US1879186A - Apparatus for igniting liquid fuel - Google Patents

Apparatus for igniting liquid fuel Download PDF

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US1879186A
US1879186A US492268A US49226830A US1879186A US 1879186 A US1879186 A US 1879186A US 492268 A US492268 A US 492268A US 49226830 A US49226830 A US 49226830A US 1879186 A US1879186 A US 1879186A
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ignition
chamber
flame
fuel
combustion
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US492268A
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Robert H Goddard
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B9/00Engines characterised by other types of ignition
    • F02B9/06Engines characterised by other types of ignition with non-timed positive ignition, e.g. with hot-spots
    • F02B9/08Engines characterised by other types of ignition with non-timed positive ignition, e.g. with hot-spots with incandescent chambers
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00Power plants
    • Y10S60/915Collection of goddard patents

Definitions

  • This invention relates to combustion apparatus in which liquid fuel is used and more particularly to apparatus in which a liquid oxidizing agent such as liquid air or oxygen is also used.
  • a liquid oxidizing agent such as liquid air or oxygen
  • Such ignition is preferably provided in the form of a flame directed into the combustion chamber which contains the mixture of fuel and oxidizin agent.
  • a further object is to provide improved means for maintaining an idle fiame or hot point for lighting the igniting flame whenever the latter is desired for use.v
  • I also provide for a safe and predetermined order of operation of the several parts of the ap aratus, to the end that danger may be eildctively avoided.
  • My invention further relates to ⁇ arrangements and combinations of parts which will be hereinafter described and more particularly pointed out in the appended claims.
  • FIG. 1 is a side elevation of a portion of a y combustion chamber having my improver. ments applied thereto; 35
  • Fig. 2 is a' detail view, looking in the direction of the arrow 2 in Fig. 1;
  • Fig. 3 is an enlarged sectional view of the ignition chamber
  • Valves 13 and 14 are provided in the pipes 11 and 12, which valves are connected by links 15 to a manually operated control lever 16 mounted upon a fixed pivot stud 17.
  • a spring 18 normally holds the lever 16 in the inoperative position shown in full lines in Fig. 1, in which the valves 13 and .14 are closed.
  • My improved ignition chamber is referably formed in two parts 20 and 21 ig. 3) separated by a suitable acking and secured together by clamping bolts 24.
  • the member 2O comprises inner walls 20* and outer walls 20b separated by a semi-spherical passage or recess
  • the member 21 comprises inner and outer walls 21* and 21" separated by an intervening space or recess 27.
  • a refractory lining is preferaby provided .for the casing members 20 and 21 and a plurality of small openings 31 are formed in the inner walls 20 and 21 and in the refractory lining 30. It will be noted that alll of said openings 31 are directed toward a common point, which is substantiall at the center of the spherical ignition cham er.
  • a liquid or gaseous fuel is conducted through a pipe 35 to one of the semi-spherical recesses and preferably to the upper recess 25.
  • An oxidizing agent such as liquid air or liquid oxygen is conducted to the other recess, such as the lower recess 27, through a pipe 36, which may be rovided with an insu ating coating 37 to re uce the rate of evaporation of the low temperature oxidizin agent.
  • More or less of the outer surface o the wall 21b of the chamber member 21 may also be covered with an insulating covering 38 for the same purpose.'
  • the outer wall of the member 20 is preferably provided With flanges 40 through which heat may be dissipated, and more or less of the surface of the member 21 may be similarly provided with flanges 41, these flanges being desirable when a gaseous oxidizing agent is used.
  • Strainers of fine wire gauze, shown dotted at 35 and 36, (Fig. 1) are preferably provided in the pipes 35 and 36, to prevent clogging of the small holes 31.
  • the mixture of combustible and oxidizing materials thus produced at the center, point of the ignition chamber maybe readily i ited in any convenient manner, as by a spar -plug 44.
  • the mixture When thus ignited, the mixture provides an intensely hot idle flame which is ositioned substantially at the center of the ignition chamber and Aspaced from the walls thereof.
  • streams of fuel and oxidizing agent are admitted to the ignition chamber through pipes 50 and51 one of which may beheat-insulated as indicated at 52.
  • the streams of liquid or gaseous materials flowing from these pipes converge and pass through the idle flame or hot-point at the middle of the ignition chamber and after beling thus ignited are directed in the form of a long and intensely hot flame through the opening 45 into the combustion chamber.
