1
Progress on performance tests of ITER-gyrotrons and design of dual-frequency gyrotron for ITER staged operation plan R. Ikeda, K. Kajiwara, T. Nakai, S. Yajima, T. Kobayashi, M. Terakado, K. Takahashi, S. Moriyama, K. Sakamoto, C. Darbos* and M. Henderson* National Institute for Quantum and Radiological Science and Technology, *ITER Organization E-mail : [email protected] Summary : Fabrication of 8 gyrotrons and the performance tests for first 4-gyrotrons were completed. It is ready to be delivered to ITER for the First Plasma. Design of 104 GHz/170 GHz dual-frequency gyrotron for ITER is successfully completed and the proto-type dual-frequency gyrotron is fabricating. For generation of H-mode plasma at very low field of 1.8 T in Pre-Fusion Power Operation 1 in ITER. 170 GHz 104 GHz 50 mm Dia. LP 01 mode : 96.0 % LP 01 mode : 95.8 % 50 mm Dia. 1. Internal wall surface structure of internal mode converter 2. Curvature and position of internal four mirrors Mode converter Mirrors 170 GHz 104 GHz 170 GHz 104 GHz (ITER gyrotron design) Optimization of RF-beam size (Dual-frequency gyrotron design) (ITER gyrotron design) 170 GHz 104 GHz Reduction of side-lobes of RF-beam 170 GHz 104 GHz (Dual-frequency gyrotron design) At outlet of mode converter At output window At 1.8 T operation: 170 GHz RF beam is necessary for plasma start-up, ECH and ECCD. At nominal operation : (2.65 T / 5.3 T) 104 GHz beam is necessary for plasma start-up by 2 nd harmonics X-mode. 170 GHz and104 GHz beams are available for ECH and ECCD. Demonstration of multi-frequency oscillations (104 / 137 / 170 / 203 GHz) were performed using a prototype ITER gyrotron (same design as ITER gyrotron). [IAEA FEC2016] 170 GHz : 1 MW 300 s (CW) 104 GHz : 1 MW up to 2 s (Non-CW) Issues for CW operation at 104 GHz Large power loss in the gyrotron Large beam size at the window Design of ITER gyrotron At aperture of mode convertor At output window Gaussian Discrepancy angle Gaussian Discrepancy angle 170 GHz 94.5% 0.60 degree 95.8% 0.23 degree 104 GHz 90.7% 96.6% Design of DF-gyrotron At aperture of mode convertor At diamond window Gaussian Discrepancy angle Gaussian Discrepancy angle 170 GHz 95.4% 0.18 degree 96.4% 0.08 degree 104 GHz 97.5% 98.0% Mode Content LP 01 (HE 11 ) 95.5% LP 02 1.0% LP 11(odd) 0.1% LP 11(even) 0.3% (Design : 96.1 %) 75.5kV 76.0kV Optimized by decreasing magnetic field Optimized by increasing beam voltage ~20s 0 0.5 1 199 Time [s] 0 20 40 60 22μs 100μs Oscillation signal Beam current 46.0 A -40 -20 0 20 Body Anode Cathode 29.0 kV -3.3 kV -47.4 kV 200μs 0.82 MW Summary of performance tests for four ITER gyrotrons Beam coupling test to waveguide MOU Gyrotron Window RF beam (Parabolic) (Phase correction) Waveguide IR camera Target RF beam Waveguide (50mm) #1 #2 #3 #4 #5 #6 #7 #8 Completion of performance tests for 4 gyrotrons Optimization for CW operation of 1 MW power Enhancement of operation reliability 5 kHz full-power modulation Operation reliability with duty cycle ¼ (Requirement : ≥ 90 %) ITER requests quick restart of the system within a couple seconds after the operation, especially if the operation is accidentally stopped. Operation optimization for 1 MW power and 50 % efficiency