Thermodynamic Cycles

Similar documents
Unit WorkBook 2 Level 4 ENG U13 Fundamentals of Thermodynamics and Heat Engines UniCourse LTD. All Rights Reserved. Sample

Content. Entropy and principle of increasing entropy. Change of entropy in an ideal gas.

MAE 11. Homework 8: Solutions 11/30/2018

FINAL EXAM. ME 200 Thermodynamics I, Spring 2013 CIRCLE YOUR LECTURE BELOW:

Name: Discussion Section:

Lecture 40: Air standard cycle, internal combustion engines, Otto cycle

9.1 Basic considerations in power cycle analysis. Thermal efficiency of a power cycle : th = Wnet/Qin

Secondary 3H Unit = 1 = 7. Lesson 3.3 Worksheet. Simplify: Lesson 3.6 Worksheet

ME 200 Final Exam December 12, :00 a.m. to 10:00 a.m.

Prof. Dr. Rishi Raj Design of an Impulse Turbine Blades Hasan-1

Lecture 38: Vapor-compression refrigeration systems

Readings for this homework assignment and upcoming lectures

Last Name: First Name: Purdue ID: Please write your name in BLOCK letters. Otherwise Gradescope may not recognize your name.

Lecture 44: Review Thermodynamics I

1. (10) Calorically perfect ideal air at 300 K, 100 kpa, 1000 m/s, is brought to rest isentropically. Determine its final temperature.


Chapter 22 : Electric potential

(1)5. Which of the following equations is always valid for a fixed mass system undergoing an irreversible or reversible process:

R13. II B. Tech I Semester Regular Examinations, Jan THERMODYNAMICS (Com. to ME, AE, AME) PART- A

Work, Energy, and Power. Chapter 6 of Essential University Physics, Richard Wolfson, 3 rd Edition

Chapter 5. Mass and Energy Analysis of Control Volumes. by Asst. Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn

ME 354 THERMODYNAMICS 2 MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number: Instructions

R13 SET - 1 '' ''' '' ' '''' Code No RT21033

OVERVIEW. Air-Standard Power Cycles (open cycle)

Lecture 35: Vapor power systems, Rankine cycle

BME-A PREVIOUS YEAR QUESTIONS

Worksheets for GCSE Mathematics. Algebraic Expressions. Mr Black 's Maths Resources for Teachers GCSE 1-9. Algebra

5/6/ :41 PM. Chapter 6. Using Entropy. Dr. Mohammad Abuhaiba, PE

Teaching schedule *15 18

T222 T194. c Dr. Md. Zahurul Haq (BUET) Gas Power Cycles ME 6101 (2017) 2 / 20 T225 T226

Course: MECH-341 Thermodynamics II Semester: Fall 2006

RETA Book 1 Chapter 1 Fundamental Items

Where F1 is the force and dl1 is the infinitesimal displacement, but F1 = p1a1

Chapter 7. Entropy. by Asst.Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn


I.C. Engine Cycles. Thermodynamic Analysis

UBMCC11 - THERMODYNAMICS. B.E (Marine Engineering) B 16 BASIC CONCEPTS AND FIRST LAW PART- A

THERMODYNAMICS, FLUID AND PLANT PROCESSES. The tutorials are drawn from other subjects so the solutions are identified by the appropriate tutorial.

ERRATA SHEET Thermodynamics: An Engineering Approach 8th Edition Yunus A. Çengel, Michael A. Boles McGraw-Hill, 2015

ME 2322 Thermodynamics I PRE-LECTURE Lesson 23 Complete the items below Name:

(1) Correspondence of the density matrix to traditional method

Refrigeration. 05/04/2011 T.Al-Shemmeri 1

Availability and Irreversibility

Introduction to Thermodynamic Cycles Part 1 1 st Law of Thermodynamics and Gas Power Cycles

Exergy and the Dead State

c Dr. Md. Zahurul Haq (BUET) Thermodynamic Processes & Efficiency ME 6101 (2017) 2 / 25 T145 = Q + W cv + i h 2 = h (V2 1 V 2 2)

CHAPTER 8 THERMODYNAMICS. Common Data For Q. 3 and Q.4. Steam enters an adiabatic turbine operating at steady state with an enthalpy of 3251.

