POWER PLANT WITH EMERGENCY FUEL SYSTEM
20180209353 ยท 2018-07-26
Assignee
Inventors
- Manfred Nixdorf (Mutterstadt, DE)
- Karl-Heinz Persicke (Niederdorfelden, DE)
- Wilhelm Thiele (Buckenhof, DE)
Cpc classification
F05D2270/335
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/72
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C3/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/09
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2230/80
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E20/16
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
F25J1/0251
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/232
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/76
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/0022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C9/46
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/141
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/224
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02C9/46
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/141
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C3/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method for operating a power plant having a gas turbine and an emergency fuel system where in a normal operating state, gas is supplied from a supply line to the combustion process of the gas turbine, and in addition gas is supplied from the supply line to a gas liquefaction plant where it is liquefied, forming a liquid gas which is stored in a liquid gas store. In special operating state, liquefied gas is drawn from the liquid gas store and is evaporated in an evaporator, and is fed in the gaseous state into the combustion process of the gas turbine.
Claims
1.-12. (canceled)
13. A method for operating a power plant having a gas turbine and an emergency fuel system, the method comprising: in a normal operating state, feeding gas from a supply line to the combustion process of the gas turbine, and, in addition, feeding gas from the supply line to a gas liquefaction plant and liquefied therein, wherein a liquefied gas is formed and stored in a liquefied gas tank, and in a special operating state, extracting liquefied gas from the liquefied gas tank, and evaporating in an evaporator, and in a gaseous state, feeding into the combustion process of the gas turbine, in the special operating state, feeding evaporated gas from the liquefied gas tank back into the supply line in order to compensate pressure fluctuations in the supply line or, in the event of a complete supply failure, to supply other consumers, which are connected to the supply line, with gas.
14. The method as claimed in claim 13, wherein, in the gas liquefaction plant, less than 5% of the electric power of the power plant is used for liquefaction of the gas.
15. The method as claimed in claim 13, wherein the gas liquefaction plant is additionally used in the normal operating state in order to utilize power control of the power plant by controlled start-up or shutdown of said gas liquefaction plant.
16. The method as claimed in claim 13, wherein, in the special operating state, the cold energy which becomes free during evaporation in the evaporator is used for cooling the intake air of the gas turbine.
17. The method as claimed in claim 15, wherein the gas liquefaction plant is additionally used in the normal operating state for frequency control or frequency back-up.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0031] Exemplary embodiments of the invention are described below based on figures. In the drawings:
[0032]
[0033]
[0034]
[0035]
DETAILED DESCRIPTION OF INVENTION
[0036]
[0037] In addition to the combustion process 4, gas 5 is also fed from the supply line 3 to a gas liquefaction plant 6. The gas 5 is liquefied in the gas liquefaction plant 6, wherein a liquefied gas (LNG) is formed. The liquefied gas (LNG) is stored in a liquefied gas tank 7. The liquefied gas tank corresponds to a tank which is designed so that the liquefied gas (LNG) can be cryogenically stored in it. In the present exemplary embodiment, the tank has a storage volume of 30 T m.sup.3.
[0038] With this, in the special operating state an operation of the gas turbine 2 would be possible for up to 14 days even in the event of failure of the supply line 3. In the present example, the gas liquefaction plant 6 has a throughput volume of 1.7 kg/s. Therefore, it is in a position to fully fill up the liquefied gas tank 7 within a year in the normal operating state of the power plant 1.
[0039]
[0040] In the example of
[0041] Not shown in
[0042]
[0043]
[0044] The gas liquefaction plant 6 is connected in a feeding manner to the supply line 3, wherein a control valve can be integrated into the connecting line in order to control the proportion of gas for the gas liquefaction plant 6. The gas liquefaction plant 6 is connected to the liquefied gas tank 7 via a line for liquefied gas. The liquefied gas tank 7 is connected via a connecting line for liquefied gas to the evaporator 8, wherein a control valve is connected into the connecting line. The liquefied gas tank 7 which is shown here is a pressurized tank which is why no subsequent pressure increase of the re-evaporated gas is required.
[0045] Not shown is an alternative variant of the liquefied gas tank 7 which is operated at atmospheric pressure and in which provision has to be made for an additional pump in order to bring the liquefied gas up to the pressure level of the gas supply line again. The pump in this case is advantageously provided between the liquefied gas tank 7 and the evaporator 8.
[0046] The evaporator 8 is connected in a feeding manner to the secondary side 15 of the heat exchanger 14. The secondary side of the heat exchanger 14 is connected in a discharging manner to the supply line 3, wherein a control valve is connected into this connecting line. The heat exchanger 14 is connected on the primary side into the intake air line 17 of the compressor unit 18 of the gas turbine, wherein the feed and discharge lines to the heat exchanger are equipped in each case with control valves.
[0047] A power plant 1, which according to this method is retrofitted with, or equipped with, an emergency fuel system 11, has the capability of selectively operating the gas turbine 2 with gas from the supply line 3 or with evaporated gas from the emergency fuel system.