CN201420688Y - Turbine type compressor applied to fuel battery system - Google Patents

Turbine type compressor applied to fuel battery system Download PDF

Info

Publication number
CN201420688Y
CN201420688Y CN2009200708221U CN200920070822U CN201420688Y CN 201420688 Y CN201420688 Y CN 201420688Y CN 2009200708221 U CN2009200708221 U CN 2009200708221U CN 200920070822 U CN200920070822 U CN 200920070822U CN 201420688 Y CN201420688 Y CN 201420688Y
Authority
CN
China
Prior art keywords
compressor
magneto
fuel cell
turbo
cell system
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 - Fee Related
Application number
CN2009200708221U
Other languages
Chinese (zh)
Inventor
董亚良
刘长海
徐亚强
钱建东
徐委连
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHANGHAI PALTON FUEL CELL SYSTEM Ltd
Shanghai Tongji Nanhui Technology Industrial Park Co Ltd
Original Assignee
SHANGHAI PALTON FUEL CELL SYSTEM Ltd
Shanghai Tongji Nanhui Technology Industrial Park Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SHANGHAI PALTON FUEL CELL SYSTEM Ltd, Shanghai Tongji Nanhui Technology Industrial Park Co Ltd filed Critical SHANGHAI PALTON FUEL CELL SYSTEM Ltd
Priority to CN2009200708221U priority Critical patent/CN201420688Y/en
Application granted granted Critical
Publication of CN201420688Y publication Critical patent/CN201420688Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/30Hydrogen technology
    • Y02E60/50Fuel cells
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

Abstract

The utility model provides a turbine type compressor applied to a fuel battery system, which comprises a permanent-magnetic motor and an air compressor. The air compressor is directly arranged on a motor shaft of the permanent-magnetic motor. The beneficial effects of the turbine type compressor are as follows: by adopting the structure that the air compressor and the permanent-magnetic motor arecoaxially arranged in an integrated manner, the density of specific volume power is high, the running is stable and the noise is low; the structure of the entire compressor is more compact, the volumeis small and the manufacturing cost is low. The turbine type compressor is mainly applied in the fuel battery system.