Unit Workbook 2 - Level 5 ENG U64 Thermofluids 2018 UniCourse Ltd. All Rights Reserved. Sample

CHAPTER 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES

I. (20%) Answer the following True (T) or False (F). If false, explain why for full credit.

Exam 2 Fall 2015

+ m B1 = 1. u A1. u B1. - m B1 = V A. /v A = , u B1 + V B. = 5.5 kg => = V tot. Table B.1.

Revision : Thermodynamics

ME Thermodynamics I. Lecture Notes and Example Problems

Spring_#7. Thermodynamics. Youngsuk Nam.

CHAPTER 8 ENTROPY. Blank

First Law of Thermodynamics Closed Systems

In the next lecture...

UNIT I Basic concepts and Work & Heat Transfer

Chapter 7. Entropy: A Measure of Disorder

Applied Thermodynamics. Gas Power Cycles

SCHOOL OF COMPUTING, ENGINEERING AND MATHEMATICS SEMESTER 2 EXAMINATIONS 2014/2015 ME258. Thermodynamics

ME 201 Thermodynamics

To receive full credit all work must be clearly provided. Please use units in all answers.

1. The graph of a function f is given above. Answer the question: a. Find the value(s) of x where f is not differentiable. Ans: x = 4, x = 3, x = 2,

SECOND ENGINEER REG. III/2 APPLIED HEAT

Chemical Engineering Thermodynamics Spring 2002

Analysis (a) Process 1-2: isentropic compression. p = 755K. R7] h87kpa.m 3/kg.K }30~ = O.906m 3/kg = V max

Answers to Practice Test Questions 8 Effect of Temperature on Equilibrium. gas gas

FUNDAMENTALS OF THERMODYNAMICS

Chapter 7. Dr Ali Jawarneh. Department of Mechanical Engineering Hashemite University

ECE309 THERMODYNAMICS & HEAT TRANSFER MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number:

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

CHAPTER 7 ENTROPY. Copyright Hany A. Al-Ansary and S. I. Abdel-Khalik (2014) 1

Chapter 5. Mass and Energy Analysis of Control Volumes

SECTION 7: STEADY-STATE ERROR. ESE 499 Feedback Control Systems

1. INTRODUCTION TO REFRIGERATION AND AIR CONDITION

This follows from the Clausius inequality as a consequence of the second law of thermodynamics. Therefore. (for reversible process only) (22.

10. Heat devices: heat engines and refrigerators (Hiroshi Matsuoka)

Worksheets for GCSE Mathematics. Quadratics. mr-mathematics.com Maths Resources for Teachers. Algebra

SHRI RAMSWAROOP MEMORIAL COLLEGE OF ENGG. & MANAGEMENT

MAE 320 HW 7B. 1e. For an isolated system, please circle the parameter which will change with time. (a) Total energy;

20 m neon m propane. g 20. Problems with solutions:

1 st Law Analysis of Control Volume (open system) Chapter 6

The First Law of Thermodynamics. By: Yidnekachew Messele

ME 200 Final Exam December 14, :00 a.m. to 10:00 a.m.

Engineering Fundamentals- Thermodynamics. By Professor Paul A. Erickson

Name: I have observed the honor code and have neither given nor received aid on this exam.

Thermodynamics Lecture Series

MAHALAKSHMI ENGINEERING COLLEGE

Excercise: Steam superheating

8.21 The Physics of Energy Fall 2009

THE VAPOR COMPRESSION REFRIGERATION PROCESS

ME6301- ENGINEERING THERMODYNAMICS UNIT I BASIC CONCEPT AND FIRST LAW PART-A

Existing Resources: Supplemental/reference for students with thermodynamics background and interests:

SEM-2017(03HI MECHANICAL ENGINEERING. Paper II. Please read each of the following instructions carefully before attempting questions.

