US2588485A - Liquid fuel burner nozzle - Google Patents
Liquid fuel burner nozzle Download PDFInfo
- Publication number
- US2588485A US2588485A US147952A US14795250A US2588485A US 2588485 A US2588485 A US 2588485A US 147952 A US147952 A US 147952A US 14795250 A US14795250 A US 14795250A US 2588485 A US2588485 A US 2588485A
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- US
- United States
- Prior art keywords
- liquid fuel
- chamber
- swirl
- fuel burner
- burner nozzle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
Definitions
- LIQUID FUEL BURNER NOZZLE Filed March 6, 1950 e] C fa/Pif@ Patented Mar. 11, 1952 LIQUID FUEL BURNER NOZZLE .
- This invention has for its object to provide improved liquid fuel burner nozzles of the swirlchamber type and having in association with the swirl-chamber flow control means responsive to the fuel pressure.
- a hollow body part a is provided at one end with a conical swirlchamber l) having the discharge orifice at its smaller end.
- the larger end communicates with an annular fuel supply duct c by' way of tangentially disposed passages
- a cylindrical chamber e containing a piston f loaded by a spring y, and from the side of the piston remote from the spring, there extends (through a 1core the body part) a control member h, the outside diameter of which is substantially equal to the diameter of the larger end of the swirl-chamber.
- Fuel can enter the end ofy the said chamber e remote from the spring through a passage and the pressure exerted on the piston in opposition to the spring serves to move the control member in the direction for varying the effective cross-sectional area of the discharge ends of the tangential passages d.
- an axial bore through which extends a hollow cylindrical stem 7' terminating in a conical portion 1c which is situated within the above mentioned swirl-chamber b.
- the conical portion of the stem is shaped to form within it a subsidiary conical swirl-chamber having a discharge orifice at its smaller end, and within the stem is located a swirl plug m formed with peripheral and helical grooves n, for admitting fuel to the associated swirl chamber from a passage o communicating with the supply duct c, the plug m being held in position by a spring p.
- the arrangement is such that variation of the pressure of the fuel admitted at q to the duct c is accompanied by variation of the rate of flow to the main swirl-chamber b, and under a conn liquid fuel through the nozzle in response to variations of fuel pressure can be effected in a simple and convenient manner.
- a liquid fuel nozzle comprising in combination a hollow body provided with an inlet for liquid fuel under pressure, and with a main swirl-chamber through which liquid fuel can be discharged from said hollow body, a hollow cylindrical member immovably secured within said, hollow body and terminating at one end in a subsidiary swirl-chamber provided with a discharge orifice, said hollow cylindrical member being in communication with said inlet, and said subsidiary swirl chamber being situated within said main swirl chamber, a movable control member surrounding said hollow cylindrical member and having one end arranged to control fuel flow from the interior of said hollow body to said main swirl chamber, and means for moving said control member in response to the pressure of the liquid fuel supplied to the said hollow body.
Description
March 11, 1952 J, s, CLARKE Er AL 2,588,485
LIQUID FUEL BURNER NOZZLE Filed March 6, 1950 e] C fa/Pif@ Patented Mar. 11, 1952 LIQUID FUEL BURNER NOZZLE .lohn Stanley Clarke, Blaeko, near Nelson, and Leslie John Goddard, Bromborough, England, assignors to Joseph Lucas Limited, Birmingham, England Application March 6, 1950, Serial No. 147,952 In Great Britain March 7, 1949 2 Claims.
This invention has for its object to provide improved liquid fuel burner nozzles of the swirlchamber type and having in association with the swirl-chamber flow control means responsive to the fuel pressure.
The accompanying drawing is a sectional side elevation illustrating one embodiment of the invention.
