AIR STANDARD CYCLE
ER. BANOJ KUMAR BEHERA
3RD SEMESTER MECHANICAL ENGINEERING
THERMAL ENGINEERING-I
MAYURBHANJ SCHOOL OF ENGINEERING (MSE),
LAXMIPOSI, BARIPADA
Process 1🡪 2 Isentropic compression
Process 2 🡪 3 Constant volume heat addition
Process 3 🡪 4 Isentropic expansion
Process 4 🡪 1 Constant volume heat rejection
v2
TC
TC
v1
BC
BC
Qout
Qin
Air-Standard Otto cycle
Compression ratio:
First Law Analysis of Otto Cycle
1🡪2 Isentropic Compression
AIR
2🡪3 Constant Volume Heat Addition
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AIR
Qin
TC
3 🡪 4 Isentropic Expansion
AIR
4 🡪 1 Constant Volume Heat Removal
AIR
Qout
BC
Effect of Compression Ratio on Thermal Efficiency
and P3 (material strength), both ~rk
Typical SI engines
9 < r < 11
k = 1.4
Process 1🡪 2 Isentropic compression
Process 2 🡪 3 Constant pressure heat addition
Process 3 🡪 4 Isentropic expansion
Process 4 🡪 1 Constant volume heat rejection
Air-Standard Diesel cycle
Qin
Qout
Cut-off ratio:
v2
TC
v1
BC
TC
BC
For cold air-standard the above reduces to:
Thermal Efficiency
recall,
Note the term in the square bracket is always larger than one so for the
same compression ratio, r, the Diesel cycle has a lower thermal efficiency
than the Otto cycle
Note: CI needs higher r compared to SI to ignite fuel
Typical CI Engines
15 < r < 20
When rc (= v3/v2)🡪1 the Diesel cycle efficiency approaches the
efficiency of the Otto cycle
Thermal Efficiency
Higher efficiency is obtained by adding less heat per cycle, Qin,
🡪 run engine at higher speed to get the same power.
Air
TC
BC
Qin
Qout
Compression
Process
Const pressure
heat addition
Process
Expansion
Process
Const volume
heat rejection
Process
Dual
Cycle
Qin
Const volume
heat addition
Process
Thermodynamic Dual Cycle
Process 1 🡪 2 Isentropic compression
Process 2 🡪 2.5 Constant volume heat addition
Process 2.5 🡪 3 Constant pressure heat addition
Process 3 🡪 4 Isentropic expansion
Process 4 🡪 1 Constant volume heat rejection
Dual Cycle
Qin
Qin
Qout
1
1
2
2
2.5
2.5
3
3
4
4
Thermal Efficiency
Note, the Otto cycle (rc=1) and the Diesel cycle (α=1) are special cases:
The use of the Dual cycle requires information about either:
(common assumption is to equally split the heat addition), or
ii) maximum pressure P3.
Transformation of rc and α into more natural variables yields
For the same inlet conditions P1, V1 and the same compression ratio:
For the same inlet conditions P1, V1 and the same peak pressure P3
(actual design limitation in engines):