Unit D-2: List of Subjects

first law of ThermodyNamics

Q. 1 Q. 25 carry one mark each.

SECTION 4: ULTRACAPACITORS. ESE 471 Energy Storage Systems

Transcription:

Thermodynamic Cycles

Content Thermodynamic Cycles Carnot Cycle Otto Cycle Rankine Cycle Refrigeration Cycle

Thermodynamic Cycles

Carnot Cycle

Derivation of the Carnot Cycle Efficiency

Otto Cycle

Otto Cycle Nomenclature for reciprocating engines TDC Top Dead Center BDC Bottom Dead Center

Otto Cycle

Otto Cycle

Otto Cycle

Otto Cycle kaire = 1.4; kco2 = 1.3; ketano = 1.667

Constant Specific Heat Otto Cycle Data: rr = vv 1 vv 2 PP 1 kpa TT 1 K qq in kj/kg RR Table A1 cc vv, kk Table A2a vv 1 = RRTT 1 PP 1

Constant Specific Heat Process 11 22 Isentropic compression Otto Cycle kk 1 kk vv 2 = vv 1 rr ; PP 2 = PP 1 rr kk PP 2 ; TT 2 = TT 1 PP 1 Process 22 33 Constant-volume heat addition oooo TT 2 = PP 2vv 2 RR vv 3 = vv 2 ; TT 3 = TT 2 + qq in TT 3 ; PP cc 3 = PP 2 vv TT 2 Process 33 44 Isentropic expansion qq in = uu = cc vv (TT 3 TT 2 ) vv 4 = vv 1 ; PP 4 = PP 3 rr kk ; TT 4 = TT 3 rr kk 1

Constant Specific Heat Otto Cycle Process 44 11 Constant-volume heat rejection qq out = cc vv (TT 4 TT 1 ) ww net = qq net = qq in qq out ηη th = ww net qq in ηη otto = 1 rr 1 kk MEP = ww nnnnnn vv 1 vv 2

Variable Specific Heat Otto Cycle Data: rr = vv 1 vv 2 PP 1 kpa TT 1 K qq in kj/kg @TT 1 (Table A17) vv rrr uu 1 RR Table A1

Variable Specific Heat Process 11 22 Isentropic compression Otto Cycle vv rrr = vv rrr rr ; @vv rrr Table A17 TT 2 uu 2 ; PP 2 = PP 1 TT 2 TT 1 rr Process 22 33 Constant-volume heat addition uu 3 = qq in +uu 2 ; @uu 3 (Table A17) TT 3 vv rrr ; PP 3 = PP 2 TT 3 TT 2 Process 33 44 Isentropic expansion vv rrr = rrrr rrr ; @vv rrr (Table A17) TT 4 TT 4 1 ; PP uu 4 = PP 3 4 TT 3 rr qq in = uu = uu 3 uu 2

Variable Specific Heat Otto Cycle Process 44 11 Constant-volume heat rejection qq out = (uu 4 uu 1 ) ww net = qq net = qq in qq out ηη th = ww net qq in ηη otto = 1 rr 1 kk vv 1 = RRTT 1 PP 1 MEP = vv 1 ww nnnnnn 1 1 rr

Example (textbook) EXAMPLE 9 2 The Ideal Otto Cycle An ideal Otto cycle has a compression ratio of 8. At the beginning of the compression process, air is at 100 kpa and 17 C, and 800 kj/kg of heat is transferred to air during the constant-volume heat-addition process. Find the thermal efficiency, and the mean effective pressure for the cycle, (a) considering constant specific heat, (b) considering variable specific heat, (c) Also, determine the power output from the cycle, in kw, for an engine speed of 4000 rpm (rev/min). Assume that this cycle is operated on an engine that has four cylinders with a total displacement volume of 1.6 L.

