Equations. P v2

Similar documents
Equations P Se va nota cu y fractia din debitul masic care intra in turbina care e extrasa din turbina pentru preincalzitorul inchis

$IfNot ParametricTable= P_ratio_gas. P ratio,gas = 14; Raport comprimare compresor aer - Pressure ratio for gas compressor (2) $EndIf

Equations P $UnitSystem K kpa. F luid$ = Air (1) Input data for fluid. $If Fluid$= Air. C P = [kj/kg K] ; k = 1.

Department of Mechanical Engineering ME 322 Mechanical Engineering Thermodynamics. Lecture 26. Use of Regeneration in Vapor Power Cycles

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

III. Evaluating Properties. III. Evaluating Properties

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

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

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

Thermodynamic Cycles

Availability and Irreversibility

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

Readings for this homework assignment and upcoming lectures

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

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)

Lecture 38: Vapor-compression refrigeration systems

Lecture 35: Vapor power systems, Rankine cycle

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

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

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

+ 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.

The exergy of asystemis the maximum useful work possible during a process that brings the system into equilibrium with aheat reservoir. (4.

CHAPTER 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES

Chapter 3 PROPERTIES OF PURE SUBSTANCES. Thermodynamics: An Engineering Approach, 6 th Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2008

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

ME Thermodynamics I. Lecture Notes and Example Problems

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

ME Thermodynamics I

Course: MECH-341 Thermodynamics II Semester: Fall 2006

ECE309 INTRODUCTION TO THERMODYNAMICS & HEAT TRANSFER. 13 June 2007

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

ME 201 Thermodynamics

A Simple Introduction to EES Version (Handout version 5.1) Copyright C. S. Tritt, Ph.D. September 20, 2005

Chemical Engineering Thermodynamics Spring 2002

ME 300 Thermodynamics II Spring 2015 Exam 3. Son Jain Lucht 8:30AM 11:30AM 2:30PM

Chapter 3 PROPERTIES OF PURE SUBSTANCES

Basic Thermodynamics Cycle analysis

Zittau/Goerlitz University of Applied Sciences Department of Technical Thermodynamics Germany. K. Knobloch, H.-J. Kretzschmar, K. Miyagawa, W.

first law of ThermodyNamics

Chapter 7. Entropy: A Measure of Disorder

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

Brown Hills College of Engineering & Technology

10 minutes reading time is allowed for this paper.

THERMODYNAMICS (Date of document: 8 th March 2016)

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

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

Fundamentals of Thermodynamics. Chapter 8. Exergy

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

25. Water Module. HSC 8 - Water November 19, Research Center, Pori / Petri Kobylin, Peter Björklund ORC-J 1 (13)

Consequences of Second Law of Thermodynamics. Entropy. Clausius Inequity

LAKEHEAD UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING MECHANICAL ENGINEERING LABORATORY ENGI-3555 WD LAB MANUAL LAB COORDINATOR: Dr.

ECE309 INTRODUCTION TO THERMODYNAMICS & HEAT TRANSFER. 20 June 2005

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

Excercise: Steam superheating

Consequences of Second Law of Thermodynamics. Entropy. Clausius Inequity

Thermodynamics I Spring 1432/1433H (2011/2012H) Saturday, Wednesday 8:00am - 10:00am & Monday 8:00am - 9:00am MEP 261 Class ZA

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

Chapter 3 PROPERTIES OF PURE SUBSTANCES

FUNDAMENTALS OF THERMODYNAMICS

Chapter 5. Mass and Energy Analysis of Control Volumes

ME 201 Thermodynamics

Hours / 100 Marks Seat No.

c Dr. Md. Zahurul Haq (BUET) Entropy ME 203 (2017) 2 / 27 T037

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

SPC 407 Sheet 5 - Solution Compressible Flow Rayleigh Flow

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


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

A MathCAD Function Set for Solving Thermodynamics Problems

Course: TDEC202 (Energy II) dflwww.ece.drexel.edu/tdec

ECE309 INTRODUCTION TO THERMODYNAMICS & HEAT TRANSFER. 12 June 2006

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

Lecture 44: Review Thermodynamics I

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

Find: a) Mass of the air, in kg, b) final temperature of the air, in K, and c) amount of entropy produced, in kj/k.

