Design Guidelines For a Thermoacoustic Refrigerator

Similar documents
Australian Journal of Basic and Applied Sciences. Rules Of Similarity For Model With Prototype Vertical Axis Wind Turbine

ESCI 485 Air/sea Interaction Lesson 4 Waves Dr. DeCaria

Physics 20 Lesson 13 Projectile Motion

Vessel Interaction A Case Study Peter O Brien, Dr Terry O Brien, Chris Hens OMC International Pty Ltd, Melbourne, Australia

Heat Transfer Effect of Inert Gas on Multi-Tubular Reactor for Partial Oxidation Reaction

Previewer Tools Show All In View: Hide All

MANOEUVRABILITY-BASED CRITICAL TIME FOR PREVENTING CLOSE-QUARTERS SITUATIONS

Experiments on elastic wave modelling in isotropic and anisotropic media

Total 0/30. 0/1 points Walker3 2.P.068. [544577]

Optimization for Bus Stop Design Based on Cellular Automaton Traffic Model

The Feature of Weak Shock Wave Propagated in a Overlong Tunnel

Name: Answer Key Date: Regents Physics. Projectiles

VALIDATION OF THE ASAR WAVE MODE LEVEL 2 PRODUCT USING WAM AND BUOY SPECTRA

Fluid-structure interaction between trains and noise-reduction barriers: numerical and experimental analysis

Momentum and Impulse. Physics 6A. Prepared by Vince Zaccone For Campus Learning Assistance Services at UCSB

Race car damping 2. Fig-1 quarter car model.

IMPROVED SPECTRAL WAVE MODELLING OF WHITE-CAPPING DISSIPATION IN SWELL SEA SYSTEMS

Data Sheet. Indexable carbide milling inserts and tooling. RS stock numbers to

Calculation of Actual Concrete Shrinkage Magnitude

SEISMIC RESPONSE ANALYSIS OF LONG-SPAN CONTINUOUS RIGID-FRAMED BRIDG

MEMORANDUM: INTERIM CONCEPTS

CREST LEVEL OPTIMIZATION OF THE MULTI LEVEL OVERTOPPING BASED WAVE ENERGY CONVERTER SEAWAVE SLOT-CONE GENERATOR. J. P. Kofoed 1 and E.

Data Sheet. Indexable carbide milling inserts and tooling. Data Pack G Issued November Square shoulder mill

INSTRUMENT INSTRUMENTAL ERROR (of full scale) INSTRUMENTAL RESOLUTION. Tutorial simulation. Tutorial simulation

PHYS 102 Quiz Problems Chapter 16 : Waves I Dr. M. F. Al-Kuhaili

Turbulence and waves in numerically simulated slope flows

MEMORANDUM. TNC Fisher Slough Final Design and Permitting Subject: Large Wood Debris Design. Jenny Baker (TNC) Dave Olson (DD3)

G.C.E (A/L) Examination March In collaboration with

Standing Waves in a String

An improvement in calculation method for apparel assembly line balancing

Brian P. Casaday and J. C. Vanderhoff Brigham Young University, Provo, Utah

Mechanical Waves: Applications in Medicine. How Elastography is Helping Doctors Avoid the Biopsy Needle

Experimental Investigation of Pressure Flushing Technique in Reservoir Storages

A Study of Ocean Waves at Fisherman s Wharf, Victoria Harbour

Chapter # 08 Waves. [WAVES] Chapter # 08

DS/EN DK NA:2015

PHY 221: Wavefunction, Wave Superposition, Standing Waves on a String

Full Internal Relief Valves Instruction Manual

Name: Answer Key Date: Regents Physics. Waves

MEASUREMENT OF DYNAMIC STRESSES ON CARRIERS WITH DETACHABLE GRIP AT STATION ENTRANCE: LA.T.I.F. EXPERIENCES AND FUTURE PROSPECTS