  • the hot-point or idle ilame shall be started before the fuel and oxidizing agent are admitted to the ignition chamber through the pipes 50 and 51 to produce the long igmtion flame. It is also necessary that th1s long flame be produced before any mixture of fuel and oxidizing agent is admitted to the combustion chamber 10.
  • the delivery of fuel and oxidizing agent to the pipes 50 and 51 which produce the long flame is controlled by spring plungers 53 and 54 (Fig. 2) which are normally held vdown by acam block 55.
  • the block 55 is mounted at the lower end of a rod 56 and connected at 57 ig. l) to a hand lever 58 pivoted at 59 on the lever 16 previously described.
  • a spring 60 holds the block 55 normally in the lowered position of Figs. 1 and 2.
  • the ring ⁇ 77 is insulated at its sides by mica or other suitable insulating material, as indicated at 80 in Fig. 3, and is also insulated around the greater part of its periphery by an insulating layer 81 (Fig. 4), which, however, is interrupted for a substantial distance at a point o posite the point of attachment of the wire 5.
  • Strips 82 of a more expansive metal are secured to the inner faces of the side portions of the ring 77.
  • the ring 77 and parts 82 assume the circular position indicated in Fig. 4, with the ring 77 out of contact with the casing of the ignition chamber.
  • the parts 77 and 82 become heated an their unequal expansion elongates the ring' 77, causing it to contact with the casing of the ignition chamber, thus 'completing the circuit and energizing the solenoid coil 71, which in turn withdraws the plunger 70 and permits manual operation of the control lever 16.
  • the beveled outer face o f the plunger 70 permits the lever to be restored to inop-l erative position at any time.
  • Apparatus for igniting liquid or gaseous fuels in a combustion chamber which comprises a substantially spherical ignition chamber associated with said combustion chamber and connected thereto by a restricted but unobstructed passage, means to introduce jets of combustible and oxidizing gases to said ignition chamber along a plurality of angularly disposed radial paths, whereby a pilot flame is maintained substantially at the center of said spherical chamber, and means to direct gases to form an ignition iiame diametrically through said ignition chamber and through said pilot flame and into said combustion chamber through said restricted opening.
  • an ignition chamber comprising a two part casing, each part being formed with a recess, means to deliver fuel to one of said recesses, means to deliver an oxidizing agent to the other recess, and means to feed said materials in a plurality of jets from said recesses to a common point within said casing.
  • a substantially spherical ignition chamber formed of hollow sections having concentric inner and outer walls, each of said sections having also a plurality of circumferential cooling flanges formed on the outer face thereof and the outer edges of said anges being disposed in parallel planes.
  • thermoelectric device at the opening between the ignition and combustion chambers controls the admission of fuel and oxidizing agent to produce the ignition flame, and in which means is provided for preventing the admission ofr fuel and oxidizing agent to the combustion chamber until after said gases are admitted to the ignition chamber.
  • an ignition chamber comprising a casing, formed with a. plurality of recesses, means to deliver fuel to one of said recesses, means to deliver an oxidizing agent to the other recess, and means to feed said materials in a plurality of jets from said recesses to a common point within said casing.
  • a combustion chamber In a combustion apparatus, a combustion chamber, an ignition chamber having a restricted communication with said combus-

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lighters Containing Fuel (AREA)

Description

sept.27, 1932. RHGODDARD l1,879,186
APPARATUS FOR IGNITING LIQUID FUEL SePt- 27, 1932. I R. H. GODDARD 1,879,186
APPARATUS FOR IGNITING LIQUID FUEL Filed Oct. 30, 1950 2 Sheets-Sheet 2 JMYM Patented Sept. 27, 1932 PATENT Vor-Flca ROBERT H. GODDABD, I' WORCESTER, MASSACHUSETTS APPARATUS FOB IGNITING LIQUID FUEL Application illed October 30, 1930. Serial No. 492,268.
This invention relates to combustion apparatus in which liquid fuel is used and more particularly to apparatus in which a liquid oxidizing agent such as liquid air or oxygen is also used. .Such combinations of liquid fuel and liquid oxidizing a ents are highly explosive and dangerous i not promptly and thoroughly ignited as soon as they are introduced into a combustion chamber. Such ignition is preferably provided in the form of a flame directed into the combustion chamber which contains the mixture of fuel and oxidizin agent.
It is t e general object of my invention to provide improved means for supplying an effective igniting flame for a combustion chamber.
