[go: up one dir, main page]

CN1392380A - Multi-stage thermoacoustic compressor - Google Patents

Multi-stage thermoacoustic compressor Download PDF

Info

Publication number
CN1392380A
CN1392380A CN 01122228 CN01122228A CN1392380A CN 1392380 A CN1392380 A CN 1392380A CN 01122228 CN01122228 CN 01122228 CN 01122228 A CN01122228 A CN 01122228A CN 1392380 A CN1392380 A CN 1392380A
Authority
CN
China
Prior art keywords
cooler
stage
folded
heater
resonant tube
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.)
Granted
Application number
CN 01122228
Other languages
Chinese (zh)
Other versions
CN1138108C (en
Inventor
陈国邦
石静蕾
蒋彦龙
邱利民
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.)
Zhejiang University ZJU
Original Assignee
Zhejiang University ZJU
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 Zhejiang University ZJU filed Critical Zhejiang University ZJU
Priority to CNB01122228XA priority Critical patent/CN1138108C/en
Publication of CN1392380A publication Critical patent/CN1392380A/en
Application granted granted Critical
Publication of CN1138108C publication Critical patent/CN1138108C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/14Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the cycle used, e.g. Stirling cycle
    • F25B9/145Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the cycle used, e.g. Stirling cycle pulse-tube cycle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/14Compression machines, plants or systems characterised by the cycle used 
    • F25B2309/1403Pulse-tube cycles with heat input into acoustic driver
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/14Compression machines, plants or systems characterised by the cycle used 
    • F25B2309/1407Pulse-tube cycles with pulse tube having in-line geometrical arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Air-Conditioning Systems (AREA)
  • Heat-Pump Type And Storage Water Heaters (AREA)

Abstract

The multi-stage thermoacoustic compressor has a first resonant tube as well as cooler, silk net, heater and the first-stage air bank connected successively to two ends of the first resonant tube. There are diffuser, cooler, silk heater, heat buffer, subsidiary cooler and a second resonant tube connected successively and perpendicularly to the first resonant tube. There are acoustic capacito, water cooler and load connected successively and perpendicularly to the second resonant tube. The present invention has multi-stage cascade amplification mode to lower the amplification requirement of each stage and this facilitates the utilization of low-grade heat energy.

