1 / 17

THERMAL CYCLE TESTS OF RF WINDOWS IN STF INPUT COUPLERS

THERMAL CYCLE TESTS OF RF WINDOWS IN STF INPUT COUPLERS. 2010/12/07 Masato Satoh (KEK). CONTENTS. STF-1 ( Cryomodule tests with 4 cavities ) Input coupler ( structure and specifications ) Vacuum leak at low temperature S1-Global Detail of vacuum leak(sniffer & color check)

vonda
Télécharger la présentation

THERMAL CYCLE TESTS OF RF WINDOWS IN STF INPUT COUPLERS

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. THERMAL CYCLE TESTS OF RF WINDOWS IN STF INPUT COUPLERS 2010/12/07 Masato Satoh (KEK)

  2. CONTENTS • STF-1(Cryomodule tests with 4 cavities) • Input coupler(structure and specifications) • Vacuum leak at low temperature • S1-Global • Detail of vacuum leak(sniffer & color check) • Thermal cycle tests with sample windows • Summary

  3. STF-0.5, STF-1(2007~2008) Cryomodule tests STF-0.5(2007) : 1 cavity STF-1(2008) : 4 cavities S1-G(now on):8 cavities

  4. STF-1: CM test for 4 cavities Input Coupler located from 300K to 2K supplies RF power into SC-cavities. Cross-section of CM Input Coupler Warm Side 2.0K Nb-cavity Warm window(300K) Cold Side Cold window(80K)

  5. Input coupler Warm window Warm window Cold window 5E-7 Pa(IP) 1E-6 Pa Choke: To protect brazing part from strong electric field, and to match impedance at RF window Cold Window Cold window Coaxial ceramic disk Input power in ILC Eacc = 31.5MV/m Beam current = 9mA Pin = 300 kW Cu Brazing Between ceramics and Cu

  6. The cooling tests • STF-0.5 : cryomodule tests for 1cavity • Cooling: 2007/10/3 ~ 2007/11/22 • STF-1: cryomodule tests for 4 cavities • 1st cooling: 2008/5/21 ~ 2008/7/25 • 2K Low power test • 2nd cooling: 2008/9/9 ~ 2008/12/19 • 2K High power test No.2 coupler ・・・ 3 thermal cycles No.1, No.3, No.4 couplers ・・・ 2 ones

  7. Vacuum leak at cold windows Warm Window Cold Window 4 warm window at 300Koccurred vacuum leak Cold window : RT~80K 3 couplers  vacuum leak 1 coupler  no leak 2×1 0-4 Pa m3 /s Vacuum leak was caused by thermal cycles.  One potential reason might be bonded between different materials. Pin :130~270kW(20~30MV/m)

  8. Confirmation of vacuum leak(1st : vacuum leak check) 2 cold couplers were installed in vacuum chamber Leak detector Vacuum pump

  9. Sniffer test(sniff:嗅) Cut down choke part Sniffer probe No vacuum leak on outer brazing Sensitivity:5E-8 Pam^3/s φ6 0 deg Result of sniffer check Vacuum leak on inner brazing for all the 3 couplers 2.0E-04 Scan pitch:3mm

  10. Results of color check (No.1,No.3) There were color reactions and cracks! No.1 Coupler No.3 Coupler 239° 65° C1 C2 R12

  11. Linear Thermal Expansion Coefficient of Cu, Ceramics, Mo Actual shrinking amount : - Δ length=length×∫LTEC dT Thermal cycles  NG Cool down  OK 16.6×10-3 2.7×10-3 7.46×10-3 0.65×10-3 5.39×10-3 0.89×10-3 Some measures against the thermal strain Cu pipe can absorb the thermal strain ! The original was designed by Noguchi san and Toshiba.

  12. Mo-Ring(Toshiba) To reduce the strain of different material bonding It was developed for Tristan input couplers in 1988 300K 1200K 300K 1200K  300K Al2O3 Al2O3 Al2O3 Mo Cu Mo-ring is brazed with ceramic disk at the same time Cu Cu

  13. Need to improve inner brazingSample windows#1,#2 2009/Sep.~ Oct. (S1-G already running) The design was changed by Noguchi & Kako Sample windows Mo-ring #2 #1 (ratio =0.8) (t1.0) Cu-Pipe Stress∝(厚度)3 Ratio3 =0.83 ~0.5 :to make stress half

  14. 300K  77Kcooling process Thickly cover Samples by Al foil(16P) Indivisually put 3 TC on Samples 4 1 5 2 6 3 8 #2 #1 #2 #1 Leak Check after Cooling Temperature Change

  15. Results of thermal cycles Type-#1 was adopted in S1-Global Sample #1, #2 (2009 Sep ~Oct) #1: Mo,0.25t #2: Mo,0.20t Sample #3, #4 (2010 Apr ~Jun) #3 and #4 same as #1 have been exposed in 22 thermal cycles  No vacuum leak

  16. The improved ones are installed in S1-Global, and they have no trouble by now.

  17. Summary • STF-0.5&1 cryomodule tests were carried out, -Vacuum leak happened on 3 cold windows which had Cu Pipe= 1.0t, Mo = 0.25t • Samples #1,#2 were made, and applied 6 thermal cycles - #1Cu Pipe= 0.8t , Mo =0.25t hadNo vacuum leak Type-#1 was adopted for S1-G cryomodule test #2 Cu Pipe = 0.8t , Mo =0.20t happened Vacuum leak • Sample #3, #4 same as #1 No vacuum leak against 22thermal cycle tests

More Related