EINRICHTUNG UM DIE BLATTSPITZENVERLUSTE BEI KOMPRESSOREN ZU VERMINDERN.

摘要

The trench inner wall surrounding the tips (28) of axial flow fan/compressor blades (26) in a turbine type power plant is angularly disposed relative to the gas path wall (20) to allow deeper penetration into the trench and minimize leakage around the tips (28). Gap closure between the inner wall (37) of the trench and tip (28) is contemplated by the contour of the blade/trench.