Thermodynamics: An Engineering Approach Seventh Edition in SI Units Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2011.

PROPERTIES OF PURE SUBSTANCES. Chapter 3. Mehmet Kanoglu. Thermodynamics: An Engineering Approach, 6 th Edition. Yunus A. Cengel, Michael A.

Thermodynamics Lecture Series

ME 022: Thermodynamics

Dishwasher. Heater. Homework Solutions ME Thermodynamics I Spring HW-1 (25 points)

Outline. Example. Solution. Property evaluation examples Specific heat Internal energy, enthalpy, and specific heats of solids and liquids Examples

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

Theoretical & Derivation based Questions and Answer. Unit Derive the condition for exact differentials. Solution:

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

Scheme G. Sample Test Paper-I

T718. c Dr. Md. Zahurul Haq (BUET) HX: Energy Balance and LMTD ME 307 (2018) 2/ 21 T793

Teaching schedule *15 18

( ) Given: In a constant pressure combustor. C4H10 and theoretical air burns at P1 = 0.2 MPa, T1 = 600K. Products exit at P2 = 0.

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

THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES

Previous lecture. Today lecture

Chapter 2: The Physical Properties of Pure Compounds

ENT 254: Applied Thermodynamics

ME 201 Thermodynamics

ME 201 Thermodynamics

MAE 320 THERODYNAMICS FINAL EXAM - Practice. Name: You are allowed three sheets of notes.

In the next lecture...

Thermodynamics: An Engineering Approach Seventh Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, Chapter 7 ENTROPY

Entropy and the Second Law of Thermodynamics

Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. hl = IOkPa = 191.

Transcription:

P10-108-v2 Equations Thermodynamics - An Engineering Approach (5th Ed) - Cengel, Boles - Mcgraw-Hill (2006) - pg. 602 Problem 10.108 (9-96) Effect of Number of Reheat Stages on Rankine Cycle Using EES (or other) software, investigate the effect of number of reheat stages on the performance of an ideal reheat Rankine cycle. The maximum and minimum pressures in the cycle are 15 MPa and 10 kpa, respectively, and steam enters all stages of the turbine at 500 C. The minimum For each case, maintain roughly the same pressure ratio across each turbine stage. Determine the thermal efficiency of the cycle and plot it against the number of reheat stages 1, 2, 4, and 8, and discuss the results. Let s modify this problem to include the effects of the turbine and pump efficiencies and also show the effects of reheat on the steam quality at the low pressure turbine exit. See Prob. 9-28 for a diagram window input version of this problem. $UnitSystem C kpa function x$(x) Functia intoarce un sir de caractere care indica starea vaporilor - this function returns a string t x$ = Vapori umezi ; (2) If(x > 1) then x$ = Abur supraincalzit ; (3) 1

If(x < 0) then x$ = Lichid subracit ; (4) end (5) procedure Reheat(NoRHStages : Q in,reheat, W t,lp, s5, h6) (6) $Common P_ratio,Eta_t,P[4],h[4],T[3],T[5] h4 1 = h 4 ; P 3 1 = P 4 ; T 3 1 = T 5 ; (7) Q in,reheat = 0; W t,lp = 0; P ratio,rh = (1/P ratio ) i max = NoRHStages 1; i = 0; repeat i = i + 1 [3] 1 NoRHStages+1 ; (8) (9) (10) (11) (12) (13) (14) h3 i = h (ST EAM, T = T 3 i, P = P 3 i ) ; s3 i = s (ST EAM, T = T 3 i, P = P 3 i ) ; (15) Q in,i = h3 i h4 i ; Q in,reheat = Q in,reheat + Q in,i ; [4s] (16) (17) (18) P 4 i+1 = P 3 i P ratio,rh ; s s4,i+1 = s3 i ; (19) h s4,i+1 = h (ST EAM, s = s s4,i+1, P = P 4 i+1 ) ; (20) T s4,i+1 = T (ST EAM, s = s s4,i+1, P = P 4 i+1 ) ; (21) [4] -iesire (22) h4 i+1 = h3 i η t (h3 i h s4,i+1 ) ; Randamentul turbinei - Definition of turbine efficiency(23) T 4 i+1 = T (ST EAM, P = P 4 i+1, h = h4 i+1 ) ; (24) s4 i+1 = s (ST EAM, P = P 4 i+1, h = h4 i+1 ) ; v4 i+1 = v (ST EAM, P = P 4 i+1, s = s4 i+1 ) ; (25) 2

