US2482260A - Liquid feeding device - Google Patents
Liquid feeding device Download PDFInfo
- Publication number
- US2482260A US2482260A US656316A US65631646A US2482260A US 2482260 A US2482260 A US 2482260A US 656316 A US656316 A US 656316A US 65631646 A US65631646 A US 65631646A US 2482260 A US2482260 A US 2482260A
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- US
- United States
- Prior art keywords
- feeding device
- liquid feeding
- slots
- annular
- liquid
- 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
- the invention relates to a device by which two diflerent combustion liquids may be fed Simultaneously to a combustion chamber and may be effectively intermingled therein.
- the two liquids are sprayed substantially in radial planes, alternately disposed in an annular'series, and furthermore the liquids are sprayed along lines which intersect substantially at 90 to each other.
- I Fig. 1 is a sectional side elevation showing the improved liquid feeding device associated with a combustion chamber, the section being taken along the irregular line l
- Fig. 2 is a front elevation, looking in the direction of the arrow 2 in Fig. 1.
- the improved feeding device or spray nozzle is shown associated with a combustion chamber C and comprises an inner member In and an outer member I I.
- the member ID may be in the form of a hollow tube having a substantially conical end portion 12 provided with radially disposed slots H.
- the outer member ll comprises an outer tube and an inner tube 2
- the outer ends of the tubes 20 and 2! are connected by an annular end portion 24 provided with radially disposed slots 25.
- the end portion 24 is preferably concave.
- a supply pipe 21 is connected into the outer tube 20, and the usual shutofl valves 28 and 29 may be provided as shown.
- FIG. 2 discloses that the slots l4 in the cone-shaped end 12 of the inner member III are disposed in radial planes which pass between adjacent slots in the annular portion 24 of the outer member I I.
- the sprays from the inner slots I4 are directed outward, as indicated by the arrows a, while the sprays .from the outer slots 25 are directed inward as indicated by the arrows b.
- the two different sets of sprays thus cross each other substantially at 90 and are disposed in radial planes which are alternately disposed in an annular series.
- Two combustion liquids such as gasoline and 2 liquid oxygen, may thus be delivered to the combustion chamber C in such alternated and intersecting relations that extremely efiective mixing and intermingling of the two liquids immediately takes place.
- the improved feedin device or spray nozzle is extremely simple in construction and economical to manufacture and may be readily constructed of materials well adapted to resist high temperatures. If desired, the exposed surfaces of the cone I2 and the annular portion 24 of the outer member I I may have protective coatings of any suitable heat-resistant material.
- a liquid feeding device comprising an inner feeding element having a plurality of outwardly directed and radially elongated end feeding slots producing an expanding laminated liquid spray, a concentric outer feeding element having an annular series of inwardly directed and radially elongated end feeding slots producing a second and contracting laminated liquid spray intersecting said first spray in an annular locus, means to feed one combustion liquid to said inner feeding element and separate means to feed a different combustion liquid to said outer feeding element, and the radially elongated slots in the inner feeding element being positioned in radial planes alternately disposed with respect to the radial planes of the radially elongated slots in the outer annular series, whereby the spray laminations of said two series of slots are alternately disposed circumferentially and said liquids are effectively intermingled.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
Description
Sept. 20, 1949. R. H. GODDARD LIQUID FEEDING DEVICE Original Filed May 20,- 1944 Patented Sept. 20, 1949 2,482,260 ICE 2,482,260 LIQUID FEEDING DEVICE Robert H. Goddard, deceased, late of Annapolis, Md., by Esther C. Goddard, executrix, Paxton, Mass., assignor of one-half to The Daniel and Florence Guggenheim Foundation, New York, N. Y., a corporation of New York Original application May 20, 1944, Serial No.
536,558. ,Divided and this application March 22, 1946, Serial No. 656,316
1 Claim. Y 1
This application is a division of original application Serial No. 536,558, filed by Robert H. Goddard on May 20, 1944, and relates to the improved liquid feeding device or spray nozzle shown but not claimed in said original application.
It is the general object of the invention to provide a liquid feeding device or spray nozzle of a new and improved construction. and by the use of which improved results may be attained.
More specifically, the invention relates to a device by which two diflerent combustion liquids may be fed Simultaneously to a combustion chamber and may be effectively intermingled therein.
In the preferred form, the two liquids are sprayed substantially in radial planes, alternately disposed in an annular'series, and furthermore the liquids are sprayed along lines which intersect substantially at 90 to each other.
The 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 I Fig. 1 is a sectional side elevation showing the improved liquid feeding device associated with a combustion chamber, the section being taken along the irregular line l| in Fig. 2; and
Fig. 2 is a front elevation, looking in the direction of the arrow 2 in Fig. 1.
Referring to the drawings, the improved feeding device or spray nozzle is shown associated with a combustion chamber C and comprises an inner member In and an outer member I I.
The member ID may be in the form of a hollow tube having a substantially conical end portion 12 provided with radially disposed slots H.
