US2729060A - Means for providing working fluid for a fluid-operable starter motor for a prime mover - Google Patents

Means for providing working fluid for a fluid-operable starter motor for a prime mover Download PDF

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US2729060A
US2729060A US293635A US29363552A US2729060A US 2729060 A US2729060 A US 2729060A US 293635 A US293635 A US 293635A US 29363552 A US29363552 A US 29363552A US 2729060 A US2729060 A US 2729060A
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fuel
starter motor
flame tube
fluid
chamber
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US293635A
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Allen Sidney
Morris A Stokes
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Armstrong Siddeley Motors Ltd
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Armstrong Siddeley Motors Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27Fluid drives

Definitions

  • This invention relates to means for providing working fluid for use in a fluid-operable starter motor for a prime mover-particularly for a gas turbine engine, though the invention is not limited in this respect.
  • the starter motor may be of the vane type, or, alternatively, a gaseous fluid turbine.
  • the main object of the invention is to provide asimple supply and combustion system, for the starter motor, which does not require the use of any fuel pump or atomising spray devices or special vaporizing means, and which can, if desired, utilize as fuel the fuel of the prime mover when this is one operating on liquid fuel.
  • the means for supplying working fluid for a fiuid-operable starter motor, includes a source of compressed air the delivery from which is controlled by a main valve, a source of liquid fuel the delivery from which is effected by the compressed air when the main valve is opened, and a combustion chamber in V which the fuel is burnt in the air, the products of combustion being passed to the starter motor as the working fluid.
  • the main valve is a pneumatically-operated one, the operating pressure being obtained from the source of compressed air when a solenoid operated valve is opened, which is the first step to be taken when the starter motor is to be operated.
  • Figure 2 is a sectional elevation to an enlarged scale of the combustion chamber of Figure l, the section being on the line 2-2 of Figure 3;
  • Figures 3 and 4 are cross sections on the lines 33 and 4-4 respectively of Figure 2;
  • Figure 5 is a fragmentary view, in sectional elevation, showing a fragment of the combustion chamber of Figure 2 but with the igniter plug in a different position.
  • the combustion chamber 11 includes an outer casing 12 having a closed end 13 to which is rigidly attached, with annular clearance from the casing wall, the closed end 15 of a cylindrical flame tube1'6 the opposite end 17. of which is open and slidably mounted in a reduced bore 18 of the casing v12 or of a part 19 attached thereto-and adapted for connection in any appropriate manner to the inlet 200i the starter motor 21.
  • the closed end 15 of the flame tube 16 is formed with a co-axial cylindrical chamber 23, hereinat'ter called the swirl chamber, of smaller diameter than that of the flame tube.
  • One end of the swirl chamber is open to the interior of the flame tube through a sharpedged aperture 25 of smaller diameter than the swirl chamber.
  • the swirl chamber 23 is connected with the annular chamber 27 formed between the flame tube 16 and outer casing 12 by means of at least one relatively-smallmediate position this tangential passage 28 communicates with a transverse passage 30 provided with a fuel metering orifice 31 which is preferably formed in the nose of a fuel supply union 31a which has a threaded engagement in the passage 30 and can also be used for attaching the flame tube to the closed end of the outer casing, as shown by Figure 2.
  • a fuel metering orifice 31 which is preferably formed in the nose of a fuel supply union 31a which has a threaded engagement in the passage 30 and can also be used for attaching the flame tube to the closed end of the outer casing, as shown by Figure 2.
  • the outer casing is provided with means for putting the annular chamber 27 into communication with a source of compressed air (for example, with an appropriate reducing valve means 34 connected to compressed air storage bottles 35) when the main valve 36 is open.
  • the flame tube wall has at least one ring of holes 38 radially or tangentially disposed in it for placing the interior of the flame tube 'in communication with the annular chamber 27, and when there are two or more tangentially disposed rings of holes, the holes in each succeeding ring may be of opposite sense (tangentially) to those in the preceding ring, as indicated by arrows 39 in Figure 4.
  • the diametrically-opposite points 33 of the outer casing are shown as being connected to pipes 40 merging into a common passage 41 connected to the main valve 36, this being a pneumatic valve which is closed when the starter motor is not being operated and is opened by air pressure from a bleed along a pipe 43, from the main supply, controlled by an e1ectrically-operated valve 44.