A further object is to provide improved means for maintaining an idle fiame or hot point for lighting the igniting flame whenever the latter is desired for use.v
I also provide for a safe and predetermined order of operation of the several parts of the ap aratus, to the end that danger may be eildctively avoided. l
My invention further relates to `arrangements and combinations of parts which will be hereinafter described and more particularly pointed out in the appended claims.
A preferred form of the invention is shown in the drawings, in which Fig. 1 is a side elevation of a portion of a y combustion chamber having my improver. ments applied thereto; 35
Fig. 2 is a' detail view, looking in the direction of the arrow 2 in Fig. 1;
Fig. 3 is an enlarged sectional view of the ignition chamber;
. uous or intermittent.
" .provided with an inlet pipe 11 for liquid fuel and an inlet pipe 12 for a liquid oxidizing agent such as liquid air or oxygen.
Valves 13 and 14 are provided in the pipes 11 and 12, which valves are connected by links 15 to a manually operated control lever 16 mounted upon a fixed pivot stud 17. A spring 18 normally holds the lever 16 in the inoperative position shown in full lines in Fig. 1, in which the valves 13 and .14 are closed. f
My improved ignition chamber is referably formed in two parts 20 and 21 ig. 3) separated by a suitable acking and secured together by clamping bolts 24. The member 2O comprises inner walls 20* and outer walls 20b separated by a semi-spherical passage or recess Similarly the member 21 comprises inner and outer walls 21* and 21" separated by an intervening space or recess 27. A refractory lining is preferaby provided .for the casing members 20 and 21 and a plurality of small openings 31 are formed in the inner walls 20 and 21 and in the refractory lining 30. It will be noted that alll of said openings 31 are directed toward a common point, which is substantiall at the center of the spherical ignition cham er.
A liquid or gaseous fuel is conducted through a pipe 35 to one of the semi-spherical recesses and preferably to the upper recess 25. An oxidizing agent such as liquid air or liquid oxygen is conducted to the other recess, such as the lower recess 27, through a pipe 36, which may be rovided with an insu ating coating 37 to re uce the rate of evaporation of the low temperature oxidizin agent. More or less of the outer surface o the wall 21b of the chamber member 21 may also be covered with an insulating covering 38 for the same purpose.'
The outer wall of the member 20 is preferably provided With flanges 40 through which heat may be dissipated, and more or less of the surface of the member 21 may be similarly provided with flanges 41, these flanges being desirable when a gaseous oxidizing agent is used. Strainers of fine wire gauze, shown dotted at 35 and 36, (Fig. 1) are preferably provided in the pipes 35 and 36, to prevent clogging of the small holes 31.
The mixture of combustible and oxidizing materials thus produced at the center, point of the ignition chamber maybe readily i ited in any convenient manner, as by a spar -plug 44. When thus ignited, the mixture provides an intensely hot idle flame which is ositioned substantially at the center of the ignition chamber and Aspaced from the walls thereof.
The gases of combustion pass through the openinnf 45 at the neck of the ignition chamber and thus enter the. combustion chamber It is desirable that the pipes 35 and 36 enter their respective casing sections at the lowest available points, so 'that any gas which maybeproduced by evaporation of the liquids therein will not back up in the pipes 35 and 36 and thus interfere with the flow of liquids to the ignition chamber.
When it is desired to operate the combustion chamber, streams of fuel and oxidizing agent are admitted to the ignition chamber through pipes 50 and51 one of which may beheat-insulated as indicated at 52. The streams of liquid or gaseous materials flowing from these pipes converge and pass through the idle flame or hot-point at the middle of the ignition chamber and after beling thus ignited are directed in the form of a long and intensely hot flame through the opening 45 into the combustion chamber.
It is necessary for safety 1n operatlon that the hot-point or idle ilame shall be started before the fuel and oxidizing agent are admitted to the ignition chamber through the pipes 50 and 51 to produce the long igmtion flame. It is also necessary that th1s long flame be produced before any mixture of fuel and oxidizing agent is admitted to the combustion chamber 10.
V In order to make certain that these operations be performed in the required order, I have provided safety devices which will now be described.
The delivery of fuel and oxidizing agent to the pipes 50 and 51 which produce the long flame is controlled by spring plungers 53 and 54 (Fig. 2) which are normally held vdown by acam block 55. The block 55 is mounted at the lower end of a rod 56 and connected at 57 ig. l) to a hand lever 58 pivoted at 59 on the lever 16 previously described. A spring 60 holds the block 55 normally in the lowered position of Figs. 1 and 2.