Referring to the drawing, a hollow body part a is provided at one end with a conical swirlchamber l) having the discharge orifice at its smaller end. The larger end communicates with an annular fuel supply duct c by' way of tangentially disposed passages Within the body part is formed a cylindrical chamber e containing a piston f loaded by a spring y, and from the side of the piston remote from the spring, there extends (through a 1core the body part) a control member h, the outside diameter of which is substantially equal to the diameter of the larger end of the swirl-chamber. Fuel can enter the end ofy the said chamber e remote from the spring through a passage and the pressure exerted on the piston in opposition to the spring serves to move the control member in the direction for varying the effective cross-sectional area of the discharge ends of the tangential passages d. i
In the piston and control member is formed an axial bore through which extends a hollow cylindrical stem 7' terminating in a conical portion 1c which is situated within the above mentioned swirl-chamber b. The conical portion of the stem is shaped to form within it a subsidiary conical swirl-chamber having a discharge orifice at its smaller end, and within the stem is located a swirl plug m formed with peripheral and helical grooves n, for admitting fuel to the associated swirl chamber from a passage o communicating with the supply duct c, the plug m being held in position by a spring p.
The arrangement is such that variation of the pressure of the fuel admitted at q to the duct c is accompanied by variation of the rate of flow to the main swirl-chamber b, and under a conn liquid fuel through the nozzle in response to variations of fuel pressure can be effected in a simple and convenient manner.
Having thus described our invention what we claim as new and desire to secure by Letters Patent is:
1. A liquid fuel nozzle comprising in combination a hollow body provided with an inlet for liquid fuel under pressure, and with a main swirl-chamber through which liquid fuel can be discharged from said hollow body, a hollow cylindrical member immovably secured within said, hollow body and terminating at one end in a subsidiary swirl-chamber provided with a discharge orifice, said hollow cylindrical member being in communication with said inlet, and said subsidiary swirl chamber being situated within said main swirl chamber, a movable control member surrounding said hollow cylindrical member and having one end arranged to control fuel flow from the interior of said hollow body to said main swirl chamber, and means for moving said control member in response to the pressure of the liquid fuel supplied to the said hollow body.
2. A liquid fuel nozzle as claimed in claim 1 and having within the subsidiary swirl-chamber a swirl plug formed with helical peripheral grooves.
JOHN STANLEY CLARKE. LESLIE JOHN GODDARD.
REFERENCES CTED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,607,805 Sprado Nov. 23,1926 2,436,815 Lum Mar. 2, 1948
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2588485X | 1949-03-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2588485A true US2588485A (en) | 1952-03-11 |
Family
ID=10910886
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US147952A Expired - Lifetime US2588485A (en) | 1949-03-07 | 1950-03-06 | Liquid fuel burner nozzle |
Country Status (1)
Country | Link |
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US (1) | US2588485A (en) |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3785570A (en) * | 1972-08-30 | 1974-01-15 | Us Army | Dual orifice fuel nozzle with air-assisted primary at low flow rates |
US3838821A (en) * | 1972-07-20 | 1974-10-01 | Cav Ltd | Fuel injection nozzle units |
US4987887A (en) * | 1990-03-28 | 1991-01-29 | Stanadyne Automotive Corp. | Fuel injector method and apparatus |
US5020500A (en) * | 1990-03-28 | 1991-06-04 | Stanadyne Automotive Corp. | Hole type fuel injector and injection method |
US20060042254A1 (en) * | 2004-09-02 | 2006-03-02 | Shouhei Yoshida | Combustor, gas turbine combustor, and air supply method for same |
US20100067908A1 (en) * | 2005-09-29 | 2010-03-18 | Broadlight, Ltd. | Enhanced Passive Optical Network (PON) Processor |
