Compact pulse combustion burner with enhanced heat transfer

• US 4,574,745 A
• Filed: 07/23/1984
• Issued: 03/11/1986
• Est. Priority Date: 07/23/1984
• Status: Expired due to Fees

• Current Assignee: Energy International Corporation
• Original Assignee: American Gas Association
• Inventors: Belles, Frank E.
• Primary Examiner(s): Green, Randall L.
• Application Number:
  US06/633,218
• Time in Patent Office: 596 Days
• Field of Search: 431/1, 431/114, 60/247, 60/39.76, 60/39.77, 122/24, 126/360 R
• US Class Current: 431/1
• CPC Class Codes: F23C 15/00 Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass for generating combustion products of high pressure or high velocity F23R7/00; starting devices F23D11/42
• CPC Class Codes: F24H 1/26 the water mantle forming an integral body

Abstract

A pulse combustion burner having a multi-apertured combustion chamber wall surrounded by a primary heat transfer zone. Gas jets issuing out of the wall apertures induce high turbulence in the gas flow path through the heat transfer zone and thereby promote an exceptionally high level of heat exchange. Dimensions of the gas flow path, including the primary heat transfer zone, are arranged to cause the primary heat transfer zone to serve as an effective portion of the tailpipe of the burner. Both the high heat transfer capability and reduced tailpipe length permit reduction in the overall size of a burner unit.

Claims

1. A pulse combustion burner comprising a combustion chamber, inlet means for admitting a combustible gaseous mixture into the chamber and restricting reverse flow therethrough, means for igniting the gaseous mixture, a wall forming the combustion chamber, the combustion chamber wall having a multitude of spaced apertures, the combustion chamber wall restricting flow of gases from said combustion chamber to passage through said apertures, a heat exchanger wall spaced from said combustion chamber wall and forming therewith passage means for receiving gases passing through said apertures, an exhaust conduit of predetermined cross section in communication with said passage means for receiving gases passing through said apertures, the collective area of said apertures being generally matched to the cross-sectional area of the exhaust conduit, said heat exchanger wall having heat transfer surface means arranged in close proximity to the path of combustion products passing through said apertures whereby jets of gas passing through such apertures create a high degree of turbulence and resulting high heat transfer rate at said heat transfer surface means.

2. A pulse combustion burner as set forth in claim 1, wherein said apertures are arranged with respect to said heat transfer surface means to direct flow of combustion products from said combustion chamber in a direction substantially perpendicular to said heat transfer surface means.

3. A pulse combustion burner as set forth in claim 2, wherein said combustion chamber wall is generally solid and said apertures are formed as holes in such solid wall.

4. A pulse combustion burner as set forth in claim 2, wherein said combustion chamber wall and said heat transfer surface means are in spaced generally parallel relation.

5. A pulse combustion burner as set forth in claim 4, wherein said apertures and heat transfer surface means are arranged in a manner wherein combustion products, after issuing from apertures into said passage relatively remote from said exhaust conduit, are impinged by jets of combustion products issuing from apertures into said passage relatively proximal to said exhaust conduit.

6. A pulse combustion burner as set forth in claim 1, wherein the cross sectional area of said passage means is generally equal to the cross-sectional area of said exhaust conduit.