GAS-TURBINE COOLED BLADE Russian patent published in 1998 - IPC

Abstract RU 2106499 C1

FIELD: power plant engineering. SUBSTANCE: blade has hollow feather with longitudinal rib from blade footing and internal tip boss with end cap. The latter rests on rib end, its diameter equals at least minimal width of feather internal channel section between boss bottom and rib end. EFFECT: improved cooling conditions. 3 dwg

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RU 2 106 499 C1

Authors

Chernjaev I.A.

Fadeev S.I.

Dates

1998-03-10Published

1995-01-11Filed