Aerospace
Aerospace fixtures must carry cutting loads without letting thin-wall structures spring out of shape. Fixturing is built around tool accessibility, effective support and a stable datum across processes.
Don't let the fixture be the reason a 5-axis part needs a sixth setup.
Thin-Wall Loads
Arrange and sequence clamping so the fixture supports cutting loads without pulling the finished geometry out of true.
Tool Access
Keep jaws, screws, risers and hoses clear of the spindle, tool and chip-evacuation paths.
Process Transfer
Preserve a re-usable datum when moving from roughing to finishing or inspection.
Define the fixturing logic before counting products.
The preferred route is a first call — confirm against drawings, machine, loads and loading method.Complex geometry creates three conflicts at once: the part needs support, the tool needs space, and the datum must survive roughing. Here are workable fixture routes for aerospace parts.
Dovetail Fixture TS96-V50
ZPP-Dovetail-Fixture-5AxisZero Point System
TS96-155 / AR96-155Self-Centering Vise CV10075
ZPP-Self-Centering-ViseEngineering Validation Path
- Datum repeatability: remove and refit, then measure key datums by the agreed method.
- Distortion check: compare thin-wall geometry unclamped, clamped and machined.
- Interference check: fully verify tool, holder, spindle and clamp envelopes.
- First-article release: release only after a representative part and real loading sequence pass.
Materials Needed for Review
- Part STEP and stock condition
- 5-axis machine model and table interface
- Key datums and thin-wall zones
- Tool list and accessibility risks
- Batch takt and process transfer
Bring real fixturing constraints — let's review your aerospace part together.
Send drawings and current bottlenecks; we compare workable fixture directions, not a quote on the spot.