CN107093752A - A kind of aircraft soild oxide hydrogen fuel cell gas turbine generating system - Google Patents
A kind of aircraft soild oxide hydrogen fuel cell gas turbine generating system Download PDFInfo
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- CN107093752A CN107093752A CN201710323518.2A CN201710323518A CN107093752A CN 107093752 A CN107093752 A CN 107093752A CN 201710323518 A CN201710323518 A CN 201710323518A CN 107093752 A CN107093752 A CN 107093752A
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- fuel cell
- hydrogen fuel
- soild oxide
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- 239000000446 fuel Substances 0.000 title claims abstract description 80
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 title claims abstract description 49
- 239000001257 hydrogen Substances 0.000 title claims abstract description 49
- 229910052739 hydrogen Inorganic materials 0.000 title claims abstract description 49
- 239000007789 gas Substances 0.000 title claims abstract description 36
- 238000002485 combustion reaction Methods 0.000 claims abstract description 16
- 238000010438 heat treatment Methods 0.000 claims abstract description 11
- 238000004891 communication Methods 0.000 claims description 12
- 230000008676 import Effects 0.000 claims description 9
- 230000005611 electricity Effects 0.000 claims description 8
- 239000002828 fuel tank Substances 0.000 claims description 5
- 239000007787 solid Substances 0.000 abstract description 6
- 238000006243 chemical reaction Methods 0.000 abstract description 4
- 230000001172 regenerating effect Effects 0.000 abstract description 4
- 230000036647 reaction Effects 0.000 abstract description 2
- 238000010248 power generation Methods 0.000 description 4
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 3
- 239000003546 flue gas Substances 0.000 description 3
- 239000003792 electrolyte Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 239000002918 waste heat Substances 0.000 description 2
- 241000937378 Everettia interior Species 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000005842 biochemical reaction Methods 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/04—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
- H01M8/04007—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids related to heat exchange
- H01M8/04014—Heat exchange using gaseous fluids; Heat exchange by combustion of reactants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/04—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
- H01M8/04007—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids related to heat exchange
- H01M8/04014—Heat exchange using gaseous fluids; Heat exchange by combustion of reactants
- H01M8/04022—Heating by combustion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
- B64D2041/005—Fuel cells
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
-
- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Life Sciences & Earth Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fuel Cell (AREA)
Abstract
A kind of aircraft soild oxide hydrogen fuel cell gas turbine generating system, belongs to the technical field of aircraft generating system.The present invention utilizes the energy not utilized including SOFC high-temperature residual heat tail gas, capacity usage ratio is improved, while the complete hydrogen fuel of unreacted drives turbine acting to drive compressor and generator operation further to improve capacity usage ratio in burning Indoor Combustion.Meanwhile, heat regenerative system heating air and hydrogen fuel meet the hot conditions that solid oxide cell reaction needs, and the used heat of discharge gas is make use of again, energy utilization efficiency is improved.Electric power is provided after the electric energy for electric energy and the fuel cell generation that turbine is produced is grid-connected jointly for aircraft.
Description
Technical field
The invention belongs to the technical field of aircraft generating system；Specifically related to a kind of aircraft soild oxide hydrogen fuel electricity
Pond gas turbine generating system.
Background technology
With the growth of aircraft hang time, how stability and high efficiency for aircraft energize one as aircraft development it is important
Problem.The generating efficiency of aircraft generating system how is improved in the case where ensureing that body is compact turns into the focus of research.
Aircraft flight requires very high in high-altitude, rarefaction of air to compressor.Whirlpool in overlength endurance high-altitude vehicle dynamical system
The main function of wheel generates electricity as secondary function to drive compressor work, and fuel cell needs elevated pressures to realize efficiently
The problem of rate.
Existing aircraft electrical power supply system structure is numerous and jumbled, and various informative, reliability is low.It is indirectly or straight using engine more than main power source
Tape splicing moves generator, and using battery etc. more than other supplementary energies, secondary energy sources, capacity usage ratio is low, and generating efficiency is low.For
For battery, service life is indefinite, deficiency in economic performance；Protect and consider for energy and environment, energy utilization rate is low, it is difficult
To realize pollution reduction.
