发明名称 |
WATER FLOW-IN PREVENTION DEVICE FUNCTIONING AT LANDING ON WATER OF AIRCRAFT, AIR PRESSURE REGULATION VALVE, AND AIRCRAFT |
摘要 |
PROBLEM TO BE SOLVED: To provide a water flow-in prevention device which can more sufficiently prevent flowing of water into an aircraft at emergency landing on water, and which actuates more stably.SOLUTION: A device 10 for preventing flowing of water into an aircraft via an air pressure control valve 1 when an aircraft 100 including the air pressure control valve 1 for regulating an air pressure inside the aircraft lands on water, includes a lid 11 for communicating with the inside and outside of the aircraft and for blocking a flow passage (duct 2) in which a valve body 3 of the air pressure control valve 1 is located from outside of the aircraft when landing on water. The lid 11 is supported at an end part 2B on the outside of the aircraft of the duct 2 via a connection part 12 which deforms at landing on water. The connection part 12 deforms in the direction for closing the lid 11 by a force of water flowing into the duct 2 from the periphery of the duct 2 at landing on water, acting on the lid 11.SELECTED DRAWING: Figure 1 |
申请公布号 |
JP2016175481(A) |
申请公布日期 |
2016.10.06 |
申请号 |
JP20150056007 |
申请日期 |
2015.03.19 |
申请人 |
MITSUBISHI AIRCRAFT CORP |
发明人 |
KONO SHINGO;UCHINO TAKASHI;HAGINO SHUICHI;URANO AKITAKA |
分类号 |
B64D25/00;B64D13/00;F16K17/36;F16K17/40 |
主分类号 |
B64D25/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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