US1451072A - Burner - Google Patents
Burner Download PDFInfo
- Publication number
- US1451072A US1451072A US481798A US48179821A US1451072A US 1451072 A US1451072 A US 1451072A US 481798 A US481798 A US 481798A US 48179821 A US48179821 A US 48179821A US 1451072 A US1451072 A US 1451072A
- Authority
- US
- United States
- Prior art keywords
- burner
- depression
- chamber
- passage
- inlet
- 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
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
- F23D14/04—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
Definitions
- Fig. l shows a central vertical section through the burner.
- Fig. 2 a section on the line 2-2 in Fig. l. Fig. 3 a section on the line 3-3 in Fig. l. lmarlrs the burner chamber from which jet projections la extend for forming the jet openings, the jet openings la being provided with any diifusing material such as gauze (not shown).
- the chamber is provided with a depression 2 to which the inlet 3 leads.
- a baille 4 extends from the inlet end over the depression 2, this bafHe being preferably inclined toward the center of the burner and forming with'the end of the depression an upturned passage 5.
- a deflector 6 is arranged over the top of the passage 5, the passage between the deflectors 4 and 6 being somewhat larger than the passage between the deflector 6 and the wall of the burner at the end of the depression. I have found it necessary with a burner of this type to slot ⁇ the deflector 6 at 7 so as to allow a'slight 40 movement of mixture through it to feed the jet openings la directly above it. Itis also desirable to form a slight projecting shoulder 8 in advance of the depression 2 to assure the feeding of fuel to the openings la near the deflector 6. With this burner equal jets are provided throughout the burner. What I claim as new is l.
- a burner having a burner chamber with jet openings leading therefrom and with a depression at the inlet end to which the inlet leads; and a baliieextending from the end of the chamber over the depression and forming an up-turned passage nearer the. inlet end of the burner*v than the center of the burner7 said baffle being inclined downwardly toward the center.
- a burner having a burner chamber with ⁇ jet openings leadingtherefrom and with a depression at the inlet end to which the inlet leads; a bafle lextending from the end of the chamber over the depression and forming an up-turned passage nearer the inlet end .of the burner than the center of the burner; andv a second baffle over the upturned passage.
- a burner having a burner chamber with jet openings leading therefrom and with a ldepression atvthe inlet en d to which the inlet leads; a baflle extending from the end of the chamber over the depression and forming an up-turned passage nearer the inlet end of the burner than the center of the burner;
- Aburner having a burner chamber with jet openings leading therefrom and with a depression at the inlet end towhich the inlet leads; a admiration extending from the end of the chamber over-the depression and forming an upf-turned passage nearer the inlet end of the burner than lthe center of the burner; and a second baffle over the up-turned passage forming a larger passage between the baffles than the opening between the second baiie andthe wall of the chamber.
- a burner having a burner chamber with jet openings leading therefrom and with a depression at the inlet end to which the inlet leads; a baffle extending from the end of the chamber over the depression and forming an up-turned passage nearer the inlet end of the burner than the center of the burner; a second baffle over the up-turned passage; and a shoulder at the bottom of the chamber in advance of the opening between the second baffle and the wall of the chamber at the end of the depression.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Description
Apr. 1o, 1923, 1;451,o72 C. H. HOFFSTETTER BURNER Filed July l, 1921 CLU@ /41 MMM lave/2501", By /Z if/ fhtw/.4
Pateniea Apr. 1o, 19,23.
lUNITI-:D STATES Acarica. N
i CARL H. HOFFSTETTER, F ERIE, PENNSYLVANIA, ASSIGNOR TO ODIN STOVE MANU- FACTURING COMPANY, OF ERIE, PENNSYLVANIA, A CORPORATION OF PENNSYL- VANIA.
BURNER.
Application filed July 1, 1921. `Serial No.`481,798.
To all'fwhom t may concern:
Be it known that I, CARL H. HOFFSTETTER, a citizen of the United States; residing at Erie, in the county of, Erie land'State of 5 Pennsylvania, have invented new and useful Improvements in Burners,l of which the following is a specification. ,Y With burners having their passages at the end and particularly burners used for heating radiants it is difiicult to so distribute the incoming mixture as. to have a uniform flow of. fuel from each jet, or portion of the burner. The present invention is designed to obviate this difficulty especially with long burners.
The invention is illustrated in the accompanying drawings as follows:-
Fig. l shows a central vertical section through the burner.