Example (textbook) a) Constant Specific Heat Data: rr = 8, PP 1 = 100 kpa, TT 1 = 17 C = 290 K, qq in = 800 kj/kg RR = 0.287 kpa m 3 /kgk (Table A1) cc vv = 0.718 kj/kgk, kk = 1.4 (Table A2a) vv 1 = RRTT 1 = (0.287 KPam3 /kgk)(290 K) PP 1 100 kpa Process 11 22 Isentropic compression vv 2 = vv 1 rr = 0.8323 m3 /kg = 0.10404 m 8 3 /kg PP 2 = PP 1 rr kk = 100 kpa 8 1.4 = 11111111. 9999 kkkkkk = 0.8323 m 3 /kg

Example (textbook) TT 2 = PP 2vv 2 RR = (1837.92 kpa)(0.10404 m3 /kg) 0.287 kpa m 3 /kgk = 666666 KK Process 22 33 Constant-volume heat addition vv 3 = vv 2 = 0.10404 m 3 /kg TT 3 = TT 2 + qq in 800 kj/kg = 666 K + = 11111111. 22 KK cc vv 0.718 kj/kgk PP 3 = PP 2 TT 3 TT 2 = 1837.92 kpa 1780.2 K 666 K = 44444444. 7777 kkkkkk

Example (textbook) Process 33 44 Isentropic expansion vv 4 = vv 1 = 0.8323 m 3 /kg PP 4 = PP 3 4912.71 kpa = rrkk (8) 1.4 = 222222. 33 kkkkkk TT 4 = TT 3 1780.2 K = = 777777. 8888 KK rrkk 1 (8) 1.4 1 Process 44 11 Constant-volume heat rejection qq out = cc vv TT 4 TT 1 = 0.718 kj/kgk 774.88 290 K = 333333. 1111 kkkk/kkkk

Example (textbook) ww net = qq net = qq in qq out = 800 348.14 kj/kg = 444444. 8888 kkkk/kkkk ηη th = ww net qq in = 451.86 kj/kg 800 kj/kg = 00. 55555555 = 5555. 4444 % ηη otto = 1 rr 1 kk = 1 8 1 1.4 = 00. 55555555 = 5555. 4444 % MEP = ww nnnnnn vv 1 vv 2 = 451.86 kj/kg 0.8323 0.10404 m 3 /kg 1 kpa m 3 /kg 1 kj = 666666. 4444 kkkkkk

Example (textbook) b) Variable Specific Heat Data: rr = 8, PP 1 = 100 kpa, TT 1 = 17 C = 290 K, qq in = 800 kj/kg RR = 0.287 kpa m 3 /kgk (Table A1) @TT 1 (Table A17) vv rrr = 676.1 uu 1 = 206.91 kj/kg Process 11 22 Isentropic compression vv rrr = vv rrr rr = 676.1 = 84.51 8 @vv rrr Table A17 TT 2 = 666666. 44 KK uu 2 = 475.11 kj/kg

Example (textbook) PP 2 = PP 1 TT 2 TT 1 rr = 100 kpa 652.4 K 290 K 8 = 11111111. 77 kkkkkk Process 22 33 Constant-volume heat addition uu 3 = qq in + uu 2 = 800 + 475.11 kj/kg = 1275.11 kj/kg @uu 3 (Table A17) TT 3 = 11111111. 11 KK vv rrr = 6.108 PP 3 = PP 2 TT 3 TT 2 = 1799.7 kpa 1575.1 K 652.4 K = 44444444 kkkkkk

