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OEM Aerospace Parts Cnc Machining Flange Bracket Alloy Non Standard

OEM Aerospace Parts Cnc Machining Flange Bracket Alloy Non Standard

Brand Name: VIGOROUS
Moq: 1 Piece
Price: Negotiable
Payment Terms: T/T,L/C
Supply Ability: 500–2000 pcs/month
Detail Information
Place of Origin:
CHINA
Productname:
Aerospace Machined Components
Manufacturingprocess:
CNC Machining, Turning, Milling, Drilling
Tolerance:
±0.001 Inch (±0.0254 Mm)
Quantity:
Prototype To Mass Production
Weight:
Varies Depending On Material And Design
Surfacefinish:
Ra 0.8 - 3.2 Microns
Heattreatment:
Available Upon Request (e.g., Annealing, Stress Relieving)
Material:
Aluminum, Titanium, Stainless Steel, Inconel
Inspectionmethods:
CMM, Visual Inspection, Ultrasonic Testing
Application:
Aircraft Structures, Engine Components, Landing Gear Parts
Leadtime:
Typically 2-6 Weeks Depending On Complexity
Compatibility:
Compatible With Aerospace Industry Standards And Specifications
Coatingoptions:
Anodizing, Passivation, Painting
Sizerange:
Up To 500 Mm In Diameter And 1000 Mm In Length
Packaging Details:
Standard packaging uses corrugated cartons. For heavy single items or large-volume sea freight orders, fumigation-free plywood wooden cases are applied. Each precision machined part is individually wrapped with bubble wrap or EPE foam to protect against sc
Supply Ability:
500–2000 pcs/month
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Product Description

Product Summary

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.

Core Product Specification Table

Item

Verified Aerospace Grade Technical Specification

Official Product Name

5-Axis CNC Milled Aerospace Porous Flange Heavy-Load Rotary Bearing Support Housing

Core Production Process

5-Axis Full Envelope Simultaneous Milling Single Fixture One-Piece Machining

Maximum Overall Boundary Envelope

245 mm Outer Flange Diameter * 152 mm Overall Axial Height

Main Bearing Seat Bore Diameter

110 mm, fully custom available range 55 mm to 250 mm per customer engineering drawings

Critical Positioning Tolerance

Full ISO 2768-f fine grade compliance, positional repeatability accuracy ≤ 0.007 mm

Raw Material Quality Assurance

100% XRF PMI positive material inspection, full batch heat treatment traceability documentation

Aerospace Approved Surface Treatment Range

Aerospace grade electropolish / Type 3 hard anodize / low emissivity thermal spray coating / irridite NCP chromate conversion coating

Full Verified Technical Data Sheet

Specification Category

Fully Validated Aerospace Technical Details

Component Classification

Flight Grade Primary Load-Bearing Rotary Bearing Support Structure

Machining Production Platform

High dynamic stiffness 5-axis gantry CNC machining center equipped with active vibration suppression and in-process tool wear monitoring system

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

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

Final As-Machined Surface Quality

Zero visible helical tool feed lines, all dynamic contact mating surfaces fine finished to Ra ≤ 1.2 μm

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

Supported Production Scales

Flight qualification first article prototype, 5-30 unit low volume trial batch, continuous serial production for aerospace serial programs

Accepted Drawing Input Formats

Native CATIA V5 / V6 source 3D files, STEP AP242, ASME Y14.5 2D GD&T standard engineering drawings

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

Material & 5-Axis Aerospace Machining Core Competitive Advantages

Monolithic 5-Axis Single-Setup Machining No Secondary Joints

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.

Aerospace Grade Cryogenic Stress Relief Process

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.

Full Aerospace FOD Prevention Machining Workflow

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.

Complete Aerospace Project Documentation Support

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.

Verified Typical Flight Critical End-Use Applications

  • Jet Engine Accessory Gearbox Main Bearing Support Housings

  • Satellite High Torque Solar Panel Rotary Actuator Mounting Structures

  • Heavy Lift Unmanned Aerial Vehicle Main Rotor Head Bearing Carriers

  • Missile Inertial Navigation System Gyroscope Ultra Precision Support Assemblies

  • Aerospace Hypersonic Test Facility High Load Dynamic Test Fixtures

Frequently Asked Questions for Aerospace Industrial Buyers

  1. 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.

  2. 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.

  3. 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.

  4. 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.

  5. 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.