Screw Compressor Basics
description
Transcript of Screw Compressor Basics
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Screw Compressor Modelling, Design and Use
Screw Compressor Basics
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Professor N. Stosic
Chair in Positive Displacement Compressor Technology
Centre forPositive Displacement Compressor Technology
City University London, U.K.
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Screw Compressor Today
Highly competitive market, speciallyin air compression and refrigeration
Continuous improvement:more compact, efficient and cost effective compressors
New rotor generation, rotors optimizedfor certain compressor duty, specializeddesign
Scope for innovation, improvement and development
INTRODUCTION
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INTRODUCTION
Basics
View from Front and Top
View from Bottom and Rear
Top and front: AdmissionBottom: Change of volumeBottom and Rear: Discharge
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INTRODUCTION
Basics
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INTRODUCTION
Swedish company SRM, pioneer and leader
Screw compressor profiles, Symmetric, Asymmetric, ‘D’ and ‘G’Screw compressor designScrew compressor technology
Licence system left many screw compressormanufacturers at margins of research anddevelopment
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INTRODUCTION
Many companies started their own development
Gardner Denver, Atlas Copco, Compair, Kaeser, GHHTrane, Ingersol-Rand, Hitachi, Fu Sheng, Hanbel, Refcomp
Holroyd
Many more or less successful rotor profiles
Many more or less successful screw compressor designs
Need exists to concentrate efforts in R&D
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Centre for Positive Displacement Compressor Technology
Improved methods of analysis
Experimental validation
Design of critical components
Complete machine design
Product development
Training in machine design
INTRODUCTION
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Methods Applied
Advanced Computerized design toolsMachine process modelling 2-D and 3-D Computational Fluid Dynamics
Modern experimental techniqueComputerized data acquisition
Users
Renown and new companies, large and small manufacturers in the U.K and abroad
INTRODUCTION
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SCREW COMPRRESSOR GEOMETRY
Before modelling the physical process, the rotor lobe profiles must be defined together with the remaining parameters with which the rotor and housing geometry can be fully specified.
Rotor profile: x and y coordinates, pressure angle
Helix/lead angle, rotor length
Interlobe, end and radial clearance
Suction/discharge ports
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SCREW COMPRESSOR GEOMETRY
General case: non-parallel and non-intersecting
( ) [ ] [ ]1 1 1 1 1 01 01 01 01 1, , , cos sin , sin cos ,t x y z x y x y pθ θ θ θ θ θ= = = − +r r
∂∂+
∂∂
∂∂−
∂∂=
∂∂
∂∂=
∂∂ 0,cossin,sincos0,, 01010101111 θθθθ
ty
tx
ty
tx
ty
tx
tr
[ ]0,,0,, 0101111 xyyx −=
∂∂
∂∂=
∂∂
θθθr
Given profile
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SCREW COMPRESSOR GEOMETRY
Meshing condition
Meshed profile
General case: non-parallel and non-intersecting
( ) [ ] [ ][ ]
2 2 2 2 2 1 1 1 1 1
02 02 02 02 2
, , , , , cos sin , sin cos
cos sin , sin cos ,
t x y z x C y z y z
