Performance of an electron linear accelerator for the first photoneutron source in China

Performance of an electron linear accelerator for the first photoneutron source in China 1 2 3 first-author 1 2 1 2 1 2 1 2 1 2 corresp Corresponding author, zhangmeng@sinap.ac.cn Corresponding author, zhangmeng@sinap.ac.cn zhangmeng@sinap.ac.cn Shanghai Institute of Applied Physics, Chinese Academy of Sciences, Shanghai 201800, China Shanghai Institute of Applied Physics, Chinese Academy of Sciences, Shanghai 201800, China Shanghai Synchrotron Radiation Facility, Chinese Academy of Sciences, Shanghai 201204, China Shanghai Synchrotron Radiation Facility, Chinese Academy of Sciences, Shanghai 201204, China University of Chinese Academy of Sciences, Beijing 100049, China University of Chinese Academy of Sciences, Beijing 100049, China A compact 15.0-MeV, 1.5-kW electron linear accelerator (LINAC) was successfully constructed to provide an electron beam for the first photoneutron source at the Shanghai Institute of Applied Physics, Shanghai, China. This LINAC consists of five main parts: a thermal cathode grid-controlled electron gun, a pre-buncher, a variable-phase-velocity buncher, a light-speed accelerating structure, and a high-power transportation beamline. A digital feedforward radio frequency compensator is adopted to reduce the energy spread caused by the transient beam loading effect. Furthermore, a real-time electron gun emission feedback algorithm is used to keep the beam stable. After months of efforts, all the beam parameters successfully met the requirements of the facility. In this paper, the beam commissioning process and performance of the LINAC are presented. Electron linear accelerator High-power transportation beamline Digital feedforward radio frequency compensation Real-time electron gun emission feedback algorithm Transmission efficiency 1 Introduction 1 The energies of neutrons produced in a target bombarded by pulses of high-energy electrons from a linear accelerator (LINAC) may be determined with high resolution by employing time-of-flight techniques [ 1 1 - 4 4 1-4 ] . A photoneutron source (PNS) with appropriate parameters is a powerful tool for producing intense pulsed neutron beams. As an auxiliary project of the Thorium Molten Salt Reactor Energy System (TMSR) Programme at the Shanghai Institute of Applied Physics (SINAP) in Shanghai, China, in the first stage, the application of the PNS focuses on thermal neutron data measurement with a relatively lower neutron flux [ 2 2 ] , and hence the facility employs a 15 MeV electron LINAC, bombarding a tungsten target with 1.5 kW electrons to produce neutrons. In the future, with the requirement for higher fast neutron flux [ 2 2 ] , the LINAC beam energy will be upgraded to 100 MeV for the final stage and at this bombarding target energy of the beam, the neutron yield will almost saturate [ 5 5 ] . Presently, we have successfully completed this first stage work, including the technical design, assembly, radio frequency (RF) and high voltage (HV) conditioning, and beam commissioning of the machine. A schematic drawing of the PNS is shown in Fig. 1 Fig. 1 . The whole PNS is composed of four main areas: the neutron experimental area, the LINAC, power source cabinets, and a control area. The results of beam acceleration testing as well as an overview of the whole LINAC system will be presented in this paper. 