US2551114A - Two-liquid feeding device for combustion chambers - Google Patents
Two-liquid feeding device for combustion chambers Download PDFInfo
- 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
- Authority
- US
- United States
- Prior art keywords
- liquid
- combustion
- feeding device
- combustion chambers
- annular
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/52—Injectors
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S60/00—Power plants
- Y10S60/915—Collection 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.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16867A US2551114A (en) | 1948-03-24 | 1948-03-24 | Two-liquid feeding device for combustion chambers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16867A US2551114A (en) | 1948-03-24 | 1948-03-24 | Two-liquid feeding device for combustion chambers |
Publications (1)
Publication Number | Publication Date |
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US2551114A true US2551114A (en) | 1951-05-01 |
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Family Applications (1)
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US16867A Expired - Lifetime US2551114A (en) | 1948-03-24 | 1948-03-24 | Two-liquid feeding device for combustion chambers |
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Cited By (29)
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2417929A (en) * | 1947-03-25 | Rotary head oil burner |
-
1948
- 1948-03-24 US US16867A patent/US2551114A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2417929A (en) * | 1947-03-25 | Rotary head oil burner |
Cited By (33)
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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