Description

Multi-stage thermoacoustic compressor
The present invention relates to a kind of multi-stage thermoacoustic compressor.
Heat sound machinery does not have moving component, does not need slipper seal, does not have the mechanical part that needs close tolerance and lubricating oil yet.Working fluid is the mixture of helium or helium and other inert gases, does not consume the ozone in the atmosphere, also can not cause greenhouse effects.The valuable point of heat sound machinery also is to adopt low-grade energy heat energy (as solar energy, combustion gas, exhaust steam etc.) to drive, and has great flexibility, and those occasions that lack electric energy are then had more practical significance.Yet, in heat sound machinery, because the restriction of heater and regenerator (heat sound plate is folded) material thermal resistance energy and wall are to the leakage warm of environment, the maximum heating temperature of heater and heating power are limiting the acting ability of single-stage heat sound machinery, become the obstacle that strengthens the thermoacoustic compressor performance.
The purpose of this invention is to provide and a kind ofly can reduce the amplification requirement folded, thereby reduce requirement, the multi-stage thermoacoustic compressor that facilitates for the utilization of low grade heat energy each grade heating-up temperature to veneer.
In order to achieve the above object, the present invention takes following measures:
Plant multi-stage thermoacoustic compressor and have first resonatron, two ends are connected to cooler, silk screen, heater, one-level air reservoir respectively successively, vertically be provided with diffuser pipe, cooler, silk screen, heater, thermal buffer, supplementary cooler, second resonatron at first resonatron successively near cooler one side, vertically be provided with acoustic capacitance, water cooler, load successively near supplementary cooler one end at second resonatron.
The multistage amplifying method that the present invention proposes has avoided because the restriction of the leakage heat of plate overlay environment and material thermal resistance energy.The temperature difference that causes setting up at the folded two ends of the single level plates of certain-length is limited, so that the amplifying power of veneer overlay sound merit is restricted.By adopting the folded mode of amplifying step by step of multi-stage board, under the condition that requires certain output sound merit, can reduce the amplification requirement folded, thereby reduce requirement, for the utilization of low grade heat energy facilitates to each grade heating-up temperature to veneer.
Below in conjunction with accompanying drawing the present invention is elaborated.
Fig. 1 is a single-stage thermoacoustic compressor structural representation;
Fig. 2 is a secondary thermoacoustic compressor structural representation.
Multi-stage thermoacoustic compressor has first resonatron 5, two ends are connected to cooler 4, silk screen 3, heater 2, one-level air reservoir 1 respectively successively, vertically be provided with diffuser pipe 7, cooler 8, silk screen 9, heater 10, thermal buffer 11, supplementary cooler 12, second resonatron 13 at first resonatron successively near cooler one side, vertically be provided with acoustic capacitance 14, water cooler 15, load 6 successively near supplementary cooler one end at second resonatron.
The present invention adopts the multi-stage thermoacoustic method that contracts to substitute single level machine and drives load (vascular refrigerator), to fold under the limited temperature difference and heating-up temperature at single plate, adopting a plurality of plates to fold is further amplified sound wave, be prevalent in the little and big inadequately deficiency of amplitude of pressure ratio in the heat sound machinery thereby remedied, satisfy the job requirement of load (vascular etc.).
The sound merit expression formula of amplifying is W · 2 = 1 4 Π δ k Δx T m β 2 ω ρ m C p ( p 1 s ) 2 ( Γ - 1 ) , Γ in the formula= T m/ T CritFor plate on folded the actual temperature gradient and the ratio of critical-temperature gradient. T mBig more, Γ is big more, output work
Figure A0112222800042
Also big more.But in fact, the single plate T on folded mCan not be very big, because maximum heating temperature and heating power are subjected to the restriction of material and structure high temperature high voltage resistant mechanical performance thereof, in order to avoid cause problems such as security and reliability.On the other hand, the cooling medium of cooler is general all with the cooling water under the room temperature, so the temperature of the folded cold junction of plate can not be lower than room temperature.Adding the folded surperficial leakage heat to environment of plate will increase along with the rising of heating-up temperature, also determine the limit of the folded two ends of plate temperature differences.Therefore, the acting ability of single-stage thermoacoustic compressor and efficient all are limited.And secondary is so that multi-stage thermoacoustic compressor can improve the output work of thermoacoustic compressor and the utilization ratio of heat by the amplification layer by layer of a plurality of plate overlay sound merits.
We investigate the multiplication factor of silk screen plate overlay sound merit.It is all less that gas in the heat sound machinery vibrates general amplitude, and the folded size of plate is much smaller than wavelength, can think the average pressure p of plate in folded mNecessarily, so ρ is arranged mT m=const, wherein ρ m, T mDisplay plate is folded the averag density and the mean temperature in cross section respectively.Because the gap that plate is folded is very little, can ignore the existence of acoustic capacitance.According to mass conservation law, ρ is arranged mU 1=const, wherein U 1Be volume flow rate, so have T h T c = U l , h U l , c , Subscript h, c be folded hot junction and the cold junction of display plate respectively.If T h T c = τ > 1 , Promptly U l , h U l , c > . Because the folded size of plate is more much smaller than wavelength, can be similar to and thinks the average pressure p at the folded two ends of plate mNecessarily, p just 1, h=p 1, c, the definition of its substitution sound merit W · = 1 2 Re [ p 1 U 1 ‾ ] = 1 2 Re [ p 1 ‾ U 1 ] = 1 2 | p 1 | | p 1 | | U 1 | cos φ pU In W · h = τ W · c . Have for the single-stage thermoacoustic compressor W · h = τ 1 W · c , The secondary machine has W · h = τ 1 τ 2 W · c , τ 1Temperature difference ratio on expression first order silk screen plate is folded, τ 2Temperature difference ratio on expression second level silk screen plate is folded is in the formula τ 2 = T h 2 T c 2 > 1 , So the big multiple of theoretical sound power amplifier η = W 2 W 1 = τ 1 τ 2 τ 1 = τ 2 . Therefore, the sound merit through multistage amplification is obviously big than the sound merit of directly drawing from one-level.

Claims (1)

1. multi-stage thermoacoustic compressor, it is characterized in that it has first resonatron [5], two ends are connected to cooler [4], silk screen [3], heater [2], one-level air reservoir [1] respectively successively, vertically be provided with diffuser pipe [7], cooler [8], silk screen [9], heater [10], thermal buffer [11], supplementary cooler [12], second resonatron [13] at first resonatron successively near cooler one side, vertically be provided with acoustic capacitance [14], water cooler [15], load [6] successively near supplementary cooler one end at second resonatron.
CNB01122228XA 2001-06-16 2001-06-16 Multi-stage thermoacoustic compressor Expired - Fee Related CN1138108C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB01122228XA CN1138108C (en) 2001-06-16 2001-06-16 Multi-stage thermoacoustic compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB01122228XA CN1138108C (en) 2001-06-16 2001-06-16 Multi-stage thermoacoustic compressor

Publications (2)

Publication Number Publication Date
CN1392380A true CN1392380A (en) 2003-01-22
CN1138108C CN1138108C (en) 2004-02-11

Family

ID=4664652

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB01122228XA Expired - Fee Related CN1138108C (en) 2001-06-16 2001-06-16 Multi-stage thermoacoustic compressor

