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Nickel based superalloy turbine blade

2000

Steam Turbine Blade of type used at Sizewell 'B' Nuclear Power Station

1990-1995

Steam Turbine Blade

1996

Steam Turbine Blade of type used for nuclear propulsion

1985-1995

Steam Turbine Blade

1996

Steam Turbine Blade of type used at Sizewell 'B' stage 7

1990-1995

Nickel based superalloy turbine blade

2000

Nickel based superalloy turbine blade

2000

Turbine blade

Single crystal turbine blade from a collection. This is the first stage of Low Pressure Turbine Blade casting for the Pegasus military turbofan engine. Maximum operating temperature in service is 1070°C.

Rolls Royce single crystal turbine blade

1995

Turbine blade. (General Electric Co. Ltd)

Turbine blade

Turbine blade made from titanium aluminide for use in a jet engine, developed by ACCESS e. V. TechCenter, Aachen, Germany, 2007.

Jet engine turbine blade made of titanium alloy

2007

Polycrystalline turbine blade from a collection. This is conventionally cast as the fourth stage of low pressure turbine blade casting for the Trent 800 Civil Turbofan engine. Its maximum operating temperature in service is 690°C. The blade is slightly damaged, with a small piece missing from the trailing edge

Rolls Royce polycrystalline turbine blade

1995

Uniaxial turbine blade from a collection. This is directionally solidified as the first stage of Low Pressure Turbine Blade casting for the Trent 800 Civil Turbofan engine. Its maximum operating temperature in service is 860°C.

Rolls Royce uniaxial turbine blade

1995