Claims
- 1-49. (Canceled)
- 50. A method for making a flying insect trapping device, said method comprising:
providing a supporting frame; providing a combustion/heat exchanger device comprising a pair of halves each formed from a heat conducting material and each having a partial combustion chamber portion and a partial heat exchanger portion formed integrally together, said partial combustion chamber portions each having a partial combustion chamber formed therein and said partial heat exchanger portions each having a partial heat exchange path formed therein; coupling said pair of halves of said combustion/heat exchanger device together such that (a) said partial combustion chamber portions are coupled to define a combustion portion of said device and said partial combustion chambers are coupled to define a combustion chamber extending through said combustion chamber extending through said combustion chamber portion and (b) said partial heat exchanger portions are coupled to define a heat exchanger portion and said partial heat exchange paths are coupled to define a heat exchange path extending through said heat exchanger portion, said combustion chamber having an inlet port for connection to the fuel supply to enable the fuel to flow into said combustion chamber for continuous combustion to create an exhaust gas that includes carbon dioxide within said combustion chamber, said heat exchange path being communicated to said combustion chamber and having an exhaust port opposite said inlet port to enable the exhaust gas to flow through said heat exchange path to said exhaust port, said heat exchange portion being constructed such that said exhaust gas flowing out from said combustion chamber flows along said heat exchange path to said exhaust port and a temperature of the exhaust gas is reduced as the gas flows along said heat exchange path via conduction through the heat conductive material of said halves of said combustion/heat exchanger device; providing an exhaust outlet on said frame in communication with the exhaust port of said combustion/heat exchanger device, said exhaust outlet being configured to allow said exhaust gas to flow outwardly therefrom so that insects attracted to the carbon dioxide in said exhaust gas will fly towards said exhaust outlet; providing an insect inlet in communication with said insect trap chamber to enable flying insects to enter said trap chamber through said insect inlet; and providing a vacuum device on communication with said insect inlet, said vacuum device being constructed and arranged to draw insects attracted to said exhaust outlet through said insect inlet and into said insect trap chamber.
- 51. A method according to claim 50, further comprising:
prior to coupling said halves together, positioning a catalyst element disposed between said partial combustion chambers such that, when said halves are coupled together as aforesaid, said catalyst element is positioned downstream of a point at which said continuous combustion occurs, said catalyst element being formed from a catalytically active material that, during operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows therethrough and into said heat exchanger path.
- 52. A method according to claim 51, further comprising:
prior to coupling said halves together, positioning turbulence reducing structure between said partial combustion chambers such that, when said halves are coupled together as aforesaid, said turbulence reducing structure is positioned between the point at which said continuous combustion occurs and said inlet port, said turbulence reducing structure having a plurality of apertures oriented in the same general direction as the conduits of said catalyst body, said apertures being configured to straighten the flow of fuel from said inlet port to thereby reduce turbulence in said fuel prior to reaching said combustion point.
- 53. A flying insect trapping device according to claim 52, wherein said catalyst element and said turbulence reducing structure are positioned within a sleeve and said sleeve is positioned between said partial combustion chambers so as to simultaneously position said catalyst element and said turbulence reducing structure between said partial combustion chambers prior to coupling said halves.
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This application claims priority to U.S. Provisional Application Ser. No. 60/326,722 (filed on Oct. 4, 2001), the entire contents of which are herein incorporated by reference.
Provisional Applications (1)
|
Number |
Date |
Country |
|
60326722 |
Oct 2001 |
US |
Divisions (1)
|
Number |
Date |
Country |
Parent |
10264260 |
Oct 2002 |
US |
Child |
10859160 |
Jun 2004 |
US |