The content of the invention
The invention solves the problems that there is the technology that power-supplying forms are more, reliability is low, system is numerous and jumbled, generating efficiency is low in prior art
Problem；There is provided a kind of new aircraft soild oxide hydrogen fuel cell-gas turbine generating system, with reference to fuel cell
With the advantage of gas turbine, the two mutual supplement with each other's advantages.Using electric power energy of the hydrogen fuel as aircraft, mass energy density is big, energy
More heats are exchanged for smaller fuel mass, and product is pollution-free.Meanwhile, it is energy invention increases heat regenerative system
Measure utilization rate higher.Present system discharges the chemical energy in hydrogen fuel using SOFC, can make fuel profit
Do not limited with being compared with conventional combustion turbine acting by Carnot cycle.Simultaneously again combine gas turbine, by fuel cell not
Chemical energy in the hydrogen fuel of reaction further discharges.Present system uses backheat subsystem again, by the high temperature of turbine outlet
Flue gas further utilizes the heat energy in tail gas successively by air preheater and fuel preheater to fuel and air preheat.Three
Behave integrate use so that whole system energy utilization reach as far as possible it is most abundant.
In order to solve the above technical problems, a kind of aircraft soild oxide hydrogen fuel cell gas turbine power generation of the present invention
System, including soild oxide hydrogen fuel cell 4, combustion chamber 5, inverter 10, generator 8, turbine 6, compressor 7, air are pre-
Hot device 9, fuel preheater 3, the outlet of fuel preheater 3 and the inlet communication of the anode of soild oxide hydrogen fuel cell 4, air
The outlet of preheater 9 and the inlet communication of the negative electrode of soild oxide hydrogen fuel cell 4, the sun of soild oxide hydrogen fuel cell 4
Pole export with cathode outlet respectively with the inlet communication on combustion chamber 5, the outlet of combustion chamber 5 and the inlet communication of turbine 6；Turbine
A 6 output work part is transmitted to the compressor coaxially connected with turbine 6, remaining part driving and the coaxially connected hair of turbine 6
Electric power generation, the outlet of compressor is connected with air preheater 9, air (i.e. interior of aircraft air) in the import of compressor and cabin
Communicate；The external output direct current of soild oxide hydrogen fuel cell 4, generator externally exports alternating current, by with solid oxidation
The inverter 10 that thing hydrogen fuel cell 4 is connected is converted to exchange electricity output.
The heating outlet of the turbine 6 is connected with the heat inlet of air preheater, and the heating outlet and fuel of air preheater 9 are pre-
The heat inlet connection of hot device 3, the heating outlet and atmosphere of fuel preheater 3, more than SOFC high temperature
The energy not utilized including hot exhaust gas, improves capacity usage ratio, while the complete hydrogen fuel of unreacted is in burning Indoor Combustion
Turbine acting is driven to drive compressor and generator operation further to improve capacity usage ratio.Meanwhile, heat regenerative system heating is empty
Gas and hydrogen fuel meet the hot conditions that solid oxide cell reaction needs, and the used heat of discharge gas is make use of again, improve
Energy utilization efficiency.Electric power is provided after the electric energy for electric energy and the fuel cell generation that turbine is produced is grid-connected jointly for aircraft.
The import of fuel preheater 3 and the outlet of blower fan 2 (or pump), the import of blower fan 2 and the outlet of fuel tank 1
Connection.
The inverter 10 is connected with electrical equipment 11, and electrical equipment 11 is aircraft electrical equipment.
HTHP tail gas promotes turbine acting after the present invention is burnt through catalytic combustor, and electricity is produced through alternating current generator
Can, and SOFC produce electric energy after inverter grid-connected confession aircraft electrical equipment (such as whirlpool oar, lighting apparatus
Deng) use so that the generating efficiency of whole power system reaches higher level.
