| 发明名称 |
FIRE EXTINGUISHING SYSTEM OF AIRCRAFT, AND AIRCRAFT |
| 摘要 |
A fire extinguishing system of an aircraft including a nozzle device that is provided on an installation member forming a compartment of the aircraft, wherein the nozzle device includes: a nozzle that is passed into an insertion hole formed in a nozzle installation section provided on the installation member, and discharges a fire extinguishing agent supplied from a supply source into the aircraft compartment; and a lid member that closes a gap between the nozzle and the nozzle installation section. |
| 申请公布号 |
US2015202477(A1) |
申请公布日期 |
2015.07.23 |
| 申请号 |
US201414583945 |
申请日期 |
2014.12.29 |
| 申请人 |
MITSUBISHI AIRCRAFT CORPORATION |
发明人 |
KONO Takafumi;SHIMAOKA Takashi;EHARA Mitsunori;FUSHIYA Koichiro |
| 分类号 |
A62C3/08;A62C35/68;A62C3/00 |
主分类号 |
A62C3/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fire extinguishing system of an aircraft comprising a nozzle device that is provided on an installation member forming a compartment of the aircraft,
wherein the nozzle device includes: a nozzle that is passed into an insertion hole formed in a nozzle installation section provided on the installation member, and discharges a fire extinguishing agent supplied from a supply source into the compartment; and a lid member that closes a gap between the nozzle and the nozzle installation section. |
| 地址 |
Aichi JP |
