Claims
- 1. A burner assembly for the combustion of liquid fuels in furnaces and the like comprising:
- fuel gun means carrying an atomizer tip providing a plurality of small passageways open directly to said furnace interior through which a mixture of combustible fuel and an atomizing medium is injected directly into the interior of said furnace;
- housing means supplying a first flow of air into said furnace to encompass said injected fuel mixture therein having an end open directly to said furnace interior and encompassing said atomizer tip,
- said housing means being attachable to said furnace, so that said combustible fuel mixture is delivered directly to the interior of said furnace for combustion;
- holding tube means carrying said fuel gun means and carried within said housing means for supplying a second flow of air unrestricted, directly into said furnace interior separate from said first flow of air; and
- swirler means having a plurality of overlapping blades, carried by said holding tube, foreclosing direct axial passage of the majority of said first flow of air therethrough, extending radially outwardly from said holding tube, terminating with a free outermost edge spaced a short distance from said housing means and providing a narrow axial space for the passage of a minor portion of said first flow of air, each said blade having a leading edge and a trailing edge, said blades being arranged so that said trailing edge of each said blade overlaps said leading edge of the adjacent blade.
- 2. A burner assembly, as set forth in claim 1, wherein said housing means comprises a cylindrical tube having an inner wall and is open to said furnace interior at one end and is closed at the opposite end.
- 3. A burner assembly, as set forth in claim 2, wherein said holding tube means pass through said closed end of said housing means and open to said furnace interior at said open end of said housing means.
- 4. A burner assembly, as set forth in claim 3, wherein said housing means provides an axial port to which a leg is attached through which said first flow of air is fed.
- 5. A burner assembly, as set forth in claim 4, wherein said holding tube provides axial port means through which said second flow of air is fed.
- 6. A burner assembly, as set forth in claim 5, further including air line means connected to said axial port means, extending into said leg means and open thereto.
- 7. A burner assembly, as set forth in claim 1, wherein at least some of said passageways provide a mixture of fuel and air.
- 8. A burner assembly, as set forth in claim 1, wherein all of said passageways provide a mixture of fuel and air.
- 9. A burner assembly, as set forth in claim 3, wherein said swirler means is carried by said holding tube means adjacent said open end thereof.
- 10. A burner assembly, as set forth in claim 2, further including a plurality of helical lands carried by said inner wall of said housing means, partially to alter the direction of movement of said first flow of air.
- 11. A burner assembly, as set forth in claim 5, further comprising second swirler means having a plurality of overlapping blades, foreclosing direct axial passage of said second flow of air therethrough, extending radially outwardly from said fuel gun means, terminating with a free outermost edge spaced a short distance from said holding tube and providing a narrow axial space for the movement of a minor portion of said second flow of air, each said blade having a leading edge and a trailing edge, said blades being arranged so that said trailing edge of each said blade overlaps said leading edge of the adjacent blade.
- 12. A burner assembly, as set forth in claim 11, wherein said second swirler means is carried by said fuel gun, upstream from said atomizer tip.
- 13. A burner assembly, as set forth in claim 12, wherein said fuel gun means provides an atomizer tip providing a plurality of small passageways open to said furnace interior.
- 14. A burner assembly, as set forth in claim 13, wherein at least some of said passageways provide a mixture of fuel and air.
- 15. A burner assembly, as set forth in claim 13, wherein all of said passageways provide a mixture of fuel and air.
- 16. A burner assembly, as set forth in claim 11, further including a plurality of helical lands carried by said inner wall of said housing means, partially to alter the direction of movement of said first flow of air.
- 17. A burner assembly for the combustion of liquid fuels in furnaces and the like comprising:
- fuel gun means carrying an atomizer tip providing a plurality of small passageways open directly to said furnace interior through which a mixture of combustible fuel and an atomizing medium is injected directly into the interior of said furnace;
- housing means supporting said fuel gun means and supplying a first flow of air into said furnace to encompass said injected fuel mixture therein having an end open directly to said furnace interior and encompassing said atomizer tip,
- said housing means being attachable to said furnace, so that said combustible fuel mixture is delivered to the interior of said furnace for combustion and
- swirler means having a plurality of overlapping blades carried by said fuel gun means, foreclosing direct axial passage of said first flow of air therethrough, extending radially outwardly from said fuel fun means, terminating with a free outermost edge spaced a short distance from said housing means and providing a narrow axial space for the movement of a minor portion of said first flow of air, each said blade having a leading edge and a trailing edge, said blades being arranged so that said trailing edge of each said blade overlaps said leading edge of the adjacent blade.
