US2965311A - Liquid fuel spraying nozzles - Google Patents
Liquid fuel spraying nozzles Download PDFInfo
- Publication number
- US2965311A US2965311A US825788A US82578859A US2965311A US 2965311 A US2965311 A US 2965311A US 825788 A US825788 A US 825788A US 82578859 A US82578859 A US 82578859A US 2965311 A US2965311 A US 2965311A
- Authority
- US
- United States
- Prior art keywords
- hollow
- diaphragm
- liquid fuel
- body part
- 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
Links
- 239000000446 fuel Substances 0.000 title description 16
- 239000007788 liquid Substances 0.000 title description 6
- 238000005507 spraying Methods 0.000 title description 5
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
- B05B7/02—Spray pistols; Apparatus for discharge
- B05B7/10—Spray pistols; Apparatus for discharge producing a swirling discharge
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
- B05B7/02—Spray pistols; Apparatus for discharge
- B05B7/06—Spray pistols; Apparatus for discharge with at least one outlet orifice surrounding another approximately in the same plane
- B05B7/062—Spray pistols; Apparatus for discharge with at least one outlet orifice surrounding another approximately in the same plane with only one liquid outlet and at least one gas outlet
- B05B7/066—Spray pistols; Apparatus for discharge with at least one outlet orifice surrounding another approximately in the same plane with only one liquid outlet and at least one gas outlet with an inner liquid outlet surrounded by at least one annular gas outlet
-
- 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
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
Definitions
- This invention relates to liquid fuel spraying nozzles of the pintle type comprising an elastic flexible diaphragm having a central discharge orifice therein, and a stationary closure member against which the diaphragm abuts when no flow occurs.
- the object of the invention is to enable improved nebulisation of the emergent fuel jet to be obtained in a simple manner.
- a nozzle of the kind aforesaid and in accordance with the invention comprises the combination with the discharge end of the body part of the nozzle, of a cap having therein a central discharge orifice and adapted to form with the diaphragm a chamber in which a swirling stream of air can be produced.
- Figure 1 is a longitudinal section of a nozzle embodying the invention.
- Figure 2 is a fragmentary view illustrating to a larger scale than Figure l a portion of the diaphragm and the associated closure member.
- an outer hollow body part a of substantially cylindrical form is adapted at one end for attachement to a fuel supply pipe. At the other end this part is enlarged to form a cylindrical cavity 12 for accommodating end portions of other component parts of the nozzle.
- a portion of the outer body part between its ends is internally screwthreaded and to this portion is secured an inner body part c having an enlarged end which is contained in the said cavity b of the outer part a.
- the body part c has secured to it, or is formed integrally with a hollow part c in which are formed slots which are covered by a filter c2 through which fuel can enter this part.
- a third hollow part d on the outer end of which is secured the elastic flexible diaphragm e and within the said third part d is contained a fourth hollow part 1 which forms the pintle.
- a closure member g which latter by contact with the rear side of the diaphragm closes the central hole h in the diaphragm when the nozzle is not in action.
- a thin axial stern i which extends through the hole in the diaphragm and terminates in a conical head k adapted to cause the emergent jet to spread in the form of a hollow cone.
- a hollow cap m adapted to close the enlarged end of the first mentioned body part a which end serves as an annular air chamber. Also the cap is shaped to form with the part d carrying the diaphragm an air chamber n which communicates with the other air chamber through a plurality of tangentially arranged ports 0.
- the air supplied to the combustion chamber from a blower flows over the exterior of the body part a of the nozzle, and a part of this air enters the above mentioned annular air chamber b of the nozzle through holes r formed in the outer portion of the body part. From this chamber the air passes through the tangential ports 0 to the air chamber it around the jet and by its swirling motion serves to promote rapid nebulisation of the fuel, the mixture of air and fuel being then discharged to the combustion chamber through the central hole s in the cap m.
- a liquid fuel spraying nozzle comprising in combination a substantially cylindrical hollow body part provided at one end with a fuel inlet, a hollow member secured coaxially within said body part and having its end portion remote from said fuel inlet surrounded by, and separated by an annular space from, the corresponding end portion of said hollow body part, the latter being provided with ports through which air under pressure is admissible to said annular space, a hollow cap closing the outer end of said annular space and provided with a central discharge opening, and also with tangential ports leading from said annular space to the interior of said hollow cap, a pintle support of hollow form secured coaxially within said hollow member with one end within said hollow cap, a hollow pintle secured within the hollow support and having one end in communication with the first mentioned end of said hollow body part, the other end of said hollow pintle being surrounded by and spaced from the end of said hollow support within said hollow cap, and being provided with outlet ports, an elastic flexible diaphragm secured to the last mentioned end of said hollow support and forming with said cap a
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Description
PM W Dec. 20, 1960 D. GASCOIGNE LIQUID FUEL SPRAYING NOZZLE S Filed July 8, 1959 LIQUID FUEL SPRAYING N OZZLES Denis Gascoigne, Fulwood, Preston, England, assignor to Joseph Lucas (Industries) Limited, Birmingham, England Filed July 8, 1959, Ser. No. 825,788
Claims priority, application Great Britain July 9, 1958 1 Claim. (Cl. 239-403) This invention relates to liquid fuel spraying nozzles of the pintle type comprising an elastic flexible diaphragm having a central discharge orifice therein, and a stationary closure member against which the diaphragm abuts when no flow occurs.
