US2551114A - Two-liquid feeding device for combustion chambers - Google Patents

Two-liquid feeding device for combustion chambers Download PDF

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Publication number
US2551114A
US2551114A US16867A US1686748A US2551114A US 2551114 A US2551114 A US 2551114A US 16867 A US16867 A US 16867A US 1686748 A US1686748 A US 1686748A US 2551114 A US2551114 A US 2551114A
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liquid
combustion
feeding device
combustion chambers
annular
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US16867A
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Esther C Goddard
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DANIEL AND FLORENCE GUGGENHEIM
DANIEL AND FLORENCE GUGGENHEIM FOUNDATION
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DANIEL AND FLORENCE GUGGENHEIM
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/52Injectors
    • 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 chambers.
  • the present invention relates particularly to combustion chambers in which two combustion liquids, as gasoline and liquid oxygen, are intermingled and consumed. s
  • I Fig. 1 is a sectional side elevation showing one form of the improved feeding device
  • Figs. 2 and 3 are views similar to Fig. 1 but showing modified constructions.
  • a two-liquid feeding device D is shown as mounted axially in a combustion chamber C.
  • the device D comprises an inner pipe or tube It] supporting a pointed or conical porous member l2 in its inner end.
  • the member I 2 is of rigid and heat-resistant material and-is preferably formed of porous or sintered metal.
  • One combustion liquid as gasoline, is supplied under pressure to the pipe or tube In and is forced through the porous member
  • annular passage P is provided between an outer tubular member 4 and inner tubular member IS.
  • the projecting ends of the annular members l4 and i5 are inwardly displaced to provide annular flanges l6 and H which are positioned to define an annular port I 8.
  • the pipe I0 and tubular members I4 are held in spaced relation by axially extending vanes or partitions and 2
  • a second combustion liquid as liquid oxygen
  • the liquid oxygen forms a thin film along said outer-surface and becomes inwith the mist or. spray of gasoline. This film of oxygen not only mixes effectively with the gasoline but also acts as a cooling agent for the outer surface of the member I2.
  • the surface area of the member I2 is reduced toward the axis thereof, the film of oxygen tends to become thicker, as it is concentrated. in a smaller area. For this reason, it is desirable that the porosity of ,the member I2 be increased toward its axis to maintain the desired ratio between the two combustion liquids.
  • one combustion liquid as gasoline
  • the member 32 is cupshaped, as shown in Fig. 2, but with an outwardly projecting conical axial portion 32a.
  • the second combustion liquid as liquid oxygen, is supplied under pressure through a passage P between an outer casing or wall 34 and an inner casing 35.
  • the projecting ends of the case ings 34 and are inwardly offset and reversely curved to provide an annular slot 31 through which the liquid oxygen is sprayed against the adjacent surface of the porous member 32 and forms a cooling film thereon, as well as mixing With the gasoline spray or mist.
  • the axial portion 32a of the member 32 is preferably made more porous to offset its decreased surface area.
  • the parts 3 I, 34 and 35 are held in spaced relation by vanes or partitions 38 and39 and the whole device is mounted in a combustion chamber C.
  • , 34 and 35 may be made in two parts to facilitate assembly.
  • gasoline under pressure is supplied to an axially positioned pipe 40 having an inner partition structure 4
  • An annular conical porous member 45 is fixed between the end of the pipe 40 and the contracted flange 46 of the cap 44.
  • the porous member 45 is also supported by the outer portions 42 of the partition structure 4
  • the gasoline enters recesses R between the parts 42 and is forced through the porous member 45 as a mist or fine spray.
  • a second combustion liquid, as liquid oxygen, is supplied through an annular passage P2 formed between an outer tube 50 and an inner tube 5
  • the outer tube 50 is inwardly contracted at 52 to provide an annular feed.
  • slot 53 at the 3 end of the tube 5
  • are held in spaced relation by vanes or partitions 55 and 56 and the whole device is mounted in an axial opening in a combustion chamber C2.
  • annular spray such as liquid oxygen
  • a mist or fine spray ofthesecond combustion liquid as gasoline
  • the area of the member 65 increases outwardly, and the porosity of said member may be correspondingly reduced outwardly to supply relatively less gasoline as'the film of liquid oxygen becomes thinner.
  • a two-liquid; feeding device for a combustionchamber comprising an axial porous feeding' member, means to force. one combustion liquid through said porous member to issue as a fine mist at its outer surface and annular means to supply a converging film of a second combustion liquidto the outer surface of said porous member at its periphery for intermingling with said fine mist of said first combustion liquid, that improvement. which comprises a porous member which is cup-shaped and outwardly concave and which has an axial raised projection.

