GB627705A - Improvements in or relating to installations for supplying motive fluid to gas turbines - Google Patents
Improvements in or relating to installations for supplying motive fluid to gas turbinesInfo
- Publication number
- GB627705A GB627705A GB24419/46A GB2441946A GB627705A GB 627705 A GB627705 A GB 627705A GB 24419/46 A GB24419/46 A GB 24419/46A GB 2441946 A GB2441946 A GB 2441946A GB 627705 A GB627705 A GB 627705A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ashes
- water
- combustion
- container
- way
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/26—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
627,705. Generating combustion products under pressure. BABCOCK & WILCOX, Ltd. Aug. 16, 1946, No. 24419. Convention date, July 3, 1941. [Class 51 (i)] Pulverized fuel is burnt under pressure and the combustion gases are cleaned by separating the coarser ash particles and then separating the dust particles. The cleaned gases are supplied to a gas turbine. Pulverized fuel is fed from a storage bin 25, Fig. 4, alternately to containers 26 and 261. The container in use is closed at the top and the corresponding valve 27 or 27<SP>1</SP> is opened to allow the contents to flow by way of a motor-driven feeder 29 to an injector 32. Air flowing through the injector entrains the fuel and carries it to a burner 7 (Fig. 1, not shown) at the entrance 71 to a combustion chamber 1, Fig. 2. Air is supplied at 17 and passes through the annular space between the outer walls 4 and 41 and liners 16 and 5 ; part of it enters the combustion space through nozzles 10 and the remainder passes by way of outlet connections' 8 to the burner 7. A coiled tube for the circulation of cooling water may be located within the liner 5. Ashes.fall'through,an outlet 19 into a water container 33, Fig. 5, and are carried away by water flowing out through a pipe 38. Steam arising from the quenching of the ashes is condensed by water sprays from atomizers 35. The level of water in the container 33 is kept' constant: by a float 36 controlling a valve 37. Ashes which fail to be carried away are periodically removed from a pocket 40. Combustion gases pass by way of an outlet 20 to a filter identical' with that described in Specification 627,706; [Group XXVIII], for the removal of dust before being used in a gas turbine. An alternative ash removal means comprises a water-jacketed chamber 90 (Fig. 9, not shown) for. cooling the ashes, communicating through a valve with a drum for the reception of the cooled ashes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR627705X | 1941-07-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB627705A true GB627705A (en) | 1949-08-15 |
Family
ID=8989197
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24419/46A Expired GB627705A (en) | 1941-07-03 | 1946-08-16 | Improvements in or relating to installations for supplying motive fluid to gas turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB627705A (en) |
-
1946
- 1946-08-16 GB GB24419/46A patent/GB627705A/en not_active Expired
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