Country Status (1)

Country Link
CN (1) CN1138108C (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1300459C (en) * 2005-03-31 2007-02-14 浙江大学 Heat sound water pumping system using solar energy as driving source and its water pumping method
CN100366991C (en) * 2003-03-26 2008-02-06 学校法人同志社 cooling device
WO2008131687A1 (en) * 2007-04-25 2008-11-06 Shenzhen Zhongke-Lihan Thermoacoustic Engineering Research Center Co., Ltd. Thermoacoustic engine system using temperature-change heat source
CN100458148C (en) * 2004-12-10 2009-02-04 中国科学院理化技术研究所 A thermoacoustic engine with a resonant cavity with expanding cross-section
CN100593678C (en) * 2006-12-31 2010-03-10 中国科学院理化技术研究所 Tandem type thermoacoustic system
CN101275541B (en) * 2007-03-27 2011-08-31 中国科学院理化技术研究所 Thermoacoustic traveling wave engine and application thereof
CN103958901A (en) * 2011-11-14 2014-07-30 通用电气公司 Wet gas compression system with thermoacoustic resonator

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100366991C (en) * 2003-03-26 2008-02-06 学校法人同志社 cooling device
CN100458148C (en) * 2004-12-10 2009-02-04 中国科学院理化技术研究所 A thermoacoustic engine with a resonant cavity with expanding cross-section
CN1300459C (en) * 2005-03-31 2007-02-14 浙江大学 Heat sound water pumping system using solar energy as driving source and its water pumping method
CN100593678C (en) * 2006-12-31 2010-03-10 中国科学院理化技术研究所 Tandem type thermoacoustic system
CN101275541B (en) * 2007-03-27 2011-08-31 中国科学院理化技术研究所 Thermoacoustic traveling wave engine and application thereof
WO2008131687A1 (en) * 2007-04-25 2008-11-06 Shenzhen Zhongke-Lihan Thermoacoustic Engineering Research Center Co., Ltd. Thermoacoustic engine system using temperature-change heat source
CN103958901A (en) * 2011-11-14 2014-07-30 通用电气公司 Wet gas compression system with thermoacoustic resonator
US9382920B2 (en) 2011-11-14 2016-07-05 General Electric Company Wet gas compression systems with a thermoacoustic resonator
CN103958901B (en) * 2011-11-14 2016-10-19 通用电气公司 There is the dampness compressibility of thermoacoustic resonator

Also Published As

Publication number Publication date
CN1138108C (en) 2004-02-11

Similar Documents

Publication Publication Date Title
CN109736909B (en) Compressed air energy storage system for multi-energy supply
US20090266075A1 (en) Process and device for using of low temperature heat for the production of electrical energy
DK1257733T3 (en) Engine driven by a liquid or compressed gas type
Dorantes et al. Mathematical simulation of a solar ejector-compression refrigeration system
US20070101695A1 (en) Highly supercharged regenerative gas turbine
Czaja et al. Selection of gas turbine air bottoming cycle for polish compressor stations
Zhi et al. Thermodynamic analysis of an innovative transcritical CO2 parallel Rankine cycle driven by engine waste heat and liquefied natural gas cold
CN1392380A (en) Multi-stage thermoacoustic compressor
Hosseinnia et al. Thermodynamic analysis of high temperature cascade heat pump with R718 (high stage) and six different low-GWP refrigerants (low stage)
US6925830B2 (en) Well-water-type liquid cooling and heating resource system
CN108131866B (en) First-class thermally-driven compression heat pump
Spoelstra et al. Thermoacoustic heat pumps for energy savings
CN117703553B (en) Coupling geothermal energy compressed air energy storage system based on idle oil gas well gas storage
JPS6079125A (en) Closed cycle power transmission system utilizing isothermal compressor
CN215506817U (en) High-low temperature environment simulation test device adopting single-compressor multi-stage self-cascade refrigeration system
EP3146276B1 (en) Multi-stage heat engine
RU2306496C1 (en) Two-stage heat pump device
CN218469301U (en) Combined air source high-temperature heating device
Najjar et al. Feasibility of gas turbine-assisted heat pumps for space heating
CN106225308B (en) Class thermally driven compression-absorption heat pump
Blagin et al. Investigation of Thermomechanical Compressor Characteristics
CN117781501A (en) Regenerative Type 1 heat-driven compression heat pump
Moen et al. Initial heat pump concepts and integration principles for SHIP200 targeting heat delivery up to 200 C (steam cycle) and 250 C (eg CO2 cycle)
CN109059349B (en) First-class thermally-driven compression heat pump
CN118328575A (en) Direct-fired first-type heat-driven compression heat pump

Legal Events

Date Code Title Description
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee