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Accelerating structure thermo-mechanical behavior Accelerating structure thermo-mechanical behavior

Accelerating structure thermo-mechanical behavior - PowerPoint Presentation

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Accelerating structure thermo-mechanical behavior - PPT Presentation

  G Riddone 25062010 CLIC meeting Contribution from R Nousiainen J Huopana T Charles Content Recall of main issues Recall of module heat dissipation Module cooling scheme Thermomechanical analysis ID: 513392

unloaded 2010 module accelerating 2010 unloaded accelerating module temperature beam heat loaded analysis dissipation mechanical structure difference thermal thermo

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Slide1

Accelerating structure thermo-mechanical behavior 

G. Riddone. 25.06.2010

CLIC meeting

Contribution from R. Nousiainen, J. Huopana, T. CharlesSlide2

Content

Recall of main issuesRecall of module heat dissipation

Module cooling schemeThermo-mechanical analysis: Accelerating structuresTwo-beam modulesRemarks

GR, BE-RF, 25/06/2010

2Slide3

Main issues

Tolerances must be preserved in static

and dynamic conditions (RF and beam dynamics constraints):

shape accuracy for machining: ± 2.5

m

m,

pre-alignment: 14 um @ 1

s

water

induced vibrations

Optimization of several parameters: temperature stabilization, pressure drop, volumetric flow, Re, heat transfer coefficient,… Compromise between opposite requirements from several technical systems

GR, BE-RF, 25/06/2010

3Slide4

Accelerating structure heat dissipation

Accelerating structure

Thermal load is

not

constant through an accelerating structure

Considered

unloaded condition and loaded

conditions

Cell-by-cell heat dissipation

EDMS 964717

Distribution of heat flux over

480 mm: superstructure

Loaded 672 W

Unloaded 821W

GR, BE-RF, 25/06/2010

4Slide5

Module heat dissipation (water cooled)

For details, see EDMS# 910399

GR, BE-RF, 25/06/2010

5Slide6

CLIC Workshop 2007

R. Nousiainen

J.

Inigo-Golfin

Total per

linac

(2007): 65 MW

Action:

reduce mass-flow rate, increase temperature difference between supply and return pipes

GR, BE-RF, 25/06/2010

6

Baseline: one access point for inlet and outlet pipesSlide7

Module cooling scheme

Twater_in

=

25

˚

C

[

± 2 ˚C] Re = 5800 (d = 7 mm)h = 3750 W/m

2

/K

V= 70 l/h [per AC. STR.]V = ~350 l/h [per MODULE]V = 3500 m/h [per LINAC]Still one inlet/outlet access point close to IP (§CES WG Dec 2008)

45 ˚C

35 ˚C

25 ˚C

45 ˚C

25 ˚C

GR, BE-RF, 25/06/2010

7Slide8

Super accelerating structure

GR, BE-RF, 25/06/2010

Max 39.7 °C

Max 38 °C

Unloaded

Loaded

[K]

T

emperature

difference

Unloaded to Loaded

Thermal analysis

8

1.9 K

0.8 K Slide9

Accelerating structure

GR, BE-RF, 25/06/2010

beam

Transverse movement induced by the thermal expansion (volumetric flow can be adjusted to limit this effect)

Max 2,5

µm

Beam pipe deformation:

unloaded to loaded structural effect

Structural analysis

Fixed

9Slide10

Two-beam module: definition

TMM model:

Static thermalStatic structuralLoading conditionsGravity

Vacuum

Nominal unloaded RF load

8 accelerating structures brazed into one 2-m long unit

GR, BE-RF, 25/06/2010

Component

Material

E [

Gpa

]

α [µ

m/m-°C]

Girder

SiC

420

5

RF structure supports

Al

EN AW 7075

72

23.6

RF structures

Cu

OFE

110

16.4

Vacuum system

Stainless steel

200

17.3

Geometry of

Baseline configuration

10Slide11

Two-beam module: unloaded case

GR, BE-RF, 25/06/2010

Surrounding air: 30˚C

Girders are at different temperature, reference T = 25 ˚C

Hottest spot in the AS – 40˚C (loads omitted)

Thermal analysis

11Slide12

GR, BE-RF, 25/06/2010

Notice lateral deformation and wave guide deformation

Gravity + Vacuum

Two-beam module: unloaded case

Gravity + Vacuum + RF (unloaded)

Structural analysis

12Slide13

Influence of T difference

2007

2010

V = 2 m/s

Tunnel pipe diameter: case of unique access point

GR, BE-RF, 25/06/2010

13Slide14

GR, BE-RF, 25/06/2010

14Slide15

Remarks

Estimation of power dissipation: temperature difference across structures compromise between several technical constraints

Thermal issues are big challenge for micrometric precision of structuresDuring RF ramp up ~15 K variation in temperature is expected

Large deformations

Unloaded to loaded ~2 K variation in temperature

Thermally caused deformations linearly proportional to temperature variation

 Minimize temperature fluctuations  mass-flow adjusted accordingly

Module thermo-mechanical analysis based on input from technical experts

Combines separate simulations results

 Shows fundamental thermo-mechanical behaviorHelps defining current improvement pointsVacuum and RF ramp up (thermal variations) causes significant deformations Thermo-mechanical effect mitigation is essentialGR, BE-RF, 25/06/201015