Compressor blade with nozzle
a compressor blade and nozzle technology, applied in the direction of blade accessories, machines/engines, gas turbine plants, etc., can solve the problems of downstream blade damage, drop impingement erosion,
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[0009]The description and the figures show only exemplary embodiments of the invention.
[0010]FIG. 1 shows a cross section of a blade airfoil, in particular of a compressor blade 4, which, in particular at its leading edge or incident flow region 5 and downstream therefrom on the suction face and / or pressure face, has a plurality of nozzles 6, 6I, 6II, . . . , out of which a fluid 7, in particular water, exits.
[0011]This is used for wet compression when operating a gas turbine 100 (FIG. 13).
[0012]The suction and pressure faces can feature the same number or different numbers of nozzles 6, 6I, 6ii. . .
[0013]In particular, a nozzle 6, 6I, . . . is present in the leading edge 5.
[0014]Perpendicular to the plane of the drawing, more nozzles 6, 6I, . . . can be present at the leading edge 5 and / or on the suction face or pressure face.
[0015]The compressor blade 4 usually has, inside it, a hollow space 3 which is surrounded by walls 2 and by means of which the fluid can be fed to the nozzle ...
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