Granted Patent B2

US 6,840,005 · App. 10/264,260 · Granted Jan 11, 2005

Abstract

Claims (149)

1. A flying insect trapping device configured to be used with a fuel supply containing combustible fuel, comprising:

a supporting frame;

an insect trap chamber carried on said supporting frame;

a combustion device carried on said supporting frame, said combustion device comprising an inlet port for connection with the fuel supply, an exhaust port, and a combustion chamber communicating said inlet port with said exhaust port, said inlet port enabling the fuel from the fuel supply to flow into said combustion chamber for continuous combustion therein to create an exhaust gas within said combustion chamber;

said combustion device further comprising a catalyst element disposed within said combustion chamber, said catalyst element having a catalyst body having a predetermined configuration with a plurality of essentially linear elongated conduits extending between upstream and downstream end portions of the body, the elongated conduits enabling the exhaust gas created in said combustion chamber to flow therethrough from the upstream end portion to the downstream end portion towards said exhaust port, said catalyst body including a catalytically active material that, during operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows through said elongated conduits;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion device and being configured to allow said exhaust gas to flow outwardly through said exhaust outlet so that insects attracted to the carbon dioxide in said exhaust gas will fly towards said exhaust outlet;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through said insect inlet; and

a vacuum device communicated to 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.

2. A flying insect trapping device according to claim 1 , wherein said combustion device further comprises turbulence reducing structure disposed within said combustion chamber upstream of laid catalyst element, 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 on said fuel.

3. A flying insect trapping device according to claim 2 , wherein said turbulence reducing structure comprises a catalytically inactive body and wherein said apertures comprise a plurality of essentially linear elongated conduits formed therethrough for straightening the flow of said fuel from said inlet port.

4. A flying insect trapping device according to claim 3 , wherein said turbulence reducing structure further comprises a relatively thin diffuser positioned within said combustion chamber between said inlet port and said catalytically inactive body, said apertures further comprising a plurality of holes formed through said diffuser, said holes being configured to initially straighten the flow of said fuel from said inlet port.

5. A flying insect trapping device according to claim 4 , wherein said diffuser has annular flanges adjacent each aperture and extending towards said catalytically inactive body.

6. A flying insect trapping device according to claim 3 , wherein said catalytically inactive body is a ceramic monolith.

7. A flying insect trapping device according to claim 1 , wherein said catalytically active material is provided by platinum coated on said catalyst body.

8. A flying insect trapping device according to claim 2 , further comprising a sleeve, said catalyst element and said turbulence reducing structure being received in said sleeve.

9. A flying insect trapping device according to claim 8 , wherein said sleeve is lined internally with insulating material.

10. A flying insect trapping device according to claim 9 , wherein said sleeve is metal.

11. A flying insect trapping device according to claim 4 , further comprising a sleeve, said catalyst element, said catalytically inactive body and said relatively thin diffuser plate being received in said sleeve.

12. A flying insect trapping device according to claim 11 , wherein said sleeve is lined internally with insulating material.

13. A flying insect trapping device according to claim 12 , wherein said sleeve is metal.

14. A flying insect trapping device according to claim 1 , further comprising a heat exchanger for reducing a temperature of said exhaust gas to approximately ambient temperature prior to reaching said exhaust outlet.

15. A flying insect trapping device according to claim 1 , wherein said vacuum device is a single fan.

16. A flying insect trapping system, comprising:

a fuel supply containing combustible fuel;

a supporting frame;

an insect trap chamber carried on said supporting frame;

a combustion device carried on said supporting frame, said combustion device comprising an inlet port for connection with the fuel supply, an exhaust port, and a combustion chamber communicating said inlet port with said exhaust port, said inlet port enabling the fuel from the fuel supply to flow into said combustion chamber for continuous combustion therein to create an exhaust gas within said combustion chamber;

said combustion device further comprising a catalyst element disposed within said combustion chamber, said catalyst element having a catalyst body having a predetermined configuration with a plurality of fixed essentially linear elongated conduits extending between upstream and downstream end portions of the body, the elongated conduits enabling the exhaust gas created in said combustion chamber to flow therethrough from the upstream end portion to the downstream end portion towards said exhaust port, said catalyst body including a catalytically active material that, during operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows through said elongated conduits;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion device and being configured to allow said exhaust gas to flow outwardly through said exhaust outlet so that insects attracted to the carbon dioxide in said exhaust gas will fly towards said exhaust outlet;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through paid insect inlet; and

a vacuum device communicated to 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.

17. A flying insect trapping system according to claim 16 , wherein said combustion device further comprises turbulence reducing structure disposed within said combustion chamber upstream of said catalyst element, 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.

18. A flying insect trapping system according to claim 17 , wherein said turbulence reducing structure comprises a catalytically inactive body and wherein said apertures comprise a plurality of generally linear elongated conduits formed therethrough for straightening the flow of said fuel from said inlet port.

