Fire suppression flow control system apparatus and system

Patent metadata

Field	Value
Publication number	US-9694221-B2
Application number	US-201615234369-A
Country	US
Kind code	B2
Filing date	Aug 11, 2016
Priority date	Apr 16, 2014
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

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.

First claim

What is claimed is:

1. A low rate discharge (“LRD”) system, comprising:
a bottle configured to hold a pressurized fire suppression agent;
a poppet valve in fluid communication with the bottle and configured to regulate a flow of fire suppression agent from the bottle in response to the LRD system being activated, the poppet valve configured to regulate the flow of fire suppression agent as a function of ambient temperature and ambient pressure and including:
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 mass flow of fire suppression agent that flows through the poppet valve, and
a bellows coupled to the poppet and having a first surface configured to be exposed to an ambient pressure and a second surface configured to be exposed to a fire suppression agent pressure such that the bellows expands or compresses in response to a change of the ambient pressure, the expansion or compression actuating the poppet at least one of towards or away from the poppet seat to adjust the amount of the flow of fire suppression agent.

2. The LRD system of claim 1 , wherein the ambient temperature and ambient pressure are associated with an aircraft structure.

3. The LRD system of claim 1 , wherein the flow of fire suppression agent is passed through and further regulated by an orifice.

4. The LRD system of claim 1 , wherein the bellows is in fluid communication with the fire suppression agent in the bottle.

5. The LRD system of claim 1 , further comprising a controller configured to monitor the poppet valve.

6. The LRD system of claim 1 , wherein the flow of the fire suppression agent is also a function of the specific volume of the fire suppression agent.

Assignees

• Kidde Tech Inc

Inventors

• Hagge Harlan

Classifications

• A62C37/44

  only the sensor being in the danger zone · CPC title

• A62C35/68

  Details, e.g. of pipes or valve systems (valves in general F16K) · CPC title

• A62C99/0018

  using gases or vapours that do not support combustion, e.g. steam, carbon dioxide · CPC title

• A62C37/10

  Releasing means, e.g. electrically released · CPC title

• A62C3/08 Primary

  in aircraft {(A62C3/0207 takes precedence)} · CPC title