ME-421 Gas Turbines

ME-421 GAS TURBINES

CREDIT HOURS

Theory = 3
Practical = 0

COURSE LEARNING OUTCOMES (CLOs)

S. No. CLOs PLO Taxonomy
1 Apply gas turbine cycles for power generation and air craft propulsion PLO-2

Coginitive
Level 3*

2 Design components and process related to gas turbine cycles PLO-3 Coginitive
Level 5*
3 Analyze off-design performance of gas turbines used in power generation and aircraft propulsion PLO-2 Coginitive
Level 4*


COURSE CONTENT

  • Effect of pressure, Temperature, Component efficiency on fuel and air consumption and Power of the simple plant, Inter-cooling, reheat, Heat exchanger cycles, Industrial open and closed plant.
  • Turboprop, Turbofan and turbojet engines, Influence of altitude and flight speed on performance.
  • Principle of operation, Work done and pressure rise, Compressibility effects, Non-dimensional quantities for plotting compressor characteristics.
  • Elementary theory, Degree of reaction, Simple design method, Blade design, Calculation of stage performance, Overall performance, compressibility effect.
  • Form of combustion system, Some important factors effecting combustion chamber designing, combustion process, Combustion chamber performance.
  • Elementary theory, Vortex theory, Choice of blade profile, pitch and cord, Estimation of stage performance, Overall turbine performance.
  • Component Characteristics, Off-design operation of the single shaft gas turbine, Equilibrium running of a gas generator, Off-design operation of free-turbine engine, Jet engine.
  • Experiments on BHP of Gas Turbine, compressor and turbine efficiencies, and specific fuel consumption will be conducted in the lab.

RECOMMENDED BOOKS

(01) Mechanics & Thermodynamics of Propulsion by Hill & Peterson

*For details of Taxonomy Levels CLICK HERE!