A method for evaluating and predicting the thermal insulation effect of thermal barrier coatings on turbine blades
A technology of thermal barrier coatings and turbine blades, which is applied in the field of evaluation and prediction of thermal barrier coatings for turbine blades, and can solve the problem of insufficient relevant data, difficulty in evaluating and predicting coating thermal insulation effects, and insufficient mechanism of action Clear and other problems to achieve the effect of improving performance
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[0015] In order to understand the above objects, features and advantages of the present invention more clearly, the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.
[0016] Many specific details are set forth in the following description to facilitate a full understanding of the present invention. However, the present invention can also be implemented in other ways different from those described herein. Therefore, the protection scope of the present invention is not limited by the specific details disclosed below. Example limitations.
[0017] A method for evaluating and predicting the thermal insulation effect of thermal barrier coatings on turbine blades, establishing a one-dimensional coating-air film theoretical heat transfer model to simulate the heat transfer process of turbine blades with thermal barrier coatings, such as figure 1 The model consists of three parts: the air film hole, the t...
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