A method and apparatus for finishing a surface of a component
A technology for equipment, components, applied in the field of polishing the surface of components, which can solve the problems of accumulation, slow method, component contamination, etc.
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[0049] refer to figure 1 , a gas turbine engine generally indicated at 10 having a main axis and an axis of rotation 11 . The engine 10 comprises an air inlet 12, a propulsion fan 13, an intermediate pressure compressor 14, a high pressure compressor 15, a combustion equipment 16, a high pressure turbine 17, an intermediate pressure turbine 18, a low pressure turbine 19 and a discharge nozzle 20 in series in axial flow. . A nacelle 21 generally surrounds the engine 10 and defines both the inlet 12 and the discharge nozzle 20 .
[0050] The gas turbine engine 10 operates in a conventional manner such that air entering the inlet 12 is accelerated by the fan 13 to generate two air flows: a first air flow into the intermediate pressure compressor 14 and a second flow through the bypass duct 22 to provide propulsion thrust. Two air streams. The medium pressure compressor 14 compresses the air flow directed thereto (before delivering the air to the high pressure compressor 15 ) w...
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