CN207925582U - A kind of fuel cell electrode auxiliary single stage turbocharger system - Google Patents
A kind of fuel cell electrode auxiliary single stage turbocharger system Download PDFInfo
- Publication number
- CN207925582U CN207925582U CN201820075214.9U CN201820075214U CN207925582U CN 207925582 U CN207925582 U CN 207925582U CN 201820075214 U CN201820075214 U CN 201820075214U CN 207925582 U CN207925582 U CN 207925582U
- Authority
- CN
- China
- Prior art keywords
- fuel cell
- turbine
- compressor
- single stage
- motor
- 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.)
- Active
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 37
- 230000001360 synchronised effect Effects 0.000 claims abstract description 4
- 238000005452 bending Methods 0.000 claims description 3
- 230000006835 compression Effects 0.000 claims 1
- 238000007906 compression Methods 0.000 claims 1
- 238000005183 dynamical system Methods 0.000 abstract description 3
- 239000007789 gas Substances 0.000 description 9
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000012528 membrane Substances 0.000 description 3
- 230000003071 parasitic effect Effects 0.000 description 3
- 238000003487 electrochemical reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 230000003137 locomotive effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005119 centrifugation Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
- Fuel Cell (AREA)
Abstract
The utility model discloses a kind of fuel cell electrode auxiliary single stage turbocharger system, including:Compressor, the turbine to recover energy and the driving motor of clean compressed air are provided to fuel cell, the compressor, turbine and driving motor are coaxially connected, and turbine is with compressor respectively at the both ends of machine shaft;The compressor uses the centrifugal compressor of radial-flow type/mixed-flow;The turbine is radial flow expansion turbine;The motor is permanent magnet synchronous motor.The utility model can meet the needs of high power fuel cell dynamical system, cover fuel cell power system full working scope range, and pressure charging system overall structure is compact, efficient.
Description
Technical field
The utility model is related to the electricity auxiliary single stage turbocharger systems and compressed air of Proton Exchange Membrane Fuel Cells
Runoff, the turbomachine in flow centrifugal compressors, and the turbomachine of radial-flow turbine that recovers energy.
Background technology
Fuel cell is the device that the chemical energy of fuel is directly changed into electric energy.Proton Exchange Membrane Fuel Cells has effect
The advantages that rate is high, power is big, power-on time is long, low noise, emission are few, becomes the car power source after traditional combustion engine
One of.Heart component of the fuel cell power system as fuel cell car is supplied by pile, air supply system, hydrogen
System and hydro-thermal management system composition.The major function of air supply system is provided completely in fuel cell car driving cycle
The compressed air of sufficient power demand, and the tail gas for recycling pile discharge does work for turbine.
Compressor is component mostly important in fuel battery air feed system, influences the pressure of fuel cell power system
Power, flow, humidity and parasitic power consumption.Power density is the important bottleneck of fuel cell industrialization, it is desirable that compressor arrangement is compact,
It is small, light-weight.The high pressure gas of pile is supplied to through compressor cannot contain impurity, in order to avoid Proton Exchange Membrane Fuel Cells
It is poisoned in electrochemical reaction process.When matching work with fuel cell power system, compressor tends in small flow, high pressure
It works under the operating mode of ratio, belongs to small discharge coefficient scope, and in often belonging to the matched turbo charge system of traditional combustion engine
Equal discharge coefficients scope, if traditional combustion engine pressure charging system is matched in fuel cell system, often nearly surging condition can not
Steady operation.
Centrifugal compressor can be applied individually to any fuel battery air feed system, can also be utilized with turbine match
Pile tail gas energy drives turbine rotation acting driving compressor.Since tail gas energy is limited, need to coordinate with high-speed electric expreess locomotive makes
With.The use of turbine can improve the efficiency of fuel cell power system with recovery section parasitic power;While pile tail gas is still
So there is higher temperature, if being directly discharged in air that thermal pollution can be caused, destroy natural environment and human residential environment.
Utility model content
The problem of in view of background technology, the purpose of this utility model is to provide one kind can meeting 60-100kW
The air supply system demand of high power fuel cell dynamical system, has the characteristics that compact-sized, efficient fuel cell
Vehicle electric assists single stage turbocharger system.
The another object of the utility model is to provide a kind of centrifugation that can cover fuel cell power system full working scope
Turbomachine structure.
To solve the above problems, technical solution adopted in the utility model is as follows:
A kind of fuel cell electrode auxiliary single stage turbocharger system, including:Clean compressed air is provided to fuel cell
Compressor, the turbine and driving motor that recover energy, the compressor, turbine and driving motor be coaxially connected, whirlpool
Turbine is with compressor respectively at the both ends of machine shaft;The compressor uses the centrifugal compressor of radial-flow type/mixed-flow;Institute
It is radial flow expansion turbine to state turbine;The motor is permanent magnet synchronous motor.
