To study the internal cooling technology of turbine blade
three types of blades
i.e.non-cooled blade using adiabatic boundary condition
non-cooled blade using conjugate heat transfer method
and air-cooled blade using conjugate heat transfer method
were studied.The results show that heat conductivity of the blade has a significant influence on blade temperature distribution;the structure of rib-roughened cooling and latticework cooling makes the blade temperature drop markedly.However
this leads to increased non-uniformity of blade temperature distribution and irregular heat transfer coefficient distribution on the blade surface.