Hydrogen and air of the present invention by preheating, into SOFC, hydrogen major part and air hair
Biochemical reaction produces electric energy, and remainder enters the burned utilization in combustion chamber.HTHP tail gas promotes turbine to do after burning
Work(, electric energy is produced through generator, grid-connected after inverter to be used for aircraft electrical equipment.Turbine outlet high-temperature tail gas, first simultaneously
To air preheat, then hydrogen fuel preheating is given, finally drain into air, heat energy is sufficiently utilized.
The fuel cell power generation efficiency high of the present invention, offgas outlet temperature is high, and gas turbine can make full use of fuel cell
The energy of incomplete reactive fuel and high-temperature tail gas, rationally make use of and does not utilize energy including fuel cell tail gas waste heat, enter
One step improves the efficiency of aircraft generating system.
Present invention employs SOFC, cycle efficieny by Carnot cycle without being limited, capacity usage ratio
Compare high, SOFC can obtain 800~1000 DEG C of high-temperature flue gas, be conducive to gas turbine power generation to obtain high
Efficiency.
Not utilized using energy by the turbine of gas turbine including fuel cell tail gas waste heat of the present invention, equivalent to whirlpool
Wheel inlet gas is preheated, and is done work and generated electricity by turbine, and the electric energy that turbine is produced and the electric energy that fuel cell is produced are common
Electric power is provided for aircraft.
Invention increases heat regenerative system, energy utilization is more abundant, while so that the structure of whole system is more compact.
The present invention is more using hydrogen fuel unit mass thermal discharge, and product is water, more environmentally-friendly without any pollution.
The present invention provides a large amount of electric energy for airplane centralized, and the accessory system of aircraft can be from this with energy equipment with other
In power taking utilize.
The present invention due to electrolyte be solid, without electrolyte evaporation with leakage the problem of.And electrode does not also corrode
The problem of, running life is long, further, since the pond body material of constituent material is entirely solid, battery appearance has flexibility.
Brief description of the drawings
Fig. 1 is the schematic diagram of the structure of the present invention.
Embodiment
Illustrated with reference to Fig. 1, a kind of aircraft is sent out with soild oxide hydrogen fuel cell gas turbine in present embodiment
Electric system is pre- including soild oxide hydrogen fuel cell 4, combustion chamber 5, inverter 10, generator 8, turbine 6, compressor 7, air
Hot device 9, fuel preheater 3,
The outlet of fuel preheater 3 and the inlet communication of the anode of soild oxide hydrogen fuel cell 4,
The outlet of air preheater 9 and the inlet communication of the negative electrode of soild oxide hydrogen fuel cell 4,
The anode export of soild oxide hydrogen fuel cell 4 and cathode outlet respectively with the inlet communication on combustion chamber 5, combustion
Burn the outlet of room 5 and the inlet communication of turbine 6；
An output work part for turbine 6 is transmitted to the compressor coaxially connected with turbine 6, remaining part driving and turbine 6
Coaxially connected electrical power generators,
The outlet of compressor is connected with air preheater 9, and the import of compressor is communicated with air in cabin；
The external output direct current of soild oxide hydrogen fuel cell 4, generator externally exports alternating current, by with solid oxygen
The inverter 10 that compound hydrogen fuel cell 4 is connected is converted to exchange electricity output.
The heating outlet of the turbine 6 is connected with the heat inlet of air preheater, and the heating outlet and fuel of air preheater 9 are pre-
The heat inlet connection of hot device 3, the heating outlet and atmosphere of fuel preheater 3.
The import of fuel preheater 3 and the outlet of pump 2, the import of pump 2 and the outlet of fuel tank 1, fuel tank 1
Built with hydrogen；
The inverter 10 is connected with whirlpool oar.
