INDUSTRY COMPONENT

Attachment Fitting

Aerospace attachment fitting for connecting structural elements in aircraft and spacecraft assemblies.

Component Specifications

Definition
An aerospace attachment fitting is a precision-engineered structural component designed to securely connect and transfer loads between primary and secondary structural elements in aircraft and spacecraft. These fittings are critical for maintaining structural integrity, ensuring proper alignment, and facilitating assembly and disassembly during maintenance operations. They are engineered to withstand extreme environmental conditions including high vibration, thermal cycling, and variable pressure loads while maintaining dimensional stability and fatigue resistance.
Working Principle
Attachment fittings function by providing a secure mechanical interface between structural components through precisely engineered mating surfaces, fastener holes, and load paths. They distribute operational loads (tension, compression, shear, and bending moments) across connected structures while minimizing stress concentrations. The working principle involves transferring forces through the fitting's geometry and material properties to maintain structural continuity and prevent relative movement between connected components under all operational conditions.
Materials
High-strength aluminum alloys (7075-T6, 2024-T3), titanium alloys (Ti-6Al-4V), advanced composites (carbon fiber reinforced polymers), and corrosion-resistant steels (A286, 15-5PH). Materials are selected based on strength-to-weight ratio, fatigue resistance, corrosion resistance, and compatibility with connected structures.
Technical Parameters
  • Weight 0.1-5.0 kg
  • Fatigue Life >100,000 cycles at design load
  • Load Capacity 10-500 kN depending on application
  • Surface Finish Ra 0.8-3.2 μm
  • Temperature Range -65°C to +200°C
  • Corrosion Protection Anodized, alodined, or cadmium plated
Standards
ISO 9001, AS9100, MIL-STD-810, NASM, DIN EN 9100

Industry Taxonomies & Aliases

Commonly used trade names and technical identifiers for Attachment Fitting.

Parent Products

This component is used in the following industrial products

Engineering Analysis

Risks & Mitigation
  • Fatigue failure under cyclic loading
  • Stress corrosion cracking
  • Improper installation leading to misalignment
  • Galvanic corrosion in dissimilar material interfaces
  • Thermal expansion mismatch
FMEA Triads
Trigger: Improper torque application during installation
Failure: Bolt loosening leading to joint slippage and excessive wear
Mitigation: Implement calibrated torque tools and torque verification procedures with witness marks
Trigger: Material defects or improper heat treatment
Failure: Reduced fatigue strength leading to premature cracking
Mitigation: Implement material certification requirements and 100% NDE inspection of critical areas
Trigger: Environmental exposure to corrosive agents
Failure: Corrosion pitting leading to stress concentration and crack initiation
Mitigation: Apply appropriate protective coatings and implement regular inspection schedules

Industrial Ecosystem

Compatible With

Interchangeable Parts

Compliance & Inspection

Tolerance
±0.05 mm for critical dimensions, ±0.1° for angular features
Test Method
Static load testing per MIL-STD-810, fatigue testing per ASTM E466, dimensional inspection per ASME Y14.5

Buyer Feedback

★★★★☆ 4.5 / 5.0 (32 reviews)

"Found 40+ suppliers for Attachment Fitting on CNFX, but this spec remains the most cost-effective."

"The technical documentation for this Attachment Fitting is very thorough, especially regarding technical reliability."

"Reliable performance in harsh Other Transport Equipment Manufacturing environments. No issues with the Attachment Fitting so far."

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Frequently Asked Questions

What are the main types of aerospace attachment fittings?

Common types include clevis fittings, lug fittings, bracket fittings, and shear tie fittings, each designed for specific load transfer requirements and installation configurations.

How are attachment fittings tested for aerospace applications?

They undergo rigorous testing including static load testing, fatigue testing, vibration testing, thermal cycling, and non-destructive examination (NDE) methods like ultrasonic and radiographic inspection.

What factors determine material selection for aerospace attachment fittings?

Key factors include specific strength requirements, weight constraints, corrosion resistance needs, thermal expansion compatibility, and manufacturing considerations for the intended aerospace application.

Can I contact factories directly?

Yes, each factory profile provides direct contact information.

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