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1. 发明授权

US09567093B2 Time domain reflectometry aircraft fuel gauge 有权
标题翻译：时域反射飞机燃油表
公开(公告)号：US09567093B2
公开(公告)日：2017-02-14
申请号：US14442966
申请日：2013-11-06
申请人： AIRBUS OPERATIONS LIMITED
发明人： Richard Haskins , Joseph K-W Lam
IPC分类号： B64D37/02 , B64D37/04 , B64D37/12 , B64D37/00 , G01F23/284 , G01F23/292 , G01F22/00
CPC分类号： B64D37/005 , B64D37/00 , B64D37/04 , G01F22/00 , G01F23/284 , G01F23/292
摘要： An aircraft fuel tank system comprising an aircraft fuel tank and a time domain reflectometry (TDR) fuel gauge for measuring a filling level of fuel in the aircraft fuel tank. The TDR fuel gauge comprises an electromagnetic signal generator and a cable, the cable comprising a first cable part and a second cable part which are coupled in series to the signal generator. The first cable part extends downwardly within the fuel tank and the second cable part extends upwardly within the fuel tank. The first and second cable parts are arranged such that for at least one filling level the first cable part extends down into the fuel from an ullage space at a first location and the second cable part extends up out of the fuel into an ullage space at a second location which is spaced apart from the first location.
摘要翻译：一种飞机燃料箱系统，包括飞机燃料箱和用于测量飞机燃料箱中的燃料的填充水平的时域反射计（TDR）燃料计。 TDR燃料计包括电磁信号发生器和电缆，电缆包括串联耦合到信号发生器的第一电缆部分和第二电缆部分。第一缆索部分在燃料箱内向下延伸，第二缆索部分在燃料箱内向上延伸。第一和第二电缆部件布置成使得对于至少一个填充水平，第一电缆部分从第一位置处的空白空间向下延伸到燃料中，并且第二电缆部分在燃料中向上延伸到空的空间中与第一位置间隔开的第二位置。

2. 发明授权

US09527576B2 Method and assembly for attaching fuel system components to a rib before the assembly is joined to an aircraft wing 有权
标题翻译：在将组件接合到飞行器机翼之前将燃料系统部件附接到肋的方法和组件
公开(公告)号：US09527576B2
公开(公告)日：2016-12-27
申请号：US13961199
申请日：2013-08-07
申请人： AIRBUS OPERATIONS LIMITED
发明人： Richard Haskins
IPC分类号： B64C3/18 , B64C3/34 , B64D37/06
CPC分类号： B64C3/187 , B64C3/34 , B64D37/06 , Y10T29/49826
摘要： A method of installing fuel system components in an aircraft wing in which the fuel system components are attached to ribs before the ribs are assembled into the wing. The ribs are structural ribs for the wing and may be assembled to form a combined rib and fuel system component assembly before the assembly is added to the wing.
摘要翻译：一种在飞行器机翼中安装燃料系统部件的方法，其中燃料系统部件在肋组装到机翼之前附接到肋条。肋是用于机翼的结构肋，并且在将组件添加到翼之前可以组装成形成组合的肋和燃料系统部件组件。

3. 发明授权

US10329026B2 Aircraft fuel system with fuel return from engine 有权
公开(公告)号：US10329026B2
公开(公告)日：2019-06-25
申请号：US14436516
申请日：2013-10-16
申请人： AIRBUS OPERATIONS LIMITED
发明人： Richard Haskins , Franklin Tichborne , Joseph K-W Lam
IPC分类号： B64D37/02 , B64D37/34 , F02M31/16 , F02M37/00 , F02M37/10 , B64D37/32 , F02C7/22
摘要： An aircraft fuel system, comprising: a fuel tank; a fuel line; and an engine; wherein the fuel line includes a first conduit configured to carry fuel from the tank towards the engine, and a second conduit configured to carry fuel from the engine towards the tank, wherein one of the first conduit or the second conduit is disposed annularly around the other of the first conduit or the second conduit. Also, a method of operating the system. The system may be used to suppress ice formation in the first conduit and/or provide leakage detection.