1.1 Overview of the LINAC 1 The 15-MeV, 1.5-kW LINAC consists of a thermal cathode grid-controlled electron gun (E-Gun), a standing-wave pre-buncher, a traveling-wave buncher (TWB), and a light-speed accelerating structure. After the beam travels through the LINAC, highly efficient beam collimation and transportation can be achieved in a high-power transportation beamline (HPTB) [ 6 6 ] . Fig. 2 Fig. 2 gives the layout of the whole LINAC for the PNS (phase-I) facility. A thermal cathode grid-controlled E-Gun is employed as the electron source [ 7 7 , 8 8 ] . The voltage between the anode (grounded) and the cathode is −60 kV. The cathode grid assembly is a Y646B from Eimac CPI, which can meet the requirement of a maximum beam current of 1 A. One amplifier, which is designed by SINAP, is adopted to drive the cathode with a 0.5–3.0 μs pulse width. An HV direct current (DC) power supply (model WR125N2 from Glassman) is adopted to provide −60 kV voltage between the anode and the cathode. To increase the efficiency of beam capture and acceleration, a bunching system consisting of a pre-buncher and a buncher in sequence is employed immediately following the E-Gun. For the cavity of the pre-buncher, we employ a conventional re-entrant type structure. This cavity is a standing-wave cavity made of stainless steel with a nickel-coated surface inside. The major design parameters of the pre-buncher cavity are listed in Table 1 Table 1 . A particular solid amplifier of maximum power of 4.0 kW is adopted to provide the RF power to the pre-buncher [ 9 9 ] . 1 1   Parameter 1 1 Value 1 1 Operating frequency (MHz) 1 1 2856 1 1 Gap voltage (kV) 1 1 ~25 (adjustable) 1 1 Q factor 1 1 963 1 1 Total length   (mm)   1 1 342.76 1 1 Drift length (mm) 1 1 176.38 1 1 Cavity length (mm) 1 1 30.6 1 1 Gap length (mm) 1 1 8.89 1 1 Beam aperture (mm) 1 1 19.05 1 1 Power capacity (kW) 1 1 2.0 1 1 Coupling coefficient 1 1 1.04 After traveling through the pre-buncher, the beam will be bunched and accelerated further by a multiple-cell disk-load TWB, which works in the 2π/3 mode. This TWB consists of 16 disk-load cells including the input and the output coupler cavities. To improve the capture efficiency, before the light-speed cells, the characteristic parameters of the first six cells vary slightly and the other 10 cells comprise the constant-phase-velocity constant-impedance structure. The cells’ main design parameters and geometry dimensions are listed in Tables 2 Tables 2 and 3 3 , respectively. In Table 3 Table 3 , β p is the normalized phase velocity of the accelerating cell, β g is the normalized group velocity of the accelerating cell, t f is the filling time of the accelerating cell, α is the attenuation constant per unit length, Q is the quality factor of the accelerating cell, R m is the shunt impedance per unit length, and f is the working frequency of the accelerating cell. 1 1   Parameter 1 1 Value 1 1 Operating frequency (MHz) 1 1 2856 1 1 Working mode 1 1 2π/3 1 1 Cell number 1 1 16 1 1 Total length (m) 1 1 0.57 1 1 Voltage standing-wave ratio (VSWR) 1 1 <1.1 1 1 Bandwidth (VSWR = 1.2) (MHz) 1 1 4 1 1 Phase advance per period (degrees) 1 1 120±2.5 1 1 Working temperature (℃) 1 1 45±0.1 1 1 Input RF power (MW) 1 1 2 1 1 Output electron energy (MeV) 1 1 2 1 1  Cell No. 1 1 β p 1 1 β g (%) 1 1 t f (ns) 1 1 α 1 1 a (mm) 1 1 b (mm) 1 1 Q 1 1 R m (MΩ/m) 1 1 f (MHz) 1 1 1 1 1 0.63 1 1 0.7167 1 1 1.02594E-08 1 1 0.4507 1 1 10 1 1 41.502 1 1 9266 1 1 25.757 1 1 2856.035 1 1 2 1 1 0.6 1 1 0.7068 1 1 1.04031E-08 1 1 0.4801 1 1 10 1 1 41.575 1 1 8820 1 1 22.834 1 1 2856.005 1 1 3 1 1 0.6 1 1 0.7068 1 1 1.04031E-08 1 1 0.4801 1 1 10 1 1 41.575 1 1 8820 1 1 22.834 1 1 2856.005 1 1 4 1 1 0.87 1 1 0.7455 1 1 9.8631E-09 1 1 0.3258 1 1 10 1 1 41.102 1 1 12321.3 1 1 49.307 1 1 2856.006 1 1 5 1 1 0.93 1 1 0.7458 1 1 9.85913E-09 1 1 0.3094 1 1 10 1 1 41.035 1 1 12968.3 1 1 54.926 1 1 2856.013 1 1 6 1 1 0.96 1 1 0.7456 1 1 9.86178E-09 1 1 0.3023 1 1 10 1 1 41.005 1 1 13277.2 1 1 57.67 1 1 2856.002 1 1 7–16 1 1 0.98 1 1 0.7452 1 1 9.86707E-09 1 1 0.298 1 1 10 1 1 40.986 1 1 13478 1 1 59.474 1 1 2856.001 Fig. 3 Fig. 3 gives the structure schematic of the disk-loaded or iris-loaded waveguide [ 10 10 - 14 14 10-14 ] . This