Example (textbook) Process 33 44 Isentropic expansion vv rrr = rrrr rrr = 8 6.108 = 48.864 @vv rrr (Table A17) TT 4 = 777777. 66 KK uu 4 = 588.74 kj/kg TT 4 1 PP 4 = PP 3 TT 3 rr = 4345 kpa 795.6 K 1575.1 K 1 8 = 222222. 3333 kkkkkk Process 44 11 Constant-volume heat rejection qq out = (uu 4 uu 1 ) = (588.74 206.91)kJ/kg = 333333. 8888 kkkk/kkkk

Example (textbook) ww net = qq net = qq in qq out = 800 381.83 kj/kg = 444444. 1111 kkkk/kkkk ηη th = ww net qq in = 418.17 kj/kg 800 kj/kg = 00. 555555 = 5555. 33 % ηη otto = 1 rr 1 kk = 1 8 1 1.4 = 00. 55555555 = 5555. 4444 % vv 1 = RRTT 1 = (0.287 kpa m3 /kg)(290 K) PP 1 100 kpa = 0.8323 m 3 /kg MEP = vv 1 ww nnnnnn 1 1 rr = 418.17 kj/kg (0.8323 m 3 /kg) 1 1 8 1 kpa m 3 /kg 1 kj = 555555 kkkkkk

Example (textbook) c) Data: nn = 4000 rpm, 4 cylinders, VV dd = 1.6 L = 0.0016 m3, WW net =? (kw) WW net = mmww netnn nn rev mm = VV dd vv 1 = 0.0016 m3 0.8323 m 3 /kg = 0.001922 kg For a four-stroke engine nn rev = 2 rev/cycle (for Ideal Otto cycle nn rev = 1 rev/cycle) WW net = (0.001922 kg)(418.17 kj/kg)(4000 rev/min) 2 rev/cycle 1 min 60 s = 2222. 88 kkkk

Carnot Vapor Cycle

Rankine Cycle

Rankine Cycle qq iiii qq oooooo + ww iiii ww oooooo = h ee h ii Pump qq = 0 : ww pppppppp,iiii = h 2 h 1 = vv pp 2 pp 1 h 1 = h fffpp1 ; vv vv 1 = vv fffpp1 Boiler (ww = 0): qq 1 = h 3 h 2 Turbine (qq = 0): ww tttttttt,oooooo = h 3 h 4 Condenser ww = 0 : qq oooooo = h 4 h 1 ww nnnnnn = qq iiii qq oooooo = ww tttttttt,oooooo ww tttttttt,iiii ηη tt = ww nnnnnn qq iiii = 1 qq oooooo qq iiii

Rankine Cycle

Rankine Cycle The simple ideal Rankine cycle Data: PP 3 kpa TT 3 K PP 4 kpa Process 1 2 Isentropic compression in a pump Process 2 3 Constant pressure heat addition in a boiler Process 3 4 Isentropic expansion in a turbine Process 4 1 Constant pressure heat rejection in a condenser

Rankine Cycle Stage 1 @PP 1 = PP 4 Stage 2 Table A5 h 1 = h ff vv 1 = vv ff PP 2 = PP 3 ww pump,in = vv 1 (PP 2 PP 1 ) ss 2 = ss 1 h 2 = h 1 + ww pump,in

Rankine Cycle Stage 3 @PP 3, TT 3 Table A6 h 3 ss 3 Stage 4 ss 4 = ss 3 If @PP 4 Table A5, ss ff < ss 4 < ss gg, then: xx 4 = ss 4 ss ff ss ffff h 4 = h ff + xx 4 h ffff

Rankine Cycle qq in = h 3 h 2 qq out = h 4 h 1 ww turb,out = h 3 h 4 ww net = ww turb,out ww pump,in = qq in qq out ηη th = 1 qq out qq in = ww net qq in

Examples (textbook) EXAMPLE 10 1 The Simple Ideal Rankine Cycle Consider a steam power plant operating on the simple ideal Rankine cycle. Steam enters the turbine at 3 MPa and 350 C and is condensed in the condenser at a pressure of 75 kpa. Determine the thermal efficiency of this cycle. Data: PP 3 = 3 MPa, TT 3 = 350 C, PP 4 = 75kPa, ηη th =? Stage 1 @PP 1 = PP 4 = 75 kpa Table A5 h 1 = h ff = 333333. 4444 kkkk/kkkk vv 1 = vv ff = 0.001037 m 3 /kg

