Bias Magnet for the Booster’s 2-nd Harmonic Cavity An attempt to evaluate the scope of work based of the existing RF design of the cavity 9/10/2015I. T.

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Presentation transcript:

Bias Magnet for the Booster’s 2-nd Harmonic Cavity An attempt to evaluate the scope of work based of the existing RF design of the cavity 9/10/2015I. T. Sept. 10 meeting presentation slides1

Geometry and Assumptions Required change of Frequency vs Time: Tan, July 17, 2015 First question is about a sale of the system  average power consumption must be found Cavity geometry: G.R., July 2015

Frequency response and average power Results of modeling by G.R. Combining functions f(t) and f(I), we get the required current shape. Having the function Iw(t) expressed analytically allows making analytical evaluation of power loss and generate other requirements needed for a power supply design.

Harmonic Representation of the Current Cycle The second order expansion reproduce the required current shape quite accurately. Iw(t) = ∙cos(2π∙t/T) ∙cos(4π∙t/T)

Coil Design -0.41” (10.41 mm) rectangular copper wire with 0.229” (5.8 mm) hole for water cooling; -Copper cross-section 80 mm 2 ; cooling hole cross-section 26.5 mm 2 ; -Number of turns – 50 (conservative), 56 max; -Double-layer winding technique  required length of wire L wire ≈ 80 m -Four reels of wire must be procured to avoid splices (90 feet reel) -Current range from I min = A to I max = 440 A -Current shape: I(w) = I0 – I1∙cos(2π∙t/T) – I2∙cos(4π∙t/T with I0 = A, I1 = A and I2 = A -Wire resistance R = Ohm -Power is found by integrating the losses through the cycle  W cycle = J; -f = 15 Hz  P = 2140 W

Coil Cooling Two cooling loops assumed. In the loop formed by the outer part of the coil, the power loss is ~1100 W. Assuming 10 ºC cooling water temperature rise, the required water flow is Q [l/s] = 0.24∙P[kW]/ΔT[C] = [l/s]  1.58 l/min  ~0.4 GPM. Water velocity in the channel with the cross-section S = 26.6 mm 2 will be v[m/s] = 1000∙Q[l/s]/S[mm 2 ] ≈ 1 m/s, which seems OK. This water flow will require the next pressure head: h = v 2 ∙L/2d 1.33 where h is measured in kG/cm 2, v is the velocity in m/s, d is the hole diameter in mm, and L is the length of the circuit in meters. For our parameters (L = 39 m) h = 1 2 ∙39/10.4 = 3.75 kG/cm 2 or ~53 PSI. Volume of the coil is cm 3  weight is ~100 kG. Power load is 2140/10500 = 0.2 W/cm 3.

Flux Return. Inductance. Voltage Central part of the flux return is made of low-frequency high permeability ferrite; peripheral part of the flux return is assembled using silicon steel plates. Thickness of the yoke will be optimized to avoid saturation. Shape of the poles will be optimized for better field uniformity in the garnet material Expected inductance of the coil is ~2.5 mH at the maximum current and ~3.5 mH at the minimum current Expected resistive voltage is ~9 V; Inductive voltage is ~45 V.

Power Loss in the Garnet Material Running a 2D RF model gives frightening numbers for the power loss: at 125 A f = MHz; Q = 3452; ΔU = 20.5 V  power scaling factor to 100 kV is 23.8E6 Maximum power loss is ~50 W/cm 3 Average power must be evaluated to have realistic understanding of the cooling problem Power loss in the hot spot – 6.1 W/m 3 ΔU = V  power scaling factor to 100 kV is 9.03E6 So, the power density at the hot spot at 100 kV is 54.2 MW/m 3 or 54.2 W/cm 3 Total dissipated power in the garnet at MHz is *9.03E6 = W Magnetic portion of the losses is *9.03E6 = W Stored energy in the cavity is 2*1.71E-8*9.03E6 = 0.31 J Based on these numbers, quality factor associated with the losses in the garnet  Q AL800 ≈ 4150

Power Loss in the AL-800 Material Table below reflects results of 2D modeling of the cavity with different current settings in the coil Comparison with the 3D modeling by G.R. Maximum and average power density Power loss in AL800 material (magnetic and total)

Average Power Loss in the AL-800 Material Let’s find the average energy deposited in the garnet block during one cycle. Current change is in accordance with the harmonic representation (as found earlier): Iw(t) = ∙cos(2π∙t/T) ∙cos(4π∙t/T) RF voltage power drops linearly from 100 kV at t = 0 to 0 at t = 23 ms. U = U 0 ∙(1 – t/τ) when t < τ and 0 when t ≥ τ This means that the power scaling factor also changes with time; additional, time dependent coefficient for the power scaling factor is λ(t) = (1-t/τ) 2 Procedure is detailed in the next sheet 

Average Power Loss in the AL-800 Material The procedure is as following: Use the expression for the current change: Iw(t) = ∙cos(2π∙t/T) ∙cos(4π∙t/T). Use expression for the frequency as a function of current: f(I) = ∙I – 0.868∙I ∙I 3 – 4.1∙10 -4 ∙I 4 (I is in kilo-Amperes) Use expression for the power loss vs frequency (P in W, f in MHz): P(f) = – *f *f 2 Apply additional scaling factor and get adjusted (for the accelerating voltage) power loss. Integrate the losses over time  J per cycle  3140 W in the garnet (0.51 W/cm 3 average power density)

Maximum Power Loss Density in the AL-800 Material Procedure: 1. Use the following expression for the current change: Iw(t) = ∙cos(2π∙t/T) ∙cos(4π∙t/T). 2. Use expression for the frequency as a function of current: f(I) = ∙I – 0.868∙I ∙I 3 – 4.1∙10 -4 ∙I 4 (I is in kilo-Amperes) 3. Use expression for the power loss density vs frequency (p in kW/cm 3, f in MHz): p(f) = 1460/(f-70) *(f-90) (at R = 128 mm, Z = 110)  4. Apply additional scaling factor for the accelerating voltage drop in time. 5. Integrate the power loss density over time in the hot spot R = 128 mm, Z = 110 mm  The accumulated heat per one cycle is 0.16 J/cm 3 per cycle. Average power density in the hot spot is 2.4 W/cm 3.

Temperature rise at the hot spot Is the found maximum power loss density dangerous? Let’s make simple evaluation. Let’s consider a plate with thickness t. Let’s have coordinate x in the direction perpendicular to the plate with x = 0 at the surface where we will find the temperature rise relative to the other surface of the plate. Power deposition density is p(x). Thermal conductivity is k. Let’s assume p(x) = p0*exp(-x/d) Power flux in the direction towards x = 0 plane is Q(x) = ∫p(x)dx with the limits from x = t to x = 0  Q(x) = -p0·d·[exp(-x/d) - exp(-t/d)] = k·dT/dx  dT/dx = -p0·d/k·[exp(-x/d) - exp(-t/d)] We assume here that the temperature derivative at x = t is zero  ΔT(x) = d 2 ·p0/k·[exp(-x/d) - exp(-t/d)] + p0·d/k·exp(-t/d)·(x-t) or ΔT(x) = d·p0/k·{[d·exp(-x/d) – (d – x + t)·exp(-t/d)]} For x = 0 with t = 2 cm and d = 10 cm, and with k = W/(m-K) and p0 = 2.4 W/m 3 we have: ΔT(0) = 685.7*(10 – 12*0.82) ≈ 120 K

I = 125 A I = 150 A I = 175 AI = 200 A I = 250 A I = 300 A I = 350 AI = 450 A