The object of the invention is to enable improved nebulisation of the emergent fuel jet to be obtained in a simple manner.
A nozzle of the kind aforesaid and in accordance with the invention comprises the combination with the discharge end of the body part of the nozzle, of a cap having therein a central discharge orifice and adapted to form with the diaphragm a chamber in which a swirling stream of air can be produced.
In the accompanying drawings:
Figure 1 is a longitudinal section of a nozzle embodying the invention.
Figure 2 is a fragmentary view illustrating to a larger scale than Figure l a portion of the diaphragm and the associated closure member.
In the example illustrated by the drawings, an outer hollow body part a of substantially cylindrical form is adapted at one end for attachement to a fuel supply pipe. At the other end this part is enlarged to form a cylindrical cavity 12 for accommodating end portions of other component parts of the nozzle. A portion of the outer body part between its ends is internally screwthreaded and to this portion is secured an inner body part c having an enlarged end which is contained in the said cavity b of the outer part a. The body part c has secured to it, or is formed integrally with a hollow part c in which are formed slots which are covered by a filter c2 through which fuel can enter this part. Into the opposite end of the part 01 is screw-threaded a third hollow part d on the outer end of which is secured the elastic flexible diaphragm e and within the said third part d is contained a fourth hollow part 1 which forms the pintle. On the latter is formed a closure member g which latter by contact with the rear side of the diaphragm closes the central hole h in the diaphragm when the nozzle is not in action. Further there is formed on the closure member a thin axial stern i which extends through the hole in the diaphragm and terminates in a conical head k adapted to cause the emergent jet to spread in the form of a hollow cone.
In the enlarged end of the second mentioned body part c is screwed a hollow cap m adapted to close the enlarged end of the first mentioned body part a which end serves as an annular air chamber. Also the cap is shaped to form with the part d carrying the diaphragm an air chamber n which communicates with the other air chamber through a plurality of tangentially arranged ports 0.
'1 5 The arrangement is such that the liquid fuel entering he first and second mentioned body parts passes into the nterior of the part f and thence through ports p therein ice to an annular space q formed by the part d carrying the diaphragm. By pressure of the fuel on the diaphragm, the latter is moved out of contact with the closure member g and the jet then issues through the hole h in the diaphragm.
The air supplied to the combustion chamber from a blower flows over the exterior of the body part a of the nozzle, and a part of this air enters the above mentioned annular air chamber b of the nozzle through holes r formed in the outer portion of the body part. From this chamber the air passes through the tangential ports 0 to the air chamber it around the jet and by its swirling motion serves to promote rapid nebulisation of the fuel, the mixture of air and fuel being then discharged to the combustion chamber through the central hole s in the cap m.
The invention is not, however, restricted to the specific example above described, as subordinate and unessential details of construction of the various components may be varied to suit different requirements.
Having thus described my invention what I claim as new and desire to secure by Letters Patent is:
A liquid fuel spraying nozzle comprising in combination a substantially cylindrical hollow body part provided at one end with a fuel inlet, a hollow member secured coaxially within said body part and having its end portion remote from said fuel inlet surrounded by, and separated by an annular space from, the corresponding end portion of said hollow body part, the latter being provided with ports through which air under pressure is admissible to said annular space, a hollow cap closing the outer end of said annular space and provided with a central discharge opening, and also with tangential ports leading from said annular space to the interior of said hollow cap, a pintle support of hollow form secured coaxially within said hollow member with one end within said hollow cap, a hollow pintle secured within the hollow support and having one end in communication with the first mentioned end of said hollow body part, the other end of said hollow pintle being surrounded by and spaced from the end of said hollow support within said hollow cap, and being provided with outlet ports, an elastic flexible diaphragm secured to the last mentioned end of said hollow support and forming with said cap a chamber to which streams of swirling air are admissible from said annular space through the tangential ports in said cap, the diaphragm being provided with a central hole, and a closure member provided on the ported end of said pintle to serve by contact with the portion of said diaphragm around the central hole therein to close said central hole when the nozzle is out of action, said diaphragm being separable from said closure member by fuel pressure in the adjacent end of said hollow support when the nozzle is in action, and said closure member having thereon an axial stem which extends with clearance through the central hole in the diaphragm, and which terminates in a conical head whereby fuel emerging from said central hole is caused to spread in the form of a hollow cone.
