Adjustable guide vane adjustment method for aero-engine compression components in response to temperature distortion
A technology of aero-engines and adjustment methods, which is applied in the direction of machines/engines, mechanical equipment, non-variable pumps, etc., to achieve the effects of improving the ability to resist temperature distortion, improving the design level, and improving performance
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[0020] In order to make the implementation purpose, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the accompanying drawings in the embodiments of the present application.
[0021] In order to overcome the shortcomings of the prior art, the present application provides a method for improving the temperature distortion resistance level of the engine by changing the adjustment method of the adjustable guide vanes of the compression component based on the design level of the existing compression component, so as to ensure that the engine is It can work stably under the condition of temperature distortion.
[0022] The method for adjusting the adjustable guide vanes of the aero-engine compression components proposed in the present application is as follows:
[0023] The main compression components of the engine, such as fans or comp...
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