发明名称 Fire suppression flow control system apparatus and system
摘要 In various embodiments, a fire suppression system includes a high rate discharge system and a low rate discharge system. The low rate discharge system may comprise components that are capable of varying mass flow of a fire suppression agent in term of the ambient conditions of the aircraft structure. In this regard, the low rate discharge system may comprise a valve that is configured to sense at least one of the ambient pressure and ambient temperature of an aircraft structure.
申请公布号 US9440103(B2) 申请公布日期 2016.09.13
申请号 US201414254646 申请日期 2014.04.16
申请人 KIDDE TECHNOLOGIES, INC. 发明人 Hagge Harlan
分类号 A62C3/00;A62C3/08;A62C35/68;A62C37/44;A62C99/00;A62C37/10 主分类号 A62C3/00
代理机构 代理人
主权项 1. A fire suppression system, comprising: a high rate discharge system configured to discharge a first portion of fire suppression agent to an aircraft structure; and a low rate discharge system configured to discharge a second portion of fire suppression agent to the aircraft structure and having: a valve configured to sense an ambient pressure of the aircraft structure and having: a poppet seat,a poppet configured to be actuated at least one of towards or away from the poppet seat to vary an amount of a mass flow of fire suppression agent that flows through the valve, anda bellows coupled to the poppet and having a first surface configured to be subjected to the ambient pressure of the aircraft structure and a second surface configured to be subjected to a fire suppression agent pressure of the second portion of fire suppression agent such that the bellows expands or compresses in response to a change of the ambient pressure of the aircraft structure, the expansion or compression actuating the poppet at least one of towards or away from the poppet seat to adjust the amount of the mass flow of fire suppression agent that flows through the valve, andan orifice configured to receive the mass flow of fire suppression agent via the valve.
地址 Wilson NC US