AURA Engineering Platform
Solved case · inverse synthesis · version 1.0

Required loads in. Three feasible conical-bearing candidates out.

This public case closes the gap between saying that AURA supports inverse design and showing a reproducible, bounded result. The design question starts with required performance and a locked shaft interface—not a preselected bearing geometry.

SOLVED399 FEASIBLE STATESSCREENING ONLYCASE ID AURA-INV-CONE-80R-360A-30D-001
Screening result: within the stated search space, AURA found opposed-conical bearing states satisfying both static criteria. The three published candidates expose different envelope, pressure and flow trade-offs; none is presented as a production release.

1. Requirements and fixed decisions

80 NRequired radial load
360 NRequired axial load
30 mmLocked shaft diameter
InputValueRole in this case
Support architectureOpposed conical pairAxial stiffness projected to the machine axis as Knormal sin²α.
Pressure basisAbsoluteSupply candidates are evaluated against pa = 1.0 bar absolute.
Radial criterionEr,req ≤ 0.70Required radial equilibrium ratio must remain inside the screening limit.
Axial criterionEz,req ≤ 0.70Required axial equilibrium ratio must remain inside the screening limit.
Operating speed20,000 rpmRecorded as a downstream machine requirement; not used to rank this static inverse search.

2. Search and ranking

  1. Generate. The solver evaluates 4,032 combinations across bounded cone angle, length, clearance, supply pressure and feed configuration while preserving the 30 mm shaft interface.
  2. Reject. Invalid physical/model states are removed before feasibility scoring; 630 combinations were rejected in this run.
  3. Filter. Both radial and axial screening criteria must pass. The run returned 399 feasible states.
  4. Rank. The published set deliberately represents three engineering preferences: balanced margin, compact envelope and lower supply pressure.

3. Candidate comparison

CandidateGeometrySupply / flowStatic outputsRequired ratios
Balanced margin
Top-ranked balanced state
α 60° · L 32.0 mm
C 20 µm · Rout 70.43 mm
5.0 bar abs
2.72 m³/h
Kr 10.38 N/µm
Ka 65.17 N/µm
Wr,max 145.39 N
Wa,max 912.35 N
Er 0.385
Ez 0.276
Compact envelope
Smallest published radial envelope
α 50° · L 22.4 mm
C 20 µm · Rout 41.70 mm
8.0 bar abs
4.35 m³/h
Kr 9.50 N/µm
Ka 30.62 N/µm
Wr,max 133.03 N
Wa,max 428.69 N
Er 0.421
Ez 0.588
Lower pressure
Lowest published supply pressure
α 60° · L 48.0 mm
C 30 µm · Rout 98.14 mm
3.0 bar abs
2.45 m³/h
Kr 6.48 N/µm
Ka 60.54 N/µm
Wr,max 136.06 N
Wa,max 1,271.27 N
Er 0.412
Ez 0.198

Why three answers? Inverse design does not remove engineering judgment. It makes the trade-off explicit. A compact state requires more pressure and flow; the lower-pressure state needs a much larger radial envelope; the balanced state retains the largest minimum screening margin of the published set.

4. Controlled handoff

What can move downstream

Case identity, fixed interface, geometry, absolute-pressure basis, feed architecture, static load capacities, projected stiffnesses, flow estimate and screening criteria can enter the machine-configuration record.

What is still missing

Manufacturing tolerances, frequency-dependent coefficients, thermal and pneumatic transients, complete rotor eigenanalysis, stability margin, uncertainty propagation and case-level experimental correlation.

Decision authority: SCREENING ONLY. The result supports candidate selection for the next engineering stage. It does not authorize geometry freeze, procurement, production speed operation or a universal performance claim. A chosen candidate must be re-evaluated in the actual spindle layout and evidence programme.

5. Reproducibility record

The public JSON record contains inputs, search counts, constraints, all three candidates and the evidence boundary. The solver remains proprietary, but the published result is no longer an unsupported capability statement.