Examples (textbook) Stage 2 PP 2 = PP 3 = 3 MPa ww pump,in = vv 1 PP 2 PP 1 = 0.001037 m 3 /kg 3000 75 kpa 1 kj 1 kpa m 3 /kg = 33. 0000 kkkk/kkkk h 2 = h 1 + ww pump,in = 384.44 + 3.03 kj/kg = 333333. 4444 kkkk/kkkk Stage 3 @PP 3 = 3 MPa, TT 3 = 350 C Table A6 h 3 = 33333333. 11 kkkk/kkkk ss 3 = 6.7450 kj/kgk

Examples (textbook) Stage 4 ss 4 = ss 3 = 6.7450 kj/kgk @PP 4 = 75 kpa Table A5 ss ff = 1.2132 kj/kgk ss gg = 7.4558 kj/kgk, ss gg < ss 4 < ss ff, h ff = 384.44 kj/kg h ffff = 2278.0 kj/kg xx 4 = ss 4 ss ff ss ffff = 6.7450 1.2132 7.4558 1.2132 = 0.8861 h 4 = h ff + xx 4 h ffff = 384.44 kj/kg + 0.8861 2278.0 kj/kg = 22222222. 00 kkkk/kkkk

Examples (textbook) qq in = h 3 h 2 = 3116.1 387.47 kj/kg = 22222222. 66 kkkk/kkkk qq out = h 4 h 1 = 2403.0 384.44 kj/kg = 22222222. 66 kkkk/kkkk ww turb,out = h 3 h 4 = 3116.1 2403.0 kj/kg = 777777. 11 kkkk/kkkk ww net = ww turb,out ww pump,in = 713.1 303 kj/kg = 777777. 11 kkkk/kkkk = qq in qq out = 2728.6 2018.6 kj/kg = 777777. 00 kkkk/kkkk ηη th = 1 qq out 2018.6 kj/kg = 1 = 00. 222222 = 2222. 00 % qq in 2728.6 kj/kg = ww net 710.0 kj/kg = = 00. 222222 = 2222. 00 % qq in 2728.6 kj/kg

Examples (textbook) EXAMPLE 10 2 An Actual Steam Power Cycle A steam power plant operates on the cycle shown in Figure. If the isentropic efficiency of the turbine is 87 percent and the isentropic efficiency of the pump is 85 percent, determine (a) the thermal efficiency of the cycle and (b) the net power output of the plant for a mass flow rate of 15 kg/s.

Examples (textbook) a) ηη th =? ηη th = ww net qq in ww nnnnnn = ww turb,out ww pump,in ww turb,out = ηη TT ww ss,turb,out = ηη TT (h 5 h 6ss ) = 0.87 3583.1 2115.3 kj/kg = 11111111. 00 kkkk/kkkk ww pump,in = ww ss,pump,in = vv 1(PP 2 PP 1 ) = 0.001009 m3 /kg 16000 9 kpa ηη PP ηη PP 0.85 1 kj 1 kpam 3 = 1111. 00 kkkk/kkkk

Examples (textbook) qq in = h 4 h 3 = 3647.6 160.1 kj/kg = 33333333. 55 kkkk/kkkk ww net = ww turb,out ww pump,in = 1277.0 19.0 kj/kg = 11111111. 00 kkkk/kkkk ηη th = ww net qq in = 1258.0 kj/kg 3487.5 kj/kg = 00. 333333 = 3333. 11 % b) WW net =? WW net = mmww net = 15 kg/s 1258.0 kj/kg = 1111. 99 MMMM