was demonstrated by increasing the beam voltage from 75.5 to 76kV in the start-up phase without applying slow response magnetic-field control. Achievement of ≥ 95 % (19 of 20 shots) Progress on performance tests of ITER-gyrotrons Design study of dual-frequency gyrotron of 170 GHz and 104 GHz for ITER Introduction : Performance tests should be conducted using the actual components (gyrotrons, matching optics units and superconducting magnets) based on ITER test-requirement before delivery to ITER. The electron beam can be controlled by anode- cathode voltage due to the advantage of triode MIG. By sending a modulation operation command or a pause command to semiconductor switches, it is possible to feed power to the anode electrode or to shorten to the cathode electrode. The side lobes of 104-GHz operation at the outlet of the mode convertor were successfully eliminated without affecting the beam pattern at 170-GHz operation. Moreover, the beam pattern for 104 GHz operation at the output window became smaller with minimal changes to the beam pattern at 170 GHz operation. The newly designed dual-frequency gyrotron largely improves the power transmission efficiency of 104 GHz operation from 95% to 99% at the output window. Power transmission efficiency equivalent to that of the ITER gyrotron was achieved. 95% 99% 95% 93% Gyrotron MOU 94% When a mode jump occurred, power supplies shut down because the oscillation of the unwanted mode was continued. But, by introducing a pause function, a reliability of 95% in 20 shots of 300 s operation with a duty cycle of ¼ was achieved easily. 0.8 MW power for 200 s was achieved under the same magnetic field and beam current as in CW operation. Operation reliability of power modulation was 100%. By stopping the electron beam temporarily and reapplying a voltage between the cathode and anode electrodes by opening the switches, the unwanted mode disappeared and the main mode of 170 GHz regenerated. Operation fault Achievement of ≥ 95 % The internal components have to be improved for CW dual frequency operation. Features : Magnetron injection gun of triode type Cavity oscillation mode of TE 31,11 mode Two mirrors Improved Equivalent IAEA FEC2020 [P3-1406] No. Frequency (170±0.3 GHz) MOU outlet power (≥ 0.96 MW) Cathode voltage / Beam current Total efficiency Full-power modulation (≥ 0.8 MW, ≥ 60 s) HE 11 mode at waveguide -in (≥ 95%) #1 169.85 GHz 1.01 MW 45.6 kV / 45.3 A 50.3 % 1 kHz/0.89 MW/200 s, 3 kHz/0.87 MW/200 s, 5 kHz/0.90 MW/200 s 96.9 % (63.5 mm WG) #2 169.85 GHz 1.02 MW 43.6 kV / 47.8 A 50.4 % 1 kHz/0.91 MW/60 s, 3 kHz/0.96 MW/60 s, 5 kHz/0.90 MW/60 s 96.5 % (63.5 mm WG) #3 169.91 GHz 1.00 MW 43.8 kV / 47.8 A 50.0 % 1 kHz/0.90 MW/60 s, 3 kHz/0.89 MW/60 s, 5 kHz/0.85 MW/60 s 95.6% (50.0 mm WG) #4 169.90 GHz 1.00 MW 43.9 kV / 46.6 A 51.1 % 1 kHz/0.81 MW/200 s, 3 kHz/0.80 MW/200 s, 5 kHz/0.82 MW/200 s 95.4% (50.0 mm WG) Operation recovery 170GHz regenerated 0 1 2 -40 -20 0 20 40 32.0 kV -0.4 kV -44.0 kV Body voltage Anode voltage Cathode voltage 0 20 40 60 226 228 230 232 234 46.3 A Beam current Time [s] 170GHz : Main mode 167GHz 170GHz Pause:1s [Recovery from mode jump by a pause function] 167GHz :Unwanted mode Shot No.16

