Fire suppression agent composition

    公开(公告)号:US11291876B2

    公开(公告)日:2022-04-05

    申请号:US16413166

    申请日:2019-05-15

    Abstract: Disclosed is a fire suppression agent composition including CF3I and an additional fire suppression agent selected from the group consisting of HFC-23, HFC-125, HFC-227ea, dodecafluoro-2-methylpentan-3-one (Novec 1230), and HCFO-1233zd(E), wherein the fire suppression agent composition passes the FAA aerosol can test.

    FIRE SUPPRESSION AGENT COMPOSITION
    4.
    发明申请

    公开(公告)号:US20200330810A1

    公开(公告)日:2020-10-22

    申请号:US16413166

    申请日:2019-05-15

    Abstract: Disclosed is a fire suppression agent composition including CF3I and an additional fire suppression agent selected from the group consisting of HFC-23, HFC-125, HFC-227ea, Novec 1230, and HCFO-1233zd(E), wherein the fire suppression agent composition passes the FAA aerosol can test.

    FIRE EXTINGUISHING AGENT NOZZLE STRUCTURE
    5.
    发明申请

    公开(公告)号:US20200054907A1

    公开(公告)日:2020-02-20

    申请号:US16103478

    申请日:2018-08-14

    Abstract: An aircraft engine fire extinguishing system includes a supply housing for containing a fire extinguishing agent. Also included is a line for routing the fire extinguishing agent from the supply housing. Further included is a nozzle structure operatively coupled to the line, the nozzle structure having a non-circular opening for expelling the fire extinguishing agent.

    CONTAINER FOR LITHIUM BATTERY
    6.
    发明申请

    公开(公告)号:US20190311594A1

    公开(公告)日:2019-10-10

    申请号:US15949627

    申请日:2018-04-10

    Abstract: A battery container includes a battery housing and an end cap. The battery housing is configured to house a battery. The battery housing comprises an opening configured to receive the battery into the battery housing. The end cap is configured to seal the opening of the battery housing. The end cap comprises two or more discharge holes configured to release expanding gas from the battery housing.

    Fire suppression system
    8.
    发明授权

    公开(公告)号:US09597533B2

    公开(公告)日:2017-03-21

    申请号:US14700422

    申请日:2015-04-30

    CPC classification number: A62C2/06 A62C2/04 A62C3/08 A62C35/68 A62C99/0018

    Abstract: A fire suppression system according to an exemplary aspect of the present disclosure includes, among other things, a high pressure inert gas source configured to provide a first inert gas output and a low pressure inert gas source configured to provide a second inert gas output. A distribution network is connected with the high pressure inert gas source and the low pressure inert gas source to distribute the first inert gas output and the second inert gas output throughout a confined space. A volume reduction system is positioned within the confined space and includes a seal member. The seal member is selectively deployable between a first position and a second position to isolate a first volume of the confined space from a second volume of the confined space and reduce an amount of the first inert gas output and the second inert gas output required to respond to a fire threat within the confined space.

    FIRE EXTINGUISHING AGENT NOZZLE STRUCTURE
    9.
    发明公开

    公开(公告)号:US20240108924A1

    公开(公告)日:2024-04-04

    申请号:US18521976

    申请日:2023-11-28

    CPC classification number: A62C3/08

    Abstract: An aircraft engine fire extinguishing system includes a supply housing for containing a fire extinguishing agent. Also included is a line for routing the fire extinguishing agent from the supply housing. Further included is a nozzle structure operatively coupled to the line, the nozzle structure having a non-circular opening for expelling the fire extinguishing agent.

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