- 18. A burner assembly, as set forth in claim 17, wherein said housing means comprises a cylindrical tube having an inner wall and is open to said furnace interior at one end and is closed at the opposite end.
- 19. A burner assembly, as set forth in claim 18, wherein said fuel gun means passes through said housing means and is partially supported thereby.
- 20. A burner assembly, as set forth in claim 19, wherein said housing means provides an axial port to which a leg is attached through which said first flow of air is fed.
- 21. A burner assembly, as set forth in claim 19, further including a plurality of helical lands carried by said inner wall of said housing means, partially to alter the direction of movement of said first flow of air.
- 22. A burner assembly, as set forth in claim 17, wherein at least some of said passageways provide a mixture of fuel and air.
- 23. A burner assembly, as set forth in claim 17, wherein all of said passageways provide a mixture of fuel and air.
- 24. A burner assembly, as set forth in claim 17, wherein said swirler means is carried by said fuel gun, upstream from said atomizer tip.
- 25. A method for supplying liquid fuel and air mixtures to furnaces and the like through a burner assembly having liquid fuel gun means, housing means attachable to the furnace and a plurality of curved, overlapping blades comprising the steps of:
- locating the tip of said fuel gun means directly at an opening in said furnace;
- injecting a mixture of liquid fuel and atomizing medium through said tip directly into the interior of said furnace;
- feeding a first flow of air through said housing means and into said furnace interior;
- providing said plurality of curved, overlapping blades within said housing means and directly adjacent said furnace interior, each said blade having a leading edge, a trailing edge and a free outermost edge terminating a short distance from said housing means;
- directly said first flow of air through a plurality of curved slotted passageways formed by said overlapping blades which foreclose direct axial passage of the major volume of said first flow of air between adjacent blades along their entire length;
- allowing said major volume of air to expand radially as it passes through said curved slotted passageways and into said furnace interior;
- directing the remaining minor volume of air around said blade edges to flow unrestricted between said blade edges and said housing means and combine with said radially expanding air as said major and minor volumes move forward within said furnace; and
- encompassing said mixture with said first flow or air as said mixture enters said furnace whereby both said volumes break up said mixture within said furnace.
- 26. A method, as set forth in claim 25, including the additional step of
- feeding a second flow of air through said burner assembly and into said furnace interior separate from
- said first flow of air.
- 27. A method, as set forth in claim 26, wherein said second flow of air is moved axially through said burner assembly and directly into said furnace between said mixture and said first flow of air.
- 28. A method, as set forth in claim 27, including the additional steps of
- supplying a single volume of air to said burner assembly; and
- dividing said air into said first and second flows within said assembly.
- 29. A method, as set forth in claim 28, including the additional step of:
- interrupting said second flow of air to provide a major volume and a minor volume;
- directing said major volume through a plurality of curved slotted passageways formed by a plurality of overlapping blades which foreclose direct axial passage between adjacent blades along their entire length;
- allowing said major volume of air to expand radially as it passes through said curved slotted passageways;
- directing said minor volume around the circumferential edge of said blades to flow unrestricted and combine with said radially expanding air as said major and minor volumes move forward into said furnace interior.
- 30. A method, as set forth in claim 25, wherein said step of injecting includes the steps of
- forcing a volume of air as said atomizing medium through a first plurality of narrow air passageways which extend through an atomizer tip; and
- forcing a volume of duel through a plurality of narrow fuel passageways which communicate with said first plurality of air passageways whereby said fuel becomes atomized by said air as it is ejected from said first plurality of passageways.
- 31. A method, as set forth in claim 30, including the additional step of
- forcing a portion of said volume of air through a second plurality of narrow air passageways which extend through said atomizer tip.
Parent Case Info
This is a continuation of application Ser. No. 07/049,804 filed on 05/12/87, now abandoned.
US Referenced Citations (39)
Foreign Referenced Citations (1)
Number |
Date |
Country |
75378 |
Feb 1953 |
DKX |
Continuations (1)
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Number |
Date |
Country |
Parent |
49804 |
May 1987 |
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