  • the switch 46 for the circuit of this valve 44 may also be arranged to complete a circuit through a spark generator 48 for an igniter plug 47. This may be co-axially mounted in the closed end of the outer casing to communicate with the swirl chamber. Alternatively, as indicated by Figure 5, it may extend through the outer casing 12 and annular chamber 27 into the flame tube 16 near the closed end thereof.
  • Liquid fuel in a closed fuel reservoir 49 is connected at the top by a pipe 50 with the common air passage 41 and at its lower end by a pipe 51 to the fuel metering orifice union or unions.
  • This reservoir may be supplied from the main fuel tank of the prime mover and can be automatically replenished as required in any preferred manner.
  • the switch 46 is actuated to open the solenoid valve 44, and thus the pneumatic valve 36, and at the same time, or by a separate switch, the igniter plug 47 is brought into operation. Compressed air is therefore supplied to the annular chamber 27, a portion of this air being fed through the tangential passages 28 communicating with the swirl chamber 23. Due to the pressure drop in the passages 28 and the pressure applied by the pipe 50 to the fuel in the reservoir 43, fuel is delivered through the metered orifices 31 into the high velocity air stream passing through the tangential passages which acts to atomise the fuel on its way to the swirl chamber, where intimate mixing takes place in the vortex so formed. As the rich mixture in this vortex passes into the flame tube the sharp-edged aperture 25 acts further to atomise the fuel particles in the mixture and prevent dribble.
  • Means for providing working fluid for use in a fluid-operable starter motor including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compressed air, the latter being connected to the source of liquid fuel so that the delivery of fuel is effected by the compressed air when the main valve is opened, the fuel is delivered under the pressure of the air and the source of compressed air can supply a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing and having a closed end rigidly attached thereto at said one end, the opposite end of said casing having a reduced bore in which the adjacent end of said flame tube is mounted, the compressed air being supplied to the annular chamber between said casing and said flame tube and being supplied to said flame tube through at least one ring of holes provided therein, said flame tube having at its closed end a cylindrical chamber communicating with said annular chamber by at least one relatively-small
  • Means for providing working fluid for use in a fluid-operable starter motor including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compressed air, and a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing to leave an annular chamber therebetween, said flame tube being cloesd at the end adjacent said one end of said casing, means for supplying the compressed air to said annular chamber and thence to said flame tube through at least one ring of holes provided therein, said flame tube having at its.
  • a cylindrical chamber communicating with said annular chamber by at least one relatively-small-diameter passage which is disposed tangentially to the bore of said cylindrical chamber and through which the air will pass at high velocity for delivering to said cylindrical chamber with a whirling motion, and means for supplying metered fuel to a transverse passage in the closed end of said flame, tube leading to said tangential passage.
  • Means for providing working fluid for use in a fluidoperable starter motor including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compressed air, and a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing to leave an annular chamber therebetween, said flame tube having a closed end rigidly attached to the closed end of said casing, the main valve connected to said annular chamber, said flame tube having along its length at least one ring of holes provided therein, and said flame tube having at its closed end a coaxial cylindrical chamber communicating with said annular chamber by at least one relatively-5mall-diameter passage which is disposed tangentially to the bore of said cylindrical chamber and through which the air will pass at high velocity for delivering to said cylindrical chamber with a whirling motion, the closed ends of said casing and flame tube also having through them a transverse
  • Means for providing working fluid for use in a fluidoperable starter motor including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compresed air, and a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing to leave an anular chamber therebetween, said flame tube having its closed end rigidly attached to the closed end of said casing, said main valve being connected to said annular chamber, said flame tube having along its length at least one ring of holes provided therein, and said flame tube having at its closed end a coaxial cylindrical chamber communicating with said annular chamber by at least one relatively-small-diameter passage which is disposed tangentially to the bore of said cylindrical chamber and through which the air will pass at high velocity for delivering to said cylindrical chamber with a whirling motion, said cylindrical chamber being of smaller diameter than said flame tube and cornmunieating with

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  • 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)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