Refrigeration

Coefficient of Performance Refrigeration Heat Pump CCCCCC RR = CCCCCC HHHH = CCCCCC HHHH = CCCCCC RR + 1 CCCCCC RR,CCCCCCCCCCCC = 1 TT HH TTLL 1 QQ LL WW nnnnnn,iiii QQ HH WW nnnnnn,iiii ; CCCCCC HHHH,CCCCCCCCCCCC = 1 1 TT LL TT HH

Carnot Refrigerator

Refrigerator Cycle

Refrigerator Cycle

Refrigerator Cycle

Refrigerator Cycle The Ideal Vapor-Compression Refrigeration Cycle Data: PP 1 = PP 4 = PP LL kpa PP 2 = PP 3 = PP HH kpa Process 1 2 Isentropic compression in a compressor Process 2 3 Constant pressure heat rejection in a condenser Process 3 4 Throttling in a expansion device Process 4 1 Constant pressure heat absorption in an evaporator

Refrigerator Cycle Stage 1 @PP 1 = PP LL Table A12 h 1 = h gg ss 1 = ss gg Stage 2 @PP 2 = PP HH, ss 2 = ss 1, Table A13 h 2 Stage 3 @PP 3 = PP HH, Table A12 h 3 = h ff Stage 4 h 4 h 3

Refrigerator Cycle QQ LL = WW in = QQ HH = mm(h 1 h 4 ) mm(h 2 h 1 ) mm h 2 h 3 = QQ LL + WW in COP R = QQ LL WW in

Example (textbook) EXAMPLE 11 1 The Ideal Vapor-Compression Refrigeration Cycle A refrigerator uses refrigerant-134a as the working fluid and operates on an ideal vapor-compression refrigeration cycle between 0.14 and 0.8 MPa. If the mass flow rate of the refrigerant is 0.05 kg/s, determine (a) the rate of heat removal from the refrigerated space and the power input to the compressor, (b) the rate of heat rejection to the environment, and (c) the COP of the refrigerator. Data: PP 1 = PP 4 = 0.14 MPa PP 2 = PP 3 = 0.8 Mpa mm = 0.05 kg/s

Example (textbook) a) QQ LL =?, WW in =? QQ LL = mm(h 1 h 4 ) WW in = mm(h 2 h 1 ) @PP 1 = PP LL = 0.14 MPa Table A12 h 1 = h gg = 222222. 1111 kkkk/kkkk ss 1 = ss gg = 0.94467 kj/kgk @PP 2 = PP HH = 0.8 MPa, ss 2 = ss 1, Table A13 {h 2 = 222222. 4444 kkkk/kkkk @PP 3 = PP HH = 0.8 MPa, Table A12 h 3 = h ff = 9999. 4444 kkkk/kkkk h 4 h 3 = 9999. 4444 kkkk/kkkk QQ LL = 0.05 kg/s WW in = 0.05 kg/s 239.19 95.48 kj/kg = 77. 1111 kkkk 275.40 239.19 kj/kg = 11. 8888 kkkk

Example (textbook) b) QQ HH =? QQ HH = mm h 2 h 3 = 0.05 kg/s 275.40 95.48 kj/kg = 99. 0000 kkkk = QQ LL + WW in = 7.19 kw + 1.81 kw = 99. 0000 kkkk c) COP R =? QQ COP R = LL = WW in 7.19 kw 1.81 kw = 33. 9999

Homework 4c Problems from the textbook (Thermodynamics, Yunus, 8th ed.): Choose 5 conceptual problems and answer them (those who you consider to provide better understanding to the subject seen in this section) Chapter 9, problems: 1-10, 23-30 Chapter 10, problems: 1, 6, 7 Chapter 11, problems: 1, 2, 5-10 Choose 5 problems and answer them (those who you consider to provide better understanding to the subject seen in this section) Chapter 9, problems: 11-22, 31-41 Chapter 10, problems: 2-5, -26 Chapter 11, problems: 3, 4, 11-23

Thermodynamic Cycles