Described pump 2 sends into fuel preheater 3 after hydrogen fuel is extracted out from fuel tank, and the hydrogen fuel after being preheated is sent
Enter soild oxide hydrogen fuel cell 4 and air reaction, produce electric energy；The complete hydrogen of unreacted, will in fuel cell tail gas
Tail gas be passed through in combustion chamber 5 with air mixed combustion, obtain high-temperature flue gas and done work into turbine 6.Turbine 6 drives coaxial pressure
Mechanism of qi 7 and generator 8 work, with the grid-connected rear drive of electric energy of fuel cell in the electric energy feeding inverter 10 that generator 8 is sent
Electrical equipment 11 is worked, and electric power is provided to aircraft.On the other hand, turbine 6 export high-temperature tail gas first pass through air preheater 9 to
Air preheat from compressor 8, preheats to hydrogen fuel by fuel preheater 3, is finally discharged into air.
The power cycle system effectiveness of the present invention is high, highly reliable.The hydrogen fuel that fuel cell does not react completely, Ke Yitong
Cross the work done of combustion turbine 6 and obtain more multi-energy, improve the power output of turbine 6, and then improve the boosting capability of compressor.With it is common
Gas turbine is compared, and improves efficiency.In addition, turbine 6 is exported into tail gas is used for backheat, energy utilization can be further improved
Rate.The present embodiment can preferably meet need of the aircraft to aricraft electrical power reliability and stability and energy utilization high efficiency
Ask.
In addition, the electric energy obtained can be used for other electronic equipments on aircraft, stable energy is provided for them, is also full electricity
One big advantage of aircraft.
Claims (6)
1. a kind of aircraft soild oxide hydrogen fuel cell gas turbine generating system, including soild oxide hydrogen fuel cell
(4), combustion chamber (5), inverter (10), generator (8), turbine (6), compressor (7), air preheater (9), fuel preheater
(3), it is characterised in that the outlet of fuel preheater (3) and the inlet communication of soild oxide hydrogen fuel cell (4) anode, air
The outlet of preheater (9) and the inlet communication of soild oxide hydrogen fuel cell (4) negative electrode, soild oxide hydrogen fuel cell
(4) anode export and cathode outlet respectively with the inlet communication on combustion chamber (5), outlet and the turbine (6) of combustion chamber (5)
Inlet communication；An output work part for turbine (6) be transmitted to the coaxially connected compressor of turbine (6), the driving of remaining part with
The coaxially connected electrical power generators of turbine (6), the outlet of compressor is connected with air preheater (9), the import of compressor and cabin
Interior air is communicated；Soild oxide hydrogen fuel cell (4) externally exports direct current, and generator externally exports alternating current, by with
The inverter (10) of soild oxide hydrogen fuel cell (4) connection is converted to exchange electricity output.
2. a kind of aircraft according to claim 1 soild oxide hydrogen fuel cell gas turbine generating system, it is special
Levy and be that the heating outlet of the turbine (6) is connected with the heat inlet of air preheater, the heating outlet and fuel of air preheater (9)
The heat inlet connection of preheater (3), the heating outlet and atmosphere of fuel preheater (3).
3. a kind of aircraft according to claim 1 soild oxide hydrogen fuel cell gas turbine generating system, it is special
The outlet for being the import of fuel preheater (3) with blower fan (2) is levied, the import of blower fan (2) connects with the outlet of fuel tank (1)
It is logical.
4. a kind of aircraft according to claim 3 soild oxide hydrogen fuel cell gas turbine generating system, it is special
Levy and be to replace blower fan (2) with pump.
5. a kind of aircraft according to claim 1 soild oxide hydrogen fuel cell gas turbine generating system, it is special
Levy and be that the inverter (10) is connected with electrical equipment (11).
