7075-T651 铝合金综合指南

308751729937665_.pic

免费样品

308771729937665_.pic

中国制造商

308781729937665_.pic

快速反应

308761729937665_.pic

批量购买折扣

308771729937665_.pic

中国制造商

主要亮点

  1. 7075-T651 is a stress-relieved variant of 7075-T6, achieved by stretching the material 1–3% after quenching to reduce residual stresses.
  2. The T651 temper maintains T6-level strength (~572 MPa tensile) while improving dimensional stability during machining.
  3. It is the preferred temper for thick plate and precision-machined aerospace components where post-machining distortion must be minimized.
  4. Zinc is the primary alloying element, delivering the highest strength among commonly available aluminum alloys.
  5. Corrosion resistance is moderate — surface treatment is recommended for harsh or marine environments.

导言

7075-T651 铝合金 is a high-strength, heat-treated material widely used in aerospace, defense, and precision machining. The T651 temper is a specific variation of T6 that adds a stress-relief step, making it the standard choice for thick plate and components that require tight dimensional tolerances after machining. This guide covers the properties, applications, and practical considerations of 7075-T651.

了解 7075-T651 铝合金

What Does T651 Mean?

The “T651” designation describes a specific heat treatment process:

  1. Solution heat treatment: The alloy is heated to dissolve the alloying elements into solid solution.
  2. Quenching: Rapid cooling (typically in water) traps the elements in solution.
  3. Stress relief by stretching: The material is stretched 1–3% in length to relieve residual quenching stresses. This is the key step that distinguishes T651 from T6.
  4. Artificial aging: A controlled precipitation hardening cycle that develops peak strength.

The stretching step is what makes T651 different from T6. In thick plates, quenching creates internal stresses that can cause warping during machining. T651 relieves these stresses, so machined parts hold their dimensions. This is why aerospace specifications for thick plate typically call for T651 rather than T6.

Mechanical Properties of 7075-T651

财产 7075-T651
拉伸强度(兆帕) 572
屈服强度(兆帕) 503
剪切强度(兆帕) 331
伸长率 (%) 11
硬度(布氏硬度) 150
密度(克/立方厘米) 2.81

与其他铝合金的比较

合金 拉伸强度(兆帕) 屈服强度(兆帕) 耐腐蚀性
7075-T651 572 503 中度
2024-T3 470 325 公平
6061-T6 310 276 良好

7075-T651 is significantly stronger than both 2024-T3 and 6061-T6. However, 6061-T6 offers better corrosion resistance and weldability at lower cost. The choice depends on whether your application prioritizes strength (7075) or versatility and cost (6061). For a detailed analysis, see our 6061与7075对比指南.

T651 vs T6: Key Differences

财产 7075-T6 7075-T651
实力 Same Same
Residual Stress 更高 Lower (stress-relieved)
Dimensional Stability After Machining 较低 更高
Preferred For Thin sections, extrusions Thick plate, precision machining

For comparison with the T73 temper (which prioritizes stress-corrosion cracking resistance over strength), see our 7075-T73 properties guide.

主要应用和行业

航空航天

7075-T651 is a standard material in aerospace manufacturing. Its high strength-to-weight ratio and dimensional stability make it ideal for:

  • Fuselage frames and bulkheads
  • Wing spars and stringers
  • 起落架部件
  • Machined structural fittings and brackets

The stress-relieved T651 temper is specifically chosen for machined aerospace parts because it minimizes post-machining distortion — critical for parts with tight tolerances. 7075-T651 aluminum sheet and plate are the most commonly specified forms.

Automotive and Transportation

In performance automotive applications, 7075-T651 is used for:

  • High-performance wheels (lighter than steel, stronger than 6061)
  • Suspension components like control arms
  • Structural reinforcements in racing and high-performance vehicles

The alloy’s high strength allows thinner, lighter components without sacrificing load capacity. For automotive applications that don’t require 7075’s strength, 7075 round bar and 6061 alternatives offer better cost-performance ratios.

Machining and Joining Considerations

7075-T651 machines well, with good chip formation and surface finish. Use carbide tooling and appropriate cutting fluids. The stress-relieved temper means machined parts will hold dimensions better than T6, which is the primary reason to specify T651 over T6 for precision parts.

Welding 7075-T651 is not recommended. The alloy is susceptible to hot cracking, and the heat-affected zone loses the T651 temper properties. Mechanical fastening — riveting or bolting — is the standard joining method. For more details, see our 7075焊接指南.

结论

7075-T651 aluminum offers the same exceptional strength as T6, with the added benefit of stress relief for better dimensional stability during machining. This makes it the preferred temper for thick plate and precision-machined aerospace components. The trade-off: it shares 7075’s moderate corrosion resistance and poor weldability, and it costs more than 6xxx series alloys. If your application requires high strength, tight tolerances, and reliable machining results, 7075-T651 is the right choice.

Linsy Aluminum supplies 7075-T651 in plate, bar, sheet, and tube forms, with customization for dimensions and surface finishes. Typical lead times are 10–60 days depending on temper, thickness, and processing requirements. 联系Linsy Aluminum to discuss your 7075-T651 specifications.

常见问题

What is the difference between 7075-T6 and 7075-T651?

The difference is stress relief. T651 includes a stretching step (1–3% elongation) after quenching that relieves residual internal stresses. Both tempers have the same nominal strength, but T651 provides better dimensional stability during machining — making it the preferred choice for thick plate and precision parts.

Is 7075-T651 corrosion resistant?

7075-T651 has moderate corrosion resistance — better than 2xxx series alloys but worse than 6xxx series. Its copper content makes it susceptible to corrosion in harsh or marine environments. For such applications, consider 7075-T73 (better SCC resistance) or apply anodizing/protective coatings.

Can 7075-T651 be welded?

Welding 7075-T651 is not recommended. The alloy is prone to hot cracking, and welding destroys the T651 temper in the heat-affected zone. Mechanical fastening (riveting, bolting) is the standard joining method. Friction stir welding is the only welding process that may be considered, but it requires specialized equipment.

What is 7075-T651 used for?

Primarily aerospace structural components (fuselage frames, wing spars, landing gear), military equipment, precision-machined fittings, high-performance automotive parts, and mold tooling. It is specified wherever maximum strength and machining precision are required in a lightweight material.

How does 7075-T651 compare to 6061-T6?

7075-T651 is nearly twice as strong as 6061-T6 (572 vs 310 MPa tensile). However, 6061-T6 is cheaper, weldable, and has better corrosion resistance. Choose 7075-T651 when strength is critical; choose 6061-T6 when versatility and cost matter more. See our forged 7075 vs 6061 guide for a detailed comparison.

黄大卫

David Huang 是中国铝合金行业备受尊敬的专家,在先进铝合金的开发、制造和应用方面拥有十多年的经验。他曾成功地为航空航天、汽车和建筑等不同领域的全球领先企业提供项目解决方案和专业技术知识。此外,David 还是中国多家主要铝材制造商值得信赖的顾问。

全天候服务 10 分钟内响应!

如需更多产品目录、详细信息和报价,请直接与我们联系!

WhatsApp 电话