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Sag of ZTF components Callahan 9/4/2014

Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

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Page 1: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Sag of ZTF components

Callahan9/4/2014

Page 2: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Corrector Trim Plate analysis

Page 3: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Analytic solution using plate model from Roark and Young predicts 1g deflections of 468 microns.

See MathCad model: sag of corrector.

Page 4: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

FEA assumptions

• Float glass• Thickness 3/8” [9.525mm]• 1 g vertical (Z-axis) loads

Page 5: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

FEA validation. See: sag of correctorFine mesh model: 458 microns

Page 6: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Loads

Page 7: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Mesh density: Fine

Page 8: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Window sag assumptions

• Fused Silica• Outer radius 4406mm• Inner radius flat• Max thickness in center 28mm

Page 9: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Fracture mechanics models determine the factor of safety for any given stress and probability if success.

• See MathCad model: Design Strength- Fused silica by Callahan

• At 99% survival probability the maximum yield strength is 36 MPa. The Factor of Safety, FOS, can now be calculated for any given applied stress.

• The current stress in the ZTF window at 1 atm (14.7psi) is 10.5 MPa with a FOS=3.4

• At an over-pressure of 1.25 x 14.7psi the FOS decreases to 2.7.

Page 10: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Z-deflection max 209 microns

Page 11: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Mesh density

Page 12: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Loads

Page 13: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

What is the contribution of gravity loading (opposite direction to the pressure load)

Very small ~1.2 microns

Page 14: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Calculate the sag of the focal plane under 1g

• Assume CCD’s weigh 174 gm each x 27• Force 27.3 N• 1g Z-axis

Page 15: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Analyze final window design

• Fused Silica• Supported on Delrin “cushions”• Apply various pressures (1 atm)

Page 16: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Mesh

Page 17: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Max principal stress

Page 18: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Add line pressure at O-ring center.

• See Parker O-ring handbook to determine the line pressure. I used a typical mid-value of 2 lbs/in.

• See: https://www.parker.com/literature/ORD%205700%20Parker_O-Ring_Handbook.pdf

Page 19: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Loads

Page 20: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Add 2 lb/in line pressure at O-ring center

• Max principal stress increased to 12 psi.

Page 21: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Substitute Delrin support at the outer location.

• Stress decreases to 6.0 Mpa!!!• Use rough contact between outer delrin and

window to allow separation.

Page 22: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Max principal 6.0MPa!Lowest stress yet… very uniform.

May be artifically low due to bonded contracts at cushions.

Page 23: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Deflection under 1 atm~100 microns

Page 24: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Update model3mm thick delrin Gasket model (1/4 model)

8.9MPa Max Principal stressAt 99% probability of survival fused silica has a maximum strength of 36MPa.

Ths means we have a Factor of safety of 4.0.

Page 25: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Change gasket to steel to simulate equal support does not change the stress significantly. Max ~8.91 MPa

Stress due to ends separating from gasket are still high.

Page 26: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

To determine the effect of the separeation of the window from the gasket at the corners I fixed the vertical displacement (Z) of the corner.

Stress only reduced to 8.3 Mpa.

Page 27: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Reduce gasket to uniform 0.24” width.Use Delrin. Stress increases to 9.7MPa

Page 28: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Change gasket to steel to see how stiffening effects stress. No change

Page 29: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Increase gasket width to 13.4mm (previously 6.1mm) reduces stress to 8.7MPa

Page 30: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis
Page 31: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Sag Absolute7.3 microns

Page 32: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

Sag under 1g plus weight of CCD package (174gm)

Page 33: Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis

New cable clearance hole size