发明名称 Aircraft refuelling system
摘要 <p>An aircraft refuelling system of an aircraft is provided. The refuelling system comprises a refuelling connector (34) mounted as part of the aircraft and configured to detachably connect to the fuel outlet (2) of a fuel supply apparatus separate from the aircraft, and a fuel pressure regulator (36) having an inlet in communication with a fuel inlet (35) of the refuelling connector (34) and having an outlet in communication with refuelling pipework (39) of the aircraft. The fuel pressure regulator (36), regulates the pressure of fuel in the refuelling pipework (39) when fuel is being passed into the refuelling pipework (39) from the fuel inlet (35) of the refuelling connector. A fuel pressure regulator apparatus for mounting in an aircraft, comprising a connector forming a fuel inlet to the fuel pressure regulator apparatus, configured to detachably connect to the fuel outlet of a fuel supply system, a fuel outlet for connection to the refuelling pipework of an aircraft and a fuel pressure regulator for regulating the pressure of fuel passing through the fuel outlet is also provided.</p>
申请公布号 GB0606200(D0) 申请公布日期 2006.05.10
申请号 GB20060006200 申请日期 2006.03.28
申请人 AIRBUS UK LIMITED 发明人
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代理机构 代理人
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