19. A flying insect trapping system according to claim 18 , wherein said turbulence reducing structure further comprises a relatively thin diffuser positioned within said combustion chamber between said inlet port and said catalytically inactive body, said apertures further comprising a plurality of holes formed through said diffuser, said holes being configured to initially straighten the flow of said fuel from said inlet port.

20. A flying insect trapping system according to claim 19 , wherein said diffuser has annular flanges adjacent each aperture and extending towards said catalytically inactive body.

21. A flying insect trapping system according to claim 19 , wherein said catalytically inactive body is a ceramic monolith.

22. A flying insect trapping system according to claim 16 , wherein said catalytically active body is platinum-coated.

23. A flying insect trapping system according to claim 17 , further comprising a sleeve, said catalyst element and said turbulence reducing structure being received in said sleeve.

24. A flying insect trapping system according to claim 23 , wherein said sleeve is lined internally with insulating material.

25. A flying insect trapping system according to claim 24 , wherein said sleeve is metal.

26. A flying insect trapping system according to claim 19 , further comprising a sleeve, said catalyst element, said catalytically inactive body and said relatively thin diffuser plate being received said sleeve.

27. A flying insect trapping system according to claim 26 , wherein said sleeve is lined internally with insulating material.

28. A flying insect trapping system according to claim 27 , wherein said sleeve is metal.

29. A flying insect trapping system according to claim 16 , further comprising a heat exchanger for reducing a temperature of said exhaust gas to approximately ambient temperature prior to reaching said exhaust outlet.

30. A flying insect trapping system according to claim 16 , wherein said combustible fuel is propane.

31. A flying insect trapping system according to claim 16 , wherein said vacuum device is a single fan.

32. A flying insect trapping device configured to be used with a fuel supply containing combustible fuel, comprising:

a supporting frame;

an insect trap chamber carried on said supporting frame;

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;

said pair of halves of said combustion/heat exchanger device being coupled together such that (a) said partial combustion chamber portions are coupled to define a combustion chamber portion of said device and said partial combustion chambers are coupled to define a 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 onto 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; and

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;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion/heat exchanger device and 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;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through said insect inlet; and

a vacuum device communicated to 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.

33. A flying insect trapping device according to claim 32 , wherein said combustion/heat exchanger device further comprises a catalyst element disposed within said combustion chamber, 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 exchange path.

34. A flying insect trapping device according to claim 32 , wherein said heat exchanger portion has a plurality of opening communicating said vacuum device to said insect inlet to enable said vacuum device to draw air through said openings to cool said heat exchanger portion.

35. A flying insect trapping device according to claim 34 , wherein said heat exchanger portion has a plurality of fins spaced apart by said openings, said fins being positioned adjacent to said heat exchange path to conduct heat away from said exhaust gas for transfer to the air drawn through said openings.

36. A flying insect trapping device according to claim 35 , wherein said combustion chamber is communicated to the air being drawn by said fan from said insect inlet for providing air to be mixed with the fuel supplied to said combustion chamber.

37. A flying insect trapping device according to claim 32 , wherein said heat conductive material is metal.

38. A flying insect trapping device according to claim 37 , wherein said metal is steel.

39. A flying insect trapping device according to claim 32 , wherein said vacuum device is a single fan.

40. A flying insect trapping device according to claim 32 , wherein said heat exchanger portion and said heat exchange path thereof are configured to reduce the temperature of said exhaust gas to approximately ambient temperature.

41. A flying insect trapping system, comprising:

a fuel supply containing combustible fuel;

a supporting frame;

an insect trap chamber carried on said supporting frame;

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;

said pair of halves of said combustion/heat exchanger device being coupled together such that (a) said partial combustion chamber portions are coupled to define a combustion chamber portion of said device and said partial combustion chambers are coupled to define a 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; and

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;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion/heat exchanger device and 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;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through skid insect inlet; and

a vacuum device communicated to 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.

42. A flying insect trapping system according to claim 41 , wherein said combustion/heat exchanger device further comprises a catalyst element disposed within said combustion chamber, 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 exchange path.

43. A flying insect trapping system according to claim 41 , wherein said heat exchanger portion has a plurality of opening communicating said vacuum device to said insect inlet to enable said vacuum device to draw air through said openings to cool said heat exchanger portion.

44. A flying insect trapping system according to claim 43 , wherein said heat exchanger portion has plurality of fins spaced apart by said openings, said fins being positioned adjacent to said heat exchange path to conduct heat away from said exhaust gas for transfer to the air drawn through said openings.

45. A flying insect trapping system according to claim 44 , wherein said combustion chamber is communicated to the air being drawn by said fan from said insect inlet for providing air to be mixed with the fuel supplied to said combustion chamber.