6. a kind of aircraft according to claim 5 soild oxide hydrogen fuel cell gas turbine generating system, it is special
Levy and be that electrical equipment (11) is aircraft electrical equipment (11).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110490040.9A CN113161578A (en) | 2017-05-09 | 2017-05-09 | Solid oxide hydrogen fuel cell gas turbine power generation system for airplane |
| CN201710323518.2A CN107093752A (en) | 2017-05-09 | 2017-05-09 | A kind of aircraft soild oxide hydrogen fuel cell gas turbine generating system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710323518.2A CN107093752A (en) | 2017-05-09 | 2017-05-09 | A kind of aircraft soild oxide hydrogen fuel cell gas turbine generating system |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN202110490040.9A Division CN113161578A (en) | 2017-05-09 | 2017-05-09 | Solid oxide hydrogen fuel cell gas turbine power generation system for airplane |
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| CN107093752A true CN107093752A (en) | 2017-08-25 |
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|---|---|---|---|
| CN201710323518.2A Pending CN107093752A (en) | 2017-05-09 | 2017-05-09 | A kind of aircraft soild oxide hydrogen fuel cell gas turbine generating system |
| CN202110490040.9A Pending CN113161578A (en) | 2017-05-09 | 2017-05-09 | Solid oxide hydrogen fuel cell gas turbine power generation system for airplane |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN202110490040.9A Pending CN113161578A (en) | 2017-05-09 | 2017-05-09 | Solid oxide hydrogen fuel cell gas turbine power generation system for airplane |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108386344A (en) * | 2018-03-09 | 2018-08-10 | 重庆大学 | The electrification energy storage system and control method of fuel cell and compressed-air energy storage coupling |
| CN108583911A (en) * | 2017-12-14 | 2018-09-28 | 南京航空航天大学 | A kind of high continuation of the journey zero-emission hybrid power system of aviation |
| CN113285093A (en) * | 2021-05-14 | 2021-08-20 | 中国人民解放军海军工程大学 | Fuel cell-solar power generation system based on methanol steam reforming |
| CN113793964A (en) * | 2021-09-10 | 2021-12-14 | 西安热工研究院有限公司 | Thermal power peak regulation system based on solid oxide fuel cell and working method |
| CN115498225A (en) * | 2022-08-15 | 2022-12-20 | 哈尔滨工业大学 | Combined power generation system and method of hot ammonia turbine and fuel cell |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101071864A (en) * | 2006-05-12 | 2007-11-14 | 田云 | Vehicular fuel cell hybrid power device |
| CN101272955A (en) * | 2005-09-29 | 2008-09-24 | 空中客车德国有限公司 | Energy supply system for supplying energy to aircraft systems |
| CN102449835A (en) * | 2009-03-30 | 2012-05-09 | 莲花汽车有限公司 | A reheated gas turbine system having a fuel cell |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103972559A (en) * | 2014-05-09 | 2014-08-06 | 东南大学 | Method and device for biomass combined cycle power generation and carbon dioxide separation |
-
2017
- 2017-05-09 CN CN201710323518.2A patent/CN107093752A/en active Pending
- 2017-05-09 CN CN202110490040.9A patent/CN113161578A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101272955A (en) * | 2005-09-29 | 2008-09-24 | 空中客车德国有限公司 | Energy supply system for supplying energy to aircraft systems |
| CN101071864A (en) * | 2006-05-12 | 2007-11-14 | 田云 | Vehicular fuel cell hybrid power device |
| CN102449835A (en) * | 2009-03-30 | 2012-05-09 | 莲花汽车有限公司 | A reheated gas turbine system having a fuel cell |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108583911A (en) * | 2017-12-14 | 2018-09-28 | 南京航空航天大学 | A kind of high continuation of the journey zero-emission hybrid power system of aviation |
| CN108386344A (en) * | 2018-03-09 | 2018-08-10 | 重庆大学 | The electrification energy storage system and control method of fuel cell and compressed-air energy storage coupling |
| CN113285093A (en) * | 2021-05-14 | 2021-08-20 | 中国人民解放军海军工程大学 | Fuel cell-solar power generation system based on methanol steam reforming |
| CN113793964A (en) * | 2021-09-10 | 2021-12-14 | 西安热工研究院有限公司 | Thermal power peak regulation system based on solid oxide fuel cell and working method |
| CN115498225A (en) * | 2022-08-15 | 2022-12-20 | 哈尔滨工业大学 | Combined power generation system and method of hot ammonia turbine and fuel cell |
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| Publication number | Publication date |
|---|---|
| CN113161578A (en) | 2021-07-23 |
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