x y x y p
θ τ
τ τ τ τ τ
= = = − Σ − Σ Σ + Σ =
− +
r r
[ ] [ ]( ) ( )
22 2 2 02 02 02 02 2
1 1 2 1 2 1
, , sin cos , cos sin ,
sin cos , sin cos , cos sin
y x p x y x y p
p y p x C p x C
τ τ τ ττ
θ
∂= − = + − =
∂Σ − Σ Σ + − Σ Σ − − Σ
r
1 1 1 1 1 2 0t tθ τ θ τ
∂ ∂ ∂ ∂ ∂ ∂ × ⋅ = − × ⋅ = ∂ ∂ ∂ ∂ ∂ ∂ r r r r r r
( ) ( )1 1 1 11 1 2 1 1 1 1 2cot cot 0
x y y xC x p p x y p p p Ct t t t
θ∂ ∂ ∂ ∂ − + − Σ + + + − Σ = ∂ ∂ ∂ ∂
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SCREW COMPRESSOR GEOMETRY
General case: non-parallel and non-intersectingcorresponds to the rotor – hobbing tool relation
Special cases:
p2=0, rotor - plate milling tool, grinding tool relation
Σ=0, screw compressor rotors
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SCREW COMPRESSOR GEOMETRY
0101 01
01
sin cos 0dy C Cky kxdx i i
θ θ − + + =
02 01 01
02 01 01
cos sin cos
sin cos sin
x x k y k Ci
y x k y k Ci
θθ θ
θθ θ
= − −
= + +
Meshing condition
Rotor profile, Σ=0, i=p2/p1, k=1-1/i
Meshed profile
Rack profile
0 01 01
0 01 01 1
cos sinsin cos
r
r
x x yy x y r
θ θθ θ θ
= −= + −
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Numerical solution of the meshing condition
Task: to find θ for a zero function
Simple iteration method:Fast and reliable, but valid only for certain function
Additional complicationIn certain areas two or more θ are the zero functionOnly one is valid, additional values found by half interval method
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SCREW COMPRESSOR GEOMETRYDemonstrator profile
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‘N’ ROTOR PROFILE- Rack generation procedure - Straight line on the rack - involute rotor contact- Small torque transmitted
- Short sealing line- Large displacement- Strong gate rotor,
SCREW COMPRESSOR GEOMETRY
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SCREW COMPRRESSOR THERMODYNAMICS
Differential approach:
Set of differential equations solved simultaneouslyEquations of continuity, momentum and energy
Preintegrated equations inadequate and inaccurate if high leakage rate and heat transfer is involved
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in in out outdU dVm h m h Q pd d
ω ωθ θ
= − + −! !
in outdm m md
ωθ
= −! !
2 22 1
2 2
1
2 lnl l l g g
p pm w A Apap
ρζ
−= =
+
!
Internal Energy
Continuity
Leakage Flow
, ,in in suc suc l g l g oil oilm h m h m h m h= + +! ! ! ! , ,out out dis dis l l l lm h m h m h= +! ! !
,in suc l g oilm m m m= + +! ! ! ! ,out dis l lm m m= +! ! ! m wAρ=!
SCREW COMPRESSOR THERMODYNAMICS
Momentum2
02l
l lg
wdp dxw dw fDρ
+ + =
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SCREW COMPRESSOR THERMODYNAMICS
Ideal Gas( )1 u RTT p
R vγ= − =
Real gasp=f1(T,v) u=f2(T,v)
Wet vapour( ) ( )1 1f g f gu x u xu v x v xv= − + = − +
( ), ( ), ( ), ,VU m V vm
θ θ θ =
( )o o oiloil
oil oil
h A T TdTd m cθ ω
−= ,
1oil p
oil
T kTT
k−
=+
6oil oil S oil
o o o
m c d ckh A hω ω
θ θ= =
∆ ∆
( ) ( ) ,oil
U mu mu= +
Oil injection
Numerical solution, Runge-Kutta IV order solver ( )oil
U mcTu
m−
=
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SCREW COMPRESSOR THERMODYNAMICS
Compressor integral parameters
in outm m m= −1 / 60m mz n=!
060 /V m ρ=!
( )1 2 1
60n n
t
F F Lnzm
ρ+=!
vt
mm
η =!!
indcycle
W Vdp= ∫
1
60ind
indW z nP =
sindcycle
VW dpm
= ∫
t at a
ind ind
W WW W
η η= =
( )21 2 1
1
ln1t a
pW RT W R T Tp
γγ
= = −−sin d
PPV
= !
