GB899255A - A gas turbine plant - Google Patents
A gas turbine plantInfo
- Publication number
- GB899255A GB899255A GB4106558A GB4106558A GB899255A GB 899255 A GB899255 A GB 899255A GB 4106558 A GB4106558 A GB 4106558A GB 4106558 A GB4106558 A GB 4106558A GB 899255 A GB899255 A GB 899255A
- Authority
- GB
- United Kingdom
- Prior art keywords
- heat
- turbine
- exchange section
- combustion chamber
- chamber
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/05—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy
- F02C1/06—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy using reheated exhaust gas
-
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/002—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid using an auxiliary fluid
- F02C1/005—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid using an auxiliary fluid being recirculated
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- High Energy & Nuclear Physics (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
899,255. Gas turbine plant. MIKULA, I. Dec. 19, 1958 [Dec. 21, 1957], No. 41065/58. Class 110 (3). [Also in Group XIII] In a gas turbine plant operating on an open cycle wherein heat is introduced into the cycle at a point downstream of the turbine, the heating of the driving medium to the admission temperature of the turbine is effected by a high temperature recuperation heater which comprises at least a first heat-exchange section for the combustion products containing the combustion chamber or coupled with the combustion chamber and arranged downstream of the turbine and at least a second heat-exchange section for the driving medium introduced upstream of the turbine, the first and second heat exchange sections being coupled together by means of a closed heat carrying circuit for a suitable liquid or molten salt circulated by a pump. Air after compression by a compressor 6 is heated before admission to the turbine 5 by means of a high temperature recuperation heater consisting of a heat-exchange section 1 heated by combustion products from a combustion chamber fed with combustion air by the turbine 5 and a heat-exchange section 2 which heats the air. The combustion chamber may consist of the actual combustion chamber and a turbulent cooling chamber. The exhaust from the section 1 may be used to dry fuel or introduced into the combustion chamber of a steam generator. The heat is transferred from the heat exchange section 1 to the heat exchange section 2 by means of a suitable liquid metal or molten salt circulated in the circuit 3 by a pump 4. Suitable metals are sodium or eutectic 56% sodium and the remainder potassium. The combustion products from industrial furnaces or a steam generator may be used to heat the heat exchange section 1. The tubes of this section may be made of aluminium-iron alloy. The active part of the heat-exchange section 2 may be enclosed in a pressure vessel so that it is not exposed to pressure stresses. A compensation chamber may be built into the circuit 3 which chamber acts as a storage container and a melting chamber which may be heated by an independent liquid fuel burner on starting. The recuperation heater may be used for reheating the working medium between the individual expansion stages of the turbine or between groups of stages or between individual turbines connected in series. Specifications 578,686, 724,176, 732,778, 733,476 and 733,483 are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CS496457 | 1957-12-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB899255A true GB899255A (en) | 1962-06-20 |
Family
ID=5393557
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4106558A Expired GB899255A (en) | 1957-12-21 | 1958-12-19 | A gas turbine plant |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH364657A (en) |
GB (1) | GB899255A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20160319746A1 (en) * | 2015-04-30 | 2016-11-03 | Fastlight Llc | Grid scale energy storage systems using thermal storage coupled with gas turbine air and steam injection |
-
1958
- 1958-12-19 GB GB4106558A patent/GB899255A/en not_active Expired
- 1958-12-20 CH CH6755858A patent/CH364657A/en unknown
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20160319746A1 (en) * | 2015-04-30 | 2016-11-03 | Fastlight Llc | Grid scale energy storage systems using thermal storage coupled with gas turbine air and steam injection |
WO2016176174A1 (en) * | 2015-04-30 | 2016-11-03 | Fastlight Llc | Grid scale energy storage systems using thermal storage coupled with gas turbine air and steam injection |
US10900417B2 (en) * | 2015-04-30 | 2021-01-26 | Powerphase Llc | Grid scale energy storage systems using thermal storage coupled with gas turbine air and steam injection |
Also Published As
Publication number | Publication date |
---|---|
CH364657A (en) | 1962-09-30 |
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