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Title:
FIRE-EXTINGUISHING FACILITY OF AIRCRAFT AND AIRCRAFT
Document Type and Number:
Japanese Patent JP2015134069
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a fire-extinguishing facility of aircraft and an aircraft having a fire-extinguishing facility which can secure a fire-extinguishing function while preventing, even when heavy impact load of explosive blast or the like is applied to a support member of a fire-extinguishing pipe, the fire-extinguishing pipe from being damaged due to excessive stress.SOLUTION: A fire-extinguishing facility 20 of aircraft includes a fire-extinguishing nozzle provided to a liner 14, and a fire-extinguishing pipe 18 which is provided to a fuselage 10 for supporting the liner 14 from back side, and which feeds a fire-extinguishing agent to the fire-extinguishing nozzle. The fuselage 10 includes a stringer 13 and a frame 12. The fire-extinguishing pipe 18 includes: a first pipe 21 supported by the stringer 13; a second pipe 22 supported by the frame 12; and a flexible tube 31 for connecting the first pipe 21 and the second pipe 22.

Inventors:
KONO TAKAFUMI
KOJIMA YUYA
FUSHIYA KOICHIRO
WADA KYOICHI
Application Number:
JP2014006647A
Publication Date:
July 27, 2015
Filing Date:
January 17, 2014
Export Citation:
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Assignee:
MITSUBISHI AIRCRAFT CORP
International Classes:
A62C3/08; B64D25/00
Domestic Patent References:
JPH06170008A1994-06-21
JP2003144568A2003-05-20
JP2011502859A2011-01-27
JP2010538890A2010-12-16
JPH06170008A1994-06-21
JP2003144568A2003-05-20
JP2011502859A2011-01-27
JP2010538890A2010-12-16
JPH045971A1992-01-09
JPH11276624A1999-10-12
JPH045971A1992-01-09
JPH11276624A1999-10-12
Foreign References:
US20120255746A12012-10-11
US20050183869A12005-08-25
US20120255746A12012-10-11
US20050183869A12005-08-25
Attorney, Agent or Firm:
大場 充
堀川 美夕紀
大竹 夕香子