Swirl type pressure fuel atomizer

• US 4,087,050 A
• Filed: 11/18/1976
• Issued: 05/02/1978
• Est. Priority Date: 09/18/1975
• Status: Expired due to Term

• Current Assignee: Ishikawajima-Harima Jukogyo Kabushiki Kaisha
• Original Assignee: Ishikawajima-Harima Jukogyo Kabushiki Kaisha
• Inventors: Fujii, Yuichi, Asai, Minoru, Tsuji, Shoichi
• Primary Examiner(s): Love, John J.
• Application Number:
  US05/743,013
• Time in Patent Office: 530 Days
• Field of Search: 239/404, 239/406, 239/425, 239/467, 239/491, 239/493, 239/498, 239/502, 239/518, 239/489, 239/568, 239/492, 239/494, 239/490, 239/466, 239/403, 239/496
• US Class Current: 239/490
• CPC Class Codes: F23D 11/383 with swirl means

Abstract

An improvement of a swirl type fuel atomizer is disclosed in which a plurality of projections, grooves or recesses are equiangularly formed around an opening of a single-nozzle hole so that the liquid fuel injected may be divided into a plurality of fuel spray patterns. The complete combustion with a relatively low temperature may be ensured so that the emission of nitrogen oxides may be substantially eliminated or reduced.

Claims

1. A burner assembly comprising a housing having a main flow passage therein adapted to receive fuel at one end thereof;

a nozzle tip secured to said housing and having an inner wall portion defining a nozzle hole aligned along a nozzle axis;

one end of said nozzle hole functioning as an outlet opening for said fuel;

a chamber of larger diameter than said nozzle hole and having one end registering with the other end of said nozzle hole;

a plurality of grooves extending tangentially to said chamber adjacent the other end thereof;

means for receiving said fuel from said main flow passage and dividing said fuel into a plurality of relatively small flow streams extending parallel to the axis of said main flow passage and said chamber and respectively registering with said grooves so that said grooves impart a swirl to said fuel as it passes through said chamber;

said inner wall of said nozzle tip defining said nozzle hole being provided with a plurality of spaced discharge grooves formed therein to divide the fuel discharging from said outlet opening into a plurality of separate spray patterns;

said discharge grooves being bevelled with respect to said axis and diverging toward said outlet opening.

2. The burner assembly of claim 1, wherein said outlet opening is circular in cross section and wherein said discharge grooves are circumferentially spaced around said wall and extend symmetrically with respect to the center of said outlet opening.

3. The burner assembly of claim 1, wherein said discharge grooves extend tangentially with respect to said outlet opening.

4. The burner assembly of claim 1, wherein said means for imparting a swirl to said fuel comprises a plurality of grooves formed in the inner wall of said nozzle tip defining said one chamber, said grooves extending tangentially to said one chamber.

5. A burner assembly comprising a housing having a main flow passage therein adapted to receive fuel at one end thereof;

a nozzle tip secured to said housing having an inner wall portion defining a nozzle hole aligned along a nozzle axis;

one end of said nozzle hole functioning as an outlet opening for said fuel;

a chamber of larger diameter than said nozzle hole having one end registering with the other end of said nozzle hole;

a plurality of grooves extending tangentially to said chamber adjacent the other end thereof;

means for receiving said fuel from said main flow passage and dividing said fuel into a plurality of relatively small flow streams extending parallel to the axis of said main flow passage and said chamber and respectively registering with said grooves so that said grooves impart a swirl to said fuel as it passes through said chamber;

said inner wall defining said nozzle hole being provided with a plurality of spaced projections which extend radially inward from said wall to divide the fuel discharging from said outlet opening into a plurality of separate spray patterns;

each of said projections having a portion bevelled with respect to said axis and another portion substantially parallel to said axis.

6. The burner assembly of claim 5, wherein said outlet opening is circular in cross section and wherein said projections are circumferentially spaced around said wall and extend symmetrically with respect to the center of said outlet opening.

7. The burner assembly of claim 5, wherein said nozzle hole and said chamber are cylindrical in shape and extend coaxially with said passage.

8. The burner assembly of claim 7, wherein the diameter of said nozzle hole is less than that of said chamber.

9. The burner assembly of claim 5, wherein said means for imparting a swirl to said fuel comprises a plurality of grooves formed in the inner wall of said nozzle tip defining said chamber, said grooves extending tangentially to said chamber.