FIELD: machine building.
SUBSTANCE: control system of blades with variable installation angle for gas turbine engine comprises annular row of blades with variable installation angle arranged around axis. Each blade comprises a feather connected at its radial outer end with a pivot pin, which forms a radial axis of rotation of the blade and is connected by means of a lever to control means arranged around said axis. Control means comprises first links mounted on pivot pins and second links located between first links. First and the second links are located essentially on one circumference around the axis and are connected to each other and to driving facilities.
EFFECT: invention allows simplifying the blade control system with variable installation angle, as well as reducing its weight.
10 cl, 4 dwg
Title |
Year |
Author |
Number |
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