46. A flying insect trapping system according to claim 41 , wherein said heat conductive material is metal.

47. A flying insect trapping system according to claim 46 , wherein said metal is steel.

48. A flying insect trapping system according to claim 41 , wherein said vacuum device is a single fan.

49. A flying insect trapping system according to claim 41 , wherein said heat exchanger portion and said heat exchange path thereof are configured to reduce the temperature of said exhaust gas to approximately ambient temperature.

50. A flying insect trapping device configured to be used with a fuel supply containing combustible fuel, comprising:

a supporting frame;

an insect trap chamber carried on said supporting frame;

a combustion device carried on said supporting frame, said combustion device comprising an inlet port for connection with the fuel supply, an exhaust port, and a combustion chamber communicating said inlet port with said exhaust port, said inlet port enabling the fuel from the fuel supply to flow into said combustion chamber for continuous combustion therein to create an exhaust gas within said combustion chamber;

said combustion device further comprising a catalyst element disposed within said combustion chamber, said catalyst element having a catalyst body with a plurality of essentially linear elongated conduits for enabling the exhaust gas created in said combustion chamber to flow therethrough towards said exhaust port, said catalyst body including a catalytically active material that, during operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows through said elongated conduits;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion device and being configured to allow said exhaust gas to flow outwardly through said exhaust outlet so that insects attracted to the carbon dioxide in said exhaust gas will fly towards said exhaust outlet;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through said insect inlet; and

a vacuum device communicated to 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;

wherein said combustion device further comprises turbulence reducing structure disposed within said combustion chamber upstream of said catalyst element, 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;

wherein said turbulence reducing structure comprises a catalytically inactive body and wherein said apertures comprise a plurality of essentially linear elongated conduits formed therethrough for straightening flow of said fuel from said inlet port;

wherein said turbulence reducing structure further comprises a relatively thin diffuser positioned within said combustion chamber between said inlet port and said catalytically inactive body, said apertures further comprising a plurality of holes formed through said diffuser, said holes being configured to initially straighten the flow of said fuel from said inlet port.

51. A flying insect trapping device according to claim 50 , wherein said diffuser has annular flanges adjacent each aperture and extending towards said catalytically inactive body.

52. A flying insect trapping device configured to be used with a fuel supply containing combustible fuel, comprising:

a supporting frame;

an insect trap chamber carried on said supporting frame;

a combustion device carried on said supporting frame, said combustion device comprising an inlet port for connection with the fuel supply, an exhaust port, and a combustion chamber communicating said inlet port with said exhaust port, said inlet port enabling the fuel from the fuel supply to flow into said combustion chamber for continuous combustion therein to create an exhaust gas within said combustion chamber;

said combustion device further comprising a catalyst element disposed within said combustion chamber, said catalyst element having a catalyst body with a plurality of essentially linear elongated conduits for enabling the exhaust gas created in said combustion chamber to flow therethrough towards said exhaust port, said catalyst body including a catalytically active material that, during operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows through said elongated conduits;

an exhaust outlet carried said frame, said exhaust outlet being communicated with the exhaust port of said combustion device and being configured to allow said exhaust gas to flow outwardly through said exhaust outlet so that insects attracted to the carbon dioxide in said exhaust gas will fly towards laid exhaust outlet;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through skid insect inlet; and

a vacuum device communicated to 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;

wherein said combustion device further comprises turbulence reducing structure disposed within said combustion chamber upstream of said catalyst element, 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;

wherein said turbulence reducing structure comprises a catalytically inactive body and wherein said apertures comprise a plurality of essentially linear elongated conduits formed therethrough for straightening the flow of said fuel from said inlet port;

wherein said catalytically inactive body is a ceramic monolith.

53. A flying insect trapping device configured to be used with a fuel supply containing combustible fuel, comprising:

a supporting frame;

an insect trap chamber carried on said supporting frame;

a combustion device carried on said supporting frame, said combustion device comprising an inlet port for connection with the fuel supply, an exhaust port, and a combustion chamber communicating said inlet port with said exhaust port, said inlet port enabling the fuel from the fuel supply to flow into said combustion chamber for continuous combustion therein to create an exhaust gas within said combustion chamber;

said combustion device further comprising a catalyst element disposed within said combustion chamber, said catalyst element having a catalyst body with a plurality of essentially linear elongated conduits for enabling the exhaust gas created in said combustion chamber to flow therethrough towards said exhaust port, said catalyst body including a catalytically active material that, during operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows through said elongated conduits;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion device and being configured to allow said exhaust gas to flow outwardly through said exhaust outlet so that insects attracted to the carbon dioxide in said exhaust gas will fly towards said exhaust outlet;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through said insect inlet; and

a vacuum device communicated to 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;

wherein said combustion device further comprises turbulence reducing structure disposed within said combustion chamber upstream of said catalyst element, 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;

a sleeve, said catalyst element and said turbulence reducing structure being received in said sleeve.

