IC Engines & Gas Turbines Flashcards

Academic Standards and Course Overview

  • Program and Regulation: R22 B.Tech. Mechanical Engineering syllabus.
  • Course Title: IC ENGINES & GAS TURBINES.
  • Academic Level: B.Tech. II Year II Semester.
  • Institution: JNTUH Hyderabad.
  • Course Credits and Teaching Schedule:
    • Lectures (LL): 3
    • Tutorials (TT): 0
    • Practical (PP): 0
    • Credits (CC): 3
  • Pre-requisite Knowledge: Proficiency in Thermodynamics is required prior to this course.

Course Objectives

  • Component Understanding: To provide a comprehensive explanation of the components and systems that constitute Internal Combustion (IC) Engines.
  • Combustion Analysis: To analyze the various stages of combustion to enhance IC engine performance, specifically focusing on fuel economy and the control of emissions within global, environmental, and social contexts.
  • Performance Evaluation: To facilitate the understanding and evaluation of performance analysis for major IC engine systems and their practical applications.
  • Compressor Explorations: To explore the mechanical components and working principles of various compressors including rotary, reciprocating, dynamic, and axial types.
  • Gas Turbine Significance: To establish the significance of gas turbines in the modern context of power generation.

Course Outcomes

Upon successful completion of the course, students will be able to:

  • Working Principles: Elaborate on the working principles and structural classifications of IC Engine systems.
  • Combustion Exploration: Explore the detailed stages of combustion in Spark Ignition (SISI) and Compression Ignition (CICI) engines, including the identifying factors that influence combustion quality.
  • Testing Proficiency: Numerically evaluate testing procedures and the various performance parameters associated with IC engines.
  • Compressor Mechanics: Explain the specific functions and working principles of rotary, reciprocating, and dynamic axial compressors.
  • Gas Turbine Analysis: Demonstrate an understanding of gas turbine working principles, classifications, and thermodynamic analysis processes.

Unit I: I.C. Engine Fundamentals and Systems

  • General Classification: Structural and operational classifications of engines (by fuel, cycle, ignition, cooling, etc.).
  • Working Principles:
    • Four-Stroke Engine: Involves the four distinct strokes: Suction, Compression, Power (Expansion), and Exhaust, completed in two revolutions of the crankshaft.
    • Two-Stroke Engine: Completes the power cycle in only one revolution of the crankshaft, utilizing ports instead of valves.
    • SI vs. CI Engines: Detailed comparison between Spark Ignition (SISI) engines and Compression Ignition (CICI) engines.
  • Timing Diagrams:
    • Valve Timing Diagram: Graphic representation of the opening and closing of intake and exhaust valves relative to the crankshaft position (TDCTDC and BDCBDC).
    • Port Timing Diagram: Specific to two-stroke engines, showing the timing of intake, transfer, and exhaust port operations.
  • Cycle Analysis:
    • Air-Standard Cycles: Theoretical cycles (like Otto, Diesel, and Dual) assuming air as the working fluid with constant specific heat (CpC_p and CvC_v).
    • Air-Fuel Cycles: Improved analysis considering the variation of specific heats, dissociation, and actual gas properties.
    • Actual Cycles: Analysis incorporating real-world losses such as time loss, heat loss, and blowdown loss.
  • Engine Systems:
    • Fuel Systems for SI Engines: Detailed study of Carburetors (venturi principle and mixture requirements) and modern Fuel Injection Systems.
    • Fuel Systems for CI Engines: Comprehensive look at Diesel fuel injection systems, including pumps and injectors.
    • Ignition Systems: Battery ignition, magneto ignition, and electronic ignition timing.
    • Cooling Systems: Air cooling (fins) and water/liquid cooling (radiators, thermostats).
    • Lubrication Systems: Mist, splash, and pressure lubrication methods.
  • Chemical Thermodynamics:
    • Fuel properties (Volatility, calorific value, viscosity).
    • Combustion Stoichiometry: Mathematical calculation of the exact air-fuel ratio (AFRAFR) required for complete combustion: Fuel+n(O2+3.76N2)CO2+H2O+3.76nN2\text{Fuel} + n(\text{O}_2 + 3.76\text{N}_2) \rightarrow \text{CO}_2 + \text{H}_2\text{O} + 3.76n\text{N}_2.