Fig. 2 a section on the line 2-2 in Fig. l. Fig. 3 a section on the line 3-3 in Fig. l. lmarlrs the burner chamber from which jet projections la extend for forming the jet openings, the jet openings la being provided with any diifusing material such as gauze (not shown). The chamber is provided with a depression 2 to which the inlet 3 leads. A baille 4 extends from the inlet end over the depression 2, this bafHe being preferably inclined toward the center of the burner and forming with'the end of the depression an upturned passage 5. A deflector 6 is arranged over the top of the passage 5, the passage between the deflectors 4 and 6 being somewhat larger than the passage between the deflector 6 and the wall of the burner at the end of the depression. I have found it necessary with a burner of this type to slot `the deflector 6 at 7 so as to allow a'slight 40 movement of mixture through it to feed the jet openings la directly above it. Itis also desirable to form a slight projecting shoulder 8 in advance of the depression 2 to assure the feeding of fuel to the openings la near the deflector 6. With this burner equal jets are provided throughout the burner. What I claim as new is l. A burner having a burner chamber with jet openings leading therefrom and with a depression at the inlet end to which the inlet leads; and a baliieextending from the end of the chamber over the depression and forming an up-turned passage nearer the. inlet end of the burner*v than the center of the burner7 said baffle being inclined downwardly toward the center.
2. A burner having a burner chamber with `jet openings leadingtherefrom and with a depression at the inlet end to which the inlet leads; a bafle lextending from the end of the chamber over the depression and forming an up-turned passage nearer the inlet end .of the burner than the center of the burner; andv a second baffle over the upturned passage.
3. A burner having a burner chamber with jet openings leading therefrom and with a ldepression atvthe inlet en d to which the inlet leads; a baflle extending from the end of the chamber over the depression and forming an up-turned passage nearer the inlet end of the burner than the center of the burner;
4and asecond baffle over the up-turned passage, said second baflie being slotted.
4. Aburner having a burner chamber with jet openings leading therefrom and with a depression at the inlet end towhich the inlet leads; a baie extending from the end of the chamber over-the depression and forming an upf-turned passage nearer the inlet end of the burner than lthe center of the burner; and a second baffle over the up-turned passage forming a larger passage between the baffles than the opening between the second baiie andthe wall of the chamber. f
5. A burner having a burner chamber with jet openings leading therefrom and with a depression at the inlet end to which the inlet leads; a baffle extending from the end of the chamber over the depression and forming an up-turned passage nearer the inlet end of the burner than the center of the burner; a second baffle over the up-turned passage; and a shoulder at the bottom of the chamber in advance of the opening between the second baffle and the wall of the chamber at the end of the depression.
In testimony whereof I have hereunto set my hand.
CARL H. I-IOFFSTETTER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US481798A US1451072A (en) | 1921-07-01 | 1921-07-01 | Burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US481798A US1451072A (en) | 1921-07-01 | 1921-07-01 | Burner |
Publications (1)
Publication Number | Publication Date |
---|---|
US1451072A true US1451072A (en) | 1923-04-10 |
Family
ID=23913438
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US481798A Expired - Lifetime US1451072A (en) | 1921-07-01 | 1921-07-01 | Burner |
Country Status (1)
Country | Link |
---|---|
US (1) | US1451072A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2870830A (en) * | 1954-10-28 | 1959-01-27 | American Infra Red Radiant Co | Gas burners |
US3192989A (en) * | 1962-11-26 | 1965-07-06 | Avy L Miller | Gas burner |
US3361367A (en) * | 1964-12-18 | 1968-01-02 | Vaillant Joh Kg | Gas burner |
US3363845A (en) * | 1965-07-15 | 1968-01-16 | Lincoln Brass Works | Burner that creates uniform flame size by using progressively smaller holes |
US5025831A (en) * | 1990-08-24 | 1991-06-25 | Exxon Research & Engineering Company | Compact radial flow distributor |
US20150147703A1 (en) * | 2013-11-22 | 2015-05-28 | Lennox Industries Inc. | Burner assembly |
-
1921
- 1921-07-01 US US481798A patent/US1451072A/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2870830A (en) * | 1954-10-28 | 1959-01-27 | American Infra Red Radiant Co | Gas burners |
US3192989A (en) * | 1962-11-26 | 1965-07-06 | Avy L Miller | Gas burner |
US3361367A (en) * | 1964-12-18 | 1968-01-02 | Vaillant Joh Kg | Gas burner |
US3363845A (en) * | 1965-07-15 | 1968-01-16 | Lincoln Brass Works | Burner that creates uniform flame size by using progressively smaller holes |
US5025831A (en) * | 1990-08-24 | 1991-06-25 | Exxon Research & Engineering Company | Compact radial flow distributor |
US20150147703A1 (en) * | 2013-11-22 | 2015-05-28 | Lennox Industries Inc. | Burner assembly |
US10151479B2 (en) * | 2013-11-22 | 2018-12-11 | Lennox Industries Inc. | Burner assembly |
US11054132B2 (en) | 2013-11-22 | 2021-07-06 | Lennox Industries Inc. | Burner assembly |
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