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公开(公告)号：US20200262576A1
公开(公告)日：2020-08-20
申请号：US16850361
申请日：2020-04-16
申请人： BOMBARDIER INC.
发明人： Vincenzo FURGIUELE
摘要： A method of and a system for operating a fuel pump management system of an aircraft. The method comprises receiving, from a fuel gauge, an electronic reading of a level of fuel fluid contained in a fuel tank; and analysing the electronic reading of the level of the fuel fluid, the analysing comprising upon determining that the level of fuel fluid is equal or below a predetermined fuel level threshold, causing a fuel pump in communication with the fuel tank to be shut down.
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公开(公告)号：US20170152056A1
公开(公告)日：2017-06-01
申请号：US15363509
申请日：2016-11-29
发明人： Dylan JAMES , Justine McCARTHY , Angus MORGAN , Michael POAD , Nicholas MORTON , Henry EDWARDS , Richard BURNESS , Christopher SLACK
摘要： An aircraft fuel tank system including a fuel tank compartment for containing liquid fuel and having a float-activated valve arranged to become positively buoyant when immersed in liquid fuel so that the float moves up to a raised position which causes the valve to close and prevent liquid fuel from flowing out of the fuel tank compartment through the valve. The float is also arranged to move down to a lowered position in response to a level of the liquid fuel in the fuel tank compartment dropping, the movement of the float to the lowered position causing the valve to open and permit liquid fuel to flow out of the fuel tank compartment through the valve. A pressure-activated valve may be used as an alternative to the float-activated valve.
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公开(公告)号：US11814188B2
公开(公告)日：2023-11-14
申请号：US16947201
申请日：2020-07-22
发明人： Jeffery Barnes , Patrick Leonard , John Hume
CPC分类号： B64D37/20 , B64D37/28 , F16L37/008 , F16L37/0847 , F16L37/40 , F16K31/44
摘要： A fuel drain engagement tool and a method for draining fuel from a fuel tank are provided. In one example, a fuel drain engagement tool includes a housing. An engagement mechanism is coupled with the housing and extending upward therefrom. The engagement mechanism is configured to engage a fuel drain valve and to move between a contracted state and an expanded state. A compression applicator is coupled with the housing and is positioned to engage the engagement mechanism when the compression applicator is compressed to apply a force to the engagement mechanism that causes the engagement mechanism to move from the expanded state to the contracted state.
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公开(公告)号：US09732678B2
公开(公告)日：2017-08-15
申请号：US14602412
申请日：2015-01-22
申请人： The Boeing Company
发明人： William H. McCabe
CPC分类号： F02C9/30 , B64D37/28 , F02C7/222 , F02C7/236 , F02C9/28 , F05D2260/80 , F05D2270/304
摘要： A system and method for supplementing fuel feed pressure and flow within an aircraft fuel system. The fuel system includes boost and override fuel pumps delivering fuel from the tanks to a fuel manifold, and a jettison fuel pump. The method includes the steps of: (a) sensing whether the aircraft engine is operating near maximum power; (b) upon sensing the condition, operating the jettison fuel pump in fluid interconnection with the override fuel pump to deliver fuel to the fuel manifold; and (c) upon sensing the cessation of the condition, deactivating the jettison fuel pump. The system includes a monitoring circuit signaling when the aircraft engine speed is greater than a predetermined threshold, and a fuel system control circuit operating a jettison fuel pump enable circuit portion in response to the signal while omitting other jettisoning operations. The jettison fuel pump consequently functions as an override fuel pump assist.
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5.发明申请公开(公告)号：US20160177838A1
公开(公告)日：2016-06-23
申请号：US14909646
申请日：2014-07-31
申请人： SNECMA
CPC分类号： F02C7/236 , B64D37/16 , B64D37/28 , F02C7/232 , F05D2220/323
摘要： A fuel circuit of an aircraft engine including a fuel tank; an engine fuel system including a low-pressure pump and a high-pressure pump, and a fuel recirculating pipeline connected to the engine fuel system; and a fuel recirculating valve arranged so as to switch between an open position and a closed position according to the pressure differential of the low-pressure pump, the valve being able to obstruct the fuel recirculating pipeline in the closed position, and to bring the fuel recirculating pipeline into communication with the fuel tank in the open position.
摘要翻译： 包括燃料箱的飞机发动机的燃料回路; 包括低压泵和高压泵的发动机燃料系统和连接到发动机燃料系统的燃料再循环管道; 以及燃料循环阀，其布置成根据低压泵的压差在打开位置和关闭位置之间切换，所述阀能够将燃料循环管道阻塞在关闭位置，并且使燃料 再循环管道与处于打开位置的燃料箱连通。
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公开(公告)号：US12006058B2
公开(公告)日：2024-06-11
申请号：US16850361
申请日：2020-04-16
申请人： BOMBARDIER INC.
