radio frequency cavity air cooling

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Radio Frequency Cavity Air Cooling A.Romanazzi 1 CFD team supports CERN development 19 May 2011

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Radio Frequency Cavity Air Cooling . General problem. New Radio Frequency cavity developed in BE dep. 2 coils dissipating 650W each by joule effect. Define cooling air mass flow to keep the coils colder than 80˚C. Improve cavity shape to reduce hotspots. Development time: about 1 month. - PowerPoint PPT Presentation

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Page 1: Radio Frequency Cavity Air Cooling

Radio Frequency Cavity Air Cooling

A.Romanazzi 1CFD team supports CERN development 19 May 2011

Page 2: Radio Frequency Cavity Air Cooling

• New Radio Frequency cavity developed in BE dep.

• 2 coils dissipating 650W each by joule effect.

• Define cooling air mass flow to keep the coils colder than 80˚C.

• Improve cavity shape to reduce hotspots.

• Development time: about 1 month

General problem

A.Romanazzi 2CFD team supports CERN development 19 May 2011

Page 3: Radio Frequency Cavity Air Cooling

Estimate mass flow in Nominal Conditions

• Thermal conductivity of the rings: 7 W/(m °C)

• Power dissipation per ring : 650 W continuous ≈1/r2

• Range of tested air mass flows: 0.1 - 0.5 kg/s

90 mm

25 mm

20 mm

A.Romanazzi 3CFD team supports CERN development 19 May 2011

Page 4: Radio Frequency Cavity Air Cooling

Mesh and numerical models• Air: compressible ideal gas model• K-Ԑ Two Layers Turbulence model• Buoyant flow• Thermal conduction over the supports and the box are neglected

CFD team supports CERN development 19 May 2011

4A.Romanazzi

Gas domain• Core Polyhedral Mesh• 10 layers cells

“boundary layer”• Extrusion on outlet sideSolid domain• Core Polyhedral Mesh

Page 5: Radio Frequency Cavity Air Cooling

0.1 0.2 0.3 0.4 0.540

50

60

70

80

90

100

110

120

130

140

Rings Temperature

T max solid [C]

T aver solid [C]Air mass flow [Kg/s]

Tem

pera

ture

[C]

Nominal ConditionsRings temperature VS air mass flow

Rings’ temperature for 0.3 kg/s case.

A.Romanazzi 5CFD team supports CERN development 19 May 2011

Page 6: Radio Frequency Cavity Air Cooling

Flow at Nominal Conditions

0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.50

500

1000

1500

2000

2500

3000

3500

Pressure Drop [Pa]

ΔP [bar]

Polynomial (ΔP [bar])

Air mass flow [kg/s]

Velocity magnitude maps on middle section0.3 kg/s case

A.Romanazzi 6CFD team supports CERN development 19 May 2011

Page 7: Radio Frequency Cavity Air Cooling

Studied Modified Geometries

V.3 V.4 V.5 V.6 V.7

Compromise between reducing pressure drop and making the most uniform the Heat transfer coefficient on the coils’ surfaces.

A.Romanazzi 7CFD team supports CERN development 19 May 2011

Page 8: Radio Frequency Cavity Air Cooling

Case: 0.3kg/sV.3 V.4 V.5 V.6 V.7

A.Romanazzi 8CFD team supports CERN development 19 May 2011

Page 9: Radio Frequency Cavity Air Cooling

0.1 0.2 0.3 0.4 0.545

55

65

75

85

95

105

115

Rings Max Temperature

v1 averv3 averv4 averv5 averPower (v5 aver)v6 averPower (v6 aver)v7 averPower (v7 aver)

Air mass flow [kg/s]

Tem

pera

ture

[C]

0.1 0.2 0.3 0.4 0.50

1000

2000

3000

4000

5000

6000

Pressure drop

v1v3v4v5Power (v5)v6Power (v6)v7Power (v7)

Air mass flow [kg/s]

Pres

sure

[Pa

]

Temperature VS Pressure Drop

A.Romanazzi 9CFD team supports CERN development 19 May 2011

Page 10: Radio Frequency Cavity Air Cooling

Final Cavity Layout

• From treated cases we learn that:– Coils’ supports interfere

with air flow/heat transfer

– No grills: lower pressure drop

– Cavity corners have to be “closed”

Version 9

A.Romanazzi 10CFD team supports CERN development 19 May 2011

Page 11: Radio Frequency Cavity Air Cooling

HTC: lower absolute value but more uniform(depends only on air flow pattern – independent from solid properties)

V.3 V.4 V.9V.7

A.Romanazzi 11CFD team supports CERN development 19 May 2011

Page 12: Radio Frequency Cavity Air Cooling

Case: 0.3kg/sV.3 V.4 V.9V.7

A.Romanazzi 12CFD team supports CERN development 19 May 2011

Page 13: Radio Frequency Cavity Air Cooling

0.1 0.2 0.3 0.4 0.560

70

80

90

100

110

120

130

140

Rings Max Temperature

v1 maxv3 maxv4 maxv7 maxv9 max

Air mass flow [kg/s]

Tem

pera

ture

[C]

0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.50

1000

2000

3000

4000

5000

6000

Pressure Drop

Air mass flow [kg/s]

Pres

sure

[Pa

]

A.Romanazzi 13CFD team supports CERN development 19 May 2011

Page 14: Radio Frequency Cavity Air Cooling

ConclusionsOur first target was to estimate a mass flow able to

guarantee T<80˚C: obtained with a mass flow of 0.3kg/s

Secondly target was to uniform the HTC over the coils’ surface to prevent from hot-spots and lower the pressure drop across the system: between the studied geometries “version 9” is the best compromise between those conditions.

Experimental test of the cavity are going to be performed in the next future to validate the cavity and the simulations.

A.Romanazzi 14CFD team supports CERN development 19 May 2011

Page 15: Radio Frequency Cavity Air Cooling

Thank you for your attention!

CFD team supports CERN development 19 May 2011

15A.Romanazzi