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BLIP capsule update Beryllium, Graphite, Titanium K. Ammigan 03.18.16
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Beryllium capsule Atmosphere: Argon Grades: PF-60, UHP, S-65F Specimen types Tensile: 12 layers of 0.5 mm thick each Bend: 6 layers of 1 mm thick each Compression: fillers in tensile specimen holes Microstructural analysis: fillers between tensile specimens HiRadMat use 1 bend specimen from each layer (will need to be wider ~ 10 mm bend specimen) or add extra 1 mm layer of just HRMT specimens (need to verify effect on peak temperature) Specimens arranged within each layer to achieve all 3 grades at all temperature regimes Total energy loss: ~ 10.41 MeV (including SS windows)
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Preliminary thermal analysis - Beryllium 20 layers including SS windows
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Beryllium capsule temperature distribution Peak temperature of specimens ~ 425 °C Peak temperature on SS window ~ 60 °C Radial gap conductance between specimens neglected More detailed analysis needed Peak temperature likely to be higher
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Beryllium capsule arrangement sketch PIE at PNNL & Oxford Specimen capsule ID of 2.375” Peak proton intensity area (D ~ 32 mm) PNNL tensile specimen (32 x 8 x 0.5 mm) Bend specimen (40 x 3 x 1 mm) Tensile specimen fillers for microstructural analysis Compression specimens in tensile holes Only 4 tensile and 2 bend specimens layers shown
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Graphite capsule Atmosphere: Vacuum Grades: ZXF-5Q, IG-430, Glassy Carbon, 3D C/C Specimen types Tensile: 2 layers of 1 mm thick each (ZXF-5Q & IG-430) Bend: 3 layers of 1 mm thick each (ZXF-5Q, IG-430, Glassy Carbon) CTE: filler between tensile specimens (3D C/C – 2 mm thick) enough fibers through thickness? HiRadMat: use 1 bend specimens from each layer (ZXF-5Q, IG-430, Glassy Carbon) Wider bend specimen ~ 10 mm Total energy loss: ~ 5.27 MeV (including SS windows)
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Preliminary thermal analysis - Graphite 7 layers including SS windows
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Graphite capsule temperature distribution Peak temperature of specimens ~ 650 °C Peak temperature on SS window ~ 50 °C Radial gap conductance between specimens neglected More detailed analysis needed Peak temperature likely to be higher
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Specimen capsule ID of 2.375” Peak proton intensity area (D ~ 32 mm) 3D C/C CTE specimen (30 x 4 x 2 mm) Tensile specimen (42 x 6 x 1 mm) Bend specimens (42 x 3 x 1 mm) Graphite capsule arrangement sketch PIE at BNL Space for filler material 2 tensile and 3 bend specimen layers (5 mm total)
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Titanium alloy capsule Atmosphere: Helium Grades FRIB: Ti 6Al-4V (4 microstructures) KEK: Ti 6Al-4V (Grade 5 and 23) Specimen types Tensile: 4 layers of 0.5 mm thick each CTE: 2 layers of 1 mm thick each (filler between tensiles) Fatigue: 3 layers of 1 mm thick each HiRadMat: use 1 filler CTE specimen between tensiles? Total energy loss: ~ 10.44 MeV (including SS windows)
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Preliminary thermal analysis – Titanium 9 layers including SS windows
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Titanium capsule temperature distribution Peak temperature of specimens ~ 330 °C Peak temperature on SS window ~ 115 °C Radial gap conductance between specimens neglected More detailed analysis needed Peak temperature likely to be higher
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Titanium capsule arrangement sketch KEK specimens PIE at BNL & PNNL 3 fatigue and 2 tensile KEK specimen layers (4 mm total) Specimen capsule ID of 2.375” Peak proton intensity area (D ~ 32 mm) Fatigue specimen (42 x 6 x 1 mm) Space for filler material Tensile specimen (32 x 8 x 0.5 mm) Filler between tensiles can be CTE/HRMT specimens
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