STUDIES OF ENERGY RECOVERY LINACS AT ... - CASA

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old current is on the order of several Amperes. As a consequence of this method, the fundamental frequency is also shifted and the cavity must be set to zero accelerating gradient, essentially making it a drift space. Because these measurements were performed in 2004, the effect was measured specifically for the 2114.156 MHz mode as it was causing BBU at the time (see Section 5.3). While the mechani- cal tuner is capable of shifting the fundamental mode frequency by ±200 kHz, the 2114.156 MHz mode shifted less than 100 kHz. Ultimately, because methods such as point-to-point focusing proved to be so effective, the effects of these frequency shifts on the threshold current were never investigated experimentally. 7.1 Cavity-based Feedback Cavity-based feedback aims to directly lower the QL of a dangerous HOM. Two feedback mechanisms were experimentally tested and are discussed in the following two sections. 7.1.1 Active Q-damping Circuit The idea of the damping circuit is as follows: couple voltage from one of the HOM ports and using a narrowband filter select the HOM frequency of interest, shift the signal by 180 ◦ in phase, amplify the signal and then return it to the cavity through the same HOM port. A schematic of the setup is given in Fig. 7.1. By adjusting the gain and phase shift, the quality factor of the HOM could be reduced by a factor of 20. However, for these optimally tuned values of the gain and phase shift, the feedback loop became very sensitive to external disturbances, such as motion in the cables and the effects of the amplifier warming up. To avoid issues with stability, the feedback circuit was set to reduce the QL of the 2106 MHz mode 163 by a factor of 4.8 (see Fig. 7.2). The threshold current was determined to be 2.3 mA
FIG. 7.1: A schematic of the feedback circuit used to damp the loaded Q of a mode. with the damping circuit off by direct observation. When the beam was turned on, the BBU threshold was determined by the BTF method with the results shown in Fig. 7.3. The threshold current became (7.6 ± 0.2) mA. 7.1.2 Passive Q-damping with a Stub Tuner A 3-stub tuner acts as an impedance transformer and is shown in Fig. 7.4. A stub tuner was attached to each cable connected to the two HOM ports of cavity 7. A schematic of the setup is illustrated in Fig. 7.5. The idea is to manipulate the stubs in such a fashion that the incident HOM voltage is reflected with a 180 ◦ phase shift. Because the stub tuner is a passive device, the attenuation in the cables from the HOM ports becomes a factor and prevented optimal Q-damping. Nevertheless, a modest decrease (a factor of 1.6) in the QL of the 2106 MHz mode and the corresponding increase in the threshold current were observed. In principle, better suppression could be attained by connecting the stub tuner 164 in the FEL vault, closer to the cryomodule, where cable attenuation would be re-
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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 . . .
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5.2 HOM Power . . . . . . . . . . .
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ACKNOWLEDGMENTS First and foremost
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6.1 Summary of the measured effects
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2.10 Illustration of quadrupole sca
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5.1 Successive frames in time (prog
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6.8 A plot of 1/Qeff versus average
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ABSTRACT An energy recovering linac
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CHAPTER 1 Introduction An increasin
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FIG. 1.1: Schematic of a generic li
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FIG. 1.2: A CEBAF 5-cell cavity wit
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The solution to Eq. (1.3) is U(t) =
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y reducing the impedance of HOMs, a
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Despite its success, this method of
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design parameters, most notably ach
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1.4.2 Machine Optics The second cat
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analytic model elucidates many impo
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CHAPTER 2 CEBAF with Energy Recover
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FIG. 2.1: Energy versus average cur
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FIG. 2.3: Additional hardware insta
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FIG. 2.4: A picture of the energy r
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dipoles and beam diagnostics such a
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FIG. 2.7: Horizontal (red) and vert
