GB621610A - Gas turbine plant in combination with at least one pressure gas producer - Google Patents
Gas turbine plant in combination with at least one pressure gas producerInfo
- Publication number
- GB621610A GB621610A GB7194/47A GB719447A GB621610A GB 621610 A GB621610 A GB 621610A GB 7194/47 A GB7194/47 A GB 7194/47A GB 719447 A GB719447 A GB 719447A GB 621610 A GB621610 A GB 621610A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- producer
- combustion chamber
- heated
- combustion
- 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
- F02C3/28—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 using a separate gas producer for gasifying the fuel before combustion
Abstract
621,610. Gas turbine plant. AKT.-GES. BROWN, BOVERI, & CIE. March 14,1947, No. 7194. Convention date, April 12, 1946. [Class 110(iii)] Water gas, as a fuel for a gas turbine, is made in a producer 1 operating with highpressure superheated steam and is expanded down to the pressure of the gas turbine combustion chamber 7 in an additional turbine 6 which provides useful power. Water supplied by a feed pump 8 is evaporated in a boiler 5 heated by the turbine exhaust and is superheated in the cooling spaces of the producer 1. Air for the combustion chamber is pre-heated in a heat-exchanger 4. The producer may be heated by the whole or part of the gases from the combustion chamber. In the latter case, the part is further compressed to provide for the pressure drop in the producer, or, the products of combustion are delivered to an intermediate point in the turbine. Two or more producers operating in sequence 1A, 1B, Fig. 3, are provided with pre-heated combustion air from the turbine compressor 2, during the heating periods, and discharge the products of combustion either to the turbine direct, or, to the turbine combustion chamber 7. The water gas generated in the intervening periods is expanded in turbine 6 in front of the combustion chamber 7. The heating shell of the producer may form the turbine combustion chamber.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH621610X | 1946-04-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB621610A true GB621610A (en) | 1949-04-12 |
Family
ID=4524121
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7194/47A Expired GB621610A (en) | 1946-04-12 | 1947-03-14 | Gas turbine plant in combination with at least one pressure gas producer |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB621610A (en) |
-
1947
- 1947-03-14 GB GB7194/47A patent/GB621610A/en not_active Expired
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