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SCREW COMPRESSOR THERMODYNAMICS
Calculation of pressure loads On compressor rotors
Radial forces
( )
( )
B
x B AAB
y B AA
R p dy p y y
R p dx p x x
= − = − −
= − = − −
∫
∫
Rotor torque
( )2 2 2 20.5B B
B A B AA A
T p xdx p ydy p x x y y= + − − + −∫ ∫
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SCREW COMPRESSOR THERMODYNAMICS
Bearing reactions androtor deflections
2
2
d MEIdz
δ =
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Optimization variables and target function
Single stage:Rotor variables:r0 Female rotor addendumr1 Male rotor lobe radiusr2 Male rotor tip radiusr3 Female rotor tip radiusCompressor variables:Built-in volume ratioOperation variables:Shaft speedOil flowInjection positionOil temperature9 Variables
Multistage:9 Variables x Number of stages+ Interstage pressures
Target function:Specific power combined with compressor price
F=w1L+w2C
SCREW COMPRESSOR OPTIMIZATION
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Box constrained simplex method for efficient and reliable multivariable optimization
1 2( , ,..., )nf x x x
, 1,i i ig x h i n≤ ≤ = , 1,i i ig y h i n m≤ ≤ = + yn+1,…,ym
1 2F w L w C= +
1 2
1 2
( ) max ( ), ( ),..., ( )( ) min ( ), ( ),..., ( )
h k
g k
f x f x f x f xf x f x f x f x
==
1
1 ,1
ki i lj
ix x x x
k =
= ≠− ∑ ( )r lx x x xα= + −
( ) ( )0.5 (1 ) ( )(1 )(2 1)r new r old h hx x cx c x x x c R = + + − + − − − 1
1
r r
r
n kn
r
r r
ncn k
+ −
= + −
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Dry Oil-Flooded Refrig.r0 [mm] 2.62 0.74 0.83r1 [mm] 19.9 17.8 19.3r2 [mm] 6.9 5.3 4.5r3 [mm] 11.2 5.5 5.2
Built-in volume ratio 1.83 4.1 3.7Rotor speed [rpm] 7560 3690 3570Oil flow [lit/min] - 12 8Injection position [o] - 65 61Oil temperature [o] - 33 32
Oil FreeOil FloodedRefrigeration
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EXAMPLE OF CALCULATION
5-6-128 mm Oil-Flooded Air Compressor
7 m3/min, max 10 m3/min at 8 bar (abs)
5-14 bar (abs), max 15 bar (max)
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EXAMPLES OF CALCULATION
5/6-128 mm, L/D 1.65Displacement 1.56 l/revInterlobe sealing line 0.13 mBlow-hole area 1.85 mm2
Rotors optimized foroil flooded operatedair compression
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EXAMPLES OF CALCULATION
CAD Interface: Compressor ports
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EXAMPLES OF CALCULATION
Experimental verification of the model
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EXAMPLES OF CALCULATION
Compressor in the test bed
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EXAMPLES OF CALCULATION
Comparison of thecalculated and test results Flow-Power
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EXAMPLES OF CALCULATION
EXAMPLES OF 3-D CFD CALCULATION
Majority of design problems can be solved by the one-dimensional approach, some of them require thetwo dimensional calculation, however, there are situations where 3-D CFD must be applied
Such are
Oil flow distribution,Fluid-Solid Interaction
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• Grid topology- polyhedral- O - grid- H - grid- C - grid
• Cell shape
Grid generation Grid generation -- 11
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Grid generation - 2
- Male rotor - Female rotor
- Suction port - Discharge port- Suction and discharge receivers
- End clearancesRotor connections, clearances,
leakage paths
• Grid topology strongly affects accuracy, efficiency and ease of calculation • Full structured block generated hexahedral 3D-O mesh• Screw compressor sub-domains:
Automatic discretizationiscretization process:process:- The rack generating procedure-- Rack Rack -- a rotor with an infinite radiusa rotor with an infinite radius
-- Divides working domain in two parts Divides working domain in two parts male and female rotor,male and female rotor,
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Screw Compressor FSI calculations Screw Compressor FSI calculations Comet Comet Mathematical model for screw compressor is based on conservationMathematical model for screw compressor is based on conservation laws laws of continuity, momentum, energy, concentration and space:of continuity, momentum, energy, concentration and space:
s( ) 0V S
d dV ddt
ρ ρ+ − ⋅ =∫ ∫ v v s
s( ) bV S S V
d dV d d dVdt
ρ ρ+ − ⋅ = ⋅ +∫ ∫ ∫ ∫v v v v s T s f
s
s
( ) +
( grad : grad ) p
hV S S
hV V S V
d hdV h d ddt
ds dV p dV d pdVdt
ρ ρ+ − ⋅ ⋅
+ ⋅ + − ⋅ +
∫ ∫ ∫
∫ ∫ ∫ ∫
v v s = q s
v S v v s
s( )o oo o c c
V S S V
d c dV c d d S dVdt
ρ ρ+ − ⋅ = ⋅ +∫ ∫ ∫ ∫v v s q s
22 div3
pµ µ= − −T D vI I!
