Small gas turbine with a radial or Slinger combustion chamber
DE19846976A1
Fuel injection system for radial or slinger combustion chamber of small gas turbine with radial or diagonal compressor located in front of combustion chamber to which is connected turbine part via axially running rotor shaft
DE19846975A1
Image acquisition method for twin blades of turbine; has displacement carriage positioned with respect to rotary table to acquire images of each individual blade
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Venting valve for compressor in gas turbine engine has the axially moving valve ring guided on a fixed seal to prevent tilting
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Turbine blade image capture method for gas turbine blade using turntable on rotary table
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Honeycomb structure seal especially for a gas turbine
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Housing formation on a gas turbine
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Rotor blade of an axial flow machine
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Passive gap system of a gas turbine
DE19749576A1
Thrust reverser of an aircraft jet engine
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Lubricating oil container for aero engines
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Suspension of an annular gas turbine combustion chamber
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Turbofan aircraft engine
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Measurement sensor for gas turbine engine
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Operating method for aircraft gas turbine engines
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Axially stepped annular combustion chamber for gas turbine
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Turbine impeller disk
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Turbine impeller disk with cooling air channels
DE19704845A1
Aircraft power plant oil separator
DE19645961A1
Fuel injector for a gas turbine combustor with a liquid cooled injector