When the operator wishes to move the lever 16 to open the valves 1'3 and 14 which control the combustionv chamber feed pipes 11 and 12the handle 58 must be grasped and the block 55 must be raised to clear a shoulder or abutment 62 before the handle can be moved. This raising of the block 55 permits the spring plungers 53 and 54 to rise, admitting fuel and oxidizing agent to the pipes 50 and 51 respectively.
It is thus evident that the necessary materials will be fed tothe ignition chamber to start the long'flame in voperation before any fuel or oxidizing agent is delivered to the combustion chamber. v f
In order to further insure tllat the hotpoint or idle flame shall be in operation before the materials ,for the long flame vare admitted to the ignition chamber, I provide a thermostatic device for locking and releasmg the lever 16. For this purpose I provide a spring plunger 70 (Fig. 5) mounted in a soleno1d coil 71 and yieldingly pressed to. 75
extends through an insulating bushing 76 to a metal ring 77 mounted in a recess 78 surrounding the neck or opening 45 ofthe ignition chamber.
The ring` 77 is insulated at its sides by mica or other suitable insulating material, as indicated at 80 in Fig. 3, and is also insulated around the greater part of its periphery by an insulating layer 81 (Fig. 4), which, however, is interrupted for a substantial distance at a point o posite the point of attachment of the wire 5. Strips 82 of a more expansive metal are secured to the inner faces of the side portions of the ring 77.
When the ignition chamber is cool, the ring 77 and parts 82 assume the circular position indicated in Fig. 4, with the ring 77 out of contact with the casing of the ignition chamber. When the products of combustion of the idle flame flow through the openin 45, the parts 77 and 82 become heated an their unequal expansion elongates the ring' 77, causing it to contact with the casing of the ignition chamber, thus 'completing the circuit and energizing the solenoid coil 71, which in turn withdraws the plunger 70 and permits manual operation of the control lever 16. The beveled outer face o f the plunger 70 permits the lever to be restored to inop-l erative position at any time.
I have thus provided means which make it certain that the idle llame shall be lighted before the lever 16 is released, and further insuring a ilow of materials to produce the long flame before the mixture -is admitted to the combustion chamber 10.
Under some conditions, it is desirable that the admission of materials to the ignition chamber and also to the combustion chambery erative position, closing the valves 13 and 14 and depressing the spring plungers 53 and 54.*
During this closing movement, the block 55 rides up over the inclined rear face of the abutment 62 and is then released to depress the plungers 53 and 54. Y
Having thus described my invention and the advantages thereof, I do not wish to be limited to the details herein disclosed, otherwise than as set forth in the claims, but what I claim is 1. Apparatus for igniting liquid or gaseous fuels in a combustion chamber which comprises a substantially spherical ignition chamber associated with said combustion chamber and connected thereto by a restricted but unobstructed passage, means to introduce jets of combustible and oxidizing gases to said ignition chamber along a plurality of angularly disposed radial paths, whereby a pilot flame is maintained substantially at the center of said spherical chamber, and means to direct gases to form an ignition iiame diametrically through said ignition chamber and through said pilot flame and into said combustion chamber through said restricted opening.
2. The combination in ignition apparatus as set forth in claim 1, in which manual means is provided for introducingfuel to said ignition chamber and to said combustion chamber in predetermined order.
3. In a combustion apparatus, an ignition chamber comprising a two part casing, each part being formed with a recess, means to deliver fuel to one of said recesses, means to deliver an oxidizing agent to the other recess, and means to feed said materials in a plurality of jets from said recesses to a common point within said casing.
4. In a combustion apparatus, a substantially spherical ignition chamber formed of hollow sections having concentric inner and outer walls, each of said sections having also a plurality of circumferential cooling flanges formed on the outer face thereof and the outer edges of said anges being disposed in parallel planes.
5. The combination in ignition apparatus as set forth in claim 1, in which means is provided which requires the feed to the ignition flame to be opened before the feed to the combustion chamber is opened.
6. The combination in/ignition apparatus as set forth in claim 1, in which a thermostatic device at the opening between the ignition and combustion chambers controls the admission of fuel and oxidizing agent to produce the ignition flame, and in which means is provided for preventing the admission ofr fuel and oxidizing agent to the combustion chamber until after said gases are admitted to the ignition chamber.
