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Title:
WATER FLOW-IN PREVENTION DEVICE FUNCTIONING AT LANDING ON WATER OF AIRCRAFT, AIR PRESSURE REGULATION VALVE, AND AIRCRAFT
Document Type and Number:
Japanese Patent JP2016175481
Kind Code:
A
Abstract:
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

Inventors:
KONO SHINGO
UCHINO TAKASHI
HAGINO SHUICHI
URANO AKITAKA
Application Number:
JP2015056007A
Publication Date:
October 06, 2016
Filing Date:
March 19, 2015
Export Citation:
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Assignee:
MITSUBISHI AIRCRAFT CORP
International Classes:
B64D25/00; B64D13/00; F16K17/36; F16K17/40
Domestic Patent References:
JP2014019174A2014-02-03
JPS56113100U1981-09-01
JP2004138177A2004-05-13
JPS5578870U1980-05-30
Foreign References:
US3478761A1969-11-18
Attorney, Agent or Firm:
Mitsuru Oba
Horikawa Miyuki
Yuko Otake