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Thermal%20grease%20application%20%20and%20QA

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During the mounting of SCT endcap modules onto the cooling structure, a thin ... to providing a good thermal interface the pad should be sufficiently tacky' ... – PowerPoint PPT presentation

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Title: Thermal%20grease%20application%20%20and%20QA


1
Thermal grease application and QA
2
Module FDR
  • What is the thermal interface material ?
  • Is it a grease ?
  • Is it a solid ?
  • How is it (the grease) applied ?
  • What QA is done during production ?

3
The problem
  • Role of Thermal Compound
  • During the mounting of SCT endcap modules onto
    the cooling structure, a thin film of a thermally
    conducting compound is applied to the cooling
    block with the aim of attaining the best possible
    thermal contact for the operational life of the
    SCT in ATLAS.
  • Choice of Compound
  • The final choice of compound has not yet been
    made. It may be a flexible pre-formed solid pad
    or a liquid grease dispensed in a controlled
    manner such that the quantity and disposition are
    well defined.

4
Module Mounting
  • Module Mounting
  • Following the application of the interface
    compound, the module is mounted and the
    connections are electrically tested.
  • The above is repeated until a certain number of
    modules have been attached (eg. All the lowers or
    all or a given ring-type).
  • Sub-system Testing
  • The (sub-)assembled disk is connected to a local
    evaporative cooling system and is installed in a
    suitable enclosure and tested.

5
Operating Environment
  • Thermal Effects
  • The disks are assembled at normal room
    temperature (i.e. 22 C) and whilst the normal
    silicon running temperature is 7C there will
    be occasions when the module temperature falls to
    the evaporation temperature of the fluid (i.e.
    about 25C). The total temperature change is 50
    C.
  • Humidity Effects
  • Disks are assembled in an environment where the
    relative humidity is 50. When installed in
    ATLAS the disks will be operated in a dry N2 gas.

6
Application of Thermal Compound
  • Solid pre-form.
  • The pads would probably exist in a pre-cut form
    on a large sheet. The in-plane dimensions of each
    pad could be checked optically. The thickness
    could be checked by measuring a few pads per
    sheet using a micrometer which would then be
    discarded.
  • In addition to providing a good thermal interface
    the pad should be sufficiently tacky to resist
    movement on the block (main concern is rotation)
    whilst the module is mounted.

7
  • Thermal grease
  • programme of work prior to the start of disk
    assembly would have to be undertaken to determine
    the optimal grease quantity and application
    technique.
  • The main concern is that a balance has to be
    struck between giving the block just enough
    coverage to give maximal thermal contact and
    minimizing the risk of excess bleed of the grease
    onto the surface of the module.
  • At the far-end the situation is somewhat
    different in that allowance has to be made for
    the contact to slide.

8
1mm3 dot -gt 7mm _at_ 0.025 mm Coverage 83
9
(No Transcript)
10
Module Mounting
  • Hybrid End
  • The module is fixed at the hybrid end using a
    suitable cone-shaped washer and nut.
  • The design of the washer is such that the force
    exerted on the module is a known function of its
    deflection due to the nut.
  • The nut is tightened such that the washer is
    somewhere near the mid-range of its deflection so
    that if there is relative movement during
    operation (eg. Changes in thermal compound
    thickness) there is still sufficient force on the
    module to hold it in place and to ensure a good
    thermal contact.

11
  • Far End.
  • Differential movement between the module and the
    block due to the different CTEs of the disk and
    the module.
  • Assuming that the modules CTE is about 5 ppm/C
    then for a 125 mm length the relative movement
    for a 50 C change in temperature is 31?m.
  • However, over a longer period of operation in a
    dry atmosphere, CME effects will cause the
    carbon-fibre disks to shrink by about 0.2 mm/m or
    about 24?m over the length of a module.

12
  • Requirement
  • The pressure exerted by the washer has to be low
    enough to allow the module to expand and contract
    safely whilst maintaining a good thermal contact.
  • Work needs to be done to determine the thickness
    of grease, nut torque setting, etc..

13
QA During Production
  • Module Survey
  • Measure Z of module
  • Planarity
  • Thermal QA
  • Measure temperature on hybrid thermistor
  • Thermal camera available as a development tool
    (Liverpool).

14
QA and IR Imaging
  • Aim
  • Use thermal imaging camera to develop thermal
    compound application procedures that give
    consistent good thermal contact results.
  • Apply these procedures during production
  • Implement QA to ensure that correct procedures
    are followed
  • Sample test using thermal camera ?
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