A method for evaluating an application effect of a thermal barrier coat for a turbine blade
A technology of thermal barrier coatings and turbine blades, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve problems such as poor thermal insulation performance, disasters, difficulties, etc., and achieve design and evaluation, and good economy benefit, reducing the effect of the application
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[0036] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in combination with specific embodiments and with reference to the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present invention.
[0037] Such as figure 1 As shown, the evaluation method of the application effect of the turbine blade thermal barrier coating of the present invention comprises the following steps:
[0038] (1) In the geometric modeling software, the geometric model of the thermal barrier coating, the geometric model of the turbine blade without thermal barrier coating and the geometric model of the external flow field are established....
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