References Cited in the file of this patent UNITED STATES PATENTS 2,144,874 Edwards Jan. 24, 1939 2,701,164 Purchas et al. Feb. 1, 1955 2,893,647 Wortman July 7, 1959 FOREIGN PATENTS 504,830 Italy Dec. 14, 1954 909,736 France Jan. 7, 1946
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2965311X | 1958-07-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2965311A true US2965311A (en) | 1960-12-20 |
Family
ID=10918739
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US825788A Expired - Lifetime US2965311A (en) | 1958-07-09 | 1959-07-08 | Liquid fuel spraying nozzles |
Country Status (1)
Country | Link |
---|---|
US (1) | US2965311A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3026048A (en) * | 1961-03-16 | 1962-03-20 | Lucas Industries Ltd | Duplex liquid fuel burner nozzles |
US3175643A (en) * | 1962-05-29 | 1965-03-30 | Gulf Research Development Co | Compressor and atomizing nozzle lubricator |
US3441223A (en) * | 1967-03-08 | 1969-04-29 | Parker Hannifin Corp | Nozzle |
US4013229A (en) * | 1974-02-19 | 1977-03-22 | Ulrich Rohs | Injection nozzle for liquids, particularly for fuels |
US4638636A (en) * | 1984-06-28 | 1987-01-27 | General Electric Company | Fuel nozzle |
US5146904A (en) * | 1991-06-20 | 1992-09-15 | Outboard Marine Corporation | Internal combustion engine fuel supply system |
US5788161A (en) * | 1994-04-15 | 1998-08-04 | Robert Bosch Gmbh | Fuel injection nozzle for internal combustion engines |
US20050217270A1 (en) * | 2004-04-02 | 2005-10-06 | Pratt & Whitney Canada Corp. | Fuel injector head |
US20160069298A1 (en) * | 2014-09-05 | 2016-03-10 | United Technologies Corporation | Variable orifice jet for a turbine engine |
GB2590659A (en) * | 2019-12-23 | 2021-07-07 | Rolls Royce Plc | Nozzle for gas turbine engine and method of manufacture thereof |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2144874A (en) * | 1937-04-03 | 1939-01-24 | Timken Roller Bearing Co | Fuel injector |
FR909736A (en) * | 1943-04-10 | 1946-05-16 | Audi Ag | Injection nozzle especially for internal combustion engines |
US2701164A (en) * | 1951-04-26 | 1955-02-01 | Gen Motors Corp | Duplex fuel nozzle |
US2893647A (en) * | 1957-05-06 | 1959-07-07 | Gen Motors Corp | Adjustable fuel nozzle |
-
1959
- 1959-07-08 US US825788A patent/US2965311A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2144874A (en) * | 1937-04-03 | 1939-01-24 | Timken Roller Bearing Co | Fuel injector |
FR909736A (en) * | 1943-04-10 | 1946-05-16 | Audi Ag | Injection nozzle especially for internal combustion engines |
US2701164A (en) * | 1951-04-26 | 1955-02-01 | Gen Motors Corp | Duplex fuel nozzle |
US2893647A (en) * | 1957-05-06 | 1959-07-07 | Gen Motors Corp | Adjustable fuel nozzle |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3026048A (en) * | 1961-03-16 | 1962-03-20 | Lucas Industries Ltd | Duplex liquid fuel burner nozzles |
US3175643A (en) * | 1962-05-29 | 1965-03-30 | Gulf Research Development Co | Compressor and atomizing nozzle lubricator |
US3441223A (en) * | 1967-03-08 | 1969-04-29 | Parker Hannifin Corp | Nozzle |
US4013229A (en) * | 1974-02-19 | 1977-03-22 | Ulrich Rohs | Injection nozzle for liquids, particularly for fuels |
US4638636A (en) * | 1984-06-28 | 1987-01-27 | General Electric Company | Fuel nozzle |
US5146904A (en) * | 1991-06-20 | 1992-09-15 | Outboard Marine Corporation | Internal combustion engine fuel supply system |
US5788161A (en) * | 1994-04-15 | 1998-08-04 | Robert Bosch Gmbh | Fuel injection nozzle for internal combustion engines |
US20050217270A1 (en) * | 2004-04-02 | 2005-10-06 | Pratt & Whitney Canada Corp. | Fuel injector head |
US7117678B2 (en) | 2004-04-02 | 2006-10-10 | Pratt & Whitney Canada Corp. | Fuel injector head |
US20160069298A1 (en) * | 2014-09-05 | 2016-03-10 | United Technologies Corporation | Variable orifice jet for a turbine engine |
US10041444B2 (en) * | 2014-09-05 | 2018-08-07 | United Technologies Corporation | Variable orifice jet for a turbine engine |
GB2590659A (en) * | 2019-12-23 | 2021-07-07 | Rolls Royce Plc | Nozzle for gas turbine engine and method of manufacture thereof |
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