Description

Be applied to the turbo-compressor of fuel cell system
Technical field
The utility model relates to a kind of compressor, relates to a kind of turbo-compressor that is applied to fuel cell system specifically.
Background technique
Fuel cell is that the chemical energy Direct Transform with confession fuel is a kind of energy conversion device of electric energy, thereby is the electricity generating device that can obtain electric power by continuous fueling continuously.
Fuel cell has following characteristics:
(1) energy conversion efficiency height: directly the chemical energy with fuel is converted into electric energy, and is middle without combustion process, thereby is not subjected to the restriction of Carnot's cycle.Fuel-the energy conversion efficiency of present fuel cell system is 45%~60%, and the efficient of thermal power generation and nuclear power is greatly about 30%~40%.
(2) harmful gas SOx, NOx and noise emissions are all very low.
(3) fuel is applied widely.
(4) scale and infield are flexible, and the fuel cell plant floor space is little, and the construction period is short, and power station power can be assembled by battery pile as required, and is very convenient.No matter the concentrated power station of conduct still is distributed electricity to fuel cell, or all most suitable as the independent power station of sub-district, factory, heavy construction.
(5) load responding is fast, the ride quality height.
Because fuel cell has above-mentioned advantage, so it has strong advantages for development and wide market prospects.
In existing fuel cell generation, the air compression feeding mechanism generally adopts the screw pump of import, and this screw pump cost height accounts for 1/3 of whole fuel cell system price, and cost performance is low.
The model utility content
In order to address the above problem, the utility model provides a kind of turbo-compressor that is applied to fuel cell system, and this turbo-compressor has simple and compact for structure, and volume is little, and specific volume power density is big, the characteristics that cost is low.
To achieve these goals, the technical solution of the utility model is as follows:
A kind of turbo-compressor that is applied to fuel cell system, it comprises magneto and gas compressor, it is characterized in that: described gas compressor is directly installed on the motor shaft of magneto.
Further, in the utility model, coaxial installation one cooling fan on the motor shaft of described magneto, the front end of this cooling fan is provided with an air inlet air guide sleeve.
Further, in the utility model, the motor shaft two ends of described magneto are provided with floating-ring bearing.
Further, in the utility model, the rotor permanent magnet of described magneto is an overall structure, and adopts overall radial to magnetize, the outer installment of rotor permanent magnet has not magnetic conduction sheath of high strength, and rotor permanent magnet and high strength do not adopt interference fit between the magnetic conduction sheath.
Further, in the utility model, described magneto also comprises an oil tank, and this oil tank covers by the front and back ends that connecting tube is connected magneto.
Further, in the utility model, the motor shaft front end of described magneto, with the impeller joint of gas compressor, be provided with piston ring seal ring and labyrinth collar.
The beneficial effects of the utility model are:
1, the utility model adopts gas compressor and the coaxial setting of magneto consubstantiality, and specific volume power density is big.
2, the compact structure of integrating compressor, volume is little, and is in light weight, and cost is low.
3, running is steady, and noise is little, moves easy to maintenance.
4, adopt floating-ring bearing to replace original plain bearing in the magneto, when motor shaft rotates, drive the floating ring rotation by the inner membrance shearing force, when inside and outside oil film action when the oil-film force of floating ring and friction torque reach balance, floating ring i.e. stable operation under fixing ring speed ratio, at this moment, motor shaft is in the work of floating-ring bearing inner suspension, and bearing is not easy wearing and tearing.
5, the utility model has been set up an oil tank, carries out oil-feed, oil return, fuel-flow control, oil pressure control and oily temperature control by oil tank.
6, coaxial installation one cooling fan in the rear end of the motor shaft of magneto produces powerful suction by it, and air circulation is flowed, and the heat of casing inside is discharged, and reaches cooling purpose.
The utility model is mainly used in the fuel cell system.
Description of drawings
Describe the utility model in detail below in conjunction with the drawings and specific embodiments:
Fig. 1 is a cross-sectional view of the present utility model.
Embodiment
For technological means, creation characteristic that the utility model is realized, reach purpose and effect is easy to understand, below in conjunction with concrete diagram, further set forth the utility model.
Referring to Fig. 1, a kind of turbo-compressor that is applied to fuel cell system, it comprises magneto 100 and gas compressor 200.
The three-dimensional flow aerodynamics computer design art designs of impeller 210 uses advanced of gas compressor 200 forms.Because the delivery pressure of gas compressor 200 has direct relation with the linear velocity of compressor impeller cylindrical, so the rotating speed of raising drive motor is one of effective measures.The utility model adopts a magneto 100 as drive motor.
Magneto 100 comprises casing 7, and casing 7 adopts non-magnetic casting aluminium material to make through machining, and front cover 2 and rear end cover 10 are installed by bolt respectively in the rear and front end of casing 7.The internal fixation of casing 7 has stator 4, and stator 4 adopts low-loss cold rolling electric sheet to make.Motor shaft 3 is provided with rotor permanent magnet 5, the material that rotor permanent magnet 5 adopts is resistant to elevated temperatures Nd-Fe-Bo permanent magnet material, this rotor permanent magnet 5 is an overall structure, and adopt overall radial to magnetize, its outer installment has not magnetic conduction sheath 6 of high strength, and rotor permanent magnet 5 and high strength do not adopt interference fit between the magnetic conduction sheath 6.After the utility model energising, the electromagnetic torque that stator 4 produces drives rotor permanent magnet 5 and rotates.The rear and front end of motor shaft 3 is provided with floating-ring bearing 11.When motor shaft rotates, drive the floating ring rotation by the inner membrance shearing force, when inside and outside oil film action when the oil-film force of floating ring and friction torque reach balance, floating ring i.e. stable operation under fixing ring speed ratio, at this moment, motor shaft is in the work of floating ring inner suspension, and bearing is not easy wearing and tearing, and can bear the rotating speed of 120000rpm.
Magneto 100 also comprises an oil tank 13, and this oil tank 13 is arranged on the below of casing 7, and oil tank 13 is connected by one group of oil inlet pipe 1 and return tube 12 on the end cap of magneto 100 (forward and backward end cap respectively has one group).Carry out oil-feed, oil return, fuel-flow control, oil pressure control and oily temperature control by oil tank 13.
In order to improve the integral heat sink effect, rear end (near rear end cover 10) at motor shaft 3 is coaxially arranged with a cooling fan 9, the front end of this cooling fan 9 is equipped with air inlet air guide sleeve 8, in the rotation process of motor shaft 3, cooling fan 9 produces powerful suction, the hot air of compressor inside is discharged from rear end cover 10 through cooling fan 9 along air inlet air guide sleeve 8, reach cooling purpose.
Because the Revolution Per Minute of magneto can directly be connected with load machinery up to commentaries on classics up to ten thousand or tens thousand of commentaries on classics.Gas compressor 200 is directly installed on the motor shaft 3 of magneto 100, the housing of gas compressor 200 is by on the front cover 2 that is bolted to magneto 100.
It is to be noted in the front end of the motor shaft 3 of magneto 100 and the joint of compressor impeller, be provided with piston ring seal ring 15 and labyrinth collar 14.Adopt the piston ring seal ring as the first road oil sealing barrier; Adopt labyrinth collar as the second road oil sealing barrier, labyrinth sealing is noncontact seal, so be not subjected to the restriction of rotating speed and temperature, its labyrinth teeth adopts and inwardly gets rid of oily structure, and the oil return structure in conjunction with on supporting better plays the oil sealing effect.In addition, compressor impeller 210 take turns dorsal part 211 the high-pressure air balance pressure reduction at labyrinth collar two ends, strengthened sealing effect.
Adopt the structure of this gas compressor and the coaxial setting of magneto consubstantiality, specific volume power density is big, running steadily, noise is little; And the structure of integrating compressor is compact more, and volume is little, and cost is low.
More than show and described basic principle of the present utility model, major character and advantage of the present utility model.The technician of the industry should understand; the utility model is not restricted to the described embodiments; what describe in the foregoing description and the specification is principle of the present utility model; the utility model also has various changes and modifications under the prerequisite that does not break away from the utility model spirit and scope, and these changes and improvements all fall in the claimed scope of the present utility model.The protection domain that the utility model requires is defined by appending claims and equivalent thereof.