4. 发明授权

US09969501B2 Aircraft fuel tank arrangement 有权
公开(公告)号：US09969501B2
公开(公告)日：2018-05-15
申请号：US14194596
申请日：2014-02-28
申请人： AIRBUS OPERATIONS LIMITED
发明人： Richard Haskins , John Jones
IPC分类号： B64D37/32 , B64D37/04 , B64D45/00
CPC分类号： B64D37/32 , B64D37/04 , B64D45/00
摘要： An aircraft fuel tank arrangement for the relief of a pressure differential between the interior of the aircraft fuel tank and the ambient atmosphere is provided. The aircraft fuel tank arrangement comprises a removable cartridge received within a cartridge-receiving body located at least partially in the fuel tank, said cartridge comprising a first burstable member operable to rupture in the presence of a pressure differential between the interior of the aircraft fuel tank and the ambient atmosphere which is greater than a predetermined pressure differential.

5. 发明授权

US09581252B2 Fluid flow control valve and actuator 有权
标题翻译：流体流量控制阀和执行器
公开(公告)号：US09581252B2
公开(公告)日：2017-02-28
申请号：US14434536
申请日：2013-10-15
申请人： AIRBUS OPERATIONS LIMITED
发明人： Richard Haskins , John Jones
IPC分类号： F16K25/00 , F16K3/312 , F16K43/00 , F16K27/06
CPC分类号： F16K3/312 , F16K27/06 , F16K43/00 , Y10T137/6011
摘要： A fluid flow control valve is housed within a canister (31) which is semi-permanently fixed in the wall (12) of a fuel tank, and has pipe connections (17, 18). The movable valve parts, including a valve sub-assembly (32, 33) and an electrical actuator (34), may be removed without requiring access to the fuel tank.
摘要翻译：流体流量控制阀容纳在半永久地固定在燃料箱的壁（12）内并具有管道连接（17,18）的罐（31）内。包括阀子组件（32,33）和电致动器（34）的可移动阀部件可以被移除而不需要进入燃料箱。

6. 发明授权

US09296485B2 Distributing gas within an aircraft 有权
标题翻译：在飞机内分配气体
公开(公告)号：US09296485B2
公开(公告)日：2016-03-29
申请号：US14297152
申请日：2014-06-05
申请人： AIRBUS OPERATIONS LIMITED
发明人： Richard Haskins , Timothy Leigh
IPC分类号： B64D37/00 , B64D37/04 , B64D37/08 , B64D37/32
CPC分类号： B64D37/005 , B64D37/04 , B64D37/08 , B64D37/32 , Y02T50/44 , Y10T137/0391 , Y10T137/2196
摘要： An aircraft comprising a Rubens' tube for distributing gas within the aircraft. The Rubens' tube comprises a tube with a plurality of outlets; an inlet for feeding the gas into the tube; and a loudspeaker arranged to set up a standing acoustic wave within the tube. Typically the Rubens' tube is arranged to feed inert gas into a fuel tank of the aircraft.
摘要翻译：一种飞机，包括用于在飞机内分配气体的鲁本斯管。鲁本斯管包括具有多个出口的管; 用于将气体供给到管中的入口; 以及布置成在管内设置声波的扬声器。通常，鲁本斯管被布置成将惰性气体进料到飞机的燃料箱中。

7. 发明申请

US20150276071A1 FLUID FLOW CONTROL VALVE AND ACTUATOR 有权
标题翻译：流体控制阀和执行器
公开(公告)号：US20150276071A1
公开(公告)日：2015-10-01
申请号：US14434536
申请日：2013-10-15
申请人： AIRBUS OPERATIONS LIMITED
发明人： Richard Haskins , John Jones
IPC分类号： F16K3/312 , F16K43/00 , F16K27/06
CPC分类号： F16K3/312 , F16K27/06 , F16K43/00 , Y10T137/6011
摘要： A fluid flow control valve is housed within a canister (31) which is semi-permanently fixed in the wall (12) of a fuel tank, and has pipe connections (17, 18). The movable valve parts, including a valve sub-assembly (32, 33) and an electrical actuator (34), may be removed without requiring access to the fuel tank.
摘要翻译：流体流量控制阀容纳在半永久地固定在燃料箱的壁（12）内并具有管道连接（17,18）的罐（31）内。包括阀子组件（32,33）和电致动器（34）的可移动阀部件可以被移除而不需要进入燃料箱。

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