Basics of Flow measurement using Hot-film anemometer

Sinusoidal Waves. Sinusoidal Waves. Sinusoidal Waves

Chapter 16. Waves-I Types of Waves

Coordination in CPG and its Application on Bipedal Walking

Chapter 14. Gas-liquid Transfer

CARPET BOWLING m

Chapter 5 Wing design - selection of wing parameters - 4 Lecture 22 Topics

Physics - Projectile Motion

Fish Farm Consent Modelling. Poll na Gille

Integration of Lean Approaches to Manage a Manual Assembly System

INFLUENCE OF THE EXHAUST GAS RECIRCULATION ON THE OXYGEN CONTENTS AND ITS EXCESS RATIO IN THE ENGINE COMBUSTION CHAMBER

Ripple Tank: Instruction Manual

A Review on Experimental Analysis for Rectangular Perforated Fin Array

The water outgassing rate of internal surfaces of vacuum systems

Flow in a shock tube

Using sea bed roughness as a wave energy dissipater

The Coriolis force, geostrophy, Rossby waves and the westward intensification

Surface Waves NOAA Tech Refresh 20 Jan 2012 Kipp Shearman, OSU

Guide on dynamic dilution methods for NO, NO 2 and SO 2 at limit values

PreClass Notes: Chapter 14, Sections

An Indian Journal FULL PAPER ABSTRACT KEYWORDS. Trade Science Inc.

Clockwise Phase Propagation of Semi-Diurnal Tides in the Gulf of Thailand

A parametric study of an offshore concrete pile under combined loading conditions using finite element method

Simulating Method of Ship s Turning-basins Designing

Artificial headlands for coastal restoration

MACHINE MILKING AND DAILY CHANGES OF COW S TEAT CONDITION

DESIGN & MODIFICATION OF ROLLERS IN TRACKS OF SURFACE DRILLING MACHINES

Waves & Interference

MODELING OF THERMAL BEHAVIOR INSIDE A BUBBLE

Ocean currents I. The directional forces Wind-water interaction The drag forces

CHANGE OF NEARSHORE SIGNIFICANT WAVES IN RESPONSE TO SEA LEVEL RISE. Se-Hyeon Cheon 1 and Kyung-Duck Suh 1

Cold Formed Steel Tension Members with Two and Three Staggered Bolts

EXPERIMENT 6 THE SPEED OF SOUND USING THE RESONANCE OF LONGITUDINAL WAVES

Pre AP Physics: Unit 7 Vibrations, Waves, and Sound. Clear Creek High School

PHYSICS - CLUTCH CH 16: WAVES & SOUND.

Student name: + is valid for C =. The vorticity

Type A. Type B. Type C

Wind Regimes 1. 1 Wind Regimes

Scientia Iranica, Vol. 14, No. 4, pp 358{368 c Sharif University of Technology, August 2007 Research Note Evaluation of Empirically Derived PVT Proper

A Graphic Method to Estimate the Wind Speed under Urban Canopy Layer

PHYSICS - GIANCOLI CALC 4E CH 15: WAVE MOTION.

LOW PRESSURE EFFUSION OF GASES revised by Igor Bolotin 03/05/12

INTRODUCTION TO WAVES. Dr. Watchara Liewrian

ABSTRACT: Ocean wave energy contains the largest energy density

g L Agenda Chapter 13 Problem 28 Equations of Motion for SHM: What if we have friction or drag? Driven Oscillations; Resonance 4/30/14 k m f = 1 2π

PENALIZED LOGISTIC REGRESSION TO ASSESS NFL QUARTERBACK PERFORMANCE

LOW PRESSURE EFFUSION OF GASES adapted by Luke Hanley and Mike Trenary

Units of Chapter 14. Types of Waves Waves on a String Harmonic Wave Functions Sound Waves Standing Waves Sound Intensity The Doppler Effect

Unit Activity Answer Sheet

NIRSA CLUB BASKETBALL CONFERENCE MANUAL

Richard S. Marken The RAND Corporation

S L G. Chapter 12: The Behavior of Gases. I. First Concepts a. The 3 states of matter most important to us: solids, liquids, and gases.

reviewed paper Public transport travel time simulation Tomáš CHLEBNICAN, Jiří CTYROKY, Marek ZDERADICKA

C6Hi (g) 6 H2O + 6 C02(g) + energy

VEHICLE NO X AND PM10 EMISSION FACTORS FROM SYDNEY S M5-EAST TUNNEL

Physics 122 Class #6 Outline

Performance Measurement of Revolving Vane Compressor

Question. A. Incorrect! Check the definition for period. B. Incorrect! Check the definition for speed.

