Turbine blade cooling

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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F01D 518

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active

058167773

ABSTRACT:
Internal heat transfer of air cooled turbine blades of a gas turbine engine is enhanced by orienting the impingement holes that interconnect the air-cooled feed passage to the hybrid passageway internally of the blade in a more radial direction to minimize pressure drop losses. By improved mixing of the cooling air in the hybrid passageway the additional mechanical turbulence promoters can be utilized without sacrificing pressure losses.

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patent: 4820123 (1989-04-01), Hal
patent: 5223320 (1993-06-01), Richardson
patent: 5241827 (1993-09-01), Lampes
patent: 5259182 (1993-11-01), Iwai et al.
patent: 5279127 (1994-01-01), Napoli

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