US2552658A - Nozzle for gas turbines - Google Patents

Nozzle for gas turbines Download PDF

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Publication number
US2552658A
US2552658A US709549A US70954946A US2552658A US 2552658 A US2552658 A US 2552658A US 709549 A US709549 A US 709549A US 70954946 A US70954946 A US 70954946A US 2552658 A US2552658 A US 2552658A
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US
United States
Prior art keywords
fuel
nozzle
nozzle body
valve
seat
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
Application number
US709549A
Inventor
Howard A Ackerman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ambac International Corp
Original Assignee
American Bosch Arma Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by American Bosch Arma Corp filed Critical American Bosch Arma Corp
Priority to US709549A priority Critical patent/US2552658A/en
Application granted granted Critical
Publication of US2552658A publication Critical patent/US2552658A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • 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
    • F23D11/26—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 with provision for varying the rate at which the fuel is sprayed
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7781—With separate connected fluid reactor surface
    • Y10T137/7832—Plural valves biased closed
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/87917—Flow path with serial valves and/or closures
    • Y10T137/88054—Direct response normally closed valve limits direction of flow

Definitions

  • This invention relates to nozzles and has particular reference to a nozzle for gas turbines or the like and which is capable of operation over a wide range of fuel flow pressures and quantities.
  • An object of the present invention is to provide a new and improved nozzle for burners such as gas turbines wherein the fuel flow controls the opening of the nozzle valve and also the operation orifice area and wherein the supply of fuel to the burner will be satisfactorily controlled over a wide fuel flow range.
  • Another object of the invention is to provide a nozzle of the type set forth which is relatively simple and economical in construction yet efficient in operation.
  • Another object of the invention is to provide a nozzle of the type set forth wherein satisfactory fuel atomization will be provided from a fuel range of from low fuel flow for idling of the engine to maximum flow of the nozzle.
  • the nozzle shown embodying the invention comprises the nozzle cap I and nozzle body holder 2 having the threaded portion 3 for securing the body holder 2 to the fuel supply line not shown.
  • the holder body 2 also has the fuel supply opening 4 adapted to supply fuel to the interior of the nozzle.
  • the nozzle cap I has the peripheral flange 5 on which is positioned the peripheral flange 6 on the nozzle body 1 and said flange 6 is retained on the flange 5 by the engagement thereon of the lower end portion 8 of the hollow nut portion 9 of the nozzle body holder 2 and which is in threaded engagement with a corresponding threaded portion on the nozzle cap I.
  • the nozzle cap I has the orifice I through which fuel is adapted to be sprayed to the combustion chamber of the burner as hereinafter described.
  • the nozzle body 4 has the central opening off the fuel chamber I I adapted to receive the valve I2 which has the valve portion I3 normally engaging a seat I4 in the nozzle body I and below which seat is the fuel chamber I adapted to receive fuel through the supply groove I6 which, in turn, receives fuel through the peripheral space H between the outer surface of the nozzle body I and the inner surface of the hollow portion 9 on the holder body.
  • the threaded plug I8 is adapted to be threaded into the upper end of the hollow portion of the nozzle body 1 and to retain the coil spring I9 on the stem of the valve I2.
  • Said spring I9- has one end in engagement with the inner surface of said plug I 8 and its other end in engagement with the spring seat 20 on the valve I2 and surrounds the stem thereof.
  • the valve has the needle projection 2I which extends through the chamber I5 and is then in relatively close flt with the nozzle body I and the lower end of said needle 2
  • the lower surface of the nozzle body I is provided with the peripheral supply groove 22 which is connected by a plurality of slots 23 to thereby supply fuel to the orifice Ill.
  • the slots 23 may be of any suitable number and may be so arranged as to provide turbulence to the fuel.
  • the pressure of fuel supplied the nozzle controls the amount of movement of the valve I3 from its seat I4 and also of the needle 2
  • fuel will be atomized into the combustion chamber over a relatively wide range of fuel flow extending from the amount of fuel necessary to idle the turbine or even below such idling speed in certain instances to maximum flow of the nozzle. In some instances such fuel flow range may vary by a ratio of '70 to 1.
  • a nozzle body holder having a fuel inlet line and having a hollow portion adapted to receive a nozzle bod and having a threaded portion, a cap adapted to retain said nozzle body in said body holder and having a threaded portion adapted to engage the threaded portion on said nozzle body holder, a nozzle body unit in said I hollow portion in said nozzle body holdervadapted to be inserted or removed as a unit, a fuel chamber in said nozzle body, a fuel outlet and valve seat in said nozzle body and a fuel outlet in said cap, said fuel outlets being aligned, and a valve in said nozzle body adapted to engage said valve seat and to be opened by fuel pressure and having an integral needle portion adapted to control the passage of fuel through said fuel outlet in said cap, a spring in said fuel chamber normally retaining said valve on its seat and a second fuel chamber in said nozzle body on the side of said valve'seat opposite said spring and communicating with said' fuel inlet line in said cap

