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STUDIES OF ENERGY RECOVERY LINACS AT ... - CASA

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6.8 A plot of 1/Qeff versus average beam current for the 2106 MHz mode<br />

with the local reflector activated. . . . . . . . . . . . . . . . . . . . . 150<br />

6.9 A schematic illustrating the effect of a 90 ◦ rotation of the betatron<br />

planes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 151<br />

6.10 Nominal betatron functions in the 4F region of the FEL (top) and<br />

with a solenoid (blue) activated to produce a 90 ◦ rotation of betatron<br />

planes with the upstream and downstream quadrupole triplets used<br />

for matching (bottom). . . . . . . . . . . . . . . . . . . . . . . . . . . 153<br />

6.11 A plot of 1/Qeff versus average beam current for the 2106 MHz mode<br />

with the rotator activated. . . . . . . . . . . . . . . . . . . . . . . . . 154<br />

6.12 Threshold current for nominal, decoupled optics as a function of the<br />

number of dipole modes per cavity and the HOM rotation angle. . . . 156<br />

6.13 Threshold current utilizing a local reflector as a function of the number<br />

of dipole modes per cavity and the HOM rotation angle. . . . . . 157<br />

6.14 Threshold current utilizing a rotator as a function of the number of<br />

dipole modes per cavity and the HOM rotation angle. . . . . . . . . . 158<br />

7.1 A schematic of the feedback circuit used to damp the loaded Q of a<br />

mode. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 164<br />

7.2 The effect on the loaded Q of the 2106 MHz mode with the cavitybased,<br />

narrowband feedback off (red curve represents Q = 6.2 × 10 6 )<br />

and on (blue curve represents Q = 1.3 × 10 6 ). . . . . . . . . . . . . . 165<br />

7.3 A plot of 1/Qeff versus average beam current for the 2106 MHz mode<br />

with the Q-damping feedback circuit on. . . . . . . . . . . . . . . . . 165<br />

7.4 A coaxial 3-stub tuner used for Q-damping. . . . . . . . . . . . . . . 166<br />

7.5 Schematic of the experimental setup using a 3-stub tuner to damp<br />

the loaded Q of a mode. . . . . . . . . . . . . . . . . . . . . . . . . . 167<br />

7.6 Generic layout for a feedback system in an ERL. . . . . . . . . . . . . 170<br />

7.7 The threshold current as a function of gain for td = 0 from the analytic<br />

model (red line) and the results of the simulation code (black open<br />

circles). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 174<br />

xvii

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