Cooling flow control device for turbine blades

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

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416 97R, 415115, F01D 518

Patent

active

045265127

ABSTRACT:
A flow control body in the aft end of a hollow core of a turbine vane provides localized increased velocity cooling air flow in a wide portion which is otherwise difficult to cool. The flow control body includes lands and grooves with the cooling air being constrained to flow through the grooves and provide localized cooling while conductive heat transfer through the lands to the flow control body provides substantial temperature uniformity along the length of the vane. Turbulence chambers may be formed in the flow control body to further control cooling and the shape or other parameters of the flow control body may be modified to accommodate uneven end-to-end heating of the vane.

REFERENCES:
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patent: 3301526 (1967-01-01), Chamberlain
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patent: 3628880 (1971-12-01), Smuland et al.
patent: 3767322 (1973-10-01), Durgin et al.
patent: 4381173 (1983-04-01), Freling
patent: 4407632 (1983-10-01), Liang
patent: 4437810 (1984-03-01), Pearce

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