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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

Nickel based superalloy turbine blade

2000

Nickel based superalloy turbine blade

2000

Nickel based superalloy turbine blade

2000

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

1990-1995

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

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

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