bunching scheme had already been successfully proved to be practicable and efficient on an industrial LINAC with 1 kW (2 MeV) averaged beam power at SINAP. In addition, to avoid beam losses transversely, the conventional focusing method of solenoid coils is employed to provide the focusing force. After the two bunching sections, a light-speed accelerating structure is employed to accelerate the beam from 2 MeV to the designed beam energy of 15 MeV. For the light-speed section, there are two kinds of structures. After investigation, including considerations of cost and efficiency, the decision was made to employ a constant impedance disk-load accelerating structure for our LINAC. It is also a traveling-wave structure that works in the 2π/3 mode, Tables 4 Tables 4 and 5 5 give the major design parameters and dimensions of the accelerating tube. In Table 5 Table 5 , β p is the normalized phase velocity of the accelerating cell, α is the attenuation constant per unit length, a is the radius of the aperture, b is the radius of the waveguide, Q is the quality factor of the accelerating cell, R m is the shunt impedance per unit length, and f is the working frequency of the accelerating cell. 1 1  Parameter 1 1 Value 1 1 Operating frequency (MHz) 1 1 2856 1 1 Working mode 1 1 2π/3 1 1 Cell number 1 1 40 1 1 Total length (m) 1 1 1.5 1 1 Shunt impedance (  MΩ/m  ) 1 1 53 1 1 Total attenuation 1 1 0.24 1 1 Group velocity ( v g / c ) 1 1 0.01546 1 1 VSWR 1 1 <1.1 1 1 Bandwidth (VSWR=1.2) (MHz) 1 1 4 1 1 Phase advance per period (degrees) 1 1 120±2.5 1 1 Working temperature (℃) 1 1 45±0.1 1 1 Input RF power (MW) 1 1 14 1 1 Output electron energy (MeV) 1 1 14.4 1 1 Cell No. 1 1 β p 1 1 α 1 1 a (mm) 1 1 b (mm) 1 1 Q 1 1 R m (MΩ/m) 1 1 f (MHz) 1 1 1-40 1 1 1 1 1 0.1411 1 1 12.115 1 1 41.475 1 1 13717 1 1 53.22 1 1 2856.001 The input RF high power for the buncher and the accelerating tube is generated simultaneously by the two-stage amplifiers. In the first stage, a solid-state amplifier having a maximum output power of 1.0 kW is employed to amplify the 0–5 dBm signal from the low-level radio frequency (LLRF). The final-stage amplifier, equipped with a Toshiba E37308 klystron, provides the maximum output of 27.5 MW. The power attenuation of the standard rectangular waveguide BJ32 is 0.46% per meter. The distance from the klystron to the buncher and the accelerating tube is ~10 m, so given the power loss of the flanges and ceramic windows; the total loss of the RF transportation line is estimated to be 10%. With the total input power of 16.4 MW to the buncher and accelerating tube, the output RF power of the klystron should be at least 18.3 MW, which is available from the power source. There is a 9 dB power divider between the buncher and the accelerating tube; through it, 2 MW of RF power is fed into the buncher. The remaining 14.4 MW of power is offered to the accelerating tube. The high-power phase shifter between the buncher and the accelerating tube can be used to control the RF phase separately for the two sections. After the accelerating tube, to transport the 15-MeV, 1.5-kW beam to the target area efficiently (see Fig. 1 Fig. 1 ), a well-designed HPTB is established. At the beginning of the HPTB, an integrating current transformer (ICT2), a beam position monitor (BPM2), and a profile (PRF2) are sequentially installed to calibrate the beam quality before it travels through the dipoles. The quadrupole triplet of Q1–Q3 is used to match the beam transverse envelope when the beam travels through the two 45-degree dipoles. Dipole B1, quadrupole Q4, and dipole B2 comprise a typical achromatic lattice to optimize the transmission efficiency between the two dipoles. The quadrupole triplet of Q5–Q7 is designed to match the envelope and the beam size on the tungsten target in the experimental zone. With ICT3, BPM3, and PRF4, we can get the beam performance after transportation. Based on the above configuration, a transmission of nearly 90% is reached. 