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

May 15, 1951 H. A. ACKERMAN I uo'z zm FOR GAS TURBINES Filed Nov.. 13, 1946 How/n20 ACKEEMAM' INVENTOR- Y? a Patented May 15, 195! NOZZLE FOR GAS TURBINES Howard A. Ackerman, Springfield, Mass., assignor to American Bosch Corporation, Springfield, Mass., a corporation of New York Application November 13, 1946, Serial No. 709,549
2 Claims. I
This invention relates to nozzles and has particular reference to a nozzle for gas turbines or the like and which is capable of operation over a wide range of fuel flow pressures and quantities.
An object of the present invention is to provide a new and improved nozzle for burners such as gas turbines wherein the fuel flow controls the opening of the nozzle valve and also the operation orifice area and wherein the supply of fuel to the burner will be satisfactorily controlled over a wide fuel flow range.
Another object of the invention is to provide a nozzle of the type set forth which is relatively simple and economical in construction yet efficient in operation.
Another object of the invention is to provide a nozzle of the type set forth wherein satisfactory fuel atomization will be provided from a fuel range of from low fuel flow for idling of the engine to maximum flow of the nozzle.
Other objects and advantages of the invention will be apparent from the following description taken in connection with the accompanying drawing. It will be understood that many changes may be made in the details of construction and arrangement of parts, as the preferred form of the invention has been shown by way of illustration only.
Referring more particularly to the drawing, the nozzle shown embodying the invention comprises the nozzle cap I and nozzle body holder 2 having the threaded portion 3 for securing the body holder 2 to the fuel supply line not shown. The holder body 2 also has the fuel supply opening 4 adapted to supply fuel to the interior of the nozzle.
The nozzle cap I has the peripheral flange 5 on which is positioned the peripheral flange 6 on the nozzle body 1 and said flange 6 is retained on the flange 5 by the engagement thereon of the lower end portion 8 of the hollow nut portion 9 of the nozzle body holder 2 and which is in threaded engagement with a corresponding threaded portion on the nozzle cap I.
The nozzle cap I has the orifice I through which fuel is adapted to be sprayed to the combustion chamber of the burner as hereinafter described.
The nozzle body 4 has the central opening off the fuel chamber I I adapted to receive the valve I2 which has the valve portion I3 normally engaging a seat I4 in the nozzle body I and below which seat is the fuel chamber I adapted to receive fuel through the supply groove I6 which, in turn, receives fuel through the peripheral space H between the outer surface of the nozzle body I and the inner surface of the hollow portion 9 on the holder body. I
The threaded plug I8 is adapted to be threaded into the upper end of the hollow portion of the nozzle body 1 and to retain the coil spring I9 on the stem of the valve I2. Said spring I9- has one end in engagement with the inner surface of said plug I 8 and its other end in engagement with the spring seat 20 on the valve I2 and surrounds the stem thereof. The valve has the needle projection 2I which extends through the chamber I5 and is then in relatively close flt with the nozzle body I and the lower end of said needle 2| is adapted to normally close the spray orifice II).
The lower surface of the nozzle body I is provided with the peripheral supply groove 22 which is connected by a plurality of slots 23 to thereby supply fuel to the orifice Ill. The slots 23 may be of any suitable number and may be so arranged as to provide turbulence to the fuel.
In operation fuel enters the nozzle body 2 through the pipe line connected to the threaded connection 3 and then through the passageway 4 to the space between the members 9 and I! from which it passes through the passageway I6 to the chamber I5. The pressure of such fuel then raises said valve I3 from its seat I4 against the action of the spring I9 whereupon said fuel passes into the chamber II and then through the passageway 24 to the peripheral groove 22 from which it passes through the slots 23 to the orifice ID from which it is sprayed into the burner or combustion chamber. The pressure of the fuel against the valve I3 which raises said valve from its seat I4 also lifts the needle 2| allowing the passage of fuel through the orifice I0.
It will be noted that with the present construction the pressure of fuel supplied the nozzle controls the amount of movement of the valve I3 from its seat I4 and also of the needle 2| out of the orifice I0 and, therefore, by controlling such fuel pressure it is possible to control the quantity of fuel supplied the combustion chamber. It will also be noted that with this construction fuel will be atomized into the combustion chamber over a relatively wide range of fuel flow extending from the amount of fuel necessary to idle the turbine or even below such idling speed in certain instances to maximum flow of the nozzle. In some instances such fuel flow range may vary by a ratio of '70 to 1.
It will also be understood that by controlling the pressure of the spring I 9, the amount of pressure required to lift the valve I3 from its seat l4 may be controlled whereby it is possible to control the pressure necessary to lift the valve and to start delivery of fuel to the turbine.
From the foregoing it will be seen that I have provided simple, efficient and economical means for obtaining all of the objects and advantages of the invention.
Having described my invention, I claim:
1. In a device of the character described, a nozzle body holder having a fuel inlet line and having a hollow portion adapted to receive a nozzle bod and having a threaded portion, a cap adapted to retain said nozzle body in said body holder and having a threaded portion adapted to engage the threaded portion on said nozzle body holder, a nozzle body unit in said I hollow portion in said nozzle body holdervadapted to be inserted or removed as a unit, a fuel chamber in said nozzle body, a fuel outlet and valve seat in said nozzle body and a fuel outlet in said cap, said fuel outlets being aligned, and a valve in said nozzle body adapted to engage said valve seat and to be opened by fuel pressure and having an integral needle portion adapted to control the passage of fuel through said fuel outlet in said cap, a spring in said fuel chamber normally retaining said valve on its seat and a second fuel chamber in said nozzle body on the side of said valve'seat opposite said spring and communicating with said' fuel inlet line in said nozzle body holderwhereby pressure of fuel from having a hollow portion adapted to receive a nozzle body and having a threaded portion, a cap adapted to retain said nozzle body in said body holder and having a threaded portion adapted to engage the threaded portion on said nozzle body holder, a nozzle body unit in said hollow portion in said nozzle body holder adapted to be inserted or removed as a unit, a fuel chamber in said nozzle body, a fuel outlet and valve seat in said nozzle body and a fuel outlet in said cap, said fuel outlets being aligned, and a valve in said nozzle body adapted to engage said valve seat and to be opened by fuel pressure and having an integral needle portion adapted to control thepassage of fuel through said fuel outlet in said cap, a spring in said fuel chamber normally retaining said valve on its seat and a second fuel chamber in said nozzle body on the side'of said valve seat opposite said spring and communicating with said fuel inlet line in said nozzle body holder whereby pressure of fuel from said fuel inlet line will open said valve against REFERENCES C ITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number 7 Name Date 2,297,487 LOrange Sept. 29, 1942 FOREIGN PATENTS Number 1 Country Date 309,835 Great Britain Apr. 8, 1930 499,937
Germany June 14, 1930
US709549A 1946-11-13 1946-11-13 Nozzle for gas turbines Expired - Lifetime US2552658A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3400440A (en) * 1964-03-18 1968-09-10 Lavette Engineering & Mfg Co Method of making and reconditioning ball valves
US4006591A (en) * 1975-08-11 1977-02-08 Faith Industries, Inc. Jet reaction turbine with rotating combustor for burning slurry fuels
US5176175A (en) * 1989-03-29 1993-01-05 Cooper Industries, Inc. Valve assembly
US20080066720A1 (en) * 2006-09-14 2008-03-20 James Scott Piper Gas turbine fuel injector with a removable pilot assembly
US20090107147A1 (en) * 2007-10-26 2009-04-30 James Scott Piper Gas turbine fuel injector with removable pilot liquid tube
US8028512B2 (en) 2007-11-28 2011-10-04 Solar Turbines Inc. Active combustion control for a turbine engine