x4 i+1 = x (ST EAM, P = P 4 i+1, h = h4 i+1 ) ; x4$ i+1 = x$(x4 i+1 ); x[4] tb > 1? (26) W t,i = h3 i h4 i+1 ; SSSF First Law for the turbine (27) W t,lp = W t,lp + W t,i ; SSSF First Law for the turbine (28) P 3 i+1 = P 4 i+1 ; Conditii initiale pentru treapta urmatoare (29) T 3 i+1 = T 5 ; until (i > i max ) s5 = s3 i ; h6 = h4 i+1 ; end (30) (31) (32) (33) Marimi de intrare NoRHStages = 2; (34) P 6 = 10 [kpa] ; P 3 = 15000 [kpa] ; (35) T 3 = 500 [C] ; T 5 = T 3 ; (36) η t = 1.0; Turbine isentropic efficiency (37) η p = 1.0; Pump isentropic efficiency (38) P extract = P 6 Presiunea de reincalzire minima - Select a lower limit on the reheat pressure (39) Calcul P ratio = P 3 P extract ; (40) Pompa - Pump analysis [1] (41) P 1 = P 6 ; x 1 = 0 Sat d liquid (42) h 1 = h (ST EAM, P = P 1, x = x 1 ) ; T 1 = T (ST EAM, P = P 1, x = x 1 ) ; (43) v 1 = v (ST EAM, P = P 1, x = x 1 ) ; s 1 = s (ST EAM, P = P 1, x = x 1 ) ; (44) [2] (45) 3

P 2 = P 3 ; (46) W p,s = v 1 (P 2 P 1 ) ; SSSF isentropic pump work assuming constant specific volume (47) W p = W p,s /η p ; (48) h 2 = h 1 + W p ; SSSF First Law for the pump (49) v 2 = v (ST EAM, P = P 2, h = h 2 ) ; s 2 = s (ST EAM, P = P 2, h = h 2 ) ; (50) T 2 = T (ST EAM, P = P 2, h = h 2 ) ; (51) Turbina de inalta presiune - High Pressure Turbine analysis [3] (52) h 3 = h (ST EAM, T = T 3, P = P 3 ) ; (53) s 3 = s (ST EAM, T = T 3, P = P 3 ) ; v 3 = v (ST EAM, T = T 3, P = P 3 ) ; (54) P extract,min = P (ST EAM, s = s 3, x = 1) ; (55) [4s] (56) s s,4 = s 3 ; (57) h s,4 = h (ST EAM, s = s s,4, P = P 4 ) ; T s,4 = T (ST EAM, s = s s,4, P = P 4 ) ; (58) [4] (59) P 4 = P 3 (1/P ratio ) 1 NoRHStages+1 ; (60) η t = h 3 h 4 h 3 h s,4 ; Randamentul turbinei - Definition of turbine efficiency (61) T 4 = T (ST EAM, P = P 4, h = h 4 ) ; s 4 = s (ST EAM, P = P 4, h = h 4 ) ; (62) v 4 = v (ST EAM, P = P 4, s = s 4 ) ; x 4 = x (ST EAM, P = P 4, h = h 4 ) ; x4$ = x$(x 4 ); x[4] tb > 1 h 3 = W t,hp + h 4 ; SSSF First Law for the high pressure turbine (64) Turbina de joasa presiune - Low Pressure Turbine analysis call Reheat(NoRHStages : Q in,reheat, W t,lp, s 5, h 6 ); (65) 4