2 Commissioning and testing 1 Beam commissioning and beam acceleration testing of the LINAC are performed in the following three steps: The first step is to perform RF power conditioning in the rectangular waveguide BJ32, the high-power phase shifter, the buncher, and the accelerating tube. Meanwhile, HV conditioning and cathode activation of the E-Gun are also performed. During this stage, because vacuum sparking and outgassing occur very frequently, it is indispensable to change the machine protection system from the beam commissioning mode to the RF conditioning mode. After approximately one week of conditioning time spent for the RF components mentioned above, the LINAC worked successfully with a modulator HV of 33 kV, an E-Gun HV of −60 kV, and a filament readback voltage of > 6.0 V [ 15 15 ] . After finishing step one above, the electron beam commissioning commenced. Because of the > 20-W beam power of every 3 μs length pulse for the nominal working mode, it is safer and more practical to perform beam commissioning with a rather shorter pulse such as ~3 ns and a lower repetition frequency such as 1 Hz. In that mode, we can adjust the configurations of solenoids, lenses, correctors, phases, and power amplitudes to get a suitable beam size on the screens of PRF1–PRF4 and ICT1–ICT3. The beam acceleration in the RF structures and beam optics transportation along the whole accelerator were optimized successfully [ 16 16 , 17 17 ] . The last key step is to increase the average power gradually by increasing the pulse length and repetition frequency sequentially. First, we gradually increased the length of the pulse to 3 μs. During this process, special attention had to be paid to the transient beam loading effect [ 10 10 ] , which can cause a rather large energy spread. Because of the limited beam pipe aperture, it would decrease the transmission efficiency of the beam when it traveled through the two 45-degree dipoles. Moreover, such a high beam power bombarding the beam pipe poses a danger to the chamber. It would probably melt the vacuum chamber and lead to air leakage. Another problem is the radiation protection corresponding to the beam loss. Therefore, a digital feedforward RF compensator, which uses a digital LLRF feedforward method to compensate for the RF power output, was successfully developed to decrease the energy spread caused by the transient beam loading effect [ 18 18 - 21 21 18-21 ] . After the LINAC configuration of the 3 μs pulse length is finished, the repetition frequency of the whole LINAC will be increased. During this process, with the increase of the beam power and temperature corresponding to the beam bombarding onto the surface of the tungsten target, the vacuum condition deteriorated seriously and quickly. It took a relatively long time for us to solve this problem. Because of space limitations, just after the exit of the accelerating tube, we employed an HPTB including two 45-degree dipoles to transport the 1.5 kV beam to the target area. There are both advantages and challenges with this design. Like the function of a real-time, online energy analysis station, the HPTB ensures that the beam quality of every pulse provided for the PNS is good enough and reproductive. Meanwhile, we should also make sure that the LINAC has higher stability and safety. For rather heavy beam loading, without changing the input RF power, the current of the beam should be stable enough to avoid beam loss in the HPTB section. However, the beam current will decrease slowly as the operating time increases or the repetition frequency increases. This might possibly be attributed to the "cooling" of the cathode, because