oc grado oD cρ=q
h grad Tκ=q
( , ), ( , )p T e e p Tρ ρ= =
s 0V S
d dV ddt
− ⋅ =∫ ∫ v s
s
2
s 1 2 3
( ) ( ) ,
( ) ( )
kV S S V
V S S V
d kdV k d d P dVdtd dV d d C P C C dVdt k kε
ρ ρ ρε
ε ερε ρε ρ ρε
+ − ⋅ = ⋅ + −
+ − ⋅ = ⋅ + − + ∇ ⋅
∫ ∫ ∫ ∫
∫ ∫ ∫ ∫
v v s q s
v v s q s v
Closed by constitutive relations and equation of stateClosed by constitutive relations and equation of stateand accompanied by turbulence model.and accompanied by turbulence model.
( ) ( )2 div
3 2 rT Tη λ
λ η α= −
+ −T D + wI
I
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Thermodynamic properties of real fluidsThermodynamic properties of real fluids-- pp--vv--TT equation equation
compressibility factor compressibility factor zz-- zz is assumed to change linearly is assumed to change linearly
with pressure err<2%with pressure err<2%
-- Antoine equation for saturationAntoine equation for saturationtemperaturetemperature
-- Clapeyron Clapeyron equation for latent heatequation for latent heat
-- Specific heat for constant pressureSpecific heat for constant pressure
-- Density of mixtureDensity of mixture
-- Coefficient in the pressure correctionCoefficient in the pressure correctionequation equation
( )p z RT z p RTρ
= ⋅ = ⋅
1 2z p B B= ⋅ +
11 v v
T
bdCdp zRT zρ
ρ ρρρ
⋅ = = − ⋅
2
1 logsatAT
A p=
−
2 30 1 2 3pvc C C T C T C T= + ⋅ + ⋅ + ⋅
1 1 satL
v l sat
dPh TdTρ ρ
= ⋅ − ⋅
2 2
11
v l
co coρ
ρ ρ
= − −
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Multiphase flowMultiphase flow( )o o o o
o ol con massd m h dh dmm h Q Q
dt dt dt= + = +! !
-- OilOil is assumed to be a passive is assumed to be a passive ‘‘speciesspecies’’
-- Mass calculated from the concentration Mass calculated from the concentration Oil drag force influence concentrationOil drag force influence concentration
-- Energy source due to heat transfer Energy source due to heat transfer between working fluid and oil is:between working fluid and oil is:
sol olL
mass L L L Lm mdmQ h h h m
dt tδ−= ≈ =! !
1
o o
k k
con o p o pdT T TQ m C m Cdt tδ
−−= ≈!
( )pm sL
L
m C T Tm
h⋅ ⋅ −
=!
