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Turbine Blades

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An increase of only 17 C can decrease the engine life by half ... But what if the engine runs out of control at speeds higher than intended? ... – PowerPoint PPT presentation

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Title: Turbine Blades


1
Turbine Blades
  • Terry Andersen
  • Nathan Stastny
  • ME 372
  • Brigham Young University
  • Fall 2001

2
Overview
  • Applications
  • Design Considerations
  • Material Considerations
  • Manufacturing Processes
  • Review
  • Questions

3
Applications
  • Gas Turbine Generators
  • Jet Engines

4
Rolls Royce
Turbine Blades
Rolls Royce Trent
5
Design Considerations
  • Geometry
  • Cooling Vanes
  • Attachment Interface
  • Safety Factors

6
Geometry
  • Strength / Fatigue Life
  • Each row will be different
  • Air Flow (CFD Package)
  • Machineability

General Turbine Blade Shape
7
Cooling Vanes
  • Blades must be kept cool
  • Often operate near the metal melting point
  • An increase of only 17 ?C can decrease the engine
    life by half
  • Cool (300 ?C ) air is run out of the blades
    through small holes (vanes), keeping the blades
    from melting.

8
Pic
9
Attachment
  • Keep Stress Concentrations Low
  • Fir Tree Attachment
  • Reduced stress
  • concentrations
  • Easy replacement
  • Also known as the
  • Christmas Tree

10
Safety Factors
  • Higher S.F. is usually the best.
  • But what if the engine runs out of control at
    speeds higher than intended?
  • The energy of the rotating blades goes up with ?2
  • What happens if the blades brake at 10 overload?
    20, 30, 40, 50 ?
  • Too much energy and the blades might break
    through the engine shroud and into the fuselage.

11
Quick VideoBoeing 777Engine Test
12
Material Considerations
  • Environment
  • Creep
  • Current Materials Used
  • Materials In Research

13
Environment
  • Air Temperature Between 850 and 1600 C
  • Melting Temperature
  • Steel1400?C
  • Nickel Alloy 1200?C
  • Titanium1650?C
  • Turbine RPM Appx. 20,000 rpm

14
Creep
  • Turbine blades elongate during their life
  • Tip clearance
  • Result of environment and grain structure
  • Soft abradable lining
  • Directional solidification (cooling)
  • Single crystal structure

15
Current Materials Used
  • Initially Steel
  • Nickel Alloys
  • Most common material is Titanium
  • Laser peening
  • Ceramic Coatings

16
Material In Research
  • Ceramic blades
  • Carbon composite blades
  • Noise reduction
  • Light weight

17
Manufacturing Processes
  • Machining (not too common)
  • Investment Casting
  • Secondary machining
  • Electro-Chemical Machining
  • Single operation

18
Design Sites
  • www.pccsmp.com (manufacturing)
  • www.turboblades.com (manufacturing)
  • www.giverin.demon.co.uk/NewFiles/HTWTurbines.html
    (information)
  • www.gas-turbines.com/begin (information)
  • www.pratt-whitney.com (engine manufacturer)

19
Review
  • Applications
  • Jet Engines
  • Gas Turbine Generators
  • Design Factors
  • Geometry
  • S.F.
  • Materials
  • Very high temperatures
  • Titanium
  • Manufacturing

20
Questions
21
Dr. Chase Squadron Commander
Nathan
Terry
Special thanks to all those who didnt believe in
us, but whom weve proved wrong.
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