Modeling experiment device for heat transfer in moving blade of aviation gas turbine
An aviation gas turbine and experimental device technology, applied in the direction of material thermal development, etc., can solve the problems of limited measurement range, inability to pressurize air, low strength, etc., and achieve the effect of reducing instability and saving time and cost
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[0038] In order to further explain the technical means and effects that the present invention adopts to achieve the intended purpose of the invention, a modeling experimental device for internal heat transfer of an aviation gas turbine blade proposed according to the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments. illustrate.
[0039] The aforementioned and other technical contents, features and effects of the present invention can be clearly presented in the following detailed description of specific implementations with accompanying drawings. Through the description of specific embodiments, the technical means and effects of the present invention to achieve the intended purpose can be understood more deeply and specifically, but the accompanying drawings are only for reference and description, and are not used to explain the technical aspects of the present invention. program is limited.
[0040] It...
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