Turbine

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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Details

416 95, 416 96R, 416220R, 415115, F01D 518, F01D 904

Patent

active

060659327

ABSTRACT:
A turbine (10) for a gas turbine engine includes an annular array of turbine aerofoil blades (12) which are mounted on a disc (19). Each of the aerofoil blades (12) is provided with a radially inner platform (21). Each platform (21) includes a passage (37) into which leaked cooling air flows. The passages (37) are disposed in a direction having a circumferential component so that cooling air is exhausted from them in a direction that is generally opposite to that in which the disc (19) operationally rotates.

REFERENCES:
patent: 4453888 (1984-06-01), Hovan et al.
patent: 5800124 (1998-09-01), Zelesky

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