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MARWADI EDUCATION FOUNDATIONS GROUP OF INSTITUTIONS FACULTY OF ENGINEERING, GAURIDAD CAMPUS. DEPARTMENT OF MECHANICAL ENGINEERING Subject / Subject Code Semester / Branch Issue Date Due Date EME / 2110006 2 ND – M.E(FOT) 03/04/2014 05/05/2014 Assignment # 5 1. In an Otto Cycle, air at 15 ° C and 1 bar is compressed adiabatically until the pressure is 15 bar. Heat is added at constant volume until pressure rises to (40+0.5 (roll no.)) bar. Calculate (i) Air standard efficiency (ii) compression ratio and (iii) mean effective pressure for cycle. Assume Cv= 0.718 k J/ Kg K. 2. Explain the essential elements of a Heat Engine. 3. Show that the efficiency of Otto cycle is a function of Compression Ratio only. 4. In air standard Otto Cycle the Maximum and Minimum temperatures are 1673 K and 288 K. The heat supplied per Kg of air is (800+10(roll no.)) KJ. Calculate. (i) The Compression Ratio.(ii) Efficiency. (iii) Max to Min Pressures. Take Cv = 0.718 KJ/Kg K & γ = 1.4 for air. 5. Prove that efficiency of Carnot Engine working between temperature limits T1 and T2 is given by the expression η= (T1- T2)/T1. 6. An air standard diesel cycle has compression ratio of 16. The pressure and temperature at the beginning of compression stroke is 1 bar and 20 °C. The maximum temperature is (1431+5(roll no)) °C. Determine the thermal efficiency and mean effective pressure for this cycle. 7. ‘For the same compression ratio the air standard efficiency of Otto cycle is greater than that of Diesel cycle.’ Justify the statement.

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Transcript of 05heatengine__2014_04_25_11_23_20 (1)

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MARWADI EDUCATION FOUNDATION’S GROUP OF INSTITUTIONS

FACULTY OF ENGINEERING, GAURIDAD CAMPUS.DEPARTMENT OF MECHANICAL ENGINEERING

Subject /Subject Code

Semester /Branch

Issue Date Due Date

EME /2110006

2ND – M.E(FOT) 03/04/2014 05/05/2014

Assignment # 5

1. In an Otto Cycle, air at 15 ° C and 1 bar is compressed adiabatically until the pressure is 15 bar. Heat is added at constant volume until pressure rises to (40+0.5 (roll no.)) bar. Calculate (i) Air standard efficiency (ii) compression ratio and (iii) mean effective pressure for cycle. Assume Cv= 0.718 k J/ Kg K.

2. Explain the essential elements of a Heat Engine.3. Show that the efficiency of Otto cycle is a function of Compression Ratio only. 4. In air standard Otto Cycle the Maximum and Minimum temperatures are 1673 K

and 288 K. The heat supplied per Kg of air is (800+10(roll no.)) KJ. Calculate. (i) The Compression Ratio.(ii) Efficiency. (iii) Max to Min Pressures. Take Cv = 0.718 KJ/Kg K & γ = 1.4 for air.

5. Prove that efficiency of Carnot Engine working between temperature limits T1 and T2 is given by the expression η= (T1- T2)/T1.

6. An air standard diesel cycle has compression ratio of 16. The pressure and temperature at the beginning of compression stroke is 1 bar and 20 °C. The maximum temperature is (1431+5(roll no)) °C. Determine the thermal efficiency and mean effective pressure for this cycle.

7. ‘For the same compression ratio the air standard efficiency of Otto cycle is greater than that of Diesel cycle.’ Justify the statement.

8. Draw P-V diagram for an ideal Diesel cycle and Derive an expression for its air standard efficiency in terms of temperatures only.

9. An engine operating on the ideal Diesel cycle has a maximum pressure of 44 bar and a maximum temperature of (1600+6(roll no))ºC.The pressure and temperature of air at the beginning of the compression stroke are 1 bar and 27 ºC respectively. Find the air standard efficiency of the cycle. For air take ɣ=1.4

10. Explain working of Rankine cycle with P-V diagram. Derive the formula for efficiency of Rankine cycle.

11. In an ideal constant volume cycle the pressure and temperature at the beginning of the compression are 97 kPa and 50 oC respectively. The volume ratio is 5. The heat supplied during the cycle is (930+12(roll no)) kj/kg of working fluid. Calculate : (1) The maximum temperature attained in the cycle. (2) The thermal efficiency of the cycle. (3) Work done during the cycle/kg of working fluid.

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MARWADI EDUCATION FOUNDATION’S GROUP OF INSTITUTIONS

FACULTY OF ENGINEERING, GAURIDAD CAMPUS.DEPARTMENT OF MECHANICAL ENGINEERING

12. An Otto cycle having compression ratio 8 has pressure and temperature at the beginning of compression are 1 bar and 270C respectively. If heat transfer per cycle is (1900+8(roll no.))KJ/Kg, find pressure and temperature at the end of each process. Take CV=0.718 KJ/Kg-K.

13. In an Otto cycle the compression ratio is 8.The temperatures at the beginning of compression and at the end of heat supply are 310 K and (1600+5(roll no.)) K respectively. Assume γ = 1.4 and Cv = 0.717 kJ/kg K . Find :(i) Heat Supplied (ii) Efficiency of the cycle.

14. The compression ratio of an oil engine working on Diesel Cycle is (15+0.3(roll no.)). Cut off takes place at 12 % of the working stroke. The air is drawn in to cylinder at 100 kPa and 270C. Assume Cp=1.006 kJ/kg K and Cv =0.717 kJ/kg K. Calculate: (i) Temperature at the end of compression (ii) Pressure at the end of compression (iii) Air std. efficiency of the cycle.

15. An air at 150 C and 1 bar is compressed adiabatically to 15 bar by an engine working on Otto cycle. The maximum pressure of the cycle is (40+0.4 (roll no.)) bar. Calculate air standard efficiency, mean effective pressure. Take Cv = 0.718 kJ/kg K and R = 0.287 kJ/kg K.

16. A hot air engine works on Carnot cycle with thermal efficiency of 70%.If final temperature of air is (20+roll no.) degree centigrade, determine initial temp.

17. In an ideal diesel cycle the temperature at beginning and at the end of Compression are 57.0 degree centigrade and 603 degree centigrade respectively. The temperatures at beginning and end of expansion are (1950+4(roll no.)) degree centigrade and 870 degree centigrade respectively. Determine the ideal efficiency of the cycle if pressure at beginning is 1.0 bar. Calculate: maximum pressure in the cycle.

18. Derive thermal efficiency formulae for Rankine cycle. 19. Define heat engine. What are the essential requirements of heat engine?

Prof. Ramesh SagapariyaSubject In-Charge,Mechanical Engineering Dept.MEFGI

Prof. Pinank A. PatelHead of Department,

Mechanical Engineering,MEFGI