Medical Devices

Medical Devices: 6061-T6 Structural Parts for a CT System

A medical imaging equipment maker needed structural members for a CT system: not visible parts, but the parts that decide whether a moving assembly runs true. Flatness and hole position were the whole job.

Extruded aluminum sections used for the CT system structural members
At a glance
  • Industry
    Medical devices
  • Process
    Extrusion + CNC (6061-T6)
  • Alloy
    6061-T6
  • Key spec
    Hole position ±0.01 mm
The brief

What the customer needed

The customer builds CT systems and needed structural aluminum members for an assembly that moves. The parts are not cosmetic; they position other components, so their flatness and hole position propagate through the whole assembly.

The quantified constraint was hole position at ±0.01 mm across faces, with flatness agreed per part because it depends on how the member is mounted. A rail that is out of flat loads the frame unevenly, and the symptom appears as binding in an axis far from the part that caused it.

Material choice was fixed at 6061-T6: stronger and more machinable than 6063, which matters when the part carries load and has a lot of material removed.

Constraints that decided the part

  • Hole position ±0.01 mm across faces
  • Flatness agreed per part, measured after relaxation
  • Material fixed at 6061-T6
  • Dimensional report before finishing
  • No medical-device certification claimed or implied
The process route

How the part was made

The same route we would propose today, in the order it actually runs.

  1. Datum strategy agreed at DFM

    We asked which face the assembly references and machined from that face. Where two faces both matter, we quantified the cost of extra setups instead of quietly choosing one.

  2. Extrusion in 6061-T6

    Blanks extruded in 6061 and aged to T6, with enough allowance for the material that will be removed.

  3. Rough machining

    Heavy removal first, then the part is allowed to relax before finishing cuts. Measuring straight after roughing is how a part passes inspection and fails in assembly.

  4. Finish machining

    Bearing seats, mounting holes and faces cut to ±0.01 mm, with as few setups as the geometry allows.

  5. Inspection before finishing

    Flatness and hole position measured and reported on the finished lot, before any surface treatment that would change the reading.

Key parameters

The numbers the part had to hold

These are the tolerances and process values that governed the job. They come from our capability, not from a customer specification we cannot publish.

Key parameters — CT Structural Parts
ParameterValueWhy it mattered
Hole position±0.01 mmPosition of downstream components in the assembly
FlatnessAgreed per partAn out-of-flat rail loads the frame unevenly
Bore and OD±0.04 mmBearing seats and locating features
Alloy and temper6061-T6Strength and machinability for structural members
Stress reliefBetween roughing and finishingStops the part moving after inspection
InspectionReport with each lotDocumented before finishing
Where it was difficult

The part of this job that nearly went wrong

This is the section worth reading. Every program has one problem that decides whether the parts come out right, and it is usually not the one on the drawing.

The part moved after it was inspected

A structural member in 6061-T6 with a lot of material removed carries residual stress. Machined to size in one sequence, it measures correctly and then relaxes over the following hours, taking the flatness with it.

The risk

A part that passes goods-in and fails at assembly, with the defect appearing days after the measurement that cleared it.

What we changed

Roughing, stress relief, then finishing. Flatness is measured after the part has relaxed rather than immediately off the machine, and the report states the stage at which each value was taken.

Hole position across two faces

Mounting holes on different faces have to stay in position relative to each other. Every additional setup adds a datum shift, and on a long member the shift accumulates along the part.

The risk

Bearing seats that do not line up, producing binding in a moving axis and a fault that is hard to trace back to a machined part.

What we changed

The datum was chosen from the assembly reference rather than from the most convenient face, and the setup count was minimised. Where a second setup was unavoidable, the fixture repeated the first datum instead of establishing a new one.

Result

Parts that measured the same after they relaxed

The members are machined in 6061-T6 with hole position at ±0.01 mm and flatness agreed per part, measured after stress relief and reported before finishing.

The change that mattered was sequencing, not equipment. Roughing, relief and finishing cost a little more machine time and removed the class of failure where a part passes inspection and then moves.

On certification: we do not claim ISO 13485, FDA or MDR approval. We machine aluminum parts to drawing and inspect them; qualification of the finished device sits with the device manufacturer, and we would rather say that plainly than imply otherwise.

FAQ

Common questions about this program

The questions this case generates from engineers and sourcing teams.

Are you certified for medical device manufacturing?

No. We do not hold or claim ISO 13485, FDA or MDR certification. We machine and inspect aluminum parts to drawing; regulatory qualification of the assembled device belongs to the device manufacturer.

Why 6061-T6 rather than 6063?

6061-T6 is stronger and machines more cleanly, which suits structural members with a lot of removed material. 6063 remains our choice for housings where the wall thickness and anodized appearance are the constraints.

How do you hold flatness on a long part?

The flatness value is agreed per part, the datum comes from the face the assembly references, and the measurement is taken after the part has relaxed. If the value you need is tighter than the geometry supports, we say so before the order rather than after.

Have a Structural Part Where Sequencing Is the Risk?

Send the drawing and tell us which face the assembly references. We will confirm the datum strategy, the flatness we can hold and what the inspection report will cover.

What to send

  • 2D drawing or 3D model (STEP, IGES, DWG, DXF, PDF)
  • Alloy and temper
  • Surface finish and color
  • Estimated annual quantity