Date Lab Time Name. Wave Motion

Wave Force on Coastal Dike due to Tsunami

Transcription:

Deign Guideline For a Theroacoutic Refrigerator Ra C. Dhuley, M.D. Atrey Deartent of Mechanical Engineering Indian Intitute of Technology Bobay, Powai Mubai-400 076 Develoent of refrigerator baed on Theroacoutic technology i a novel olution to the reent day need of cooling without cauing environental hazard. With added advantage of abence of oving art and circulating refrigerant, thee device can attain very low teerature aintaining a coact ize. The reent theoretical work i baed on theory of linear theroacoutic[1]. Under the hort tack and invicid aution, an algorith for deign of a tanding wave theroacoutic refrigerator, with ain focu on the tack, i decribed. A tack i deigned for a given cooling requireent of the refrigerator and certain choen oeration araeter. Key Word: deign, theroacoutic, refrigeration Noenclature reure (N -2 ) Q c cooling ower (W) T teerature (K) W acoutic ower (W) f frequency (Hz) COP coefficient of erforance ρ denity (kg -3 ) L length of reonator () a ound eed ( -1 ) L length of tack () λ wavelength () A cro ection area of tack ( 2 ) k wave nuber ( -1 ) l half late thickne () ω angular frequency (rad -1 ) y 0 half late acing () γ ratio of ecific heat П late erieter () δ k theral enetration deth () x tack centre oition () β theral exanion coefficient (k -1 ) K theral conductivity (W -1 k -1 ) Subcrit C iobaric ecific heat (J kg -1 k -1 ) ean Γ noralized teerature a alitude gradient 1 local alitude ecific entroy (J kg -1 k -1 ) er late

INTRODUCTION Theroacoutic i the interaction between heat and ound. Of the everal alication[1,2] of theroacoutic in energy converion, the theroacoutic refrigerator i a well known device. A theroacoutic refrigerator ue the energy of ound or reure wave to bring about refrigeration. The ain coonent of a theroacoutic refrigerator are the reonator, the tack, the acoutic driver and the heat exchanger a hown below in Figure 1. OPERATING AND DESIGN PARAMETERS[6] The ai of the reent analyi i to develo a deign rocedure for a theroacoutic refrigerator and to deterine the deign araeter baed on certain given oerating araeter. Variou oerating and deign araeter are given in Table 1. The roertie of working ga like denity, theral conductivity, ratio of iobaric to iochoric ecific heat and eed of ound in ga lay an iortant art in thi analyi. The working ga hould have a low boiling oint, high ound eed and hould be inert to the coonent of the refrigerator. Table 1 Oerating and Deign araeter Figure 1 Scheatic of theroacoutic refrigerator The tanding reure wave generated by acoutic driver in the reonator caue to-and-fro otion of the ga fro one end of the tack to the other thereby roviding a ean of tranorting heat. The ga near the reure node get cooled due to rarefaction and ick u heat fro the tack aking one end of tack cold. Thi ga ove toward reure antinode and get heated u due to coreion. It loe heat to the tack and ake the other end of tack hot. Thu, a teerature gradient i et u along the tack length. With heat exchanger at the two end of the tack, thi teerature gradient can be ued to roduce refrigeration. A detailed decrition of theroacoutic cooling cycle ha been given by Arnott et. al[3]. Braun et. al[4] have develoed a deign otiization rogra baed on the theroacoutic iulation rogra known a DELTAE develoed by Swift[1]. A deign otiization rocedure baed on noralization of araeter ha been given by Wetzel et. al[5] and Tijani et. al[6] Oerating araeter ean reure, ean teerature, T frequency, f reure alitude, a ASSUMPTIONS[1,6] Deign Paraeter reonator length, L tack length, L tack cro ection area, A late thickne, 2l late acing, 2y 0 tack centre oition, x Following are the aution ade in the reent analyi 1. The length of the tack i uch aller a coared to the wavelength of the tanding wave L <<λ (Short tack aroxiation). It can be aued that the local reure and velocity alitude of the ocillating ga olecule i ore or le ae over the entire length of the tack. 2. The flow of the ga in the tack i aued to be invicid. Friction at the inner wall of the reonator i alo neglected.