IAEA FEC2020 [P3-1406] Progress on performance tests of

  • Upload
    others

  • View
    10

  • Download
    0

Embed Size (px)

Citation preview

Page 1: IAEA FEC2020 [P3-1406] Progress on performance tests of

Progress on performance tests of ITER-gyrotrons and design of dual-frequency gyrotron for ITER staged operation plan

R. Ikeda, K. Kajiwara, T. Nakai, S. Yajima, T. Kobayashi, M. Terakado, K. Takahashi, S. Moriyama, K. Sakamoto, C. Darbos* and M. Henderson*

National Institute for Quantum and Radiological Science and Technology, *ITER OrganizationE-mail : [email protected]

Summary : Fabrication of 8 gyrotrons and the performance tests for first 4-gyrotrons were

completed. It is ready to be delivered to ITER for the First Plasma. Design of 104 GHz/170 GHz dual-frequency gyrotron for ITER is successfully

completed and the proto-type dual-frequency gyrotron is fabricating.

For generation of H-mode plasma at very low field of 1.8 T in Pre-Fusion Power Operation 1 in ITER.

170 GHz

104 GHz

50 mm Dia.

LP01 mode : 96.0 %

LP01 mode : 95.8 %

50 mm Dia.

1. Internal wall surface structure of internal mode converter

2. Curvature and position of internal four mirrors

Mode converter

Mirrors

170 GHz104 GHz

170 GHz104 GHz(ITER gyrotron design)

Optimization of RF-beam size

(Dual-frequency gyrotron design)

(ITER gyrotron design)170 GHz104 GHz

Reduction of side-lobes of RF-beam

170 GHz104 GHz(Dual-frequency gyrotron design)

At outlet of mode converter At output window

At 1.8 T operation:

170 GHz RF beam is necessary for plasma start-up, ECH and ECCD.At nominal operation :

(2.65 T / 5.3 T)

104 GHz beam is necessary for plasma start-up by 2nd harmonics X-mode.170 GHz and104 GHz beams are available for ECH and ECCD.

Demonstration of multi-frequency oscillations (104 / 137 / 170 / 203 GHz) were performed using a prototype ITER gyrotron (same design as ITER gyrotron). [IAEA FEC2016]

170 GHz : 1 MW 300 s (CW)104 GHz : 1 MW up to 2 s (Non-CW)

Issues for CW operation at 104 GHz• Large power loss in the gyrotron • Large beam size at the window

Design of ITER gyrotron

At aperture of mode convertor At output window

Gaussian Discrepancy angle Gaussian Discrepancy angle

170 GHz 94.5%0.60 degree

95.8%0.23 degree

104 GHz 90.7% 96.6%

Design of DF-gyrotron

At aperture of mode convertor At diamond window

Gaussian Discrepancy angle Gaussian Discrepancy angle

170 GHz 95.4%0.18 degree

96.4%0.08 degree

104 GHz 97.5% 98.0%

Mode ContentLP01 (HE11) 95.5%

LP02 1.0%LP11(odd) 0.1%LP11(even) 0.3%(Design : 96.1 %)

75.5kV 76.0kV

Optimized by decreasing magnetic field Optimized by increasing beam voltage

~20s

0

0.5

1

199Time [s]

0204060

22μs100μs

Oscillation signal

Beam current

46.0 A

-40-20

020 Body

Anode

Cathode

29.0 kV

-3.3 kV

-47.4 kV

200μs 0.82 MW

Summary of performance tests for four ITER gyrotrons

Beam coupling test to waveguide

MOU

Gyrotron

Window

RF beam

(Parabolic)

(Phase correction)

Waveguide

IR camera

Target

RF beam

Waveguide(50mm)

#1 #2 #3 #4 #5 #6 #7 #8

Completion of performance tests for 4 gyrotrons

Optimization for CW operation of 1 MW power Enhancement of operation reliability 5 kHz full-power modulation

Operation reliability with duty cycle ¼ (Requirement : ≥ 90 %)

ITER requests quick restart of the system within a couple seconds after the operation, especially if the operation is accidentally stopped. Operation optimization for 1 MW power and 50 % efficiency was demonstrated by increasing the beam voltage from 75.5 to 76kV in the start-up phase without applying slow response magnetic-field control.