Jan. 3, 1956 s. ALLEN ET AL 2,729,060
MEANS FOR PROVIDING WORKING FLUID FOR A FLUID-OPERABLE STARTER MOTOR FOR A PRIME MOVER 1 2 Sheets-Sheet 1 Filed June 14, 1952 VIM J3 M/VHZIMRS 5. AME/V 4 Jan. 3, 1956 s. ALLEN ET AL 2,729,060
WORKING FLUID MEANS FOR PROVID FOR A FLUID-OPERABLE START MOTOR FOR A PRIME MOVER Filed June 14, 1952 2 Sheets-Sheet 2 {fill [M7088 5.14LLHV i M 14. STU/{ES United States Patent MEANS FOR PROVIDING WORKING FLUID FOR A FLUID-OPERABLE STARTER MOTOR FOR A PRIME MOVER Sidney Allen and Morris A. Stokes, Coventry, England,
assignors to Armstrong Siddeley Motors Limited, Coventry, England Application June 14, 1952, Serial No. 293,635
Claims priority, application Great Britain July 7, 1951 4 Claims. (Cl. 6039.14)
This invention relates to means for providing working fluid for use in a fluid-operable starter motor for a prime mover-particularly for a gas turbine engine, though the invention is not limited in this respect. The starter motor may be of the vane type, or, alternatively, a gaseous fluid turbine.
The main object of the invention is to provide asimple supply and combustion system, for the starter motor, which does not require the use of any fuel pump or atomising spray devices or special vaporizing means, and which can, if desired, utilize as fuel the fuel of the prime mover when this is one operating on liquid fuel.
According to the invention, the means for supplying working fluid, for a fiuid-operable starter motor, includes a source of compressed air the delivery from which is controlled by a main valve, a source of liquid fuel the delivery from which is effected by the compressed air when the main valve is opened, and a combustion chamber in V which the fuel is burnt in the air, the products of combustion being passed to the starter motor as the working fluid.
Preferably the main valve is a pneumatically-operated one, the operating pressure being obtained from the source of compressed air when a solenoid operated valve is opened, which is the first step to be taken when the starter motor is to be operated.
In the accompanying drawings- Figure 1 is a diagram of one form of apparatus accord ing to the invention;
Figure 2 is a sectional elevation to an enlarged scale of the combustion chamber of Figure l, the section being on the line 2-2 of Figure 3;
Figures 3 and 4 are cross sections on the lines 33 and 4-4 respectively of Figure 2; and
Figure 5 is a fragmentary view, in sectional elevation, showing a fragment of the combustion chamber of Figure 2 but with the igniter plug in a different position.
In the construction of Figures 1 to 4, the combustion chamber 11 includes an outer casing 12 having a closed end 13 to which is rigidly attached, with annular clearance from the casing wall, the closed end 15 of a cylindrical flame tube1'6 the opposite end 17. of which is open and slidably mounted in a reduced bore 18 of the casing v12 or of a part 19 attached thereto-and adapted for connection in any appropriate manner to the inlet 200i the starter motor 21. The closed end 15 of the flame tube 16 is formed with a co-axial cylindrical chamber 23, hereinat'ter called the swirl chamber, of smaller diameter than that of the flame tube. One end of the swirl chamber is open to the interior of the flame tube through a sharpedged aperture 25 of smaller diameter than the swirl chamber.
The swirl chamber 23 is connected with the annular chamber 27 formed between the flame tube 16 and outer casing 12 by means of at least one relatively-smallmediate position this tangential passage 28 communicates with a transverse passage 30 provided with a fuel metering orifice 31 which is preferably formed in the nose of a fuel supply union 31a which has a threaded engagement in the passage 30 and can also be used for attaching the flame tube to the closed end of the outer casing, as shown by Figure 2. Preferably there are two or more such tangential passages and fuel metering orifices.
At diametrically opposite points 33 the outer casing is provided with means for putting the annular chamber 27 into communication with a source of compressed air (for example, with an appropriate reducing valve means 34 connected to compressed air storage bottles 35) when the main valve 36 is open. The flame tube wall has at least one ring of holes 38 radially or tangentially disposed in it for placing the interior of the flame tube 'in communication with the annular chamber 27, and when there are two or more tangentially disposed rings of holes, the holes in each succeeding ring may be of opposite sense (tangentially) to those in the preceding ring, as indicated by arrows 39 in Figure 4.
The number of such holes in a ring and the number of such rings axially spaced along the length of the flame tube would be in accordance with the combustion requirements depending on whether the starter motor 21 which has to be operated requires a working fluid of relatively high or low temperature.
The diametrically-opposite points 33 of the outer casing are shown as being connected to pipes 40 merging into a common passage 41 connected to the main valve 36, this being a pneumatic valve which is closed when the starter motor is not being operated and is opened by air pressure from a bleed along a pipe 43, from the main supply, controlled by an e1ectrically-operated valve 44. The switch 46 for the circuit of this valve 44 may also be arranged to complete a circuit through a spark generator 48 for an igniter plug 47. This may be co-axially mounted in the closed end of the outer casing to communicate with the swirl chamber. Alternatively, as indicated by Figure 5, it may extend through the outer casing 12 and annular chamber 27 into the flame tube 16 near the closed end thereof.
Liquid fuel in a closed fuel reservoir 49 is connected at the top by a pipe 50 with the common air passage 41 and at its lower end by a pipe 51 to the fuel metering orifice union or unions. This reservoir may be supplied from the main fuel tank of the prime mover and can be automatically replenished as required in any preferred manner.
To put the combustion system into operation, the switch 46 is actuated to open the solenoid valve 44, and thus the pneumatic valve 36, and at the same time, or by a separate switch, the igniter plug 47 is brought into operation. Compressed air is therefore supplied to the annular chamber 27, a portion of this air being fed through the tangential passages 28 communicating with the swirl chamber 23. Due to the pressure drop in the passages 28 and the pressure applied by the pipe 50 to the fuel in the reservoir 43, fuel is delivered through the metered orifices 31 into the high velocity air stream passing through the tangential passages which acts to atomise the fuel on its way to the swirl chamber, where intimate mixing takes place in the vortex so formed. As the rich mixture in this vortex passes into the flame tube the sharp-edged aperture 25 acts further to atomise the fuel particles in the mixture and prevent dribble.
