US2515645A - Feeding means for rotating combustion chambers - Google Patents
Feeding means for rotating combustion chambers Download PDFInfo
- Publication number
- US2515645A US2515645A US736444A US73644447A US2515645A US 2515645 A US2515645 A US 2515645A US 736444 A US736444 A US 736444A US 73644447 A US73644447 A US 73644447A US 2515645 A US2515645 A US 2515645A
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- United States
- Prior art keywords
- combustion
- liquid
- feeding means
- combustion chambers
- opening
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- 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
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/66—Combustion or thrust chambers of the rotary type
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- 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 means for feeding liquid combustion elements, such as gasoline and liquid oxygen, to a combustion chamber of the type used in propulsion apparatus.
- the invention is capable of somewhat general application in combustion chambers, but is particularly designed for use in combustion chambers of the rotating type.
- the invention relates to an improved spray head by which two different liquids may be concentrically fed and effectively intermingled.
- the liquid which is fed nearer the axis of the spray head is given a whirling motion while the outer liquid is fed without rotation. Impact of the whirling liquid on the enclosing and straight-moving liquid produces most effective intermingling.
- FIG. 1 is a sectional elevation of a portions of a'rotating combustion chamber having this invention applied thereto;
- Fig. 2 is an enlarged sectional elevation of certain parts shown in Fig. 1;
- Fig. 3 is an enlarged partial sectional elevation of a slightly modified'construction.
- a portion of a combustion chamber wall is indicated at l and a second chamber wall portion, is shown at H.
- An outer casing l2 coacts with the wall portion ID to enclose a jacket space S
- an outer casing I4 similarly coacts with the wall portion Il' tov enclose a jacket space S.
- These jacket spaces are. closed at their adjacent ends by wall portions l6 and H.
- the two chamber units contain combustion 1iquids under pressure and have areas which abut along a slightly conical surface 20.
- the chamber units may be secured in assembled relation by clamping bolts 22. p
- a sleeve (Fig. 2) extends across the space S between the chamber wall portion II and the outer casing portion a.
- Thesleeve 30 is firmly secured in position coaxially with a spray opening 32 in the wall portion H, which opening is portions a of the casing l4 and Illa or the chamber wall l0.
- An inner and bell-shaped sleeve is mounted within the sleeve 30 but is spaced therefrom by an outwardly projecting flange 4
- the sleeve 40 is contracted toward its lower end, and its lower end portion is held in spaced relation to the sleeve 30 by a conical brace member 45.
- An annular airspace 46 is thus provided between the sleeves 30 and 40, which air space may be vented through a small 'hole 41.
- the sleeve 40 has a spray opening 48 at its lower end, concentric with the spray opening 32 previously described.
- An annular conical slot 50 is formed between the beveled upper annular surface surrounding the spray opening 32 and the conical under surface of the brace member 45. Openings 52 are provided in the lower end portion of the sleeve 30, so that a combustion liquid from the space S may be sprayed through the annular slot 50. This spray will tend to assume a conical form, as indicated by the arrows a, but will have no substantial rotation or whirling motion.
- a substantially conical plug is mounted in the lower portion of the inner sleeve 40, and the pointed lower end 6
- the plug 60 is preferably streamlined at its upper end, as indicated at 63, to reduce friction.
- the plug 60 is provided with angularly disposed vanes 65, the outer ends of which engage and are secured to the inner surface of the sleeve 48.
- The-plug is thus secured in position and acts to impart a'substantial whirling motion to the second combustion liquid, which is fed under pressure from the space S through the passages 33 and 34 to the upper end of the sleeve 40.
- the second combustion liquid thus enters along lines indicated by the arrows b but with a substantial whirling motion.
- the two combustion liquids thuscross each other as they enter the combustion chamber, and, furthermore, one combustion liquid, as oxygen, is rapidly whirling while the other combustion liquid, as gasoline, tends to travel in straight lines. Most eifective and rapid intermingling of the combustion liquids thus takes place, particularly if the combustion chamber itself is also rotating.
- any desired number of spray heads may be provided in a combustion chamber.
- are set at a smaller angle, so that the rate of rotation of the liquid passing the vanes will be correspondingly increased.