The outer member ll comprises an outer tube and an inner tube 2| spaced from the outer tube 20 to provide an annular passage 22. The outer ends of the tubes 20 and 2! are connected by an annular end portion 24 provided with radially disposed slots 25. The end portion 24 is preferably concave. A supply pipe 21 is connected into the outer tube 20, and the usual shutofl valves 28 and 29 may be provided as shown.
Reference to Fig. 2 discloses that the slots l4 in the cone-shaped end 12 of the inner member III are disposed in radial planes which pass between adjacent slots in the annular portion 24 of the outer member I I. The sprays from the inner slots I4 are directed outward, as indicated by the arrows a, while the sprays .from the outer slots 25 are directed inward as indicated by the arrows b. The two different sets of sprays thus cross each other substantially at 90 and are disposed in radial planes which are alternately disposed in an annular series.
Two combustion liquids, such as gasoline and 2 liquid oxygen, may thus be delivered to the combustion chamber C in such alternated and intersecting relations that extremely efiective mixing and intermingling of the two liquids immediately takes place.
The improved feedin device or spray nozzle is extremely simple in construction and economical to manufacture and may be readily constructed of materials well adapted to resist high temperatures. If desired, the exposed surfaces of the cone I2 and the annular portion 24 of the outer member I I may have protective coatings of any suitable heat-resistant material.
Having thus described 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 claim, but that what is claimed is:
A liquid feeding device comprising an inner feeding element having a plurality of outwardly directed and radially elongated end feeding slots producing an expanding laminated liquid spray, a concentric outer feeding element having an annular series of inwardly directed and radially elongated end feeding slots producing a second and contracting laminated liquid spray intersecting said first spray in an annular locus, means to feed one combustion liquid to said inner feeding element and separate means to feed a different combustion liquid to said outer feeding element, and the radially elongated slots in the inner feeding element being positioned in radial planes alternately disposed with respect to the radial planes of the radially elongated slots in the outer annular series, whereby the spray laminations of said two series of slots are alternately disposed circumferentially and said liquids are effectively intermingled.
ESTHER C. GODDARD, Emecutria: of the Last Will and Testament of Robert H. Goddard, Deceased.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES, PATENTS Number Name Date 453,346 Myers June 2, 1891 1,063,352 Jacobs June 3, 1913 2,247,768 Huwyler July 1, 1941 2,383,433 Burnam Aug. 21, 1945 2,405,465 Summerfleld Aug. 6, 1948 2,414,442 Breault Jan. 21, 1947 2,417,835 Moore Mar. 25, 1947 FOREIGN PATENTS Number Country Date 558,291 Mar. 23, 1923
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US656316A US2482260A (en) | 1944-05-20 | 1946-03-22 | Liquid feeding device |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US536558A US2558483A (en) | 1944-05-20 | 1944-05-20 | Feeding apparatus, including injectors adapted to supply combustion liquids under pressure to a combustion chamber |
US656316A US2482260A (en) | 1944-05-20 | 1946-03-22 | Liquid feeding device |
Publications (1)
Publication Number | Publication Date |
---|---|
US2482260A true US2482260A (en) | 1949-09-20 |
Family
ID=27065179
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US656316A Expired - Lifetime US2482260A (en) | 1944-05-20 | 1946-03-22 | Liquid feeding device |
Country Status (1)
Country | Link |
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US (1) | US2482260A (en) |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619387A (en) * | 1948-09-11 | 1952-11-25 | Richard T Cornelius | Beverage mixing and dispensing device |
US2679295A (en) * | 1949-12-30 | 1954-05-25 | Gen Electric | Helicopter blade jet combustion chamber |
US2709887A (en) * | 1950-05-25 | 1955-06-07 | Esther C Goddard | Zonal spray combustion chamber for rockets and rocket craft |
US2753687A (en) * | 1950-10-02 | 1956-07-10 | Gen Electric | Injection head for jet propulsion system |
US2850323A (en) * | 1955-07-15 | 1958-09-02 | Arrow Tools Inc | Mist coolant atomizer |
US2928236A (en) * | 1957-01-14 | 1960-03-15 | Hartmann J Kircher | Rocket engine injector |
US2930533A (en) * | 1956-07-10 | 1960-03-29 | Cletus Meyer | Spray gun |
US3059429A (en) * | 1958-03-25 | 1962-10-23 | Sunstrand Corp | Reaction chamber |