As an improvement of the above technical solution, the compressor impeller uses semi-open type, and blade conduit side is by wheel disk seal
It closes, the other side is opened wide.
As an improvement of the above technical solution, the compressor impeller blade curve form is hypsokinesis swept-back, and blade goes out
The bending direction and inclined direction of mouth are different with impeller direction of rotation.
Compared with prior art, the utility model has the beneficial effects that:
The utility model is related to a kind of fuel cell electrodes to assist single stage turbocharger system, the electricity auxiliary single-stage turbine
Pressure charging system includes compressor, turbine and driving motor.Compressor, turbine and driving motor are coaxially connected, compressor leaf
It is hypsokinesis swept-back that wheel, which uses semi-open type, blade curve form,;Turbine uses radial flow expansion turbine;Motor uses permanent magnetism
Synchronous motor, maximum speed reach 100000r/min or more;Bearing uses oil-free lubrication air paillon hydrodynamic bearing, compressed
The pressure-air of machine outlet does not contain impurity.The utility model can meet the needs of high power fuel cell dynamical system, cover
Lid fuel cell power system full working scope range, pressure charging system overall structure are compact, efficient.
Description of the drawings
Fig. 1 is the structural schematic diagram of the fuel cell turbo charge system for the embodiment for indicating the utility model.
Fig. 2 is to indicate Centrufugal compressor impeller blade pattern and discharge velocity triangle figure.
Specific implementation mode
The following examples illustrate the utility model, but is not intended to limit the scope of the present invention.Without departing substantially from this
In the case of utility model spirit and essence, to modifications or substitutions made by the utility model method, step or condition, belong to
The scope of protection of the utility model.
In fuel battery air feed system, the course of work of electricity auxiliary single-stage turbocharger is as follows:
Air passes through the filtering of air filter (1), into centrifugal compressor (2), the High Temperature Gas being pressurized through compressor (2)
Body is cooled by charge air cooler (9), and subsequently into fuel cell pile (5), electrochemical reaction, pile (5) occurs with hydrogen
The water that air and reaction generation is discharged enters condenser (6) together, and what is come out from condenser (6) is wet with overbottom pressure residual temperature
Air enters turbine (4), does work through turbine (4), drives compressor (2) to rotate together with motor (3), then passes through pipeline
Into mixing chamber (7), the use of turbine (4) can improve the efficiency of fuel cell power system with recovery section parasitic power;
Pile (5) tail gas still has higher temperature, if being directly discharged in air that thermal pollution can be caused, destroys natural environment and the mankind
Living environment.The water come out simultaneously from condenser (6) also enters mixing chamber, with react after be discharged to the hydrogen one of mixing chamber (7)
It is same to be discharged into air.
Centrifugal compressor is mainly formed by air intake duct, impeller body, without leaf or vaned diffuser, spiral case etc..Compressor
Impeller uses semi-open type, blade conduit side to be closed by wheel disc, and the other side is opened wide.Compressor impeller blade curve form is hypsokinesis
Swept-back, the bending direction and inclined direction of blade exit are different with impeller direction of rotation.Backward leaning vane,,, referring to Fig. 2.Back ward impeller air stream outlet absolute velocity is smaller so that air-flow flow losses in diffuser
It is small.Pressure rise is mainly completed in impeller internal, and the air-flow in impeller is acted on by centrifugal force, is not likely to produce boundary layer point
From so flow losses of the gas in impeller are smaller than in diffuser.The leaf road of back ward impeller is long, blade curvature compared with
Small, sectional area increase in leaf road is slower, and the equivalent divergent angle in the leaf road roads diffusion Du Heye is smaller, it is not easy to gas be made to be flowed in Ye Daozhong
Boundary layer separation is generated when dynamic, therefore efficiency is higher.Since fuel-cell vehicle centrifugal air compressor is to there is more stall margin
Harsh requirement is adopted different from diesel locomotive with centrifugal air compressor to make designed stall margin be extended to low discharge operating mode
Lean forward backward leaning vane export structure, using hypsokinesis swept-back exit vane structure, improves low flow rate condition centrifugal impeller
Working performance.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements done should be included in the utility model
Within protection domain.
The above content is in conjunction with specific embodiments to being described in detail made by the utility model, and it cannot be said that this practicality is new
Type specific implementation is only limitted to these explanations.For those skilled in the art of the present invention, this is not being departed from
Under the premise of utility model is conceived, a number of simple deductions or replacements can also be made, all shall be regarded as belonging to the utility model guarantor
The range of shield.
Claims (3)
1. a kind of fuel cell electrode assists single stage turbocharger system, which is characterized in that including:It is provided to fuel cell clean
The compressor (2) of compressed air, the turbine (4) to recover energy and driving motor (3), the compressor (2), turbine
(4) coaxially it is connected with driving motor (3), turbine (4) is with compressor (2) respectively at the both ends of motor (3) shaft;The compression
Machine (2) uses the centrifugal compressor of radial-flow type/mixed-flow;The turbine (4) is radial flow expansion turbine;The motor
(3) it is permanent magnet synchronous motor.