- feeding means for two diflferent combustion liquids comprising a casing supplied with a first combustion liquid and having an opening into said chamber, a partition structure having an axial spray opening, said structure being mounted in said casing and spaced from the edge of said first opening to provide an annular feeding slot for said first combustion liquid, means to supply a second combustion liquid within said partition structure, a conical plug mounted within said partition structure and in coaxial and spaced relation therewith,
Description
July 18, 1950 R. H. GODDARD FEEDING MEANS FOR ROTATING COMBUSTION CHAMBERS Filed March 22, 1947 m .0 a v@ ww MEN I n l 1 I l u 7 ATTORN EY' Patented July 18, 1950 orrlca .FEEDING MEANS FOR RGTATING COMBUSTION CHAMBERS Robert H. Goddard, deceased, late of Annapolis,
Md., by Esther C. Goddard, executrix, Worcester, M
and Florence Gugg York, N. Y.,
ass., assignor oi one-half to The Daniel enheim Foundation, New a corporation of New York Application March 22, 1947, Serial No. 736,444
3 Claims.
1 This invention relates to means for feeding liquid combustion elements, such as gasoline and liquid oxygen, to a combustion chamber of the type used in propulsion apparatus. The invention is capable of somewhat general application in combustion chambers, but is particularly designed for use in combustion chambers of the rotating type.
It is the general object of the invention to provide improved means for injecting combined sprays of two difierent combustion liquids to a combustion chamber.
More specifically, the invention relates to an improved spray head by which two different liquids may be concentrically fed and effectively intermingled.
In the preferred form, the liquid which is fed nearer the axis of the spray head is given a whirling motion while the outer liquid is fed without rotation. Impact of the whirling liquid on the enclosing and straight-moving liquid produces most effective intermingling.
The invention further relates to arrangements and combinations of partswhich will be hereinafter described and more particularly pointed out in the appended claims.
A preferred form of the invention is shown in the drawing, in which Fig. 1 is a sectional elevation of a portions of a'rotating combustion chamber having this invention applied thereto;
Fig. 2 is an enlarged sectional elevation of certain parts shown in Fig. 1; and
Fig. 3 is an enlarged partial sectional elevation of a slightly modified'construction.
Referring to Fig. 1, a portion of a combustion chamber wall is indicated at l and a second chamber wall portion, is shown at H. An outer casing l2 coacts with the wall portion ID to enclose a jacket space S, and an outer casing I4 similarly coacts with the wall portion Il' tov enclose a jacket space S. These jacket spaces are. closed at their adjacent ends by wall portions l6 and H.
The two chamber units contain combustion 1iquids under pressure and have areas which abut along a slightly conical surface 20. The chamber units may be secured in assembled relation by clamping bolts 22. p
A sleeve (Fig. 2) extends across the space S between the chamber wall portion II and the outer casing portion a. Thesleeve 30 is firmly secured in position coaxially with a spray opening 32 in the wall portion H, which opening is portions a of the casing l4 and Illa or the chamber wall l0.
An inner and bell-shaped sleeve is mounted within the sleeve 30 but is spaced therefrom by an outwardly projecting flange 4| at its upper end. The sleeve 40 is contracted toward its lower end, and its lower end portion is held in spaced relation to the sleeve 30 by a conical brace member 45. An annular airspace 46 is thus provided between the sleeves 30 and 40, which air space may be vented through a small 'hole 41. The sleeve 40 has a spray opening 48 at its lower end, concentric with the spray opening 32 previously described.
An annular conical slot 50 is formed between the beveled upper annular surface surrounding the spray opening 32 and the conical under surface of the brace member 45. Openings 52 are provided in the lower end portion of the sleeve 30, so that a combustion liquid from the space S may be sprayed through the annular slot 50. This spray will tend to assume a conical form, as indicated by the arrows a, but will have no substantial rotation or whirling motion.
A substantially conical plug is mounted in the lower portion of the inner sleeve 40, and the pointed lower end 6| of the plug 60 extends into the inner spray opening 48 but is spaced therefrom. The plug 60 is preferably streamlined at its upper end, as indicated at 63, to reduce friction.
The plug 60 is provided with angularly disposed vanes 65, the outer ends of which engage and are secured to the inner surface of the sleeve 48. The-plug is thus secured in position and acts to impart a'substantial whirling motion to the second combustion liquid, which is fed under pressure from the space S through the passages 33 and 34 to the upper end of the sleeve 40. The second combustion liquid thus enters along lines indicated by the arrows b but with a substantial whirling motion.
The two combustion liquids thuscross each other as they enter the combustion chamber, and, furthermore, one combustion liquid, as oxygen, is rapidly whirling while the other combustion liquid, as gasoline, tends to travel in straight lines. Most eifective and rapid intermingling of the combustion liquids thus takes place, particularly if the combustion chamber itself is also rotating.
It will be understood that any desired number of spray heads may be provided in a combustion chamber.
aligned with passages 33 and 34 in the abutting 55 In the slightly modified construction shown in Fig. 3, the vanes 80 on the plug 8| are set at a smaller angle, so that the rate of rotation of the liquid passing the vanes will be correspondingly increased.