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FIG. 2.8: Illustration of the cryom
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linac and θNL is the RF phase. The
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2.4 Transverse Emittance One of the
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where σ2 is the rms beam size meas
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eams. The effects of varying the qu
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FIG. 2.12: A typical wire scan near
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quadratic fit and a multiple regres
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ting the data is difficult. Without
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primary source of error is measurin
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identified, although the phase dela
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TABLE 2.3: Comparison of Twiss para
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the results of the fits. The vertic
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FIG. 2.18: Schematic illustrating t
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FIG. 2.19: The GASK signal measured
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FIG. 2.20: The measured normalized
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CHAPTER 3 The Jefferson Laboratory
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FIG. 3.1: Schematic of the 10 kW FE
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FIG. 3.2: Layout of the DC photocat
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accelerating gradient at the front
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eason for making the endloops achro
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FIG. 3.7: Illustration of path leng
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3.5 Longitudinal Dynamics This sect
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FIG. 3.9: The effect of a thin focu
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Under the constraint that each orde
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form of beam breakup not only occur
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4.1 The Pillbox Cavity Although the
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FIG. 4.2: Electric field (red) and
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where the full 4×4 transfer matrix
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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
Page 131 and 132: CHAPTER 5 Experimental Measurements
Page 133 and 134: threshold current - preferably with
Page 135 and 136: occurred at approximately 2 mA of a
Page 137 and 138: FIG. 5.5: FFT of a pure 2106.007 MH
Page 139 and 140: FIG. 5.6: Illustration to show the
Page 141 and 142: 5.4 Measuring the Threshold Current
Page 143 and 144: for the HOM-beam system and is deri
Page 145 and 146: FIG. 5.10: Schematic of the experim
Page 147 and 148: FIG. 5.12: A plot of 1/Qeff versus
Page 149 and 150: measured HOMs in zone 3, a BTF meas
Page 151 and 152: FIG. 5.16: HOM voltage measured fro
Page 153 and 154: FIG. 5.18: A plot of the three valu
Page 155 and 156: the beam’s response in regions wh
Page 157 and 158: CHAPTER 6 BBU Suppression: Beam Opt
Page 159 and 160: FIG. 6.1: Schematic of a FODO cell
Page 161 and 162: plane [85]. Equations (6.7) and (6.
Page 163 and 164: 6.2.3 Discussion The method of poin
Page 165 and 166: FIG. 6.3: Beam envelopes (horizonta
Page 167 and 168: FIG. 6.6: Beam position monitor rea
Page 169 and 170: FIG. 6.8: A plot of 1/Qeff versus a
Page 171 and 172: ⎛ ⎞ ⎜ ⎝ 0 0 0 0 0 −1/K 0
Page 173 and 174: FIG. 6.11: A plot of 1/Qeff versus
Page 175 and 176: FIG. 6.12: Threshold current for no
Page 177 and 178: FIG. 6.14: Threshold current utiliz
Page 179 and 180: TABLE 6.1: Summary of the measured
Page 181: CHAPTER 7 BBU Suppression: Feedback
Page 185 and 186: FIG. 7.4: A coaxial 3-stub tuner us
Page 187 and 188: All of these considerations are con
Page 189 and 190: FIG. 7.6: Generic layout for a feed
Page 191 and 192: in Section 4.2.1, however, in the p
Page 193 and 194: FIG. 7.7: The threshold current as
Page 195 and 196: FIG. 7.8: Threshold current versus
Page 197 and 198: FIG. 7.10: The threshold current as
Page 199 and 200: CHAPTER 8 Conclusions The work pres
Page 201 and 202: le were experimentally measured. Du
Page 203 and 204: APPENDIX A The Pillbox Cavity Start
Page 205 and 206: FIG. A.1: A pillbox cavity exhibiti
Page 207 and 208: Ez(ρ, φ) = ψ(ρ, φ) = E0Jm(γρ
Page 209 and 210: FIG. B.1: Relationship of the S-par
Page 211 and 212: FIG. C.1: Impedance and frequency o
Page 213 and 214: FIG. C.5: Impedance and frequency o
Page 215 and 216: BIBLIOGRAPHY [1] M. Tigner, Nuovo C
Page 217 and 218: [22] L. Merminga, in Proceedings of
Page 219 and 220: [50] C. Hernandez-Garcia et al., in
Page 221 and 222: [79] L. Merminga et al., in Proceed
Page 223 and 224: VITA Christopher D. Tennant Christo
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