Generatorul de abur - Boiler analysis Q in,boiler + h 2 = h 3 SSSF First Law for the Boiler (66) Q in = Q in,boiler + Q in,reheat ; (67) Condensatorul - Condenser analysis [6] (68) h 6 = Q out + h 1 SSSF First Law for the Condenser (69) T 6 = T ( steam, h = h 6, P = P 6 ) ; (70) s 6 = s ( steam, h = h 6, P = P 6 ) ; x 6 = x (ST EAM, h = h 6, P = P 6 ) ; (71) x6s$ = x$(x 6 ); (72) Ciclul - Cycle Statistics W t = W t,hp + W t,lp ; W net = W t W p ; η th = W net /Q in ; (73) (74) (75) Solution Variables in Main program η p = 1 η t = 1 η th = 0.4206 NoRHStages = 2 P extract = 10 [kpa] P extract,min = 1969 [kpa] P ratio = 1500 Q in = 4534 [kj/kg] Q in,boiler = 3102 [kj/kg] Q in,reheat = 1432 [kj/kg] Q out = 2627 [kj/kg] W net = 1907 [kj/kg] W p = 15.14 [kj/kg] W p,s = 15.14 [kj/kg] W t = 1922 [kj/kg] W t,hp = 590.2 [kj/kg] W t,lp = 1332 [kj/kg] x4$ = Vapori umezi x6s$ = Abur supraincalzit Variables in Procedure Reheat NoRHStages = 2 Q in,reheat = 1432 [kj/kg] W t,lp = 1332 [kj/kg] s5 = 8.772 [kj/kg-k] h6 = 2819 [kj/kg] P RAT IO = 1500 η T = 1 P [4] = 1310 [kpa] H[4] = 2719 [kj/kg] T [3] = 500 [C] T [5] = 500 [C] h4[1] = 2719 [kj/kg] P 3[1] = 1310 [kpa] T 3[1] = 500 [C] P ratio,rh = 0.08736 i max = 1 i = 2 P RAT IO = 1500 η T = 1 P [4] = 1310 [kpa] H[4] = 2719 [kj/kg] T [3] = 500 [C] T [5] = 500 [C] H3[1] = 3475 [kj/kg] S3[1] = 7.634 [kj/kg-k] Q IN,1 = 756.1 [kj/kg] P 4[2] = 114.5 [kpa] S S4,2 = 7.634 [kj/kg-k] H S4,2 = 2812 [kj/kg] T S4,2 = 168.7 [C] H4[2] = 2812 [kj/kg] T 4[2] = 168.7 [C] 5

S4[2] = 7.634 [kj/kg-k] V 4[2] = 1.767 [m 3 /kg] X4[2] = 100 X4$[2] = Abursupraincalzit W T,1 = 663.2 [kj/kg] P 3[2] = 114.5 [kpa] T 3[2] = 500 [C] H3[2] = 3488 [kj/kg] S3[2] = 8.772 [kj/kg-k] Q IN,2 = 676 [kj/kg] P 4[3] = 10 [kpa] S S4,3 = 8.772 [kj/kg-k] H S4,3 = 2819 [kj/kg] T S4,3 = 169 [C] H4[3] = 2819 [kj/kg] T 4[3] = 169 [C] S4[3] = 8.772 [kj/kg-k] V 4[3] = 20.39 [m 3 /kg] X4[3] = 100 X4$[3] = Abursupraincalzit W T,2 = 669 [kj/kg] P 3[3] = 10 [kpa] T 3[3] = 500 [C] Arrays Row P i T s,i T i s s,i s i h s,i h i v i x i [kpa] [C] [C] [kj/kg-c] [kj/kg-c] [kj/kg] [kj/kg] [m 3 /kg] 1 10 45.79 0.6489 191.7 0.00101 0 2 15000 46.3 0.649 206.9 0.001004 3 15000 500 6.345 3309 0.0208 4 1310 192 192 6.345 6.345 2719 2719 0.1449 0.9654 5 500 8.772 6 10 169 8.772 2819 100 NoRHStages Run NoRHStages Q in W net η th [kj/kg] [kj/kg] 1 1 4084 1673 0.4097 2 2 4534 1907 0.4206 3 3 4812 2050 0.4261 4 4 4994 2143 0.429 5 5 5122 2206 0.4307 6 6 5217 2253 0.4318 7 7 5291 2289 0.4326 8 8 5349 2317 0.4332 9 9 5396 2339 0.4336 10 10 5435 2358 0.4339 6

T-s: Steam 7

Thermal Efficiency vs Number of Reheat Stages 8

Q in, W net vs Number of Reheat Stages 9