Blade cooling
a technology of blades and cooling plates, applied in the field of blade cooling, can solve the problems of reducing the pressure differential, increasing the mechanical stress level and the requirement for thicker materials, and adding significantly to the fabrication cost, and achieving the effect of limiting the flow pressure loss of coolan
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first embodiment
[0014]Referring to FIG. 1 illustrating a cooling arrangement in accordance with the present invention. Thus, a mounting hub or disk 11 has a turbine blade 3 secured adjacent to it with a gap or coolant distribution gallery 4 between a mounting or root end 2 of the blade 3 and a top surface 11 of the mounting disk 1. A coolant flow illustrated by broken arrow 5 is drawn into the gallery 4 from a coolant supply system under a positive pressure differential. The gallery 4 has a passage opening 7 which extends to a passage 8 coupled to a coolant passage network within the blade 3 to provide cooling of that blade 3.
[0015]In accordance with the present invention a flow deflector 6 located adjacent and around the opening 7 deflects the coolant flow 5 into the passage 8 through the opening 7. The deflector 6 is substantially flat and creates a wedge or ramp to progressively deflect the coolant flow 5 through the opening 7. In such circumstances, there is less direct or perpendicular collisi...
second embodiment
[0021]FIGS. 2 and 3 illustrate the present invention. Thus, in a similar arrangement to that depicted in FIG. 1 a mounting hub or disk 21 has a turbine blade 23 secured to it with a gap between a blade root end 22 and a top surface 32 of the mounting hub or disk 21. This gap is a coolant gallery 24 through which a coolant flow shown by arrow head 25 passes in order to enter through a passage opening 27 a passage 28 coupled to a coolant passage network of the turbine blade 23. The coolant air flow 25 is deflected by a flow deflector 26 associated and adjacent to the passage opening 27. This flow deflector 26 is located substantially around the passage opening 27 to block the gallery 24 by a close fit association. However, if bypass holes are provided to the respective sides of the deflector 26, coolant air flow 25 can bypass the flow deflector 26 on either side to impinge upon other flow deflectors within the coolant gallery 24.
[0022]The flow deflector 26 has a curved surface 30 whic...
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