US3093157A (en) * | 1960-12-02 | 1963-06-11 | Adrien J Aitken | Metering and mixing apparatus |
DE1179663B (en) * | 1957-12-31 | 1964-10-15 | Rudolf O Bracke Dipl Ing | Oil burner |
US3180394A (en) * | 1955-04-26 | 1965-04-27 | Bloom Eng Co Inc | Gas burner |
US3199600A (en) * | 1962-04-17 | 1965-08-10 | Jacobs Alan | Fog-projecting fire extinguisher construction |
US3289405A (en) * | 1964-01-16 | 1966-12-06 | Eng Harvard | Propellant oxidizer mixing system for rocket motors |
DE1292886B (en) * | 1965-10-14 | 1969-04-17 | Bodenseewerk Perkin Elmer Co | Flame ionization detector |
US4445444A (en) * | 1982-08-12 | 1984-05-01 | Texaco Inc. | Burner for combusting oxygen-coal mixture |
US4664619A (en) * | 1985-11-29 | 1987-05-12 | Otis Engineering Corporation | Burner nozzle |
US4708637A (en) * | 1986-04-22 | 1987-11-24 | Dutescu Cornel J | Gaseous fuel reactor |
US5044558A (en) * | 1989-05-09 | 1991-09-03 | Halliburton Company | Burner nozzle with replaceable air jetting assembly |
US5067657A (en) * | 1989-11-01 | 1991-11-26 | Halliburton Company | Burner nozzle |
US9840822B2 (en) | 2015-08-21 | 2017-12-12 | Kevin Jason Foster | Drain assisting water fixture |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US453346A (en) * | 1891-06-02 | Oil-burner | ||
US1063352A (en) * | 1911-12-22 | 1913-06-03 | Francis A Jacobs | Oil-burner. |
FR558291A (en) * | 1922-11-04 | 1923-08-24 | Device for automatic washing of containers | |
US2247768A (en) * | 1936-08-06 | 1941-07-01 | Huwyler Eugen | Firing equipment for the combustion of liquid fuels |
US2383433A (en) * | 1942-06-01 | 1945-08-21 | Thompson W Burnam | Nozzle |
US2405465A (en) * | 1943-05-07 | 1946-08-06 | Aerojet Engineering Corp | Jet propulsion motor |
US2414442A (en) * | 1944-02-03 | 1947-01-21 | Delphis C Breault | Burner construction |
US2417835A (en) * | 1936-09-25 | 1947-03-25 | Harry H Moore | Combustion device |
-
1946
- 1946-03-22 US US656316A patent/US2482260A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US453346A (en) * | 1891-06-02 | Oil-burner | ||
US1063352A (en) * | 1911-12-22 | 1913-06-03 | Francis A Jacobs | Oil-burner. |
FR558291A (en) * | 1922-11-04 | 1923-08-24 | Device for automatic washing of containers | |
US2247768A (en) * | 1936-08-06 | 1941-07-01 | Huwyler Eugen | Firing equipment for the combustion of liquid fuels |
US2417835A (en) * | 1936-09-25 | 1947-03-25 | Harry H Moore | Combustion device |
US2383433A (en) * | 1942-06-01 | 1945-08-21 | Thompson W Burnam | Nozzle |
US2405465A (en) * | 1943-05-07 | 1946-08-06 | Aerojet Engineering Corp | Jet propulsion motor |
US2414442A (en) * | 1944-02-03 | 1947-01-21 | Delphis C Breault | Burner construction |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619387A (en) * | 1948-09-11 | 1952-11-25 | Richard T Cornelius | Beverage mixing and dispensing device |
US2679295A (en) * | 1949-12-30 | 1954-05-25 | Gen Electric | Helicopter blade jet combustion chamber |
US2709887A (en) * | 1950-05-25 | 1955-06-07 | Esther C Goddard | Zonal spray combustion chamber for rockets and rocket craft |
US2753687A (en) * | 1950-10-02 | 1956-07-10 | Gen Electric | Injection head for jet propulsion system |
US3180394A (en) * | 1955-04-26 | 1965-04-27 | Bloom Eng Co Inc | Gas burner |
US2850323A (en) * | 1955-07-15 | 1958-09-02 | Arrow Tools Inc | Mist coolant atomizer |
US2930533A (en) * | 1956-07-10 | 1960-03-29 | Cletus Meyer | Spray gun |
US2928236A (en) * | 1957-01-14 | 1960-03-15 | Hartmann J Kircher | Rocket engine injector |
DE1179663B (en) * | 1957-12-31 | 1964-10-15 | Rudolf O Bracke Dipl Ing | Oil burner |
US3059429A (en) * | 1958-03-25 | 1962-10-23 | Sunstrand Corp | Reaction chamber |
US3093157A (en) * | 1960-12-02 | 1963-06-11 | Adrien J Aitken | Metering and mixing apparatus |
US3199600A (en) * | 1962-04-17 | 1965-08-10 | Jacobs Alan | Fog-projecting fire extinguisher construction |
US3289405A (en) * | 1964-01-16 | 1966-12-06 | Eng Harvard | Propellant oxidizer mixing system for rocket motors |
DE1292886B (en) * | 1965-10-14 | 1969-04-17 | Bodenseewerk Perkin Elmer Co | Flame ionization detector |
US4445444A (en) * | 1982-08-12 | 1984-05-01 | Texaco Inc. | Burner for combusting oxygen-coal mixture |
US4664619A (en) * | 1985-11-29 | 1987-05-12 | Otis Engineering Corporation | Burner nozzle |
US4708637A (en) * | 1986-04-22 | 1987-11-24 | Dutescu Cornel J | Gaseous fuel reactor |
US5044558A (en) * | 1989-05-09 | 1991-09-03 | Halliburton Company | Burner nozzle with replaceable air jetting assembly |
US5067657A (en) * | 1989-11-01 | 1991-11-26 | Halliburton Company | Burner nozzle |
US9840822B2 (en) | 2015-08-21 | 2017-12-12 | Kevin Jason Foster | Drain assisting water fixture |
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