STUDIES OF ENERGY RECOVERY LINACS AT ... - CASA

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FIG. 2.10: Illustration of quadrupole scan method to measure the transverse emittance. The strength of a quadrupole is varied while the downstream beam size is measured. From Eq. (2.11) and Eq. (2.13) the emittance can be extracted by fitting data with a quadratic fit. scan and is illustrated in Fig. 2.10. In practice, the quadrupole is scanned over many values of the strength. By fitting the data with a least-squares quadratic fit the unknown quantities are extracted. Because the transfer matrix has a unit determinant, the following relation holds [38] 39 βγ − α 2 ≡ 1 (2.12) where γ ≡ (1 + α 2 )/β. Using the three fitting parameters from the quadratic fit, (β1ɛg), (γ1ɛg), (α1ɛg), and using Eq. (2.12), the emittance can be calculated ɛ 2 g = (β1ɛg)(γ1ɛg) − (α1ɛg) 2 (2.13) The technique described above is straightforward for a linac, however for a recir- culating linac like CEBAF, the situation becomes more complicated. The difficulty arises because the quadrupole used for the scan is common to two co-propagating
eams. The effects of varying the quadrupole strength on the energy recovered beam, in terms of machine performance, is minimal because the beam is immedi- ately deflected to the dump. The accelerated beam, however, also feels the effects of the quadrupole change which creates a mismatch between the beam and the design machine optics. The consequences of this mismatch is twofold. First, since the emittance measurement assumes that the beta functions prior to the scanning quadrupole remain constant, if left uncorrected, the mismatched beam will recircu- late through the machine and arrive at the quadrupole with different beta functions. Second, for large excursions of the quadrupole strength the mismatch can become severe, leading to excessive beam loss and thereby causing the machine to trip off. The solution for both problems is to produce compensatory optics downstream of the scanning quadrupole to re-match the beam to the rest of the machine. Note that placing a quadrupole in the dump beamline would avoid this com- plication altogether. In this case the quadrupole could be scanned without the need to produce compensating optics. Unfortunately due to constraints in time and in the available space on the dump beamline, this option was not feasible. 2.4.2 Measuring Beam Sizes The beam profile monitor used for the measurement is an intercepting device known as a wire scanner, although other beam profile monitoring devices such as flu- orescent screens and OTR monitors could also be used. Wire scanners are routinely used throughout the CEBAF accelerator to measure the beam profile by recording the charge and position of a thin wire as it passes through the beam [39]. The wire scanner consists of an assembly that rigidly holds three 25 µm tungsten wires oriented along the x, x-y and y axes. An illustration of a 3-wire scanner is shown in Fig. 2.11. 40
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STUDIES OF ENERGY RECOVERY LINACS A
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DEDICATION To my wife Danielle and
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2 CEBAF with Energy Recovery . . .
Page 7 and 8: 5.2 HOM Power . . . . . . . . . . .
Page 9 and 10: ACKNOWLEDGMENTS First and foremost
Page 11 and 12: 6.1 Summary of the measured effects
Page 13 and 14: 2.10 Illustration of quadrupole sca
Page 15 and 16: 5.1 Successive frames in time (prog
Page 17 and 18: 6.8 A plot of 1/Qeff versus average
Page 19 and 20: ABSTRACT An energy recovering linac
Page 21 and 22: CHAPTER 1 Introduction An increasin
Page 23 and 24: FIG. 1.1: Schematic of a generic li
Page 25 and 26: FIG. 1.2: A CEBAF 5-cell cavity wit
Page 27 and 28: The solution to Eq. (1.3) is U(t) =
Page 29 and 30: y reducing the impedance of HOMs, a
Page 31 and 32: Despite its success, this method of
Page 33 and 34: design parameters, most notably ach
Page 35 and 36: 1.4.2 Machine Optics The second cat
Page 37 and 38: analytic model elucidates many impo
Page 39 and 40: CHAPTER 2 CEBAF with Energy Recover
Page 41 and 42: FIG. 2.1: Energy versus average cur
Page 43 and 44: FIG. 2.3: Additional hardware insta
Page 45 and 46: FIG. 2.4: A picture of the energy r
Page 47 and 48: dipoles and beam diagnostics such a
Page 49 and 50: FIG. 2.7: Horizontal (red) and vert
Page 51 and 52: FIG. 2.8: Illustration of the cryom
Page 53 and 54: linac and θNL is the RF phase. The
Page 55 and 56: 2.4 Transverse Emittance One of the
Page 57: where σ2 is the rms beam size meas
Page 61 and 62: FIG. 2.12: A typical wire scan near
Page 63 and 64: quadratic fit and a multiple regres
Page 65 and 66: ting the data is difficult. Without
Page 67 and 68: primary source of error is measurin
Page 69 and 70: identified, although the phase dela
Page 71 and 72: TABLE 2.3: Comparison of Twiss para
Page 73 and 74: the results of the fits. The vertic
Page 75 and 76: FIG. 2.18: Schematic illustrating t
Page 77 and 78: FIG. 2.19: The GASK signal measured
Page 79 and 80: FIG. 2.20: The measured normalized
Page 81 and 82: CHAPTER 3 The Jefferson Laboratory
Page 83 and 84: FIG. 3.1: Schematic of the 10 kW FE
Page 85 and 86: FIG. 3.2: Layout of the DC photocat
Page 87 and 88: accelerating gradient at the front
Page 89 and 90: eason for making the endloops achro
Page 91 and 92: FIG. 3.7: Illustration of path leng
Page 93 and 94: 3.5 Longitudinal Dynamics This sect
Page 95 and 96: FIG. 3.9: The effect of a thin focu
