- To reduce size of the engine.
- To reduce crankpin dia.
- If not oblique cut not able to lift same from top with piston.
- If not oblique cut have palm bolts ,increase in production cost.
- Apart from this , as engines are becoming more efficient the liner bore dia is not increasing but as the power output is increasing the bottom end bearing size is increasing , because it has to transmit so much of the peak pressure (downward thrust) .Because the thrust is increasing the bottom end bearing size has to increase , liner dia and bore remains almost same.
1. High cost: Manganese bronze is a costly alloy, making it less economical for large propellers. 2. Low strength-to-weight ratio: Compared to other propeller materials like nickel-aluminum bronze or stainless steel, manganese bronze has a lower strength-to-weight ratio. 3. Susceptible to corrosion: Manganese bronze can corrode in seawater, especially when exposed to high velocities and turbulence. 4. Poor cavitation resistance: Manganese bronze is more prone to cavitation damage than other materials. 5. Difficult to cast and machine: Manganese bronze is challenging to cast and machine, making it less desirable for complex propeller geometries. 6. Limited weldability: Manganese bronze has poor weldability, making repairs and modifications difficult. Nickel-aluminum bronze or stainless steel are commonly used for propellers due to their: - High strength and durability - Excellent corrosion resistance - Good cavitation resistance - Ease of casting and machining - Weldability
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