the more thermionic electrons that are emitted, the more heat will be taken from the cathode. Therefore, we developed a real-time E-Gun emission feedback algorithm to keep the emitted beam current constant by changing the filament current setting value of the E-Gun in steps of 1 mA in real time. Even with the algorithm deployed, several serious vacuum leakage events occurred, one of which led to breakage of the observing glass window of PRF4, perhaps because it had been somewhat compromised from radiation damage. Another main event was that the vacuum bellow close to the tungsten target was broken by high power beam bombardment. We improved the vacuum bellow by adding a stainless-steel lining inside and solved this problem successfully. After solving the above problems, about six months later, in January 2018, we passed the accelerator performance experts' test successfully. Table 6 Table 6 gives the main measured parameters of the LINAC. At a repetition rate of 70 Hz, we reached > 1.5 kW of average power. 1 1 Parameter 1 1 Measured 1 1 Designed 1 1 Energy (MeV) 1 1 16.6 1 1 ≥15 1 1 Power on the tungsten target (W) 1 1 1558.37 1 1 ≥1500 1 1 Stability of the beam current 1 1 0.37%/30 min 1 1 ≤1%/30 min 1 1 Pulse width (μs) 1 1 2.83 1 1 0.5–3.0 The transmission efficiency is another main parameter with which we are concerned. After a careful beam commissioning and long-time operating test, the transmission efficiency of the HPTB reached ~90%, as shown in Fig. 4 Fig. 4 (and calculated by Area(3) × 2/Area(2) = 88.8%); this is consistent with the design value. If the input RF power is constant, because of the beam loading effect, changing the injected beam current would affect the energy at the exit of the LINAC. A study of the characteristics of the relationship between the energy and the injected beam current was conducted and the results indicate that the measurements agree well with the analytical results, as shown in Fig. 5 Fig. 5 . The power remaining through the output coupler of the accelerating tube can be calibrated by the LLRF too [ 22 22 ] . As the beam current increases, the RF power remaining decreases from 3.8 to 1.8 MW. The relation is shown in Fig. 6 Fig. 6 , and the measured values are fairly well reproduced by the calculated values. Comparing Fig. 5 Fig. 5 with Fig. 6 Fig. 6 , we can see the obvious beam loading effect on a high average beam power LINAC. 3 Conclusion 1 An electron LINAC with an energy of 15 MeV and an average power of 1.5 kW was designed and constructed successfully for the first photoneutron source (PNS phase-I) in China. It consists of an E-Gun, a pre-buncher, a buncher, an accelerating structure, and an HPTB. 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Tech . 29 , 128 ( 2018 ). doi: 10.1007/s41365-018-0460-7 http://doi.org/10.1007/s41365-018-0460-7 Beam-based optimization of SwissFEL low-level RF system We would like to express our sincere thanks to SINAP members of the Department of Reactor Physics. We are also very grateful to the SINAP members of the Vacuum Group, Power Supply Group, Beam Instrumentation Group, Control Group, and Pulse Group for technical assistance. 10.1007/s41365-019-0576-4 This work was supported by the Youth Innovation Promotion Association CAS (No. 2018300). 2018-08-30 2018-10-25 2018-10-31 2019-03-07 2019-04-01 2021-04-10 © China Science Publishing & Media Ltd. (Science Press), Shanghai Institute of Applied Physics, the Chinese Academy of Sciences, ChineseNuclear Society and Springer Nature Singapore Pte Ltd. 2019 This is a post-peer-review, pre-copyedit version of an article published in Nuclear Science and Techniques. The final authenticated version is available online at: http://dx.doi.org/10.1007/s41365-019-0576-4 http://dx.doi.org/10.1007/s41365-019-0576-4 . 2019 Nuclear Science and Techniques 04 30