सभी उत्पाद
7075 T6 Aerospace Grade Aluminum Sheet 3.0mm Zinc Magnesium Copper Alloy High Strength for Aircraft Wing Components
| उत्पत्ति के प्लेस | शेडोंग, चीन |
|---|---|
| ब्रांड नाम | CHALCO |
| प्रमाणन | ISO 9001:2015, ASTM B209, AMS 4045, SAE AMS-QQ-A-250/12 |
| मॉडल संख्या | AL7075-T6-3.0 |
| न्यूनतम आदेश मात्रा | 1 टन |
| मूल्य | USD 3850-4450 / Ton |
| पैकेजिंग विवरण | संक्षारण रोधी तेल कोटिंग, दोनों तरफ पीई सुरक्षात्मक फिल्म, स्टील स्ट्रैपिंग के साथ प्रबलित लकड़ी के |
| प्रसव के समय | आदेश की पुष्टि के बाद 15-25 कार्य दिवस |
| भुगतान शर्तें | टी/टी, एल/सी नजर में |
| आपूर्ति की क्षमता | प्रति माह 3000 टन |
उत्पाद विवरण
| मिश्र धातु | 7075 | गुस्सा | T6 (कृत्रिम रूप से प्रयुक्त ऊष्मा उपचारित समाधान) |
|---|---|---|---|
| मोटाई | 3.0 मिमी | चौड़ाई | 1219 मिमी / 1500 मिमी |
| लंबाई | 2438 मिमी / 3000 मिमी / 4000 मिमी | जस्ता सामग्री | 5.1-6.1% |
| मैग्नीशियम सामग्री | 2.1-2.9% | तन्यता ताकत | ≥540 एमपीए |
| नम्य होने की क्षमता | ≥470 एमपीए | कठोरता | ≥150 एचबी |
| प्रमुखता देना | Aerospace Grade Zinc Alloy,Ultra High Strength 7075 Sheet,3.0mm Aircraft Structural Wing Plate |
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उत्पाद विवरण
7075 T6 Aerospace Grade Aluminum Sheet 3.0mm Zinc Magnesium Copper Alloy High Strength for Aircraft Wing Components
Ultra-High Strength at One-Third the Weight of Steel
Our 7075 T6 Aerospace Grade Aluminum Sheet is the highest strength aluminum alloy commercially available, with tensile strength exceeding 540 MPa — approaching that of structural steel at only one-third the weight. Engineered with a zinc-magnesium-copper alloy system and fully heat treated to T6 temper, this 3.0mm sheet is the definitive choice for aircraft structural components, wing spars, fuselage frames, and high-stress aerospace applications where failure is not an option.
Key Features
- Ultra-High Strength: ≥540 MPa tensile strength and ≥470 MPa yield strength, comparable to mild structural steel (S235) but at only 34% of the weight
- Zinc-Magnesium-Copper Alloy: 5.1-6.1% Zn, 2.1-2.9% Mg, and 1.2-2.0% Cu provides precipitation hardening capability for maximum mechanical properties
- Full T6 Heat Treatment: Solution treated at 480°C, water quenched, and artificially aged at 120°C for 24 hours for peak strength and hardness
- Excellent Fatigue Properties: Superior fatigue crack growth resistance critical for cyclic loading in aerospace structures
- Outstanding Strength Retention: Maintains significant strength at moderately elevated temperatures up to 120°C continuous service
Applications
- Aircraft wing spars and ribs
- Fuselage frames
- Missile components
- High-performance bicycle frames
- Rock climbing equipment
- Competition firearms receivers
- Molds for plastic injection
- Precision structural components where weight reduction is critical
Quality Assurance
Comprehensive Testing & Certification
Every sheet undergoes electrical conductivity testing (32-36% IACS for T6 verification), ultrasonic C-scan inspection for internal integrity per AMS-STD-2154 Class A, chemical analysis by OES, tensile testing per ASTM E8, and hardness testing. AMS 4045 aerospace specification compliance with full melt-to-product traceability. NADCAP-accredited testing laboratory certification available.
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