1 (2drag o drag o oA Cρ= − − −f v v v v)
-- Liquid phaseLiquid phase is assumed to be an active is assumed to be an active ‘‘speciesspecies’’
-- Mass source Mass source evaporated/condensed mass evaporated/condensed mass
-- Energy source Energy source energy of evaporation/condensationenergy of evaporation/condensation
o om m C= ⋅
EulerEuler--Lagrange approachLagrange approach
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Boundary conditionsBoundary conditions
-- Wall boundaries with wall functions are Wall boundaries with wall functions are introduced on the housing and rotors. introduced on the housing and rotors.
constadd
p const const
p pdm Vmdt p t
ρδ=
− ⋅ = ≈ ⋅ !
addadd add add add
p const
dmQ h m hdt =
= = ⋅ !! !
-- Compressor positioned between suction Compressor positioned between suction and discharge receivers of small volumeand discharge receivers of small volume
-- Inlet & outlet receivers and oil port are Inlet & outlet receivers and oil port are treated as boundary domains:treated as boundary domains:
-- Mass equation corrected by mass Mass equation corrected by mass source to maintain constant pressuresource to maintain constant pressure
-- Energy equation corrected by energy Energy equation corrected by energy source to update energy balancesource to update energy balance
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Screw Compressor performanceScrew Compressor performance
-- Volume flow (inlet and outlet)Volume flow (inlet and outlet)
-- Mass flow (inlet, outlet and oil) Mass flow (inlet, outlet and oil)
-- Boundary forcesBoundary forces
-- Restraint Forces and TorqueRestraint Forces and Torque
-- Compressor shaft powerCompressor shaft power
-- Specific powerSpecific power
-- EfficiencyEfficiencyVolumetric and adiabaticVolumetric and adiabatic
( ) ( )3
160 min ,
end
start
t It t
f f fi fit t i
V V m V v S= =
= ⋅ = ∑ ∑! ! !
[ ]( ) ( ) secend
start
tt t
ft t
m V kgρ=
= ⋅∑ !!
* ; * ; *x b xb y b yb z b zbF p A F p A F p A= = =
1 1
1 1
( ),[ ]; ( ), [ ]
( ),[ ]; ( ), [ ]
I I
rS rS rD rDi iI I
a ai i
F F i N F F i N
F F i N T T i Nm
= =
= =
= =
= =
∑ ∑
∑ ∑2 ( ) [ ]M FP n T T Wπ= ⋅ ⋅ ⋅ +
3 min1000speckWPP mV
= ⋅ !
; adv i
d
PVV Pη η= =!
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Oil injected Oil injected -- Pressure in axial sectionPressure in axial section
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Oil injected Oil injected -- Pressure and velocity Pressure and velocity
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Oil injected Oil injected -- Pressure 3D viewPressure 3D view
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Real fluid Real fluid -- Ammonia Ammonia –– pressurepressure
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Experimental verification Experimental verification –– PP--αααααααα diagramdiagram
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Oil injected Oil injected –– DeformationDeformationPressure1Pressure1 Pinl=1 b Pout=7 b n=5000 rpm
tinl=20 oC tout=40 oC
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Pinl=1 b Pout=7 b n=5000 rpm tinl=20 oC tout=40 oC
Oil injected Oil injected –– DeformationDeformationPressurePressure--11
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Pinl=1 b Pout=7 b n=5000 rpm tinl=20 oC tout=40 oC mag=20,000x
Oil injected Oil injected –– DeformationDeformationPressurePressure--22
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Oil injected Oil injected –– DeformationDeformationTemperatureTemperature Pinl=1 b Pout=3 b n=5000 rpm
tinl=20 oC tout=150oC mag=1,000x
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Oil injected Oil injected –– DeformationDeformationPressure+TemperaturePressure+Temperature Pinl=30 b Pout=90 b n=5000 rpm
tinl=0 oC tout=40 oC mag=2,000x
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DESIGN EXAMPLES
Oil-free air compressorOil-flooded air compressorRetrofit rotors of an air compressorRefrigeration compressor
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Compressors for Oil-Free Air Delivery
Design aims:
Delivery: 350-700 and 700-1000 m3/hWorking pressure: 1-2.5 (2.7) bar
Volumetric efficiency 90 % +Low specific powerSimple, reliable and compact machine
DESIGN EXAMPLES
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3/5 lobe rotorsLarge displacementConvenient gear ratio 5/3=1.67
DESIGN EXAMPLES
