Inspection system and method for simulated working conditions of aeroengine guide vanes
A technology of aero-engines and guide vanes, which is applied in the direction of engine functions, engine components, machines/engines, etc., can solve problems such as prone to surge, reduce compressor surge margin, increase troubleshooting cycle and maintenance costs, etc. Achieve the effect of reducing the risk of test run and shortening the troubleshooting cycle
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[0018] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
[0019] Such as figure 1 , by researching and analyzing the manifestations of the problem of poor followability of the adjustment angle of the compressor guide vane and sluggish work during the use of an aeroengine, and the working principle and structural characteristics of the engine compressor guide vane, the invention provides an aero-engine guide The static inspection system of the blade simulates the working condition, including the hydraulic pum...
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