IC Engine Working Principle is based on the 3 Fundamental Thermodynamic Theoretical Cycles.
Otto Cycle (heat add & reject at constant Vol)
Diesel Cycle (heat add at constant Pr & reject at constant Vol)
Dual Combustion Cycles (heat add partly at constant Vol & Pr & heat reject at constant Vol)
Actual engines do not operate strictly following these ideal cycles
One Cycle consists of 4 operations:
(1) Suction / Induction / Scavenge
(2) Compression
(3) Power / Expansion / Working / Firing
(4) Exhaust
(i) 4 Stroke Cycle Engine
One complete sequence of 4 OPERATIONS is completed in:
TWO REVOLUTIONS of the Crank Shaft
(or)
FOUR STROKES of the Piston
(ii) 2 Stroke Cycle Engine
One complete sequence of 4 OPERATIONS is completed in:
ONE REVOLUTION of the Crank Shaft
(or)
TWO STROKES of the Piston
Basic Marine Engineering BookPage No. 242 Fig 14.1 and Page No. 243 Fig 14.2
PV Diagram
Difference between Four Stroke Engine & two-stroke engine
Four Stroke Engine | Two Stroke Engine | |
1. | It has one power stroke for every two revolutions of the crankshaft. | It has one power stroke for each revolution of the crankshaft. |
2. | Heavy flywheel is required and engine runs unbalanced because turning moment on the crankshaft is not even due to one power stroke for every two revolutions of the crankshaft. | Lighter flywheel is required and engine runs balanced because turning moment is more even due to one power stroke for each revolution of the crankshaft. |
3. | Engine is heavy. Power to weight ratio is low | Engine is light. Power to weight ratio is high |
4. | Engine design is complicated due to valve mechanism. | Engine design is simple due to absence of valve mechanism. |
6. | Less mechanical efficiency due to more friction on many parts. More wear and tear. More maintenance is required | More mechanical efficiency due to less friction on a few parts. Less wear and tear. Less maintenance is required |
7. | More output due to full fresh charge intake and full burnt gases exhaust.
mep is high |
Less output due to mixing of fresh charge with the hot burnt gases.
mep is low |
8. | Power developed is less | Power developed is more (almost double) |
9. | Gear box [to reduce speed & reversing] is connected between engine and propeller shaft | Engine directly connected to propeller shaft. Engine is reversible |
10. | Engine consists of inlet and exhaust valve. | Engine consists of inlet port and exhaust port/valve. |
11. | More thermal efficiency. | Less thermal efficiency, as effective compression ratio is less |
12. | Separate cylinder L.O is not required | Separate cylinder L.O is required |
13. | High speed & Short Stroke – Costly fuel of better ignition quality should be used | Slow speed & Long Stroke – effective scavenging and cheap fuel of low ignition quality can be burnt |