US20120012099A1 (en) * | 2010-06-07 | 2012-01-19 | David Deng | Heating system |
US8985094B2 (en) | 2011-04-08 | 2015-03-24 | David Deng | Heating system |
US9222670B2 (en) | 2010-12-09 | 2015-12-29 | David Deng | Heating system with pressure regulator |
US9423123B2 (en) | 2013-03-02 | 2016-08-23 | David Deng | Safety pressure switch |
US9739389B2 (en) | 2011-04-08 | 2017-08-22 | David Deng | Heating system |
US9752779B2 (en) | 2013-03-02 | 2017-09-05 | David Deng | Heating assembly |
US9752782B2 (en) | 2011-10-20 | 2017-09-05 | David Deng | Dual fuel heater with selector valve |
US10073071B2 (en) | 2010-06-07 | 2018-09-11 | David Deng | Heating system |
US10222057B2 (en) | 2011-04-08 | 2019-03-05 | David Deng | Dual fuel heater with selector valve |
US10240789B2 (en) | 2014-05-16 | 2019-03-26 | David Deng | Dual fuel heating assembly with reset switch |
US10429074B2 (en) | 2014-05-16 | 2019-10-01 | David Deng | Dual fuel heating assembly with selector switch |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1607805A (en) * | 1926-11-23 | op milwaukee | ||
US2436815A (en) * | 1944-03-15 | 1948-03-02 | Gen Electric | Pressure operated valve |
-
1950
- 1950-03-06 US US147952A patent/US2588485A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1607805A (en) * | 1926-11-23 | op milwaukee | ||
US2436815A (en) * | 1944-03-15 | 1948-03-02 | Gen Electric | Pressure operated valve |
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3838821A (en) * | 1972-07-20 | 1974-10-01 | Cav Ltd | Fuel injection nozzle units |
US3785570A (en) * | 1972-08-30 | 1974-01-15 | Us Army | Dual orifice fuel nozzle with air-assisted primary at low flow rates |
US4987887A (en) * | 1990-03-28 | 1991-01-29 | Stanadyne Automotive Corp. | Fuel injector method and apparatus |
US5020500A (en) * | 1990-03-28 | 1991-06-04 | Stanadyne Automotive Corp. | Hole type fuel injector and injection method |
USRE34999E (en) * | 1990-03-28 | 1995-07-25 | Stanadyne Automotive Corp. | Hole type fuel injector and injection method |
USRE35101E (en) * | 1990-03-28 | 1995-11-28 | Stanadyne Automotive Corp. | Fuel injector method and apparatus |
US20060042254A1 (en) * | 2004-09-02 | 2006-03-02 | Shouhei Yoshida | Combustor, gas turbine combustor, and air supply method for same |
US20110011092A1 (en) * | 2004-09-02 | 2011-01-20 | Shouhei Yoshida | Combustor, gas turbine combustor, and air supply method for same |
US7891191B2 (en) * | 2004-09-02 | 2011-02-22 | Hitachi, Ltd. | Combustor, gas turbine combustor, and air supply method for same |
US8047003B2 (en) | 2004-09-02 | 2011-11-01 | Hitachi, Ltd. | Combustor, gas turbine combustor, and air supply method for same |
US20100067908A1 (en) * | 2005-09-29 | 2010-03-18 | Broadlight, Ltd. | Enhanced Passive Optical Network (PON) Processor |
US8752541B2 (en) | 2010-06-07 | 2014-06-17 | David Deng | Heating system |
US20120012099A1 (en) * | 2010-06-07 | 2012-01-19 | David Deng | Heating system |
US8851065B2 (en) * | 2010-06-07 | 2014-10-07 | David Deng | Dual fuel heating system with pressure sensitive nozzle |
US9021859B2 (en) | 2010-06-07 | 2015-05-05 | David Deng | Heating system |
US10073071B2 (en) | 2010-06-07 | 2018-09-11 | David Deng | Heating system |
US9222670B2 (en) | 2010-12-09 | 2015-12-29 | David Deng | Heating system with pressure regulator |
US8985094B2 (en) | 2011-04-08 | 2015-03-24 | David Deng | Heating system |
US10222057B2 (en) | 2011-04-08 | 2019-03-05 | David Deng | Dual fuel heater with selector valve |
US9739389B2 (en) | 2011-04-08 | 2017-08-22 | David Deng | Heating system |
US9752782B2 (en) | 2011-10-20 | 2017-09-05 | David Deng | Dual fuel heater with selector valve |
US9752779B2 (en) | 2013-03-02 | 2017-09-05 | David Deng | Heating assembly |
US9518732B2 (en) | 2013-03-02 | 2016-12-13 | David Deng | Heating assembly |
US9423123B2 (en) | 2013-03-02 | 2016-08-23 | David Deng | Safety pressure switch |
US10240789B2 (en) | 2014-05-16 | 2019-03-26 | David Deng | Dual fuel heating assembly with reset switch |
US10429074B2 (en) | 2014-05-16 | 2019-10-01 | David Deng | Dual fuel heating assembly with selector switch |
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