CRAB cavities Cryomodule review Tuner

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Presentation transcript:

CRAB cavities Cryomodule review Tuner ( (CERN) Kurt Artoos, Rama Calaga, Ofelia Capatina, Teddy Capelli, Federico Carra, L. Dassa, Norbert Kuder, Raphael Leuxe, P. Minginette Colleagues USLARP , STFC

Contents Tuning principle DQW and RFD Tuning forces, stress and range DQW pre tuning Tuning frame Status SM18 tuner Studies SPS tuner

Centre of the actuation is floating Symmetric actuation on cavity through tuner frame and concentric tubes. Motorization outside cryostat Centre of the actuation is floating DQW : 186 kHz/mm * S. Vérdu Andrés , B. Xiao RFD : 345 kHz/mm * H. Park * Measured as tuner stroke or Δdistance between 2 plates

DQW Cavity (RT , no PCB) with He vessel + pretuning device Input force 2.5 kN Displacement z 0.53/0.6 mm Maximum eq. Stress 225 MPa Corresponds to about 0.21 MHz (0.42 MHz pp) * For 400 MPa/1.2= 333 MPa -> 0.31 MHz (0.62 MHz) range (linear), 3.7 kN, ±1.6 mm Force/tuner stroke 2.2 kN/mm 199 MPa/mm At RT for 50 MPa , 0.25 mm maximum tuner stroke for 0.5 kN

RFD Cavity (RT , no PCB) with He vessel Input force 2 kN Displacement z 0.4/0.41 mm Maximum eq. Stress 95 MPa Corresponds to about 0.280 MHz (0.560 MHz pp) For 400 MPa/1.2= 333 MPa -> 0.980 MHz (1.96 MHz) range (linear), 7 kN, ± 2.8 mm Force/tuner stroke 2.5 kN/mm 115 MPa/mm At RT for 50 MPa , 0.42 mm max tuner stroke for 1 kN

Pre tuning DQW At warm Bellows are outside of the helium vessel 3 M6 screws (pull) and studs (push) Pitch 1 mm Bellows (Ti) will be probably edge welded Sensitivity 0.8023 MHz/mm (distance between plates) (Binping Xiao)

Deformation Top : 0.21 mm screw motion -> 0.11 mm plate deformation Bottom: 0.23 mm screw -> 0.16 mm centre plate def. Force: about 3 kN /screw M6x1 σi screw = 178 MPa (0.3 friction) Flexibility gives the resolution 0.8023 MHz/ mm

Pretuning stress Pre-tuning 0.2 mm (distance plates) + pressure > 50 MPa Ref. L. Dassa For the helium vessel as pressure vessel this would be a limit (needs some thinking) 0.16 MHz (0.32 MHz) for 0.8 MHz/mm > 75 MPa

Design tuning frame Modal analysis of the support structure indicated presence of low vibration modes of the titanium tuning frame A first improvement was made to divide the mass by 2 Calculations T. Jones 7 kN load Some optimisation still to be done Flexibility of the frame could be used to increase the tuning resolution Buckling analysis Multiplier 4.2 Calculations N. Kuder

Flexural guide 1 mm thick Titanium Gr. 5 Plate (or CuBe) Calculations T. Jones 3 mm displacement Axial stiffness 22 N/mm Lateral stiffness 17 106 N/m Torsional stiffness 0.1 mrad/Nm See talk T. Jones for results modal behaviour

Tolerances tuner axis = 1.49° 545 mm→14 mm 212 mm→ 5.5 mm Adjustments to be foreseen Introduce hinges (flexural)

Status SM18 p.o.p. tuner Design: P. Minginette Motor 1.3 Nm Bipolar Nema 23 (1.8 deg/step) HD HFUS-20-100-2SO Ratio i : 0.01 , repeat. peak Torque 82 Nm, average torque 49 Nm Accuracy < 1 arcmin, precision <0.1 arcmin Fa Dyn 7.7 kN, η=~0.80 (grease, 20 °C) Roller screw Rollvis RV 12 x 1 η=0.79 , static load capacity 17 kN M= p i F/2000 π η = 0.01 Nm F= 4 kN, p= 1 Detend torque 0.017 Nm, self locking

Instrumentation Design: P. Minginette Precision linear motor: 1 step= 1.8° x 0.01 → 0.1 μm (p=1 mm) Precision HD 0.1 arcmin or 0.0017° → 10 nm Altered by friction in guides DQW ~ 20-2 Hz RFD ~ 35-3.5 Hz Instrumentation: Potentiometer Megatron RC13-25 M 25 mm range , 1 kΩ, resolution ~10 μm Load cell Kistler 4576A55C1 class 0.1 DQW (2.2 kN/mm) →1.5 μm precision RFD (2.5 kN/mm) → 1.3 μm precision limit switches Mechanical stops

Pressure compensation 1 atm = 101.325 kPa , Force = 844 N (on 2 tuning tubes) Day variations 3 mbar 2.5 N Week variations 10 mbar 8.3 N 10 mbar variation R = 51.5 mm Surface 0.0083 m2 1 atm = 0.19 mm on each plate Load compensating springs : 3 x 5 N/mm

Status p.o.p. tuner test Linear motor protoype tested without load Fully assembled and tested with 400 microsteps (with LVDT) 1 mm cycle (40000 steps) 60 µm 4 µm LVDT not adapted Sensor noise Friction in sensor Drift (thermal ?) Estimate: Precision ~0.5 µm ~ 100 Hz DQW, 175 Hz RFD Steps 10 microsteps Measurement E. Gallay

Next steps p.o.p. tuner test Test on p.o.p. DQW in SM18 at 2 K Measure directly frequency resolution + precision Test pressure compensation Status: several parts available, in preparation Action : Build a test bench for prototype motor testing + fatigue cycles + qualification radiation resistance Integrate a spring to represent the load from cavity Integrate an optical linear encoder without frictional guides and nm resolution Test in temperature stable room

Drawbacks first design: Size … Mass ~ 10 kg Motorisation can not be replaced without opening cryostat (maintainability)

Status design for SPS test (v1) Size ok Smaller mass Can be dismounted from cryostat Design: P. Minginette

Status design for SPS test (v2) Only concept so far Compact 10 to 20 times better resolution Centre of actuation is materialised Dismountable Design: P. Minginette

Conclusions Calculations for DQW and RFD show the tuning ranges available that are smaller than the error on p.o.p. A first prototype of the tuner motorisation has been built, tests with p.o.p. DQW in preparation Options for the SPS tuner are under study, taking care of integration, resolution, pressure and load compensation and instrumentation To be included in study: radiation, thermal optimisation Test program to be prepared

Thank you The HiLumi LHC Design Study is included in the High Luminosity LHC project and is partly funded by the European Commission within the Framework Programme 7 Capacities Specific Programme, Grant Agreement 284404