Combustion takes place in the flame tube, air for this purpose being led from the annular chamber through it will be understood that control of the amount of fuel depends on the size of the metering orifices 31 which can be chosen to suit the particular application. Also, the supply of compressed air into the annular chamber 27 need not be as described, as, in some cases, a single feed thereto may be sufficient.
What we claim as our invention and desire to secure by Letters Patent of the United States is:
1. Means for providing working fluid for use in a fluid-operable starter motor, including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compressed air, the latter being connected to the source of liquid fuel so that the delivery of fuel is effected by the compressed air when the main valve is opened, the fuel is delivered under the pressure of the air and the source of compressed air can supply a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing and having a closed end rigidly attached thereto at said one end, the opposite end of said casing having a reduced bore in which the adjacent end of said flame tube is mounted, the compressed air being supplied to the annular chamber between said casing and said flame tube and being supplied to said flame tube through at least one ring of holes provided therein, said flame tube having at its closed end a cylindrical chamber communicating with said annular chamber by at least one relatively-small-diameter passage disposed tangentially to the bore of said cylindrical chamber whereby air will pass at high velocity through said passage and enter said cylindrical chamber with a whirling motion, and the closed ends of said casing and flame tube carrying a fuel metering device disposed in a transverse passage leading to said tangential passage whereby the high velocity air passing through the latter will eject and atomise fuel from said device for burning in said combustion chamber.
2. Means for providing working fluid for use in a fluid-operable starter motor, including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compressed air, and a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing to leave an annular chamber therebetween, said flame tube being cloesd at the end adjacent said one end of said casing, means for supplying the compressed air to said annular chamber and thence to said flame tube through at least one ring of holes provided therein, said flame tube having at its. closed end a cylindrical chamber communicating with said annular chamber by at least one relatively-small-diameter passage which is disposed tangentially to the bore of said cylindrical chamber and through which the air will pass at high velocity for delivering to said cylindrical chamber with a whirling motion, and means for supplying metered fuel to a transverse passage in the closed end of said flame, tube leading to said tangential passage.
3. Means for providing working fluid for use in a fluidoperable starter motor, including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compressed air, and a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing to leave an annular chamber therebetween, said flame tube having a closed end rigidly attached to the closed end of said casing, the main valve connected to said annular chamber, said flame tube having along its length at least one ring of holes provided therein, and said flame tube having at its closed end a coaxial cylindrical chamber communicating with said annular chamber by at least one relatively-5mall-diameter passage which is disposed tangentially to the bore of said cylindrical chamber and through which the air will pass at high velocity for delivering to said cylindrical chamber with a whirling motion, the closed ends of said casing and flame tube also having through them a transverse passage leading to said tangential passage and connected to the source of fuel, and a metered orifice in said transverse passage whereby the high velocity air passing through said tangential passage will eject and atomisc fuel from said orifice for burning in said combustion chamber.
4. Means for providing working fluid for use in a fluidoperable starter motor, including a source of compressed air, a source of liquid fuel, a main valve controlling the delivery from the source of compresed air, and a combustion chamber in which the fuel is burnt in the compressed air and which delivers the products of combustion to the starter motor as the working fluid, said combustion chamber including an outer casing having one end closed, a flame tube having annular clearance from said casing to leave an anular chamber therebetween, said flame tube having its closed end rigidly attached to the closed end of said casing, said main valve being connected to said annular chamber, said flame tube having along its length at least one ring of holes provided therein, and said flame tube having at its closed end a coaxial cylindrical chamber communicating with said annular chamber by at least one relatively-small-diameter passage which is disposed tangentially to the bore of said cylindrical chamber and through which the air will pass at high velocity for delivering to said cylindrical chamber with a whirling motion, said cylindrical chamber being of smaller diameter than said flame tube and cornmunieating with the latter through a sharp-edged aperture of still less diameter, and the closed ends of said casing and flame tube carrying a fuel metering device connected to the source of fuel and disposed in a transverse passage leading to said tangential passage.
References Cited in the file of this patent UNITED STATES PATENTS 710,130 Weiss Sept. 30, 1902 943,833 Leavitt Dec. 21, 1909 1,451,063 Anthony Apr. 10, 1923 2,397,834 Bowman Apr. 2, 1946 2,595,759 Buckland et a1 May 1, 1952 2,602,290 Goddard July 8, 1952
US293635A 1951-07-07 1952-06-14 Means for providing working fluid for a fluid-operable starter motor for a prime mover Expired - Lifetime US2729060A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3903692A (en) * 1972-07-24 1975-09-09 Us Army Hot gas generator
US4777793A (en) * 1986-04-14 1988-10-18 Allied-Signal Inc. Emergency power unit