54. A flying insect trapping device according to claim 53 , wherein said sleeve is lined internally with insulating material.

55. A flying insect trapping device according to claim 54 , wherein said sleeve is metal.

56. A flying insect trapping device according to claim 50 , further comprising a sleeve, said catalyst element, said catalytically inactive body and said relatively thin diffuser plate being received in said sleeve.

57. A flying insect trapping device according to claim 56 , wherein said sleeve is lined internally with insulating material.

58. A flying insect trapping device according to claim 57 , wherein said sleeve is metal.

59. A flying insect trapping system, comprising:

a fuel supply containing combustible fuel;

a supporting frame;

an insect trap chamber carried on said supporting frame;

a combustion device carried on said supporting frame, said combustion device comprising an inlet port for connection with the fuel supply, an exhaust port, and a combustion chamber communicating said inlet port with said exhaust port, said inlet port enabling the fuel from the fuel supply to flow into said combustion chamber for continuous combustion therein to create an exhaust gas within said combustion chamber;

said combustion device further comprising a catalyst element disposed within said combustion chamber, said catalyst element having a catalyst body with a plurality of essentially linear elongated conduits for enabling the exhaust gas created in said combustion chamber to flow therethrough towards said exhaust port, said catalyst body including a catalytically active material that, luring operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows through said elongated conduits;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion device and being configured to allow said exhaust gas to flow outwardly through said exhaust outlet so that insects attracted to the carbon dioxide in said exhaust gas will fly towards said exhaust outlet;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through said insect inlet; and

a vacuum device communicated to 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;

wherein said combustion device further comprises turbulence reducing structure disposed within said combustion chamber upstream of said catalyst element, 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;

wherein said turbulence reducing structure comprises a catalytically inactive body and wherein said apertures comprise plurality of generally linear elongated conduits formed therethrough for straightening the flow of said fuel from said inlet port;

wherein said turbulence reducing structure further comprises a relatively thin diffuser positioned within said combustion chamber between said inlet port and said catalytically inactive body, said apertures further comprising a plurality of holes formed through said diffuser, said holes being configured to initially straighten the flow of said fuel from said inlet port.

60. A flying insect trapping system according to claim 59 , wherein said diffuser has annular flanges adjacent each aperture and extending towards said catalytically inactive body.

61. A flying insect trapping system according to claim 59 , wherein said catalytically inactive body is a ceramic monolith.

62. A flying insect trapping system, comprising:

a fuel supply containing combustible fuel;

a supporting frame;

an insect trap chamber carried on said supporting frame;

a combustion device carried on said supporting frame, said combustion device comprising an inlet port for connection with the fuel supply, an exhaust port, and a combustion chamber communicating said inlet port with said exhaust port, said inlet port enabling the fuel from the fuel supply to flow into said combustion chamber for continuous combustion therein to create an exhaust gas within said combustion chamber;

said combustion device further comprising a catalyst element disposed within said combustion chamber, said catalyst element having a catalyst body with a plurality of essentially linear elongated conduits for enabling the exhaust gas created in said combustion chamber to flow therethrough towards said exhaust port, said catalyst body including a catalytically active material that, during operation, converts carbon monoxide in said exhaust gas to carbon dioxide as said exhaust gas flows through said elongated conduits;

an exhaust outlet carried on said frame, said exhaust outlet being communicated with the exhaust port of said combustion device and being configured to allow said exhaust gas to flow outwardly through said exhaust outlet so that insects attracted to the carbon dioxide in said exhaust gas will fly towards said exhaust outlet;

an insect inlet communicated with said insect trap chamber to enable flying insects to enter said trap chamber through paid insect inlet; and

a vacuum device communicated to 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;

wherein said combustion device further comprises turbulence reducing structure disposed within said combustion chamber upstream of said catalyst element, said turbulence reducing structure having a plurality of apertures oriented in the same general direction as the conduits of said catalyst body, skid apertures being configured to straighten the flow of fuel from said inlet port to thereby reduce turbulence in said fuel;

a sleeve, said catalyst element and said turbulence reducing structure being received in said sleeve.

63. A flying insect trapping system according to claim 62 , wherein said sleeve is lined internally with insulating material.

64. A flying insect trapping system according to claim 63 , wherein said sleeve is metal.

65. A flying insect trapping system according to claim 59 , further comprising a sleeve, said catalyst element, said catalytically inactive body and said relatively thin diffuser plate being received in said sleeve.

66. A flying insect trapping system according to claim 65 , wherein said sleeve is lined internally with insulating material.

67. A flying insect trapping system according to claim 66 , wherein said sleeve is metal.

Assignments (20)