Having thus described the invention and the advantages thereof, it will be understood that the invention is not to be limited thereto, otherwise than as set forth in the claims, but what is claimed is:
1. In a combustion chamber, feeding means for two diflferent combustion liquids comprising a casing supplied with a first combustion liquid and having an opening into said chamber, a partition structure having an axial spray opening, said structure being mounted in said casing and spaced from the edge of said first opening to provide an annular feeding slot for said first combustion liquid, means to supply a second combustion liquid within said partition structure, a conical plug mounted within said partition structure and in coaxial and spaced relation therewith,
' and means to rapidly rotate said second liquid as it-approaches said axial spray opening in said partition structure.
2. The combination in feeding means for ahaving a lower wall with an opening into said chamber, a cylindrical partition member mounted in said casing concentric with said opening, a conical member mounted in said partition member and spaced from the lower wall of said casing to provide an annular feeding slot for said first liquid at said opening, an inner partition member mounted within said first partition member and which is substantially bell-shaped and with an axial spray opening in its contracted lower end, a conical plug positioned above said axial opening but spaced therefrom, and a plurality of short angularly disposed vanes secured between said plug and said inner partition member and imparting a whirling motion to a second combustion liquid as it approaches said axial opening.
ESTHER. C. GODDARD. Ezecutria: o/ 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 391,865 Schutte Oct. 30, 1888 872,288 Koons Nov. 26, 1907 1,678,459 Bowland July 24, 1928 2,395,114 Goddard Feb. 19, 1946 2,396,567 Goddard Mar. 12, 1946 2,417,835 Moore Mar. 25, 1947
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US736444A US2515645A (en) | 1947-03-22 | 1947-03-22 | Feeding means for rotating combustion chambers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US736444A US2515645A (en) | 1947-03-22 | 1947-03-22 | Feeding means for rotating combustion chambers |
Publications (1)
Publication Number | Publication Date |
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US2515645A true US2515645A (en) | 1950-07-18 |
Family
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US736444A Expired - Lifetime US2515645A (en) | 1947-03-22 | 1947-03-22 | Feeding means for rotating combustion chambers |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2667740A (en) * | 1950-06-06 | 1954-02-02 | Daniel And Florence Guggenheim | Means for supplying and cooling rocket type combustion chambers |
US2688371A (en) * | 1951-03-01 | 1954-09-07 | Jet Helicopter Corp | Apparatus for controlling air velocity in blades of jet operated helicopters |
US3258917A (en) * | 1961-11-07 | 1966-07-05 | Atlantic Res Corp | Process and apparatus for gas generation from semi-solids |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US391865A (en) * | 1888-10-30 | schutte | ||
US872288A (en) * | 1907-01-04 | 1907-11-26 | John H Koons | Liquid-fuel burner. |
US1678459A (en) * | 1927-02-21 | 1928-07-24 | Bowland Andreas | Valve for fluid-fuel burners |
US2395114A (en) * | 1942-10-12 | 1946-02-19 | Daniel And Florence Guggenheim | Rotating combustion chamber for rocket apparatus |
US2396567A (en) * | 1940-11-19 | 1946-03-12 | Daniel And Florence Guggenheim | Combustion apparatus |
US2417835A (en) * | 1936-09-25 | 1947-03-25 | Harry H Moore | Combustion device |
-
1947
- 1947-03-22 US US736444A patent/US2515645A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US391865A (en) * | 1888-10-30 | schutte | ||
US872288A (en) * | 1907-01-04 | 1907-11-26 | John H Koons | Liquid-fuel burner. |
US1678459A (en) * | 1927-02-21 | 1928-07-24 | Bowland Andreas | Valve for fluid-fuel burners |
US2417835A (en) * | 1936-09-25 | 1947-03-25 | Harry H Moore | Combustion device |
US2396567A (en) * | 1940-11-19 | 1946-03-12 | Daniel And Florence Guggenheim | Combustion apparatus |
US2395114A (en) * | 1942-10-12 | 1946-02-19 | Daniel And Florence Guggenheim | Rotating combustion chamber for rocket apparatus |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2667740A (en) * | 1950-06-06 | 1954-02-02 | Daniel And Florence Guggenheim | Means for supplying and cooling rocket type combustion chambers |
US2688371A (en) * | 1951-03-01 | 1954-09-07 | Jet Helicopter Corp | Apparatus for controlling air velocity in blades of jet operated helicopters |
US3258917A (en) * | 1961-11-07 | 1966-07-05 | Atlantic Res Corp | Process and apparatus for gas generation from semi-solids |
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