Method and apparatus for optically detecting and locating a fire in an enclosed space

• US 20040213320A1
• Filed: 04/22/2004
• Published: 10/28/2004
• Est. Priority Date: 04/26/2003
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Deutschland GmbH (Airbus SE)
• Inventors: Bobenhausen, Axel
• Granted Patent: US 7,118,272 B2
• Time in Patent Office: Days
• US Class Current: 374/55
• CPC Class Codes: A62C 2/065 having as the main closure device materials, whose characteristics undergo an irreversible change under high temperatures, e.g. intumescent
• CPC Class Codes: A62C 3/08 in aircraft A62C3/0207 takes precedence
• CPC Class Codes: A62C 37/36 an actuating signal being generated by a sensor separate from an outlet device
• CPC Class Codes: B64D 25/00 Emergency apparatus or devices, not otherwise provided for parachutes B64D17/00, B64D19/00; jettisoning of fuel tanks or fuel per se B64D37/00; specially adapted for protection against criminal attack, e.g. anti-hijacking systems B64D45/0015 ; safety belts or body harnesses in general A62B35/00; safety belts or body harnesses for land vehicles B60R22/00; jettisonable parts of fuselage facilitating emergency escape B64C
• CPC Class Codes: G08B 17/125 by using a video camera to detect fire or smoke

Abstract

Thermally reactive elements of an intumescent material that expands when heated above a trigger temperature are arranged in an enclosed space, e.g a freight compartment of an aircraft. An optical sensor in the enclosed space has a field of view encompassing the elements. An evolving fire heats one of the elements above the trigger temperature so the intumescent material expands. This expansion of the element is sensed by the optical sensor, for an early detection of the fire at temperatures substantially below 300° C. With the elements arranged in a predefined pattern, the location of the fire can be determined based on the element(s) that has/have expanded. The intumescent material may be an adhesive tape adhered onto the ceiling of the freight compartment. Light sources or optical targets arranged along lines of sight behind the elements enhance the unambiguous recognition of the thermally expanded condition of a respective element.

Claims

1. An apparatus for detecting a fire in an enclosed space, comprising:

at least one thermally reactive element respectively arranged in said enclosed space and comprising a thermally intumescent material that undergoes an expansion in volume when heated above a trigger temperature; and

an optical sensor arrangement arranged in said enclosed space and having an optical field of view encompassing said at least one thermally reactive element within said enclosed space, such that said expansion of said thermally intumescent material when said material is heated above said trigger temperature can be optically sensed by said optical sensor arrangement.

2. The apparatus according to claim 1, wherein said optical sensor arrangement comprises a visual light video camera that provides a video signal of a visual light image of a scene including said at least one thermally reactive element sensed by said video camera in said field of view within said enclosed space.

3. The apparatus according to claim 1, wherein said optical sensor arrangement comprises an infrared camera that provides an image signal of an infrared light image of a scene including said at least one thermally reactive element sensed by said infrared camera in said field of view within said enclosed space.

4. The apparatus according to claim 1, wherein said optical sensor arrangement includes a light sensor that has said field of view encompassing only a single said thermally reactive element and that is adapted to provide an analog or digital output signal indicating merely whether or not said thermally intumescent material has undergone said expansion.

5. The apparatus according to claim 1, further comprising a light source arranged in said enclosed space within said field of view, with one said thermally reactive element located along a line of sight between said optical sensor arrangement and said light source such that said optical sensor arrangement senses said light source along said line of sight when said thermally intumescent material has not undergone said expansion and such that said light source is blocked behind said thermally reactive element and thus not sensed by said optical sensor arrangement along said line of sight when said thermally intumescent material has undergone said expansion.

6. The apparatus according to claim 1, further comprising a optically discernible target arranged in said enclosed space within said field of view, with one said thermally reactive element located along a line of sight between said optical sensor arrangement and said optically discernible target such that said optical sensor arrangement senses said optically discernible target along said line of sight when said thermally intumescent material has not undergone said expansion and such that said optically discernible target is blocked behind said thermally reactive element and thus not sensed by said optical sensor arrangement along said line of sight when said thermally intumescent material has undergone said expansion.

7. The apparatus according to claim 1, wherein said at least one thermally reactive element is arranged on a ceiling of said enclosed space.

8. The apparatus according to claim 1, wherein said at least one thermally reactive element comprises a plurality of said thermally reactive elements arranged in a dispersed pattern in said enclosed space with each respective element among said thermally reactive elements located at a respective unique distance and respective unique angular position relative to a vertex of said field of view of said optical sensor arrangement so that each said element unambiguously links said respective unique angular position thereof to said respective unique distance thereof in said field of view.

9. The apparatus according to claim 1, wherein said trigger temperature of said thermally intumescent material is below 300°

C.

10. The apparatus according to claim 1, wherein said trigger temperature of said thermally intumescent material is about 160°

C.

11. The apparatus according to claim 1, wherein said intumescent material has a property of foaming-up to cause said expansion in volume when heated above said trigger temperature.

12. The apparatus according to claim 1, wherein said thermally reactive element is a strip of an adhesive tape comprising said thermally intumescent material.

13. In an aircraft having a cargo or freight compartment with cargo load units selected from the group consisting of containers and pallets arranged therein,

an improvement comprising an apparatus for detecting a fire in said cargo or freight compartment, wherein said apparatus comprises:

plural thermally reactive elements arranged in a prescribed pattern above said cargo load units in said cargo or freight compartment, wherein each one of said thermally reactive elements comprises a thermally intumescent material that undergoes an expansion in volume when heated above a trigger temperature; and

at least one camera selected from the group consisting of visual light video cameras and infrared cameras arranged in said cargo or freight compartment and having a field of view directed to encompass said thermally reactive elements such that said expansion of said thermally intumescent material of at least one of said thermally reactive elements when said material is heated above said trigger temperature is optically sensed by said at least one camera and is represented in an image signal output by said at least one camera.

14. The apparatus in the aircraft according to claim 13, wherein said thermally reactive elements are respectively affixed on a ceiling of said cargo or freight compartment at respective locations respectively above said cargo load units, and said at least one camera is oriented with said field of view extending parallel to and along said ceiling in a space above said cargo load units and below said ceiling.

15. A method of detecting a fire in an enclosed space in an aircraft, comprising the steps:

a) arranging in said enclosed space at least one thermally reactive element comprising a thermally intumescent material that is adapted to expand in volume when heated above a trigger temperature;

b) upon the occurrence of a fire, heating said thermally intumescent material above said trigger temperature with heat from said fire, thereby expanding said thermally intumescent material;

c) optically monitoring said at least one thermally reactive element in said enclosed space using an optical monitoring system, and thereby optically sensing said expanding of said thermally intumescent material; and

d) in response to said sensing of said expanding of said thermally intumescent material, concluding that said fire exists in said enclosed space.

16. The method according to claim 15, wherein said step a) comprises arranging a plurality of said thermally reactive elements in said enclosed space, and further comprising a step of determining a location of said fire in said enclosed space in response to and dependent on which one or ones of said thermally reactive elements is or are optically sensed as having undergone said expanding.

17. The method according to clam 15, further comprising arranging a light source or an optical target behind a respective one said thermally reactive element along a line of sight of said optical monitoring system, wherein said step c) comprises sensing a change in a sensed image of said light source or said optical target along said line of sight before and after said expanding of said thermally intumescent material of said respective thermally reactive element.