Dual band infra red optical fire detector

Patent metadata

Field	Value
Publication number	US-12437623-B2
Application number	US-202318157924-A
Country	US
Kind code	B2
Filing date	Jan 23, 2023
Priority date	Jan 23, 2023
Publication date	Oct 7, 2025
Grant date	Oct 7, 2025

Abstract

A flame detector for an aircraft includes a housing and two sensors positioned in the housing to detect light signals indicative of a flame event. The two sensors include a first sensor configured to detect light signals in at a first infrared wavelength range, and a second sensor configured to detect light signals at a second wavelength range. A controller is configured to receive signals from the two sensors, and to determine the presence of the flame event only if the signals indicative of the flame event are received from both of the two sensors. A method of detecting a flame event includes providing two sensors in a detector housing. A detection area is observed via the sensors, and detection signals received from the sensors are evaluated at a controller. The presence of a flame event is determined only if detection signals are received from both of the two sensors.

First claim

What is claimed is:

1. A flame detector for an aircraft, comprising:
a housing;
two sensors disposed in the housing to detect light signals indicative of a flame event, the two sensors including:
a first sensor configured to detect light signals at a first infrared wavelength range; and
a second sensor configured to detect light signals at a second wavelength range;
a controller to receive signals from the two sensors, and to determine the presence of the flame event only if the signals indicative of the flame event are received from both of the two sensors; and
a light source disposed in the housing to emit light signals for test of the flame detector, wherein the light source is a light emitting diode configured to emit light signals only detectable by one of the two sensors.

2. The flame detector of claim 1 , wherein the two sensors detect emissions having different wavelength signatures.

3. The flame detector of claim 1 , wherein a first sensor of the two infrared sensors is configured to detect infrared emissions having a 4.3-4.4 micron signature.

4. The flame detector of claim 3 , wherein a second sensor of the two sensors is configured to detect emissions having a 0.88 micron signature.

5. The flame detector of claim 1 , wherein the two sensors share a common window in the housing.

6. The flame detector of claim 1 , wherein the controller is disposed in the housing.

7. A flame detector system of an aircraft, comprising:
an engine disposed in an engine compartment; and
a flame detector disposed in the engine compartment, the flame detector including:
a housing;
two sensors disposed in the housing to detect light signals indicative of a flame event, the two sensors including:
a first sensor configured to detect light signals at a first infrared wavelength range; and
a second sensor configured to detect light signals at a second wavelength range;

a controller to receive signals from the two sensors, and to determine the presence of the flame event only if signals indicative of the flame event are received from both of the two sensors; and
a light source disposed in the housing to emit light signals for test of the flame detector, wherein the light source is a light emitting diode configured to emit light signals only detectable by one of the two sensors.

8. The flame detector system of claim 7 , wherein the two sensors detect emissions having different wavelength signatures.

9. The flame detector system of claim 7 , wherein a first sensor of the two sensors is configured to detect infrared emissions having a 4.3-4.4 micron signature.

10. The flame detector system of claim 9 , wherein a second sensor of the two sensors is configured to detect emissions having a 0.88 micron signature.

11. The flame detector system of claim 7 , wherein the two sensors share a common window in the housing.

12. The flame detector system of claim 7 , wherein the controller is disposed in the housing.

13. A method of detecting a flame event, comprising:
providing two sensors in a detector housing, the two sensors including:
a first sensor configured to detect light signals at a first infrared wavelength range; and
a second sensor configured to detect light signals at a second wavelength range;
observing a detection area via the two sensors;
evaluating detection signals received from the two sensors at a controller;
determining the presence of a flame event only if detection signals are received from both of the two sensors; and

testing the flame detector via a light source disposed in the housing, wherein the light source is a light emitting diode configured to emit light signals only detectable by one of the two sensors.

14. The method of claim 13 , further comprising initiating one or more alarms or alerts when the presence of a flame event is determined.

15. The method of claim 13 , wherein the two sensors detect emissions having different wavelength signatures.

16. The method of claim 13 , wherein a first sensor of the two sensors is configured to detect infrared emissions having a 4.3-4.4 micron signature.

17. The method of claim 16 , wherein a second sensor of the two sensors is configured to detect emissions having a 0.88 micron signature.

Assignees

• Kidde Tech Inc

Inventors

• Newlin Scott K
• Kramer Donald G
• Cherian Judy
• Codispoti Benjamin

Classifications

• A62C3/08

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

• G08B29/145

  of fire detection circuits · CPC title

• G01J5/0018

  Flames, plasma or welding · CPC title

• B64D2045/009

  Fire detection or protection; Erosion protection, e.g. from airborne particles · CPC title

• G01J5/0014

  for sensing the radiation from gases, flames · CPC title