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB309835A (en) * 1928-04-13 1930-04-08 Motorenfabrik Deutz Ag Improvements in or relating to cooled nozzles for fuel valves in internal combustionengines
DE499937C (en) * 1926-09-30 1930-06-14 Prosper L Orange Dipl Ing Fluid-controlled fuel injector
US2297487A (en) * 1938-09-06 1942-09-29 Rudolf L Orange Injector for internal combustion engines

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE499937C (en) * 1926-09-30 1930-06-14 Prosper L Orange Dipl Ing Fluid-controlled fuel injector
GB309835A (en) * 1928-04-13 1930-04-08 Motorenfabrik Deutz Ag Improvements in or relating to cooled nozzles for fuel valves in internal combustionengines
US2297487A (en) * 1938-09-06 1942-09-29 Rudolf L Orange Injector for internal combustion engines

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3400440A (en) * 1964-03-18 1968-09-10 Lavette Engineering & Mfg Co Method of making and reconditioning ball valves
US4006591A (en) * 1975-08-11 1977-02-08 Faith Industries, Inc. Jet reaction turbine with rotating combustor for burning slurry fuels
US5176175A (en) * 1989-03-29 1993-01-05 Cooper Industries, Inc. Valve assembly
US20080066720A1 (en) * 2006-09-14 2008-03-20 James Scott Piper Gas turbine fuel injector with a removable pilot assembly
US8166763B2 (en) 2006-09-14 2012-05-01 Solar Turbines Inc. Gas turbine fuel injector with a removable pilot assembly
US20090107147A1 (en) * 2007-10-26 2009-04-30 James Scott Piper Gas turbine fuel injector with removable pilot liquid tube
US8286433B2 (en) 2007-10-26 2012-10-16 Solar Turbines Inc. Gas turbine fuel injector with removable pilot liquid tube
US8028512B2 (en) 2007-11-28 2011-10-04 Solar Turbines Inc. Active combustion control for a turbine engine

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