7. In a combustion apparatus, an ignition chamber comprising a casing, formed with a. plurality of recesses, means to deliver fuel to one of said recesses, means to deliver an oxidizing agent to the other recess, and means to feed said materials in a plurality of jets from said recesses to a common point within said casing.
8. The combination in combustion apparas tus as set forth in claim 7, in which said delivery means is provided withfne strainers to prevent clogging.
9. The combination in combustion apparatus as set forth in claim 7, in which said common point is substantially spaced from the walls of the casing in all directions.
10. The combination in combustion apparatus as set forth in claim 7, in which the casing is substantially spherical, with a restricted outlet at one side thereof.
11. The combination in combustion apparatus as set forth in clainf'?, in which feed pipes for fuel and an oxidizing agent enters said recesses at the lowermost points thereof.
12. In a combustion apparatus, a combustion chamber, an ignition chamber having a restricted communication with said combus-
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Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447758A (en) * 1948-08-24 Igniting device fob combustion
US2470564A (en) * 1944-11-15 1949-05-17 Reaction Motors Inc Reaction motor control system
US2479888A (en) * 1943-07-06 1949-08-23 Reaction Motors Inc Controlling system for reaction motors
US2498263A (en) * 1947-08-23 1950-02-21 Daniel And Florence Guggenheim Ignition apparatus for combustion chambers using intermingled combustion liquids
US2500334A (en) * 1944-06-19 1950-03-14 Aerojet Engineering Corp Jet motor operable by monopropellant and method of operating it
US2523656A (en) * 1947-11-01 1950-09-26 Daniel And Florence Guggenheim Combustion apparatus comprising successive combustion chambers
US2532709A (en) * 1946-11-30 1950-12-05 Daniel And Florence Guggenheim Liquid cooled baffles between mixing and combustion chambers
US2563023A (en) * 1946-04-12 1951-08-07 Daniel And Florence Guggenheim Combustion chamber with multiple discharge nozzles
US2563022A (en) * 1944-02-12 1951-08-07 Daniel And Florence Guggenheim Fuel feeding mechanism for detonating combustion apparatus
US2563028A (en) * 1948-12-04 1951-08-07 Daniel And Florence Guggenheim Combustion apparatus comprising a combustion chamber with target type premixing extension
US2569887A (en) * 1941-11-18 1951-10-02 Daniel And Florence Guggenheim Combustion apparatus, including flame type ignition means
US2574495A (en) * 1945-05-16 1951-11-13 Jr Frank A Parker Flame igniter for jet propulsion units
US2575070A (en) * 1948-04-06 1951-11-13 William A Reed Jacketed combustion pot with fuel and air nozzle head
US2609658A (en) * 1946-05-11 1952-09-09 Daniel And Florence Guggenheim Target type combustion chamber having a closed end portion receiving conical fuel and oxidizer sprays
US2633700A (en) * 1946-04-12 1953-04-07 Daniel And Florence Guggenheim Combustion chamber for propulsion apparatus and having multiple discharge nozzles
US2651173A (en) * 1949-01-26 1953-09-08 Standard Oil Dev Co Process and apparatus for operating engines at high altitudes
US2658340A (en) * 1945-02-01 1953-11-10 Power Jets Res & Dev Ltd Apparatus for igniting fuel in fast-moving hot gas streams
US2659202A (en) * 1950-06-06 1953-11-17 Fay E Null Augmented thrust pulse jet pump or motor and method of creating augmented thrust or suction
US2686400A (en) * 1948-07-12 1954-08-17 Us Air Force Regenerative liquid fuel rocket motor
US2701445A (en) * 1950-09-08 1955-02-08 Armstrong Siddeley Motors Ltd Ignition equipment for the combustion equipment of rocket motors
US2706382A (en) * 1949-07-09 1955-04-19 Carborundum Co Devices for confinement and release of high velocity, hot gases
US2714286A (en) * 1944-07-14 1955-08-02 Aerojet General Co Liquid propellant injection system for jet motors
US2722800A (en) * 1949-02-21 1955-11-08 Rolls Royce Fuel systems for gas turbine engines or the like with main and pilot fuel injectors
US2741085A (en) * 1952-05-12 1956-04-10 Phillips Petroleum Co Safety device, including fusible member for rocket engine starting control
