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Section 15.6

Turbine Section

Impulse/reaction turbines, nozzle guide vanes, fir-tree blade roots, creep and blade cooling.

Notes

Turbine section — summary notes

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Main ideas
  • The turbine extracts energy from the hot, high-pressure gas to drive the compressor and accessories (and, in turboprop/shaft engines, the propeller/rotor). Nozzle guide vanes (NGVs) ahead of each rotor accelerate and turn the gas onto the blades.
  • Turbines are impulse, reaction or (usually) impulse-reaction. In an impulse stage the gas is turned by fixed nozzles and the pressure drop is across the vanes; in a reaction stage the blades themselves act as nozzles and the pressure drops across the moving blades.
  • Blades are attached to the disc by a 'fir-tree' root that allows for expansion and is retained axially; they run in the hottest gas stream, so they suffer creep (slow permanent stretch under load at temperature), thermal fatigue and oxidation.
  • Cooling lets turbine entry temperature exceed the metal's melting point: cool compressor air is fed through internal passages and out of film-cooling holes to blanket the blade surface; single-crystal blades and ceramic thermal-barrier coatings raise the limit further.
  • The NGVs are the first components to see combustion gas and set the mass flow through the engine; the turbine's condition is watched through EGT/ITT limits.
  • ⚠ Exam trap: turbine blades are held by a loose-fitting 'fir-tree' root to allow thermal expansion; creep is the life-limiting slow stretch under centrifugal load at high temperature, and film cooling lets gas temperature exceed the blade's melting point.
Solved examples
  1. How can a turbine run in gas hotter than the melting point of its blade material without the blades melting?

    The blades are internally air-cooled: relatively cool air bled from the compressor passes through passages inside each blade and exits through tiny film-cooling holes, forming a thin insulating film of cooler air over the surface. Combined with thermal-barrier ceramic coatings and single-crystal alloys, this keeps the metal below its limit even though the gas is hotter than the melting point.

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Turbine Section

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