Page 97 and 98: Under the constraint that each orde
Page 99 and 100: form of beam breakup not only occur
Page 101 and 102: 4.1 The Pillbox Cavity Although the
Page 103 and 104: FIG. 4.2: Electric field (red) and
Page 105 and 106: where the full 4×4 transfer matrix
Page 107 and 108: The threshold is inversely proporti
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4.3 BBU Simulation Codes: Particle
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6. The second pass beam bunch then
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which excites it. The BBU instabili
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Equation (4.41) is a dispersion rel
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FIG. 4.4: Output from MATBBU showin
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FIG. 4.5: Setup for measuring cavit
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Consequently, depending on the exte
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The projection of the beam displace
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TABLE 4.1: Experimental measurement
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FIG. 4.10: A plot showing the effec
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these cryomodules. Modes from these
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CHAPTER 5 Experimental Measurements
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threshold current - preferably with
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occurred at approximately 2 mA of a
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FIG. 5.5: FFT of a pure 2106.007 MH
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FIG. 5.6: Illustration to show the
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5.4 Measuring the Threshold Current
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for the HOM-beam system and is deri
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FIG. 5.10: Schematic of the experim
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FIG. 5.12: A plot of 1/Qeff versus
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measured HOMs in zone 3, a BTF meas
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FIG. 5.16: HOM voltage measured fro
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FIG. 5.18: A plot of the three valu
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the beam’s response in regions wh
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CHAPTER 6 BBU Suppression: Beam Opt
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FIG. 6.1: Schematic of a FODO cell
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plane [85]. Equations (6.7) and (6.
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6.2.3 Discussion The method of poin
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FIG. 6.3: Beam envelopes (horizonta
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FIG. 6.6: Beam position monitor rea
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FIG. 6.8: A plot of 1/Qeff versus a
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⎛ ⎞ ⎜ ⎝ 0 0 0 0 0 −1/K 0
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FIG. 6.11: A plot of 1/Qeff versus
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FIG. 6.12: Threshold current for no
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FIG. 6.14: Threshold current utiliz
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TABLE 6.1: Summary of the measured
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CHAPTER 7 BBU Suppression: Feedback
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FIG. 7.1: A schematic of the feedba
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FIG. 7.4: A coaxial 3-stub tuner us
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All of these considerations are con
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FIG. 7.6: Generic layout for a feed
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in Section 4.2.1, however, in the p
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FIG. 7.7: The threshold current as
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FIG. 7.8: Threshold current versus
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FIG. 7.10: The threshold current as
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CHAPTER 8 Conclusions The work pres
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le were experimentally measured. Du
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APPENDIX A The Pillbox Cavity Start
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FIG. A.1: A pillbox cavity exhibiti
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Ez(ρ, φ) = ψ(ρ, φ) = E0Jm(γρ
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FIG. B.1: Relationship of the S-par
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FIG. C.1: Impedance and frequency o
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FIG. C.5: Impedance and frequency o
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BIBLIOGRAPHY [1] M. Tigner, Nuovo C
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[22] L. Merminga, in Proceedings of
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[50] C. Hernandez-Garcia et al., in
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[79] L. Merminga et al., in Proceed
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VITA Christopher D. Tennant Christo
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