GB597151A - Improvements in apparatus for the combustion of fuel - Google Patents
Improvements in apparatus for the combustion of fuelInfo
- Publication number
- GB597151A GB597151A GB14560/43A GB1456043A GB597151A GB 597151 A GB597151 A GB 597151A GB 14560/43 A GB14560/43 A GB 14560/43A GB 1456043 A GB1456043 A GB 1456043A GB 597151 A GB597151 A GB 597151A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- conical
- jacket
- conical members
- outer casing
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
- F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
597,151. Generating combustion products under pressure. BONVILLIAN, C. A., BRIERLY, R. C., and LETVIN, S. Sept. 6, 1943, No. 14560. Convention date, March 13. [Class 51 (i)] [Also in Groups XIII and XXVI] In apparatus for generating combustion products under pressure, for use in gas turbine systems, vapour generators or superheaters, fluid heaters or for the jet propulsion of aircraft, comprising a combustion chamber into which fuel and primary air are projected, secondary air being supplied from a surrounding air space, the chamber is formed by a number of co-axial conical members fitted with outwardly directed radiating members arranged longitudinally. In the form shown in Fig. 2, the apparatus comprises an outer casing 25 of generally ellipsoidal shape in which is mounted a number of truncated conical members 116, 120, 121, 122 and 123, the latter having an outwardly flared part 124 and the members being arranged so that there are gaps 26 through which secondary air is supplied from a surrounding space, the members being provided with radial longitudinally disposed fins 126 ... 129. The member 116 is fitted with a flange 117 to which is secured a second flange 119 carrying a conical member 118 into which the flame is projected, an observation tube 131 being provided. The conical members are under the influence of spring pistons 52 to permit expansion and the gap between the members 122, 123 may be adjusted by screw and nut devices 134. In another form, the outer casing 25, Fig. 3, is cylindrical with a conical discharge end and is provided with a jacket 48 through which a medium to be heated is passed thus serving as a waste-heat boiler, a superheater, or smoke producer as well as for cooling the casing 25. The jacket may be divided by a partition 51 which may be perforated and serve as a support or solid to divide the jacket into compartments which serve separate purposes. The radial vanes 39 are arranged in the gaps 26 between the conical members 27 some or all of which can be adjusted longitudinally by a rack 41 and pinion 44. Fig. 7 shows a similar form in which the outer casing 60 at one end provides a jacket 48 leading by a passage 60<1> to the space outside the conical members 27 whereby a medium introduced at 61 into the jacket is brought into direct contact with the combustion gases. In other forms the vanes on the conical members are separated by ring spacers or the conical members may be replaced by a helix. In a further modification the conical members overlap concentrically, the spaces between them leading from different supplies. Specification 597,205 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US597151XA | 1943-03-13 | 1943-03-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB597151A true GB597151A (en) | 1948-01-20 |
Family
ID=22024777
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14560/43A Expired GB597151A (en) | 1943-03-13 | 1943-09-06 | Improvements in apparatus for the combustion of fuel |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB597151A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2617255A (en) * | 1947-05-12 | 1952-11-11 | Bbc Brown Boveri & Cie | Combustion chamber for a gas turbine |
DE1052750B (en) * | 1954-02-26 | 1959-03-12 | Rolls Royce | Wall of a combustion chamber for liquid fuel, especially in gas turbines |
DE1059719B (en) * | 1955-06-16 | 1959-06-18 | Jan Jerie Dr Ing | Cooled wall of a combustion chamber, especially for gas turbines |
US3352106A (en) * | 1964-12-23 | 1967-11-14 | Pianko Marc | Combustion chamber with whirling slots |
CN113028406A (en) * | 2021-03-09 | 2021-06-25 | 信丰县包钢新利稀土有限责任公司 | Device and method for efficiently and environmentally separating oil substances in neodymium iron boron waste |
-
1943
- 1943-09-06 GB GB14560/43A patent/GB597151A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2617255A (en) * | 1947-05-12 | 1952-11-11 | Bbc Brown Boveri & Cie | Combustion chamber for a gas turbine |
DE1052750B (en) * | 1954-02-26 | 1959-03-12 | Rolls Royce | Wall of a combustion chamber for liquid fuel, especially in gas turbines |
DE1059719B (en) * | 1955-06-16 | 1959-06-18 | Jan Jerie Dr Ing | Cooled wall of a combustion chamber, especially for gas turbines |
US3352106A (en) * | 1964-12-23 | 1967-11-14 | Pianko Marc | Combustion chamber with whirling slots |
CN113028406A (en) * | 2021-03-09 | 2021-06-25 | 信丰县包钢新利稀土有限责任公司 | Device and method for efficiently and environmentally separating oil substances in neodymium iron boron waste |
CN113028406B (en) * | 2021-03-09 | 2023-08-15 | 信丰县包钢新利稀土有限责任公司 | Device and method for efficiently and environmentally-friendly separating oily substances from NdFeB waste |
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