3. The teerature difference acro the tack end i aued to be all a coared to the ean teerature T <<T. It can be aued that the thero-hyical roertie of the ga do not vary ignificantly over the tack length and hence can be aued contant. 4. The whole analyi i carried out at teady tate oeration of the refrigerator. The ean teerature of the ga i T and the teerature gradient acro the tack reain contant with tie. 5. Conductivity of late aterial i neglected. GOVERNING EQUATIONS[1] The equation governing the entire analyi i the general heat tranfer equation exreed in ter of entroy tranort. Neglecting vicoity of the ga, it can be written a where k=2π/λ. On account of the oroity B of the tack, eqn.3 get odified to, a u1 in( kx) ab (4) The critical teerature gradient i an iortant araeter governing the refrigeration action of a theroacoutic device. It i given by, T crit ( 1) kb cot( kx) (5) where β i the theral exanion coefficient of the ga. For ideal ga, it i equal to the invere of the abolute teerature. Of utot concern in the deign rocedure are the cooling ower roduced by the tack, the work inut needed to roduce thi cooling ower and thu the COP. Thee are given by the following exreion :- T( v ) ( KT ) t (1) Q k T ( 1) 1u1 4 (6) where i ecific entroy. The equation tate that the rate of change of aount of heat at a certain oint deend on convective flow of heat by ean of entroy and conduction of heat. Variou other exreion[1] relevant to reent analyi uch a thoe for the cooling ower and the acoutic ower can be derived fro eq(1). Referring to Figure 2, the acoutic driver roduce a region of axiu reure variation at x=0 i.e a reure antinode and velocity node. Subequently, following equation can be written down for local reure and velocity alitude in the reonator :- 1 a co( kx) a u1 in( kx) a (2) (3) W 2 2 k LT ( 1 ) ( 1) 4 C T a COP tan( kx) BL ( 1) (7) (8) where, δ k i the theral enetration deth of the ga and i an iortant araeter governing the late acing of the tack. It i defined a the ditance through which heat diffue in the ga in tie 1/ω and i given by k 2K C (9) Π i the erieter of the cro ection of the late. Auing the thickne of the late to

be very all, the erieter i equal to twice the late width (Π=2w). Γ i the ratio of actual teerature gradient to the critical teerature gradient of the tack. region within δ k fro the late and hence the late acing i choen to be 2δ k [8]. Hence, 2y 0 =0.212. DESIGN PROCEDURE Thi ection decribe the deign rocedure of a refrigerator roducing a cooling ower of 4 W and a cold end teerature of 210 K. The oerating araeter choen are hown in Table 2[6]. Table 2 Oerating and working ga araeter Oerating araeter Heliu roertie =10 bar ρ =1.9244 kg/ 3 T =250 K a=935 / f=400 Hz k=0.14 W/K a =0.2 bar T h =283 K γ=1.67 Deterining the deign araeter Reonator length The allet oible length of the reonator which will roduce a tanding wave i equal to quarter of the wavelength. A tanding wave can be generated by keeing one end of reonator cloed (driver end) and iulating the other end a oen. Thi can be done by attaching a ufficiently large buffer[6,7] of ga at T at thi end. For thi ot fundaental cae we get L=58.8 c. Plate acing The theral enetration deth of the ga at the given frequency i found out to be 0.106. Figure 3 how variation of heat flux with ditance fro the late. It can be een that alot all the tranort of heat take lace in Figure 3 Heat tranort v. ditance fro late. Plate thickne The late thickne can be found out fro the exreion 1 2 2 ( 1) l y0 B (10) where B i the oroity of the tack. The oroity i defined a the ratio of oen area in the cro ection to the total cro ection area of the tack. The oroity i choen uch a not to diturb the acoutic tanding wave ignificantly and i norally taken in the range 0.7-0.8[5,6]. Chooing B=0.75, we get 2l=0.07. Stack length, centre oition and area of cro ection A grahical aroach ha been ileented to deterine the tack length, centre oition and the cro ection area. It i aued that the tack i ade of n arallel late over one another and the cro ection of the tack i a quare of width w. In thi cae, the erieter of the late cro ection becoe 4nl+4(n-1)y 0. Knowing the fact that total cooling ower roduced by