US2954666A (en) * 1955-08-05 1960-10-04 Jr Carl A Brownell Method and apparatus for pre-mixing rocket motor fuel
US2956403A (en) * 1951-11-29 1960-10-18 Thiokol Chemical Corp Igniter
US2972225A (en) * 1950-12-04 1961-02-21 James M Cumming Motor mechanism for missiles
US2977755A (en) * 1947-10-20 1961-04-04 Aerojet General Co Method and means for initiating the decomposition of propellant in a rocket motor
US3738333A (en) * 1970-07-17 1973-06-12 Volkewagenwerk Ag Cylinder arrangement having a precombustion chamber for combustion engines

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447758A (en) * 1948-08-24 Igniting device fob combustion
US2569887A (en) * 1941-11-18 1951-10-02 Daniel And Florence Guggenheim Combustion apparatus, including flame type ignition means
US2479888A (en) * 1943-07-06 1949-08-23 Reaction Motors Inc Controlling system for reaction motors
US2563022A (en) * 1944-02-12 1951-08-07 Daniel And Florence Guggenheim Fuel feeding mechanism for detonating combustion apparatus
US2500334A (en) * 1944-06-19 1950-03-14 Aerojet Engineering Corp Jet motor operable by monopropellant and method of operating it
US2714286A (en) * 1944-07-14 1955-08-02 Aerojet General Co Liquid propellant injection system for jet motors
US2470564A (en) * 1944-11-15 1949-05-17 Reaction Motors Inc Reaction motor control system
US2658340A (en) * 1945-02-01 1953-11-10 Power Jets Res & Dev Ltd Apparatus for igniting fuel in fast-moving hot gas streams
US2574495A (en) * 1945-05-16 1951-11-13 Jr Frank A Parker Flame igniter for jet propulsion units
US2563023A (en) * 1946-04-12 1951-08-07 Daniel And Florence Guggenheim Combustion chamber with multiple discharge nozzles
US2633700A (en) * 1946-04-12 1953-04-07 Daniel And Florence Guggenheim Combustion chamber for propulsion apparatus and having multiple discharge nozzles
US2609658A (en) * 1946-05-11 1952-09-09 Daniel And Florence Guggenheim Target type combustion chamber having a closed end portion receiving conical fuel and oxidizer sprays
US2532709A (en) * 1946-11-30 1950-12-05 Daniel And Florence Guggenheim Liquid cooled baffles between mixing and combustion chambers
US2498263A (en) * 1947-08-23 1950-02-21 Daniel And Florence Guggenheim Ignition apparatus for combustion chambers using intermingled combustion liquids
US2977755A (en) * 1947-10-20 1961-04-04 Aerojet General Co Method and means for initiating the decomposition of propellant in a rocket motor
US2523656A (en) * 1947-11-01 1950-09-26 Daniel And Florence Guggenheim Combustion apparatus comprising successive combustion chambers
US2575070A (en) * 1948-04-06 1951-11-13 William A Reed Jacketed combustion pot with fuel and air nozzle head
US2686400A (en) * 1948-07-12 1954-08-17 Us Air Force Regenerative liquid fuel rocket motor
US2563028A (en) * 1948-12-04 1951-08-07 Daniel And Florence Guggenheim Combustion apparatus comprising a combustion chamber with target type premixing extension
US2651173A (en) * 1949-01-26 1953-09-08 Standard Oil Dev Co Process and apparatus for operating engines at high altitudes
US2722800A (en) * 1949-02-21 1955-11-08 Rolls Royce Fuel systems for gas turbine engines or the like with main and pilot fuel injectors
US2706382A (en) * 1949-07-09 1955-04-19 Carborundum Co Devices for confinement and release of high velocity, hot gases
US2659202A (en) * 1950-06-06 1953-11-17 Fay E Null Augmented thrust pulse jet pump or motor and method of creating augmented thrust or suction
US2701445A (en) * 1950-09-08 1955-02-08 Armstrong Siddeley Motors Ltd Ignition equipment for the combustion equipment of rocket motors
US2972225A (en) * 1950-12-04 1961-02-21 James M Cumming Motor mechanism for missiles
US2956403A (en) * 1951-11-29 1960-10-18 Thiokol Chemical Corp Igniter
US2741085A (en) * 1952-05-12 1956-04-10 Phillips Petroleum Co Safety device, including fusible member for rocket engine starting control
US2954666A (en) * 1955-08-05 1960-10-04 Jr Carl A Brownell Method and apparatus for pre-mixing rocket motor fuel
US3738333A (en) * 1970-07-17 1973-06-12 Volkewagenwerk Ag Cylinder arrangement having a precombustion chamber for combustion engines

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