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INTRODUCTION:
Growth/productivity change in last 50 years:
- Big growth from new manufacturing revolutions:
- 1850 → steam engine (operative energy)
- 1900 → mass production model (Ford)
- 1970 → automation
- IV manufacturing revolution → advanced robots
Technology & software → productivity↑
Opportunity New→ flexibility → reconfig
- Different forms of energy: Manual, mechanical, chemical (reactive)
- New and advanced materials (ceramic, carbon fiber...)
- New or different products → few parts, miniaturization, higher tolerance, easier assembly
- Reduce fixed time cost and timer very expensive better
Phenomenon reality → Model = description → Mathematical modeling → Physical modeling
- “black box” → empirical modeling
THERMAL MODEL
heat transfer = temperature difference
Fourier Law
conduction
jxqx = -K ∂T/∂x
K = thermal conductivity [W/m°C]
Newton Law
convection
qc = h(Ts - T∞) h = convection coeff [W/m²K]
assumptions
K constant; K=K(T) no
isotropic and homogeneous material (constant volume, temperature energy)
energy balance
thermodynamic law => Ein + Ep - Eout = Es
equation in form of energy conservation
T(x,y,z,t) 3D problem of energy conservation
∂²T/∂x² + ∂²T/∂y² + ∂²T/∂t² = 1/α ∂T/∂t
x = thermal diffusivity [m²/s] = K/ρCp
(T(x,t)) ∝ I eliminate heat flow ∝ II eliminate ∝ ∂T/∂t
ΔT(x,t) = I eliminate heat flow
ΔT(x,t) = II eliminate ∝ ∂T/∂t/(specific heat capacity) ∝ ∂T(x,y,z,t) - T00(t) = -∂T/∂x
T(x,t) = T(x,tg)
Initial heat source mean internal neutron speed
Tp = T∞ constant
isotropic and homogeneous material ∂²x = ρ/α ∂x/∂t
same thermal and chemical property of material
No internal heat source
1D semi infinite geometry *0 x
pure conduction, no convection or radiation
T(x,0) T
To(x,t)
Boas heat flow po and rich t
T(x,t) = Y0√(x/√αt) ierfc {√(x/√αt) * f-1}
ierfc = integral of normalized Gaussian function
erfc = complementary error function
ierfc = integral complementary error function
D = √(αt)1/√π
Mutual distance between material affected by heat source
Laser Source
λCO2 = 10600 nm
P = 1.7 - 6 KW
ηCO2~5 - 15%
Nd:YAG = 1064 nm
M23 = 2; pulse amp
P = 100 W
η = 3 - 8%; diode pumped
RPP cK23: 3.0
M23 Nd:YAG = 1064 nm
P = 6 KW
RThz~10
Yb-glass = 1040 or 1020 nm or 1064 nm M2 Y
P = 6 KW RThz~40%
λdisc = 940 nm
Pave = KW - Pmax = 6 KW Pdisc~40%
λgas source = CO2
He explained, energized and charged each carbon dioxide, easy to be excited, can relax and vibrate so reducing pairs excitation rates or energy level:
- E0 equilibrium
- E2 symmetric stretching mode
- E3 bending mode
- E4 asymmetric stretching mode
He = 45%: good heat conduction and so dispersion effect
N2 = 45%: electric current can't excite directly, CO2 so N2 is excited and through collision excites CO2 atom
CO2 = 10%: active medium
M23 ηCO2 = 10600 nm
M2 Y1 e
λCO2 = 10600 nm
P = 1.7 - 6 KW
Semiconductor Source - Diode
- Top = 3GAS ➞ compound engineered with vacuum (metal) of electrons
- Bottom = ARCAPS ➞ compound engineered with extra electron
N-P junction with mirrored surface
aluminium, gallium, arsenide
When current is applied, electrons extra and holes meet & junction release photon. This phase encourages release photon. Other holes and electrons coupling, diverge and release their own photon with same, phase, direction.
Influence of Energy
- Low thickness (t1 < 10mm)
- High velocity ➔ low oxidation
- Low velocity ➔ more oxidation
- N2 (O2) and (H2) (except)
- High pressure ➔ Reweld
tl ➔ spread ➔ less fusion
I = AbsP . ds = dq(t1 = 0) ➔ I = I
- Low density
Reactive Fusion Cutting
- High thickness (t1)
- High velocity ➔ maximum
- Density ➔ cutting possibility
- O2 N2 + O2 ➔ oxide
Only value above ➔ keep
If so, then we have an extra term
Thus by oxidation (exothermic reaction):
V ➔ ➔ oxidations (steady for reactivefusion cutting)
Variation of surface &right; importantbecause surface receptive
Equation I ➔ V because AbsP ➔ Oxide layer and improve absorption
Melt Capacity Model
Freezing rateAbsP = ρ(cp(TM - T1) + L + V + (M)) = const
V functional variables
Q ➔ thermal capacities/multiple uses
U ➔ easier heat of fusion
U = Easier heat of vaporization
I^i ➔ constant
If we have more power vectorone faster in higher power
HP
- No conduction
- No convection
- No radiation in beam
- Only W' variable
- TM = TV - all fixed numbers
We can change the power with avery higher number
Comparison cutting with ω2
On Earth, and materials that cannot melt (wood) or lower TM, ➔ it is more used for metals — beam energy
HP
radial off distance
If Φ ➔ reactive fusion cutting ➔ faster on surfaceIf Φ < S ➔ vaporization and melt and ➔ faster inside piece compare abruption length to bite distribute absorbance
We need on high gravity enough to maintain a constant distancebetween laser head and surface, because it loses more significantly even in flat
PAbs = const 11 (ρc2, ρLρo, .dsk) d Ψ = const
romeo (car stereotype) -> model estimate
leak initial position -> energy required to remove 1 electron from an atom
- xye thermal commitment (T) -> reference tempo of energy
leotinity -> tendency to react with work pigs (ex 0-vation)
ΔH -> Σoints atltright | Σ < 200 hooked for antonance atries, we must excite energy from qxiation, but plus excitation in chair
N2 estimate -> detect nuisance in leo enter pooring, for the sis
A. (air pal) -> mixed inquirial phase because cow ionization pointwise
H35 (mix A1-H35: F H height is escaption) -> t > 10mm deposit present because highly exploits
continued of as is
Pac makes qxidetions and attintions, HAZ has limited force on the workpiece
ABS split reomics, con ous oep wilowers, in ole contsertous
We don't hove ou height equiny new as fairs, because the voltage V is an identical measure op need-off dinnonia
This equinix air inturdition equinix leow > 5"mapper limood
pu ednierisuf
it -> dow piece increase
increase
wee Sour snloes
V speed
bull inflisio
kiger ilision
" скушman" и "anvator" motion
kerf
regail indication depends on totic aitation
from workpiece, because enclosed halo a plumo airion
HAZ -> coupons oncal
bitrim of returns !