| Brand Name: | VIGOROUS |
| Moq: | 1 Piece |
| Price: | Negotiable |
| Payment Terms: | T/T,L/C |
| Supply Ability: | 500–2000 pcs/month |
We manufacture flight-qualified custom 5-axis single-setup milled porous flange heavy-duty bearing housings purpose-built for high-overload dynamic rotary assemblies in commercial and defense aerospace programs. The entire complex multi-orifice distributed flange array, precision segmented oil groove ring, full through lubrication network and monolithic two-point support feet are fully completed in one single continuous 5-axis machining cycle, eliminating all accumulated fixturing misalignment error that would otherwise break the high concentricity requirement between the main bearing seat bore and all distributed assembly bolt holes. The monolithic one-piece structure delivers exceptional anti-vibration rigidity and zero hidden assembly gaps, making it the ideal structural carrier for flight-critical main load-bearing rotary motion applications.
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Item |
Verified Aerospace Grade Technical Specification |
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Official Product Name |
5-Axis CNC Milled Aerospace Porous Flange Heavy-Load Rotary Bearing Support Housing |
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Core Production Process |
5-Axis Full Envelope Simultaneous Milling Single Fixture One-Piece Machining |
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Maximum Overall Boundary Envelope |
245 mm Outer Flange Diameter * 152 mm Overall Axial Height |
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Main Bearing Seat Bore Diameter |
110 mm, fully custom available range 55 mm to 250 mm per customer engineering drawings |
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Critical Positioning Tolerance |
Full ISO 2768-f fine grade compliance, positional repeatability accuracy ≤ 0.007 mm |
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Raw Material Quality Assurance |
100% XRF PMI positive material inspection, full batch heat treatment traceability documentation |
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Aerospace Approved Surface Treatment Range |
Aerospace grade electropolish / Type 3 hard anodize / low emissivity thermal spray coating / irridite NCP chromate conversion coating |
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Specification Category |
Fully Validated Aerospace Technical Details |
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Component Classification |
Flight Grade Primary Load-Bearing Rotary Bearing Support Structure |
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Machining Production Platform |
High dynamic stiffness 5-axis gantry CNC machining center equipped with active vibration suppression and in-process tool wear monitoring system |
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Fully Qualified Material Portfolio |
AISI 304 / 316L aerospace stainless steel, Ti-6Al-4V ELI extra low interstitial titanium, 7075-T73 high strength aluminum, Inconel A286 / Haynes 188 high temperature superalloy |
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Complete Integrated Geometric Features |
Multi-ring distributed precision orifice flange array, integrated segmented oil reservoir groove ring, full through interconnected lubrication channel network, dual monolithic reinforced mounting feet, anti-rotation drive keyway in main bearing seat |
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Final As-Machined Surface Quality |
Zero visible helical tool feed lines, all dynamic contact mating surfaces fine finished to Ra ≤ 1.2 μm |
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Tolerance Control Level |
All bearing interface critical dimensions held within ± 0.007 mm, ultra-precision gyro bearing service can be further tightened down to minimum ± 0.004 mm upon custom project request |
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Supported Production Scales |
Flight qualification first article prototype, 5-30 unit low volume trial batch, continuous serial production for aerospace serial programs |
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Accepted Drawing Input Formats |
Native CATIA V5 / V6 source 3D files, STEP AP242, ASME Y14.5 2D GD&T standard engineering drawings |
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Premium High Performance Material Upgrade Options |
17-4 PH H1150 precipitation hardening stainless steel, Rene 41 high temperature nickel alloy for Mach 3+ high speed aerospace operational environments |
Unlike traditional 3-axis split workflow that requires at least 4 separate re-fixturing cycles to machine the front flange, back face, internal bore cavities and mounting feet independently, this entire heavy-duty bearing housing is fully machined from a single solid block of raw aerospace certified metal stock in one uninterrupted 5-axis machining cycle. No secondary welding, threaded fastener assembly or adhesive bonding operations are ever introduced into the primary load path. This eliminates all micro gaps, misalignment interfaces and residual stress concentrations that would degrade structural rigidity and accelerate premature fatigue crack initiation under repeated 10G+ peak aerospace dynamic overload conditions.
Every individual raw machined part undergoes mandatory dedicated post roughing cryogenic stress relief processing at -196°C liquid nitrogen environment before final precision finishing operations. This treatment fully releases all internal residual forming and machining stress locked inside the metal grain structure, guaranteeing zero long-term dimensional drift across thousands of repeated thermal cycles ranging from -65°C deep space cold soak up to +230°C continuous high temperature operation, a critical performance requirement that standard industrial grade CNC parts cannot satisfy.
Every threaded hole, precision assembly bolt bore, lubrication channel opening and countersink on the complete part is manually inspected and precision deburred by certified aerospace machinists after final machining. No micro loose burr, hidden machining chip or sharp fractured edge is allowed to remain on any flight critical mating surface, fully eliminating the risk of foreign object debris detaching and being drawn into high speed moving bearing assemblies during high vibration flight operation, a mandatory AS9100 quality safety requirement far exceeding general industrial part quality standards.
We are fully capable of delivering the full regulated documentation package required for formal aerospace program audit systems, including complete raw material mill test reports, full batch heat treatment records, 3D CMM full point cloud dimensional inspection reports, surface treatment certification documents, full material traceability chain logs and formal level 3 First Article Inspection (FAI) forms to fully satisfy all AS9100D quality system compliance requirements.
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What drawing file formats do you accept for custom aerospace porous flange bearing housings?
We accept STEP, IGES, native CATIA / SolidWorks 3D part files and ASME Y14.5 standard 2D engineering drawings. Please explicitly mark all GD&T geometric tolerance callouts, flight critical mating surfaces and required surface treatment specifications on your drawing package.
What is the maximum achievable tolerance for the main precision bearing seat bore?
Standard production units deliver guaranteed ± 0.007 mm tolerance. We can achieve strictest tolerance down to ± 0.004 mm for ultra-high precision navigation gyro bearing applications on formal aerospace qualification programs.
Are you able to provide full formal AS9100 compliant First Article Inspection documentation for flight hardware parts?
Yes. Our standard quality package already includes full material certification, complete dimensional inspection reports and heat treatment traceability. Level 3 full FAI inspection documentation is available as a formal audited optional service.
What aerospace qualified surface treatment options are available for these heavy-duty bearing housings?
We offer full passivation for stainless steel variants, type 3 hard coat anodizing for high strength aluminum units, specialized low-friction dry film lubricant coating and high temperature thermal spray coating options for enhanced extreme environment wear and oxidation resistance.
What is the standard delivery lead time for aerospace prototype and serial production custom bearing housings?
Flight qualified first article prototype units typically ship in 12-22 business days. Final lead time for larger serial mass production batches will be confirmed after full engineering manufacturability review and final drawing approval.