7050-T7451 Aerospace Round Aluminum Bar Stress Corrosion Resistant Zinc Alloy For Aircraft Fuselage Wing Structures
Product Overview
The 7050-T7451 round aluminum bar is a premium aerospace-grade zinc alloy engineered for superior stress corrosion cracking resistance and high fracture toughness. The T7451 over-aged temper provides an optimal balance of high strength and exceptional durability, making it the preferred choice for critical aircraft structural components where reliability under sustained stress is paramount.
Key Features
- Zinc-based 7xxx series alloy with excellent stress corrosion cracking resistance
- T7451 over-aged temper for optimal strength-toughness balance
- High fracture toughness for damage-tolerant design applications
- Superior performance in thick-section structural components
- Conforms to AMS 4050, ASTM B221, and BAC 5431 standards
Typical Applications
- Aircraft fuselage frames and bulkhead structures
- Wing spars and rib components
- Landing gear structural parts
- High-integrity aerospace forgings and machined parts
Packaging & Delivery
All bars are coated with anti-rust oil and wrapped in waterproof kraft paper, then packed in fumigation-free plywood cases. Standard delivery within 5 working days for stock sizes, 20-30 days for custom production orders.