Wear Protection: Shielding the socket’s bearing cavity and main shaft from direct metal-to-metal contact, reducing abrasion caused by high-speed rotation (500–1500 rpm) and axial loads (up to thousands of kilonewtons).
Friction Reduction: Providing a low-friction surface (coefficient of friction ≤0.15 under lubrication) to minimize energy loss and heat generation between the main shaft and socket.
Load Distribution: Evenly distributing axial and radial loads from the main shaft to the socket, preventing localized stress concentration and extending the service life of both components.
Alignment Compensation: Allowing minor misalignment between the main shaft and socket through its slight elasticity, reducing vibration and noise during operation.
Liner Body: A hollow cylindrical sleeve made of bearing bronze (e.g., ZCuSn10Pb1), babbitt metal (tin-based: Sn 83–85%, Sb 11–13%), or steel-backed bimetallic material (steel shell with a sintered bronze layer). The wall thickness ranges from 5–15 mm, depending on the crusher size.
Inner Bearing Surface: A precision-machined surface with a low roughness (Ra0.8–1.6 μm) that directly contacts the main shaft. It often features circumferential oil grooves (0.5–2 mm deep) to retain lubricant and enhance friction reduction.
Outer Surface: A cylindrical or slightly tapered surface that fits into the socket’s bearing cavity with an interference fit (0.01–0.05 mm) to prevent rotation relative to the socket.
Flange (Optional): A radial flange at one end to limit axial movement in the socket, ensuring the liner remains seated under heavy axial loads.
Lubrication Features:
Oil Grooves: Axial or spiral grooves on the inner surface that distribute lubricant evenly along the contact area, preventing dry friction.
Oil Holes: Small holes (φ3–φ6 mm) connecting the outer surface to the inner grooves, aligning with the socket’s lubrication channels to ensure oil flow.
Chamfers: Rounded edges (0.5–2 mm radius) at both ends to facilitate installation and prevent stress concentration at the liner-shaft interface.
Material Selection:
Bearing bronze (ZCuSn10Pb1) is preferred for its high compressive strength (≥300 MPa), good thermal conductivity, and compatibility with steel shafts. Its composition is controlled to Sn 9–11%, Pb 0.5–1.0%, Cu balance, with a hardness of HB 80–100.
Casting:
Centrifugal Casting: Molten bronze is poured into a rotating mold (1000–3000 rpm) to form a cylindrical sleeve with a dense, uniform structure. This method ensures concentricity and minimizes porosity (≤5% by volume).
Sand Casting: For flanged liners, sand molds are used with cores to form oil grooves or holes. Pouring temperature is 1000–1100°C to ensure complete filling of thin sections.
Heat Treatment:
Bronze liners undergo annealing at 500–600°C for 1–2 hours, followed by slow cooling, to relieve casting stress and improve machinability.
Machining and Finishing:
Rough Machining: The cast blank is turned on a lathe to machine outer diameter, inner bore, and flange (if applicable), leaving 0.5–1 mm finishing allowance.
Finish Machining: Inner and outer surfaces are precision-turned to achieve dimensional tolerances (IT6–IT7) and surface roughness Ra0.8 μm. The inner bore is honed for superior roundness (≤0.005 mm).
Oil Groove Machining: Grooves are milled or broached into the inner surface with precise depth and spacing to optimize lubricant retention.
Steel Shell Preparation: A low-carbon steel (Q235) sleeve is drawn or machined to the desired outer dimensions, then cleaned and roughened (e.g., via sandblasting) to enhance bonding with the bearing layer.
Bearing Layer Application:
Sintering: A bronze powder (e.g., CuSn10) is sintered onto the steel shell at 800–900°C in a protective atmosphere (nitrogen), forming a 0.5–2 mm thick porous layer.
Roll Bonding: A thin bronze sheet (0.3–1 mm thick) is cold-rolled onto the steel shell under high pressure (100–200 MPa), creating a metallurgical bond.
Final Machining: The inner surface is finish-machined to the required dimensions and roughness, with oil grooves added as needed.
Material Testing:
Chemical composition analysis (spectrometry) verifies compliance with material standards (e.g., ZCuSn10Pb1: Sn 9–11%, Pb 0.5–1.0%).
Hardness testing (Brinell) ensures bronze liners have a hardness of HB 70–90, balancing wear resistance and ductility.
Dimensional Accuracy Checks:
A coordinate measuring machine (CMM) inspects inner/outer diameters, wall thickness uniformity, and flange thickness, with tolerances controlled to ±0.01 mm for critical dimensions.
Roundness and cylindricity of the inner surface are measured using a roundness tester, ensuring values ≤0.005 mm to prevent uneven wear.
Microstructural Analysis:
Metallographic examination checks for porosity (≤5% in bronze) and bonding quality in bimetallic liners (no delamination between steel and bearing layers).
Performance Testing:
Friction Coefficient Testing: A tribometer measures friction under simulated load (10–50 MPa) and speed (500–1500 rpm), requiring values ≤0.15 with lubrication.
Wear Testing: A pin-on-disk test subjects the liner material to 10⁶ cycles, with weight loss limited to ≤5 mg to ensure long service life.
Fit and Assembly Checks:
The liner is trial-fitted into a test socket to verify the interference fit: it should require light press force (5–20 kN) without distortion.
The inner bore is checked for compatibility with a standard main shaft sample, ensuring smooth rotation without binding under load.