IP Library Granted Patent US 9,751,633
Granted Patent B2
US 9,751,633 · App. 14/613,575 · Granted Sep 5, 2017

Aircraft safety device

Inventors: Yuta Takahashi (Tokyo, JP); Tsuyoshi Kitamura (Tokyo, JP); Tsutomu Kawamizu (Tokyo, JP); Shingo Kawano (Tokyo, JP); Ushio Komoda (Aichi, JP)
Assignee: MITSUBISHI AIRCRAFT CORPORATION
B64D37/32
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Quick Facts
Patent No.
US 9,751,633
App. No.
14/613,575
Granted
Sep 5, 2017
Kind
B2
Abstract

The present invention provides an aircraft safety device which can reliably prevent explosion of a fuel tank even if an inflammable gas is ignited. A safety device for explosion-proofing a fuel tank which stores fuel of an aircraft includes: a flame propagation blocking part which blocks propagation of a flame from the outside to the inside of the fuel tank through a ventilation passage which allows ventilation between the inside and the outside of the fuel tank; and a gas supply suppressing part which, when heated by the heat of the flame, suppresses supply of an inflammable gas containing the fuel gas to the flame through the ventilation passage.

Claims (14)

1. An aircraft safety device for explosion-proofing a fuel tank which stores fuel of an aircraft, the fuel tank comprising a ventilation passage that permits ventilation between an inside of the fuel tank and an outside of the fuel tank, the aircraft safety device comprising:

a flame propagation blocking part which blocks propagation of a flame from the outside of the fuel tank to the inside of the fuel tank through the ventilation passage; and

a gas supply suppressing part which, suppresses a supply of an inflammable gas containing gas of the fuel to the flame through the ventilation passage when the gas supply suppressing part is heated by the flame,

wherein the gas supply suppressing part comprises:

a support which constitutes part of the ventilation passage; and

a thermal expansion part which is provided on the inner periphery of the support and is configured to expand when heated by the flame.

2. The aircraft safety device according to claim 1 , wherein the gas supply suppressing part is positioned closer to the outside of the fuel tank than the flame propagation blocking part.

3. The aircraft safety device according to claim 1 , wherein the aircraft safety device is provided in the ventilation passage.

4. The aircraft safety device according to claim 1 , wherein the flame propagation blocking part is incorporated in the ventilation passage.

5. An aircraft safety device for explosion-proofing a fuel tank which stores fuel of an aircraft, comprising:

a flame propagation blocking part which blocks propagation of a flame from the outside to the inside of the fuel tank through a ventilation passage which allows ventilation between the inside and the outside of the fuel tank; and

a gas supply suppressing part which, when heated by the heat of the flame, suppresses supply of an inflammable gas containing gas of the fuel to the flame through the ventilation passage,

wherein the gas supply suppressing part comprises:

a support which constitutes part of the ventilation passage, and a thermal expansion part which is provided on the inner periphery of the support and expands when heated by the flame.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 4, 2015
From: TAKAHASHI, YUTA; KITAMURA, TSUYOSHI; KAWAMIZU, TSUTOMU; KAWANO, SHINGO; KOMODA, USHIO
To: MITSUBISHI AIRCRAFT CORPORATION
Reel/Frame 034889/0324 →
Priority Claims (1)
JP 2014-29317 · Feb 19, 2014 · national
Continuity (1)
Related Publication 20150232193A1 · Aug 20, 2015