Claims (6)

1. turbo-compressor that is applied to fuel cell system, it comprises magneto and gas compressor, it is characterized in that: described gas compressor is directly installed on the motor shaft of magneto.
2. the turbo-compressor that is applied to fuel cell system according to claim 1 is characterized in that: coaxial installation one cooling fan on the motor shaft of described magneto, the front end of this cooling fan is provided with an air inlet air guide sleeve.
3. the turbo-compressor that is applied to fuel cell system according to claim 1 is characterized in that: the motor shaft two ends of described magneto are provided with floating-ring bearing.
4. the turbo-compressor that is applied to fuel cell system according to claim 1, it is characterized in that: the rotor permanent magnet of described magneto is an overall structure, and adopt overall radial to magnetize, the outer installment of rotor permanent magnet has not magnetic conduction sheath of high strength, and rotor permanent magnet and high strength do not adopt interference fit between the magnetic conduction sheath.
5. the turbo-compressor that is applied to fuel cell system according to claim 1 is characterized in that: described magneto also comprises an oil tank, and this oil tank covers by the front and back ends that connecting tube is connected magneto.
6. the turbo-compressor that is applied to fuel cell system according to claim 1 is characterized in that: the motor shaft front end of described magneto, with the impeller joint of gas compressor, be provided with piston ring seal ring and labyrinth collar.
CN2009200708221U 2009-04-21 2009-04-21 Turbine type compressor applied to fuel battery system Expired - Fee Related CN201420688Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009200708221U CN201420688Y (en) 2009-04-21 2009-04-21 Turbine type compressor applied to fuel battery system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009200708221U CN201420688Y (en) 2009-04-21 2009-04-21 Turbine type compressor applied to fuel battery system

Publications (1)

Publication Number Publication Date
CN201420688Y true CN201420688Y (en) 2010-03-10

Family

ID=41807340

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009200708221U Expired - Fee Related CN201420688Y (en) 2009-04-21 2009-04-21 Turbine type compressor applied to fuel battery system

Country Status (1)

Country Link
CN (1) CN201420688Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107893772A (en) * 2017-10-09 2018-04-10 中国第汽车股份有限公司 A kind of centrifugal fuel battery air compressor with energy recovery function
CN110959073A (en) * 2017-07-26 2020-04-03 罗伯特·博世有限公司 Turbomachine, in particular for a fuel cell system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110959073A (en) * 2017-07-26 2020-04-03 罗伯特·博世有限公司 Turbomachine, in particular for a fuel cell system
CN110959073B (en) * 2017-07-26 2021-11-09 罗伯特·博世有限公司 Turbomachine, in particular for a fuel cell system
CN107893772A (en) * 2017-10-09 2018-04-10 中国第汽车股份有限公司 A kind of centrifugal fuel battery air compressor with energy recovery function

Similar Documents

Publication Publication Date Title
CN201896664U (en) Electricity generating device of miniature gas turbine
CN103089405B (en) Rotor clutch type motor-driven power generation turbocharger
US20060220388A1 (en) Rankine - microturbine for generating electricity
CN102900533A (en) Micro gas turbine generating device
CN208221133U (en) A kind of back-to-back type fuel cell centrifugal air compressor
CN201420688Y (en) Turbine type compressor applied to fuel battery system
CN202851154U (en) Micro gas turbine generation device
CN208252368U (en) Fuel cell air suspension centrifugal compressor
CN113790089A (en) Low-temperature waste heat power generation system
CN105201683A (en) Low-quality engine waste heat recovery device
CN209781245U (en) Shell assembly of two-stage air suspension centrifugal electric direct-drive air compressor
CN202348543U (en) Dual-impeller-rotation hydroelectric generator
CN201393160Y (en) High-speed grease bearing permanent magnet motor
CN213899157U (en) Novel full-through-flow three-phase asynchronous hydraulic generator
CN102425531A (en) Multi-energy jointly powdered engine
US8508059B2 (en) Thrust reaction utilization method and system
CN204783804U (en) Use ultrasonic vibration bearing's air compressor
CN201509124U (en) Isolated minitype generator set
CN102748191A (en) Integrated through-flow water turbine generator set
CN201424967Y (en) Backpressure steam turbine
CN214280951U (en) Cylinder type permanent magnetic force heating system
CN218472922U (en) Motor casing convenient to installation
CN214045047U (en) Series cylinder type excitation magnetic heating system
CN220849878U (en) Horizontal water turbine
CN216241071U (en) Vortex heating device based on vertical axis wind wheel

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100310

Termination date: 20180421

CF01 Termination of patent right due to non-payment of annual fee