ACTIVE ODORANT WARNING

• US 20120217028A1
• Filed: 02/24/2011
• Published: 08/30/2012
• Est. Priority Date: 02/24/2011
• Status: Abandoned Application

• Current Assignee: Kidde Technologies, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Kidde Technologies, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Chattaway, Adam, Glaser, Robert, Rennie, Paul, Gatsonides, Josephine Gabrielle
• Application Number:
  US13/033,665
• Publication Number:
  US 20120217028A1
• Time in Patent Office: Days
• US Class Current: 169/62
• CPC Class Codes: A62C 3/08 in aircraft A62C3/0207 takes precedence
• CPC Class Codes: A62C 99/0018 using gases or vapours that do not support combustion, e.g. steam, carbon dioxide

Abstract

A fire suppression and warning system for an aircraft includes an inert gas delivery system, an inert gas indicator, an on-ground indicator, and a warning device. The inert gas delivery system delivers an inert gas output to an enclosed space on the aircraft. The inert gas indicator signals that the inert gas delivery system has delivered the inert gas output to the enclosed space. The on-ground indicator signals that the aircraft is located on the ground. The warning device actively warns that the inert gas output is present in the enclosed space in response to a signal from the inert gas indicator and a signal from the on-ground indicator.

Claims

1. A fire suppression and warning system for an aircraft, the system comprising:

an inert gas delivery system for delivering an inert gas output to an enclosed space on the aircraft;

an inert gas indicator for signaling that the inert gas delivery system delivered the inert gas output to the enclosed space;

an on-ground indicator for signaling that the aircraft is located on the ground; and

a warning device for warning that the inert gas output is present in the enclosed space, the warning device being activated in response to a signal from the inert gas indicator and a signal from the on-ground indicator.

2. The system of claim 1, wherein the inert gas indicator monitors activation of the inert gas delivery system, presence of inert gas within a storage container, or concentration of oxygen within the enclosed space.

3. The system of claim 1, wherein the on-ground indicator monitors a door to the enclosed space, activation of a landing gear, presence of weight on wheels, or a change in pressure within the aircraft.

4. The system of claim 1, wherein the warning device produces at least one warning output configured to alert at least one human sensory system.

5. The system of claim 4, wherein the warning device includes at least one of an odorant, digital display, light, and alarm.

6. The system of claim 1, wherein the warning device includes an odorant delivery system comprising:

an odorant storage container for storing odorant;

an odorant activation mechanism for activating the odorant delivery system; and

an odorant discharge agent for discharging odorant from the odorant storage container to the enclosed space.

7. The system of claim 6, wherein the odorant activation mechanism includes a cartridge valve, a solenoid valve, or a flapper valve.

8. The system of claim 6, wherein the odorant discharge agent includes a gas propellant, a solid propellant, or a spring-loaded container.

9. A method for warning of a presence of inert gas in an enclosed space on an aircraft, the method comprising:

detecting the presence of the inert gas;

detecting that the aircraft is located on ground; and

activating a warning that the inert gas is present in the enclosed space when the aircraft is located on ground.

10. The method of claim 9, wherein detecting the presence of inert gas includes monitoring activation of an inert gas delivery system, monitoring presence of inert gas within a storage container, or monitoring presence of oxygen within the enclosed space.

11. The system of claim 9, wherein detecting that the aircraft is located on the ground includes monitoring a door to the enclosed space, monitoring activation of a landing gear, monitoring presence of weight on wheels, or monitoring a change in pressure within the aircraft.

12. The system of claim 9, wherein activating the warning that the inert gas is present in the enclosed space includes releasing an odorant, activating a digital display, turning on a light, or emitting a siren.

13. A fire suppression and warning system for an aircraft, the system comprising:

an enclosed space located on the aircraft;

an inert gas delivery system for delivering inert gas to the enclosed space;

an odorant storage container for storing an odorant; and

an odorant activation mechanism for initiating release of the odorant from the odorant storage container to the enclosed space, the odorant activation mechanism initiating release of the odorant when inert gas is present in the enclosed space and the aircraft is located on ground.

14. The system of claim 13, further comprising:

a distribution network fluidly connecting the inert gas delivery system to the enclosed space.

15. The system of claim 14, wherein the odorant storage container is fluidly connected to the distribution network.

16. The system of claim 13, wherein the odorant activation mechanism includes a cartridge valve, a solenoid valve, or a flapper valve.

17. The system of claim 13, further comprising:

an odorant discharge agent for discharging odorant from the odorant storage container to the enclosed space.

18. The system of claim 17, wherein the odorant discharge agent includes a gas propellant, a solid propellant, or a spring-loaded container.