C51900 Bronze

Alloy Designation

• International: UNS C51900, CDA 519, CuSn6 (EN Standard)

• Chinese: QSn6.5-0.1 (GB/T 4423-1992)

• Alias: Tin-phosphor bronze, Instrument bronze, featuring 6-7% tin and 0.1-0.25% phosphorus.

Key Features

C51900 balances high strength with functionality:

• High Strength & Elasticity: Tensile strength ≥480 MPa (cold-worked), elastic modulus 115 GPa; ideal for precision springs.

• Corrosion/Wear Resistance: Corrosion rate <0.01 mm/year in atmosphere/freshwater; low friction coefficient (0.18-0.25).

• Special Properties: Non-magnetic (μ<1.01), spark-resistant for explosion-proof applications.

• Processing Flexibility: Excellent hot/cold workability, weldability, brazing, and machinability.

Product Forms & Dimensions

Table 1: Product Forms & Specifications

Note: Custom sizes (e.g., hex bars, profiles) available with ±0.05mm tolerance.

Chemical Composition

Table 2: Chemical Composition (wt%, Cu bal.)

*Standards: GB/T 4423-1992, ASTM B139.*

Physical Properties

Table 3: Physical Properties (20°C)

Mechanical Properties

Table 4: Mechanical Properties (Room Temp, Bar Samples)

*Note: Sample diameter 5-12mm (longitudinal direction).

Core Advantages

• Strength-Conductivity Balance: 15-16% IACS + 480 MPa tensile strength (H02), outperforms C51000/C51100.

• Extended Wear Life: 2× longer bearing life vs. brass (PV limit: 2.5 MPa·m/s).

• Cryogenic Suitability: No brittleness at -200°C for aerospace/superconducting equipment.

• Processing Compatibility: Supports cold heading, stamping (≤30% deformation), TIG welding (SCu5210 filler).

  
  

Applications

• Electronics: High-reliability connectors, relay springs, test probes (>100k mating cycles).

• Precision Instruments: Hairsprings, diaphragms, brush holders, gears (non-magnetic).

• Industrial: Bellows, bearing bushes, chemical pump seals (resists weak acids/seawater).

• Transportation: Aircraft sensor springs, automotive seat brackets (cold-stamped).

Processing Guidelines

• Hot Working: Strictly 750-770°C; >800°C causes grain growth, <700°C increases deformation resistance.

• Cold Working: ≤30% per-pass reduction; intermediate anneal (600-650°C×1h) to relieve hardening.

• Welding: Prefer TIG (SCu5210 filler + 200-250°C preheat); post-weld anneal at 500-550°C.

• Surface Treatment: Avoid lead-containing coolants to prevent SCC; chromate passivation enhances corrosion resistance.

Key Application Scenarios

• Aerospace Connectors: Stable performance under high vibration (Airbus A350 certified).

• Marine Valve Bushings: ≥10-year design life in seawater.

• Smart Meter Springs: Elastic hysteresis <0.05% (meets Class 0.1 accuracy).

• Explosion-Proof Tools: Spark-free impact for oil platform maintenance.

FAQ

Q1: C51900 vs. QSn4-3 (C51100)?

A1: C51900 has higher Sn (6.5% vs. 4%), 30% higher strength/elasticity, but 20% higher cost. Use C51100 for general springs; C51900 for high-stress springs/wear parts.

Q2: Extra protection in seawater?

A2: Corrosion rate <0.015 mm/year (static). For flow >2 m/s, use passivation/cathodic protection; avoid direct contact with stainless steel.

Q3: Microcracks after cold working?

A3: Caused by excessive deformation/surface defects. Solutions:

1. Limit per-pass reduction to ≤25%;

2. Acid-clean oxide layers pre-processing;

3. Intermediate anneal (620°C×1h).

Q4: Insufficient hardness post-heat treatment?

A4: Verify parameters:

• Annealed: 600-650°C + air cooling;

• Aging: 320-340°C×2-3h (hardness ↑10-15%).

Reference Standards

Testing Standards

• Chemistry: ASTM E54 (Sn), ASTM E62 (P)

• Mechanical: ASTM E8 (tensile), ASTM E92 (hardness)

• Metallography: ASTM E112 (grain size)

Note: Data synthesized from ASTM, GB, JIS, and manufacturer specs. Performance may vary slightly with processing. Conduct application-specific validation before use.