Description

May 1, 1951 R. H. GODDARD 2,551,114
TWO-LIQUID FEEDING DEVICE FOR COMBUSTION CHAMBERS Filed March 24, 1948 INVENTOR.
Eatfiaz G. Goddaza, QBGZLW.
W ATTORNEY Iatented May 1, 1951 I UNITED STATES PATENT OFFICE TWO-LIQUID .DEVICE FOR Robert H. Goddard, deceased, late of Annapolis, Md., by Esther -C. Goddard, executrix, Worcester, Mass, assignor of one-half to The Daniel and Florence Guggenheim Foundation, New
York, N. Y., a Corporation of New York Application March 24, 1948, Serial No. 16,867
This invention relates to combustion chambers.
as used in propulsion apparatus. The present invention relates particularly to combustion chambers in which two combustion liquids, as gasoline and liquid oxygen, are intermingled and consumed. s
It is the general object of the present invention to provide an improved feeding device for such a combustion chamberthrough which .two'
member.
The invention further relates to arrangements and combinations of parts which will be hereinafter described and more particularly pointed out in the appended claims.
Preferred forms of the invention are shown in the drawing, in which I Fig. 1 is a sectional side elevation showing one form of the improved feeding device; and
Figs. 2 and 3 are views similar to Fig. 1 but showing modified constructions.
Referring to Fig. 1, a two-liquid feeding device D is shown as mounted axially in a combustion chamber C. The device D comprises an inner pipe or tube It] supporting a pointed or conical porous member l2 in its inner end. The member I 2 is of rigid and heat-resistant material and-is preferably formed of porous or sintered metal.
One combustion liquid, as gasoline, is supplied under pressure to the pipe or tube In and is forced through the porous member |2 in the form of a very fine mist or spray.
3 Claims. (01. 60-44) timately. intermingled An annular passage P is provided between an outer tubular member 4 and inner tubular member IS. The projecting ends of the annular members l4 and i5 are inwardly displaced to provide annular flanges l6 and H which are positioned to define an annular port I 8. The pipe I0 and tubular members I4 and are held in spaced relation by axially extending vanes or partitions and 2|.
A second combustion liquid, as liquid oxygen, is supplied under pressure to the passage P and is delivered through the slot -|8 and against the outer surface of the member l2 as an annular sheet or spray. The liquid oxygen forms a thin film along said outer-surface and becomes inwith the mist or. spray of gasoline. This film of oxygen not only mixes effectively with the gasoline but also acts as a cooling agent for the outer surface of the member I2.
As the surface area of the member I2 is reduced toward the axis thereof, the film of oxygen tends to become thicker, as it is concentrated. in a smaller area. For this reason, it is desirable that the porosity of ,the member I2 be increased toward its axis to maintain the desired ratio between the two combustion liquids.
In Fig. 2, one combustion liquid, as gasoline, is fed under pressure through a pipe to a recess R within its enlarged end portion 3i, and is forced against the inner surface of a porous or permeable member 32, clamped in the enlarged pipe portion 3|. The member 32 is cupshaped, as shown in Fig. 2, but with an outwardly projecting conical axial portion 32a.
The second combustion liquid, as liquid oxygen, is supplied under pressure through a passage P between an outer casing or wall 34 and an inner casing 35. The projecting ends of the case ings 34 and are inwardly offset and reversely curved to provide an annular slot 31 through which the liquid oxygen is sprayed against the adjacent surface of the porous member 32 and forms a cooling film thereon, as well as mixing With the gasoline spray or mist. I
In this construction also the axial portion 32a of the member 32 is preferably made more porous to offset its decreased surface area. The parts 3 I, 34 and 35 are held in spaced relation by vanes or partitions 38 and39 and the whole device is mounted in a combustion chamber C. The parts 3|, 34 and 35 may be made in two parts to facilitate assembly.
In the construction shown in Fig. 3, gasoline under pressure is supplied to an axially positioned pipe 40 having an inner partition structure 4| which is outwardly extended at 42 to support a cap 44. An annular conical porous member 45 is fixed between the end of the pipe 40 and the contracted flange 46 of the cap 44. The porous member 45 is also supported by the outer portions 42 of the partition structure 4|. The gasoline enters recesses R between the parts 42 and is forced through the porous member 45 as a mist or fine spray.
A second combustion liquid, as liquid oxygen, is supplied through an annular passage P2 formed between an outer tube 50 and an inner tube 5|. The outer tube 50 is inwardly contracted at 52 to provide an annular feed. slot 53 at the 3 end of the tube 5|. The parts 40, 5D and 5| are held in spaced relation by vanes or partitions 55 and 56 and the whole device is mounted in an axial opening in a combustion chamber C2.
With this construction, an annular spray, such as liquid oxygen, is directed against the outer surface of the porous member 45 at its smaller diameter and spreads outward against the ex.- panding and substantially conical surface thereof, while a mist or fine spray ofthesecond combustion liquid, as gasoline, is forced through the porous member 45 and intermingles with the spray of liquid oxygen.
In this form of the invention, the area of the member 65 increases outwardly, and the porosity of said member may be correspondingly reduced outwardly to supply relatively less gasoline as'the film of liquid oxygen becomes thinner.
In all three forms of the invention, a very effective interminging ofi two combustion liquids is efiected andthe exposed surfaces of the feeding' devices are all. adequately liquid cooled.
. Having thus dscribed the invention and the advantages thereof, it will be understood that the invention is not to be limited to the details herein disclosed, otherwise than as set forth in the claims, but what isclaimed is:
1. In a two-liquid; feeding device for a combustionchamber comprising an axial porous feeding' member, means to force. one combustion liquid through said porous member to issue as a fine mist at its outer surface and annular means to supply a converging film of a second combustion liquidto the outer surface of said porous member at its periphery for intermingling with said fine mist of said first combustion liquid, that improvement. which comprises a porous member which is cup-shaped and outwardly concave and which has an axial raised projection.
2. The combination in a two-liquid feeding device for a combustion chamber as set forth in claim 1, in which the annular means directs the second combustionv liquid against said porous member in a reverse direction and away from the discharge end of said chamber and toward the axis of. said member.
3; The combination in a two-liquid feeding device for a combustion chamber as set forth in claim 1, in which the porosity of said feeding member is increased towards its axis.
ESTHER C. GODDARD. Emecutria: of the Last Will and Testament of Robert H. Goddard, Deceased.
REFERENCES. CITED UNITED STATES PATENTS Name Date Hanson Mar. 25, 1947 Number.
US16867A 1948-03-24 1948-03-24 Two-liquid feeding device for combustion chambers Expired - Lifetime US2551114A (en)