the tack i n tie that roduced by a ingle late, it can be written Q [ ( (11) c n n l y0) y0] [ T 1] k u 1 1 L T crit obtained. The cro ection area of thi tack coe out to be 7.06 c 2. Thi tack will roduce a cooling ower of 4 W at COP cloe to 2. Putting the known quantitie in eq(11), an equation in three variable x, L and n i obtained, 2 0.282n 0.212 n 509.54 0 tan( kx) in(2 kx)(0.221 1) L (12) Siilarly, fro eq(8) we get, tan( kx) COP 0.75 L (13) Figure 5 Variation of nuber of late with tack length. COP and n are lotted with L for different oition of tack centre in the reonator. Theoretically, every oint on uch a curve will give u a tack roducing a cooling ower of 4 W and a cold end teerature 210 K. Figure 4 and Figure 5 how variation of COP and n reectively with L at different tack centre location. Figure 4 Variation of COP with tack length For intance, if L =0.1 i choen at x =0.1, a tack with 95 arallel late i RESULTS AND DISCUSSIONS The deign araeter obtained fro the analyi are hown in Table 3 Paraeter Table 3 Reult Value L 588 L 100 A 706 2 2l 0.07 2y 0 0.212 100 x The tack length (L =10 c) i very all a coared to the wavelength of the acoutic field (λ=235.2 c). Hence, the aution of hort tack i erfectly valid. At the tack centre location (x =10 c) the critical teerature gradient i 1235.13 K/. The actual teerature gradient acro the tack end i 750 K/. Clearly, Γ=0.607<1 which i riary neceity[1] for the device to function a a refrigerator, i et. Another erfectly valid choice of tack roducing the ae cooling ower at ae

cold end teerature i L =8.5 c and x =8c. In thi cae, the tack will conit of 102 late and a cro ection of 8.2 c 2. The correonding COP i 1.9. Tijani et al.[6] obtained a tack with cro ection 11.8 c 2 and COP of 1.5 with ae tack length and et of oeration araeter. The difference in the cro ection can be accounted for the author in [6] had taken vicoity into account and hence needed ore nuber of tack late to roduce 4 W ower. Referring to Figure 4, high value of COP (~3) are exected fro the analyi. But, it hould be noted that thi i COP of the tack and not of the refrigerator. Even when the vicoity i neglected, ore ower ha to be inut to account for loe at heat exchanger, driver, etc. (though not a art of thi analyi). cooling alication, International Journal of Refrigeration, 32, (2007), 1059-1071. 5. Wetzel M., Heran C., Deign Otiization of theroacoutic refrigerator, International Journal of Refrigeration, 20, (1997), 3-21. 6. Tijani M.E.H., Zeeger J.C.H., dewaele A.T.A.M.., Deign of theroacoutic refrigerator, Cryognenic, 42, (2002), 49-57 7. Tijani M.E.H., Zeeger J.C.H., dewaele A.T.A.M.., Contruction and working of a theroacoutic refrigerator, Cryognenic, 42, (2002), 59-66 8. Tijani M.E.H., Zeeger J.C.H., dewaele A.T.A.M., Otial tack acing for theroacoutic Refrigeration, J Acout Soc. A, 112(1), (2002), 128-133 CONCLUSIONS A ile deign rocedure for a tanding wave theroacoutic refrigerator ha been decribed. With a choice of oerating araeter and heliu a working ga, grahical aroach ha been ued to deterine the geoetrical araeter of the tack. A refrigerator roducing a cooling ower of 4W at cold end teerature of 210K at teady tate i deigned theoretically uing thi deign rocedure. Reference 1. Swift G.W., Theroacoutic engine, J Acout Soc. A, 84, (1998), 1146-1180 2. Swift G.W., Theroacoutic- A unifying erective of oe engine and refrigerator, Acoutical Society of Aerica Publication (2002). 3. Arnott W, Raet R, Ba H.E, Theroacoutic Engine, Ultraonic Syoiu, (1991), 995-1003. 4. Paek I.,Braun J.E., Mongeau L., Evaluation of tanding-wave theroacoutic cycle for