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2902823A (en) * 1956-11-21 1959-09-08 Clarence E Wagner Design for a stainless steel or aluminum gas generator wall spraying system for combustion chamber

Citations (6)

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US710130A (en) * 1899-05-09 1902-09-30 Carl W Weiss Regenerator-burner.
US943833A (en) * 1907-08-27 1909-12-21 Bliss E W Co Air-heater for automobile torpedoes.
US1451063A (en) * 1923-04-10 Burner
US2397834A (en) * 1942-06-08 1946-04-02 Mabel J Bowman Rocket motor
US2595759A (en) * 1948-11-30 1952-05-06 Gen Electric Atomizing nozzle for spraying viscous liquids
US2602290A (en) * 1947-05-07 1952-07-08 Daniel And Florence Guggenheim Rotational fuel feed for combustion chambers

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US2110209A (en) * 1934-10-13 1938-03-08 Baker Perkins Co Inc Furnace
GB578764A (en) * 1942-09-08 1946-07-11 Rover Co Ltd Improvements relating to combustion chambers for internal combustion turbines
FR917884A (en) * 1943-04-01 1947-01-23 Power Jets Res & Dev Ltd Improvements to combustion devices
GB616695A (en) * 1944-04-21 1949-01-26 British Thomson Houston Co Ltd Improvements in and relating to gas turbine power plants
GB619036A (en) * 1944-10-09 1949-03-02 Bendix Aviat Corp Improvements in or relating to combustion gas generators for gas turbines and like power plants
FR928867A (en) * 1945-05-16 1947-12-10 Bendix Aviat Corp Burners improvements
CH269303A (en) * 1948-11-06 1950-06-30 Oerlikon Maschf Process for atomizing liquid fuel by means of air in combustion chambers, in particular those of gas turbine systems.
US2551276A (en) * 1949-01-22 1951-05-01 Gen Electric Dual vortex liquid spray nozzle

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Publication number Priority date Publication date Assignee Title
US1451063A (en) * 1923-04-10 Burner
US710130A (en) * 1899-05-09 1902-09-30 Carl W Weiss Regenerator-burner.
US943833A (en) * 1907-08-27 1909-12-21 Bliss E W Co Air-heater for automobile torpedoes.
US2397834A (en) * 1942-06-08 1946-04-02 Mabel J Bowman Rocket motor
US2602290A (en) * 1947-05-07 1952-07-08 Daniel And Florence Guggenheim Rotational fuel feed for combustion chambers
US2595759A (en) * 1948-11-30 1952-05-06 Gen Electric Atomizing nozzle for spraying viscous liquids

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3903692A (en) * 1972-07-24 1975-09-09 Us Army Hot gas generator
US4777793A (en) * 1986-04-14 1988-10-18 Allied-Signal Inc. Emergency power unit

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GB708548A (en) 1954-05-05
CH310327A (en) 1955-10-15
DE942603C (en) 1956-05-03

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