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Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2692800A (en) * 1951-10-08 1954-10-26 Gen Electric Nozzle flow control
US2698514A (en) * 1952-01-14 1955-01-04 Edwin H Hull Rocket motor
US2734775A (en) * 1956-02-14 Fuel nozzle
US2784029A (en) * 1953-02-19 1957-03-05 Martin Von Schulthess & Co Method and apparatus for spraying metal
US2828609A (en) * 1950-04-03 1958-04-01 Bristol Aero Engines Ltd Combustion chambers including suddenly enlarged chamber portions
US2841213A (en) * 1952-04-10 1958-07-01 Owens Corning Fiberglass Corp Gas burner apparatus for forming glass fibers
US2961497A (en) * 1957-05-01 1960-11-22 Heppner Mfg Co Magnetic loudspeaker
US2974723A (en) * 1955-12-27 1961-03-14 Worcester Taper Pin Co Evaporating nozzle for a liquid fuel burning torch
US3074470A (en) * 1952-04-10 1963-01-22 Owens Corning Fiberglass Corp Liquid fuel burner for forming glass fibers
US3085394A (en) * 1959-06-17 1963-04-16 United Aircraft Corp Rocket propellant injector
US3242670A (en) * 1962-08-27 1966-03-29 United Aircraft Corp Segmented baffle injector design
US3352545A (en) * 1966-05-31 1967-11-14 John F Denine Carburetor construction
US3379855A (en) * 1963-05-13 1968-04-23 Electro Optical Systems Inc Fluid feed system
US3436328A (en) * 1965-04-19 1969-04-01 Gen Monitors Apparatus for gas detection
US3446023A (en) * 1966-08-05 1969-05-27 United Aircraft Corp Catalytic attitude-control rocket motor
US3464633A (en) * 1967-11-16 1969-09-02 Trw Inc Multiple fluid controlling shear valve
US3583635A (en) * 1969-02-24 1971-06-08 Jerome H Lemelson Spraying systems
US3802193A (en) * 1972-11-29 1974-04-09 Us Air Force Barrier ring injector
US4877082A (en) * 1989-04-13 1989-10-31 United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Convergent strand array liquid pumping system
EP0497255A2 (en) * 1991-01-30 1992-08-05 Ing. Erich Pfeiffer GmbH Delivering nozzle for media
US5259995A (en) * 1991-10-30 1993-11-09 Liquid Carbonic Industries Corporation Vapor pressure device
US5314121A (en) * 1990-08-29 1994-05-24 Shell Oil Company Discharge device
US5449288A (en) * 1994-03-25 1995-09-12 Hi-Z Technology, Inc. Aspirated wick atomizer nozzle
WO1998029178A1 (en) * 1996-12-31 1998-07-09 Atmi Ecosys Corporation Inlet structures for introducing a particulate solids-containing and/or solids-forming gas stream to a gas processing system
US5833888A (en) * 1996-12-31 1998-11-10 Atmi Ecosys Corporation Weeping weir gas/liquid interface structure
US5846275A (en) * 1996-12-31 1998-12-08 Atmi Ecosys Corporation Clog-resistant entry structure for introducing a particulate solids-containing and/or solids-forming gas stream to a gas processing system
US5890476A (en) * 1996-08-07 1999-04-06 Grant; Barry Fuel delivery nozzle
US20110198417A1 (en) * 2010-02-12 2011-08-18 Applied Materials, Inc. Process chamber gas flow improvements
DE102010012554A1 (en) * 2010-03-23 2011-09-29 Technische Universität Dortmund Dual-material internal mixing nozzle assembly and method for atomizing a liquid