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Features of 3/5 ‘N’ Rotors
- Highest possible displacement- Higher delivery- Better volumetric efficiency- Better adiabatic efficiency- Stronger gate rotor- Long durability- High reliability- Easy manufacturing- Easy compressor assembly- Reasonable noise
DESIGN EXAMPLES
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General ArrangementXK18 Screw CompressorDESIGN EXAMPLES
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New design, fully customized by the manufacturer
New rotors,
New, improved compressor
New concept, better screw compressor compared with competition
DESIGN EXAMPLES
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Comparison of Test Results
R1- GHH C80R2- Drum D9000R3- Mouvex TyphoonR4- GHH CS-1000
DESIGN EXAMPLES
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Screw Compressor Family for Oil-Flooded Operation
Design aims:
Delivery: 0.6-60 m3/minWorking pressure: 5-13 bar
Volumetric efficiency 90 % +Low specific powerSimple, reliable and compact machine
DESIGN EXAMPLES
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Improved capacity and efficiencyLower power consumptionReduced manufacturing cost
Reasonable efficiency formoderate pressure ratios, at least thesame as for 4/6 rotors
4/5 Rotors
DESIGN EXAMPLES
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Five compressors, rotor diameters:
74, 102, 159, 225 and 285 mm, L/D 1.55
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Performance of the Compressor Family
DESIGN EXAMPLES
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Proven design, fully customized to the the manufacturer’s needs
New rotors,
New, improved compressor
DESIGN EXAMPLES
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Test Results, Compressors 73 and 159 mm
DESIGN EXAMPLES
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Retrofit ‘N’ Rotors
5.4 % more displacement6.5 % higher delivery4 % better volumetric efficiency2.5 % better adiabatic efficiency75 % less torque on the gate rotor
DESIGN EXAMPLES
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‘N’ Rotor retrofit for more efficient screw compressors
Asymmetric Rotors,the most common screw compressor rotors
DESIGN EXAMPLES
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Design of a semihermetic compressor for air-conditioning and refrigeration
based on ‘N’ rotors
• Semihermetic, convertible to open• All existing refrigerants• Modern, better than competition • 5/6-102 mm L/D=1.55• Efficient rotors for air condition and
refrigeration
DESIGN EXAMPLES
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5/6-102 mm L/D=1.55 compressor
• Theoretical displacement 0.72 l/rev• Gear-box 1500-10000 rpm• Delivery 0.920-5.80 m3/min • R-22• Air condition 5/40 oC 60-380 kW• COP 4.20 at 3000 rpm• Refrigeration -5/30 oC 33-210 kW• COP 3.95 at 3000 rpm
DESIGN EXAMPLES
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Refrigeration Application
DESIGN EXAMPLES
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Application of Design Optimization: A Family of Two-Stage Compressors
1st
2nd
Range: 22-250 kW8-16 bar (abs)
Two-stages: 19 Variables Target Function:Minimum specific power And only specific power
Number of framesVFD vs gearboxStage sizeStage speedStage rotor profile
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CONCLUSIONSThe screw compressor is a mature product at the milleniummeeting point. Orchestrated efforts of a large number of companies driven by market forces resulted in the compact and efficient compressor machine. Every detail counts today. A small difference will give a small, but distinctive improvement which may be used as an individual advantage.
Optimization opens hidden spots still left for better compressors. They result in stronger but lighter rotors with higher displacement, more compact and more efficient compressor machines at all areas of their application.
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EPILOGUE
The Centre for Positive Displacement Compressor Technology carries out research and provide a service to manufacturing companies in all aspects of compressor design and development. Through the everyday activity the Centre is gaining experience in the compressor research, development and design. Some of the recent experience is given in this presentation.