How exploring parallel fabrication architectures eliminated tolerance stacking, removed 14 distinct fasteners, and reduced unit cycle times across the production floor.
Early in the pre-production run, the mechanical enclosure presented chronic fitment issues. The initial design relied on four stamped aluminum brackets welded to a structural rail, carrying the optical sensor mount and internal drive motor. While individual part fabrication met drawing tolerances, accumulated angular variations across consecutive bend radii created unpredictable 1.8 mm offset deviations across the mounting plane.
Assembly technicians were forced to manually shim every third subassembly during line trials. This manual adjustment ballooned build times from 8 minutes to nearly 26 minutes per unit. Instead of continuing patch-up rework routines or tightening stamping vendors to unsustainable micro-tolerances, the engineering lead paused tooling release to branch alternative manufacturing strategies.
Tightening tolerances on a fundamentally error-prone sheet-metal sequence only raises scrap rates. Changing the component architecture solves the problem permanently.
The core objective shifted: eliminate human calibration during assembly without expanding the exterior envelope or driving piece-part costs beyond acceptable unit economic targets.
Three distinct design branches were created inside Onshape to test competing fabrication paths against cycle time, upfront tooling expenditure, and structural rigidity:
High initial tooling cost with near-zero manual assembly. Required an 18-week mold build cycle that conflicted with pilot delivery milestones.
Monolithic 6061-T6 aluminum part eliminating all weld joints, fastener alignment points, and secondary bending operations.
Retained thin-gauge approach with integrated alignment tabs and self-clinching studs. Reduced part count but retained baseline bend error risk.
Running physical prototype cycles for Fork B and Fork C concurrently gave the team verified cycle data within nine days. Fork B proved that 5-axis machining reduced total unit assembly steps from 19 down to 3, while preserving precise sensor alignment without secondary fixture adjustments.
Detailed time studies and dimensional inspection reports confirmed substantial operational gains when migrating to the single monolithic machined unibody:
Although raw billet machining raised individual piece-part material expense by $4.20 per unit, total manufactured cost dropped by $11.80 when factoring in saved labor hours, fixturing upkeep, and zeroed rework stations.
Early budget assumptions favored sheet-metal stampings under the impression that lower per-part raw material cost would directly translate to lower overall manufacturing cost. The hidden expense of manual shimming, welding fixtures, and alignment labor only became measurable during physical assembly testing.
No. Selective pocketing, ribbed wall profiles, and topology thinning during CAD refinement allowed the single aluminum part to weigh 85 grams less than the combined multi-bracket assembly it replaced, while increasing torsional stiffness by 34%.
Instead of iterating sequentially through failed stamping revisions, the team explored the machined unibody and progressive die options simultaneously. When the unibody prototype cleared optical calibration on day one, convergence happened immediately without waiting for secondary tooling loops.
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