Unit II: Combustion in SI and CI Engines

  • Spark Ignition (SI) Engines:
    • Normal Combustion: Flame propagation from the spark plug throughout the chamber.
    • Flame Speed: The importance of flame velocity and the effects of engine variables (turbulence, fuel-type, temperature).
    • Abnormal Combustion: Detailed study of Pre-ignition and Knocking (detonationdetonation) in SI engines.
    • Fuel Rating: Identification of fuel requirements and the use of Octane Numbers and anti-knock additives.
    • Combustion Chambers: Requirements and types of SI engine combustion chambers.
  • Compression Ignition (CI) Engines:
    • Four Stages of Combustion: Ignition delay (1), Uncontrolled combustion (2), Controlled combustion (3), and Afterburning (4).
    • Delay Period: Calculation and importance of the ignition delay period.
    • Diesel Knock: Causes and remedies for knocking in CI engines, contrasted with SI knock.
    • Air Movement and Turbulence: The necessity for suction-induced, compression-induced, and combustion-induced turbulence to ensure proper mixing.
    • Chamber Designs: Comparison between Open and Divided (Pre-combustion) chambers.
    • Diesel Fuel Rating: Requirements and Cetane Number rating.

Unit III: Performance Testing and Reciprocating Compressors

  • Parameters of Performance:
    • Measurement techniques for cylinder pressure, fuel consumption, and air intake.
    • Exhaust gas composition analysis.
    • Power Calculations:
      • Brake Power (BPBP): Measured at the output shaft, typically using a dynamometer: BP=2×τ×N×τ60,000 kWBP = \frac{2 \times \tau \times N \times \tau}{60,000} \text{ kW}.
      • Indicated Power (IPIP): Power generated inside the cylinder.
      • Frictional Losses: Difference between IPIP and BPBP, often determined via the Morse Test or Willan’s line.
  • Heat Balance Sheet: A full accounting of the energy input from fuel versus energy output (useful work, heat to cooling water, heat to exhaust gases, and radiation losses).
  • Compressor Classification:
    • Distinction between Fans, Blowers, and Compressors based on pressure ratios.
    • Positive displacement vs. Dynamic types.
    • Reciprocating vs. Rotary types.
  • Reciprocating Compressors:
    • Work Required: Mathematical derivation for work: W=nn1P1V1[(P2P1)n1n1]W = \frac{n}{n-1} P_1 V_1 [(\frac{P_2}{P_1})^{\frac{n-1}{n}} - 1].
    • Efficiencies: Isothermal efficiency and Volumetric efficiency.
    • Clearance Volume: The effect of clearance volume on air delivery.
    • Staged Compression: Advantages of multi-stage compression, including under-cooling (inter-cooling) and the condition for minimum work: Pi=sqrt(P1×P2)P_i = \text{sqrt}(P_1 \times P_2).

Unit IV: Rotary and Dynamic Compressors

  • Rotary Compressors (Positive Displacement):
    • Roots Blower: Mechanical details and principle of operation.
    • Vane Sealed Compressor: Working principles and efficiency considerations.
  • Centrifugal Compressors (Dynamic):
    • Mechanical details: Impeller, diffuser, and casing.
    • Energy Transfer: Velocity and pressure variations throughout the compressor.
    • Impeller Blades: Influence of radial, forward, and backward leaning blades.
    • Losses and Factors: Slip factor (slip\text{slip}), Power input factor, Pressure coefficient, and Adiabatic coefficient.
    • Velocity Diagrams: Construction and analysis of velocity triangles for power calculation.
  • Axial Flow Compressors:
    • Mechanical details and stage-by-stage principle of operation.
    • Velocity Triangles: Analysis of energy transfer per stage.
    • Degree of Reaction (RR): Definition and its effect on stage design.
    • Performance Metrics: Work done factor, Isentropic efficiency, and Polytropic efficiency calculations.

Unit V: Gas Turbines

  • Gas Turbine Plants: Overview of simple plants, including Closed Cycle and Open Cycle configurations.
  • Thermodynamic Cycles:
    • Constant Pressure Cycle (Brayton Cycle): Ideal logic and cycle efficiency: Eff=11rpν1ν\text{Eff} = 1 - \frac{1}{r_p^{\frac{\nu-1}{\nu}}}.
    • Constant Volume Cycle: Theoretical considerations.
  • Cycle Parameters:
    • Work Ratio: Ratio of net work to turbine work.
    • Optimum Pressure Ratio: Determination of the pressure ratio that yields maximum specific work output.
    • Performance Analysis: Evaluation of parameters in both ideal and actual cycles (considering isentropic efficiencies of the compressor and turbine).

Recommended Resources

  • Textbooks:
    1. I.C. Engines by V. Ganesan, 4th Edition, McGraw Hill.
    2. Thermal Engineering by Mahesh M Rathore, Tata McGraw Hill, 2010.
  • Reference Books:
    1. Applied Thermodynamics for Engineering Technologists by Eastop & McConkey, Pearson.
    2. Fundamentals of Classical Thermodynamics by Vanwylen G.J. and Sonntag R.E., Wiley Eastern.
    3. Internal Combustion Engines Fundamentals by John B. Heywood, McGraw Hill Ed.