2. a kind of fuel cell electrode as described in claim 1 assists single stage turbocharger system, which is characterized in that the pressure
Contracting machine impeller uses semi-open type, blade conduit side to be closed by wheel disc, and the other side is opened wide.
3. a kind of fuel cell electrode as described in claim 1 assists single stage turbocharger system, which is characterized in that the pressure
Contracting machine impeller blade curve form is hypsokinesis swept-back, bending direction and inclined direction and the impeller direction of rotation phase of blade exit
It is different.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820075214.9U CN207925582U (en) | 2018-01-17 | 2018-01-17 | A kind of fuel cell electrode auxiliary single stage turbocharger system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820075214.9U CN207925582U (en) | 2018-01-17 | 2018-01-17 | A kind of fuel cell electrode auxiliary single stage turbocharger system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207925582U true CN207925582U (en) | 2018-09-28 |
Family
ID=63604314
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820075214.9U Active CN207925582U (en) | 2018-01-17 | 2018-01-17 | A kind of fuel cell electrode auxiliary single stage turbocharger system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207925582U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108172867A (en) * | 2018-01-17 | 2018-06-15 | 安徽明天氢能科技股份有限公司 | A single-stage turbocharging system assisted by fuel cell electricity |
| CN112290057A (en) * | 2019-07-24 | 2021-01-29 | 银隆新能源股份有限公司 | A fuel cell gas supply system based on turbocharging and its control method |
-
2018
- 2018-01-17 CN CN201820075214.9U patent/CN207925582U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108172867A (en) * | 2018-01-17 | 2018-06-15 | 安徽明天氢能科技股份有限公司 | A single-stage turbocharging system assisted by fuel cell electricity |
| CN112290057A (en) * | 2019-07-24 | 2021-01-29 | 银隆新能源股份有限公司 | A fuel cell gas supply system based on turbocharging and its control method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102644499B (en) | Bootstrap system based on Brayton cycle and UTILIZATION OF VESIDUAL HEAT IN electromotor | |
| CN104632356B (en) | Parallel type engine two-stage pressurization system with compressed air storage device and vehicle | |
| CN217641432U (en) | Fuel cell system and vehicle | |
| CN104500214A (en) | Engine supercharging system with compressed air storage device and vehicle with engine supercharging system | |
| CN105626266A (en) | Anti-surge air escape energy recycling system of gas turbine | |
| CN108172867A (en) | A single-stage turbocharging system assisted by fuel cell electricity | |
| CN101598038A (en) | Two-layer flow path variable area turbine of turbine supercharger | |
| CN101451464A (en) | Fuel cell engine air turbine compressor with energy recovery | |
| CN109167087A (en) | Fuel cell air management system | |
| KR20140014175A (en) | A turbine wheel, a turbine and use thereof | |
| CN110534772A (en) | Device for air supply to fuel cell | |
| CN207925582U (en) | A kind of fuel cell electrode auxiliary single stage turbocharger system | |
| CN111536057A (en) | Two-stage compressor of hydrogen fuel turbine range extender | |
| CN209115369U (en) | A kind of two stages of compression air supply system of fuel cell | |
| CN108533387B (en) | A turbocharger with motor/generator | |
| CN201443420U (en) | A turbocharger double-layer channel variable-section turbine | |
| CN101182805B (en) | Internal-combustion engines exhaust turbine dynamoelectric compressor system | |
| CN1305161C (en) | Hybrid power system for vehicle-use fuel cell gas curbine | |
| CN209312917U (en) | Air Supply System for High Power Fuel Cells | |
| CN202560331U (en) | Double-region type worm wheel for pressurizing | |
| CN209087991U (en) | A fuel cell and its air supply system | |
| CN113623064A (en) | Generator set of charged turbocharger | |
| CN218953427U (en) | Turbocharger utilizing bypass waste gas for cooling and power generation | |
| CN215633853U (en) | Separated turbocharging air compressor, motor cooling unit thereof and hydrogen fuel cell system | |
| CN104847480B (en) | The exhaust-driven turbo-charger exhaust-gas turbo charger of two-stage supercharging |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder |
Address after: 237000 intersection of Xinyang Avenue and 312 National Road, Jin'an District, Lu'an City, Anhui Province Patentee after: MINGTIAN HYDROGEN ENERGY TECHNOLOGY Co.,Ltd. Address before: 237000 the 6 floor of the Management Committee of Yu an District concentrated demonstration park, Lu'an, Anhui. Patentee before: MINGTIAN HYDROGEN ENERGY TECHNOLOGY Co.,Ltd. |
|
| CP02 | Change in the address of a patent holder |