发明人： Vincenzo Furgiuele
CPC分类号： B64D37/28 , B64D37/00 , B64D37/005 , B64D37/02 , B64D37/32
摘要： A method of and a system for operating a fuel pump management system of an aircraft. The method comprises receiving, from a fuel gauge, an electronic reading of a level of fuel fluid contained in a fuel tank; and analysing the electronic reading of the level of the fuel fluid, the analysing comprising upon determining that the level of fuel fluid is equal or below a predetermined fuel level threshold, causing a fuel pump in communication with the fuel tank to be shut down.
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公开(公告)号：US11635031B2
公开(公告)日：2023-04-25
申请号：US16678905
申请日：2019-11-08
发明人： Charles E. Reuter , Gerald P. Dyer
摘要： Apparatus and associated methods relate to simultaneously pumping and measuring density of an aircraft fuel. The aircraft fuel is pumped by a centrifugal pump having an impeller. A rotational frequency of the impeller is determined while the centrifugal pump is pumping the aircraft fuel. Flow rate of the aircraft fuel through the centrifugal pump is sensed. Pressure of the aircraft fuel is measured at two different points within or across the centrifugal pump or a differential pressure is measured between the two different points while the centrifugal pump is pumping the aircraft fuel. Density of the aircraft fuel is determined based on a head-curve relation characterizing the centrifugal pump. The head-curve relation relates the fuel density to the rotational frequency, the flow rate, and pressures at the two different points or the differential pressure between the two different points.
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公开(公告)号：US20180292953A1
公开(公告)日：2018-10-11
申请号：US15480249
申请日：2017-04-05
申请人： THE BOEING COMPANY
IPC分类号： G06F3/0482 , B64D37/26 , B64D37/28
摘要： A system includes display equipment and a processor coupled to the display equipment. The processor is configured to cause the display equipment to display an electronic checklist associated with an aircraft. The processor is configured determine whether the electronic checklist includes a checklist item associated with a particular control page of a plurality of control pages. The processor is configured to, based on determining that the electronic checklist includes the checklist item associated with the particular control page, cause the display equipment to display the particular control page that includes a control element that is selectable to cause a control command to be sent to one or more components.
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9.发明申请公开(公告)号：US20050113984A1
公开(公告)日：2005-05-26
申请号：US10720605
申请日：2003-11-24
申请人： Kurt Rupe
发明人： Kurt Rupe
摘要： Methods and apparatus for fuel control systems using inertial measurement data are disclosed. In one embodiment, a method for controlling a fuel flow includes comparing an acceleration condition of the aircraft with a predetermined threshold at which normal fuel fluid characteristics begin to become unpredictable, and comparing the acceleration condition with a time-based acceleration profile for a given flight profile. Next, the method determines whether the aircraft is about to enter a prolonged negative acceleration regime. The method further includes maintaining normal fuel control and, after a predetermined amount of time has passed, initiating an alternate fuel source to the engine.
摘要翻译： 公开了使用惯性测量数据的燃料控制系统的方法和装置。 在一个实施例中，一种用于控制燃料流的方法包括将飞行器的加速度条件与正常燃料流体特性开始变得不可预测的预定阈值进行比较，并将加速条件与给定飞行的基于时间的加速度曲线进行比较 个人资料 接下来，该方法确定飞机是否即将进入长时间的负加速度状态。 该方法还包括维持正常燃料控制，并且在预定量的时间过去之后，向发动机启动替代燃料源。
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公开(公告)号：US10677206B2
公开(公告)日：2020-06-09
申请号：US15653936
申请日：2017-07-19
发明人： Jay Wheelwright , Jacob Dobbs , Christian Martin
IPC分类号： B01D36/00 , B60K15/03 , C10G33/06 , F02M37/22 , F02M37/24 , B64D37/28 , B01D61/36 , B01D69/10 , B01D71/02 , B64D37/02
摘要： A combination of a fuel tank assembly and a tool for opening an outlet of the fuel tank assembly. The assembly includes a tank for storing a liquid hydrocarbon; and an operator-openable valve arrangement configured to move between a closed flow condition in which flow through the valve arrangement is prevented and an open flow condition in which liquid is allowed to drain out of the tank. The tool is connectable to the valve arrangement, such that in a connected condition of the tool and the arrangement a liquid flow path exists between the interior and the exterior of the tank. The liquid flow path is at least partly defined by a conduit in the tool. A filter, in the flow path, includes a water-permeable member configured to enable water to pass through the water-permeable member and substantially prevent passage of liquid hydrocarbon.
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