Fire extinguishing container

Patent metadata

Field	Value
Publication number	US-10974085-B2
Application number	US-201816038577-A
Country	US
Kind code	B2
Filing date	Jul 18, 2018
Priority date	Jun 17, 2016
Publication date	Apr 13, 2021
Grant date	Apr 13, 2021

Abstract

An enclosure, vehicle, and method for containing an overheating device are provided. An enclosure includes a body and a door that form a volume. The body includes is connected to a Venturi tube that is in communication with a fluid flow path flowing across an opening at an opposite end. In the event an overheating device is placed in the enclosure, a pressure sensor measures a pressure in the volume and a controller opens a first valve in a flow path through the Venturi tube so that air is pumped from the volume via the Venturi effect. The first valve is closed when the measured pressure drops below a threshold pressure. The enclosure can also include an extinguishing agent that can be expelled into the volume if a temperature sensor measures a temperature above a threshold temperature.

First claim

What is claimed is:

1. An enclosure, comprising:
a container having a door and defining a volume therein, the volume fluidly coupled to a fluid flow path through a Venturi tube, the fluid flow path flowing across an opening of a downstream end of the Venturi tube;
a first valve arranged to control fluid flow through the Venturi tube between the volume and the fluid flow path, wherein the first valve is movable between an open state and a closed state;
a temperature sensor arranged in the volume of the container, wherein the temperature sensor is operable to output a temperature signal;
a pressurized extinguishing agent; and
a second valve arranged in a flow path between the pressurized extinguishing agent and the volume in the container, wherein the second valve is changeable from a closed state to an open state; and
a controller having an operable state and an inactive state, the controller transitioning from the inactive state to the operable state upon the door of the container being moved from a closed position to an open position and returned to the closed position, wherein the controller is operable, in an operable state, to:
receive a pressure signal from a pressure sensor indicative of a pressure within the volume; and
output first valve control signals to:
move the first valve to the open state in the event a value of the pressure signal indicates a pressure threshold level within the volume is exceeded, thereby reducing pressure in the volume to a first reduced pressure through a Venturi effect; and
move the first valve to the closed state upon the value of the pressure signal indicating the pressure within the volume is below the pressure threshold level to maintain the pressure within the volume at the first reduced pressure;

receive the temperature signal from the temperature sensor; and
output a second valve control signal to change the second valve from the closed state to the open state upon:
a value of the temperature signal indicating a temperature threshold level is exceeded; and
the volume being maintained at the first reduced pressure.

2. The enclosure of claim 1 , wherein the enclosure further comprises an activation input on an exterior of the container, and wherein the controller transitions from the inactive state to the operable state upon the controller receiving an activation signal from the activation input.

3. The enclosure of claim 1 , wherein the container includes an interior layer, an exterior layer, and an insulating layer arranged between the interior layer and exterior layer.

4. The enclosure of claim 3 , wherein the interior layer and exterior layer each comprise at least one of a steel alloy and a titanium alloy.

5. The enclosure of claim 3 , wherein the insulating layer comprises at least one of: a refractory material and a phase change material.

6. An aircraft, comprising:
a passenger compartment;
a container arranged in the passenger compartment, the container defining a volume therein, the container including a body having a port,
a Venturi tube in communication with the container and comprising a first tube portion attached to the container and a second tube portion attached to a fuselage of an aircraft, wherein a downstream end of the Venturi tube is in communication with a freestream air flow path over an exterior of the fuselage of the aircraft, the downstream end of the Venturi tube flush with the exterior of the fuselage;
a first valve arranged in an air flow path through the port, wherein the first valve is movable between an open state and a closed state; and
a controller operable, in an operable state, to:
receive a pressure signal from a pressure sensor indicative of a pressure within the volume of the container; and
output first valve control signals to:
move the first valve to the open state in the event a value of the pressure signal indicates a pressure threshold level within the volume is exceeded, thereby reducing pressure in the volume to a first reduced pressure through a Venturi effect; and
move the first valve to the closed state upon the value of the pressure signal indicating the pressure within the volume is below the pressure threshold level to maintain the pressure within the volume at the first reduced pressure.

7. The aircraft of claim 6 , further comprising:
a temperature sensor arranged in the volume in the container, wherein the temperature sensor is operable to output a temperature signal;
a pressurized extinguishing agent; and
a second valve arranged in a flow path between the pressurized extinguishing agent and the volume in the container, wherein the second valve is changeable from a closed state to an open state,
wherein the controller is further operable, in the operable state, to:
receive the temperature signal from the temperature sensor; and
output a second valve control signal to change the second valve from the closed state to the open state upon a value of the temperature signal indicating a temperature threshold level is exceeded.

8. The aircraft of claim 7 , wherein the controller outputs the second valve control signal upon the temperature signal indicating a temperature threshold level is exceeded and upon the pressure signal dropping indicating the pressure within the volume of the container is below the pressure threshold level.

9. The aircraft of claim 6 , wherein the controller is further operable to transmit an activation signal to avionics in a flight deck of the aircraft, and wherein the avionics display a notification to a pilot of the aircraft in response to receiving the activation signal.

10. A method for containing an overheating device in a passenger compartment of an aircraft, comprising:
opening a container that includes a body and a door, wherein the body includes a port in communication with an upstream end of a Venturi tube, the Venturi tube comprising a first tube portion attached to the container and a second tube portion attached to a fuselage of the aircraft, and wherein a downstream end of the Venturi tube is in communication with a fluid flow path across an exterior of the fuselage, the downstream end flush with the exterior of the fuselage;
placing the overheating device in a volume in the container;
closing the door such that the door forms an airtight seal with the body;
using a controller in an operable state;
receiving a pressure signal from a pressure sensor indicative of a pressure within the volume of the container;
output first valve signals to open a first valve arranged in an airflow path through the port to decrease pressure in the volume through a Venturi effect in the event a value of the pressure signal indicates a pressure threshold level within the volume is exceeded, the first valve movable between an open state and a closed state;
measuring the pressure of the volume; and
using the controller, closing the first valve upon the measured pressure of the volume decreasing below the pressure threshold level to maintain a decreased pressure within the container while maintaining the overheating device therein.

11. The method of claim 10 , further comprising:
using a temperature sensor, measuring a temperature in the volume; and
using the controller, opening a second valve to enable entry of a pressurized extinguishing agent into the volume upon the measured temperature exceeding a temperature threshold level.

12. The method of claim 11 , wherein opening the second valve using the controller comprises opening a second valve to enable entry of a pressurized extinguishing agent into the volume upon the measured temperature exceeding a temperature threshold level and upon the measured pressure dropping

Assignees

• Boeing Co

Inventors

• Koreis Rocke R
• Scarce Joseph A

Classifications

• A62C3/16 Primary

  in electrical installations, e.g. cableways · CPC title

• B64D37/32

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title

• A62C4/02

  in gas-pipes (safety valves F16K17/00) · CPC title

• A62C3/08 Primary

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

• A62C37/00

  Control of fire-fighting equipment (heat-sensitive devices G01K) · CPC title