speed of rotation of the electric motor/generator as a function of a setpoint value for the flow rate of fuel to be injected.
摘要翻译： 本发明涉及一种用于调节从由发动机推进的飞行器的燃料回路获取的燃料的流量的装置。 该装置包括：容积式泵，其从飞行器的燃料回路接收燃料并以与其旋转速度成比例的流量输送燃料; 具有预定传动比的差速齿轮，机械联接到飞行器发动机的第一入口，机械耦合到电动机/发电机的第二入口，以及机械联接到所述正排量泵以驱动其旋转的出口; 以及用于根据要喷射的燃料的流量的设定点值来调节电动机/发电机的转速的电子控制系统。
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公开(公告)号：US20130206902A1
公开(公告)日：2013-08-15
申请号：US13703497
申请日：2011-06-06
摘要： An aircraft electrical supply circuit including: a power distribution network, onboard the aircraft, for electrical devices located in an engine of the aircraft or near the engine; and a power supply generator built into the engine of the aircraft to supply AC voltage power to a deicing or anti-icing system. The power supply generator is connected to a thrust reverser electromechanical actuator by a rectifier for supplying DC voltage power to the actuator.
摘要翻译： 一种飞机供电电路，包括：飞机上的配电网，位于飞机发动机或发动机附近的电气设备; 以及内置于飞行器发动机中的电源发生器，以向除冰或防冰系统提供交流电压。 电源发生器通过用于向致动器提供直流电压电力的整流器连接到推力反向器机电致动器。
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