发明名称 IMPLEMENT FOR DRAINING AIRCRAFT FUEL
摘要 <p>PROBLEM TO BE SOLVED: To provide an implement capable of safely and easily draining a fuel remaining in a fuel tank by a simple configuration without damaging the airframe of an aircraft.SOLUTION: A fuel draining implement 20 for draining a fuel from a fuel drain valve provided at the lower face of the airframe of an aircraft is provided with: a funnel part 7 applied to the airframe to cover the fuel drain valve; a drain pipe 6 connected to an opening of the small diameter side of the funnel part 7; and a pressing protrusion 17 which erects inside the funnel part 7, extends in the lengthwise direction of the funnel part 7 and presses the open valve of the fuel drain valve when the funnel part 7 is applied to the airframe. The edge part of an opening of at least a large diameter side in the funnel part 7 is formed of an elastic body.</p>
申请公布号 JP2014184802(A) 申请公布日期 2014.10.02
申请号 JP20130060231 申请日期 2013.03.22
申请人 MITSUBISHI HEAVY IND LTD 发明人 NAKAJIMA HIROSHI
分类号 B64F5/00;B64D37/20 主分类号 B64F5/00
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