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417929A (en) * 1947-03-25 Rotary head oil burner

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417929A (en) * 1947-03-25 Rotary head oil burner

Cited By (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2734775A (en) * 1956-02-14 Fuel nozzle
US2828609A (en) * 1950-04-03 1958-04-01 Bristol Aero Engines Ltd Combustion chambers including suddenly enlarged chamber portions
US2692800A (en) * 1951-10-08 1954-10-26 Gen Electric Nozzle flow control
US2698514A (en) * 1952-01-14 1955-01-04 Edwin H Hull Rocket motor
US3074470A (en) * 1952-04-10 1963-01-22 Owens Corning Fiberglass Corp Liquid fuel burner for forming glass fibers
US2841213A (en) * 1952-04-10 1958-07-01 Owens Corning Fiberglass Corp Gas burner apparatus for forming glass fibers
US2784029A (en) * 1953-02-19 1957-03-05 Martin Von Schulthess & Co Method and apparatus for spraying metal
US2974723A (en) * 1955-12-27 1961-03-14 Worcester Taper Pin Co Evaporating nozzle for a liquid fuel burning torch
US2961497A (en) * 1957-05-01 1960-11-22 Heppner Mfg Co Magnetic loudspeaker
US3085394A (en) * 1959-06-17 1963-04-16 United Aircraft Corp Rocket propellant injector
US3242670A (en) * 1962-08-27 1966-03-29 United Aircraft Corp Segmented baffle injector design
US3379855A (en) * 1963-05-13 1968-04-23 Electro Optical Systems Inc Fluid feed system
US3436328A (en) * 1965-04-19 1969-04-01 Gen Monitors Apparatus for gas detection
US3352545A (en) * 1966-05-31 1967-11-14 John F Denine Carburetor construction
US3446023A (en) * 1966-08-05 1969-05-27 United Aircraft Corp Catalytic attitude-control rocket motor
US3464633A (en) * 1967-11-16 1969-09-02 Trw Inc Multiple fluid controlling shear valve
US3583635A (en) * 1969-02-24 1971-06-08 Jerome H Lemelson Spraying systems
US3802193A (en) * 1972-11-29 1974-04-09 Us Air Force Barrier ring injector
US4877082A (en) * 1989-04-13 1989-10-31 United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Convergent strand array liquid pumping system
US5314121A (en) * 1990-08-29 1994-05-24 Shell Oil Company Discharge device
EP0497255A2 (en) * 1991-01-30 1992-08-05 Ing. Erich Pfeiffer GmbH Delivering nozzle for media
DE4102632A1 (en) * 1991-01-30 1992-08-06 Pfeiffer Erich Gmbh & Co Kg DISCHARGE NOZZLE FOR MEDIA
EP0497255A3 (en) * 1991-01-30 1993-02-03 Ing. Erich Pfeiffer Gmbh & Co. Kg Delivering nozzle for media
US5295628A (en) * 1991-01-30 1994-03-22 Ing. Erich Pfeiffer Gmbh & Co. Kg Discharge nozzle for media
US5259995A (en) * 1991-10-30 1993-11-09 Liquid Carbonic Industries Corporation Vapor pressure device
US5449288A (en) * 1994-03-25 1995-09-12 Hi-Z Technology, Inc. Aspirated wick atomizer nozzle
US5890476A (en) * 1996-08-07 1999-04-06 Grant; Barry Fuel delivery nozzle
WO1998029178A1 (en) * 1996-12-31 1998-07-09 Atmi Ecosys Corporation Inlet structures for introducing a particulate solids-containing and/or solids-forming gas stream to a gas processing system
US5833888A (en) * 1996-12-31 1998-11-10 Atmi Ecosys Corporation Weeping weir gas/liquid interface structure
US5846275A (en) * 1996-12-31 1998-12-08 Atmi Ecosys Corporation Clog-resistant entry structure for introducing a particulate solids-containing and/or solids-forming gas stream to a gas processing system
US20110198417A1 (en) * 2010-02-12 2011-08-18 Applied Materials, Inc. Process chamber gas flow improvements
US8828182B2 (en) * 2010-02-12 2014-09-09 Applied Materials, Inc. Process chamber gas flow improvements
DE102010012554A1 (en) * 2010-03-23 2011-09-29 Technische Universität Dortmund Dual-material internal mixing nozzle assembly and method for atomizing a liquid

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