Achievement of ≥ 95 %(19 of 20 shots)

Progress on performance tests of ITER-gyrotrons

Design study of dual-frequency gyrotron of 170 GHz and 104 GHz for ITER

Introduction : Performance tests shouldbe conducted using the actual components(gyrotrons, matching optics units andsuperconducting magnets) based on ITERtest-requirement before delivery to ITER.

The electron beam can be controlled by anode-cathode voltage due to the advantage of triodeMIG. By sending a modulation operationcommand or a pause command to semiconductorswitches, it is possible to feed power to the anodeelectrode or to shorten to the cathode electrode.

The side lobes of 104-GHz operation at the outlet of the mode convertor were successfully eliminated withoutaffecting the beam pattern at 170-GHz operation. Moreover, the beam pattern for 104 GHz operation at the outputwindow became smaller with minimal changes to the beam pattern at 170 GHz operation.

The newly designed dual-frequency gyrotron largely improves the power transmissionefficiency of 104 GHz operation from 95% to 99% at the output window.Power transmission efficiency equivalent to that of the ITER gyrotron was achieved.

95%

99%

95%

93%

Gyrotron MOU

94%

When a mode jump occurred, power supplies shut down because the oscillation ofthe unwanted mode was continued. But, by introducing a pause function, a reliabilityof 95% in 20 shots of 300 s operation with a duty cycle of ¼ was achieved easily.

0.8 MW power for 200 s was achievedunder the same magnetic field and beamcurrent as in CW operation. Operationreliability of power modulation was 100%.

By stopping the electron beam temporarily andreapplying a voltage between the cathode andanode electrodes by opening the switches, theunwanted mode disappeared and the mainmode of 170 GHz regenerated.

Operation fault

Achievement of ≥ 95 %

The internal components have to be improved for CW dual frequency operation.

Features : Magnetron injection gun of triode typeCavity oscillation mode of TE31,11 mode

Two mirrors

Improved

Equivalent

IAEA FEC2020 [P3-1406]

No.Frequency

(170±0.3 GHz)

MOU outlet power

(≥ 0.96 MW)

Cathode voltage / Beam current Total efficiency

Full-power modulation(≥ 0.8 MW, ≥ 60 s)

HE11 mode at waveguide -in

(≥ 95%)

#1 169.85 GHz 1.01 MW45.6 kV / 45.3 A

50.3 %

1 kHz/0.89 MW/200 s, 3 kHz/0.87 MW/200 s,5 kHz/0.90 MW/200 s

96.9 % (63.5 mm WG)

#2 169.85 GHz 1.02 MW43.6 kV / 47.8 A

50.4 %

1 kHz/0.91 MW/60 s,3 kHz/0.96 MW/60 s,5 kHz/0.90 MW/60 s

96.5 % (63.5 mm WG)

#3 169.91 GHz 1.00 MW43.8 kV / 47.8 A

50.0 %

1 kHz/0.90 MW/60 s,3 kHz/0.89 MW/60 s,5 kHz/0.85 MW/60 s

95.6%(50.0 mm WG)

#4 169.90 GHz 1.00 MW43.9 kV / 46.6 A

51.1 %

1 kHz/0.81 MW/200 s,3 kHz/0.80 MW/200 s,5 kHz/0.82 MW/200 s

95.4%(50.0 mm WG)

Operation recovery

170GHz regenerated0

1

2

-40-20

02040

32.0 kV

-0.4 kV-44.0 kV

Body voltage

Anode voltageCathode voltage

0

20

40

60

226 228 230 232 234

46.3 ABeam current

Time [s]

170GHz : Main mode167GHz170GHz

Pause:1s

[Recovery from mode jump by a pause function]

167GHz :Unwanted mode

Shot No.16