ОПТИМИЗИРОВАННАЯ ЛОПАТКА СПРЯМЛЯЮЩЕГО АППАРАТА, СЕКТОР СПРЯМЛЯЮЩЕГО АППАРАТА, СТУПЕНЬ СЖАТИЯ, КОМПРЕССОР И ГАЗОТУРБИННЫЙ ДВИГАТЕЛЬ, СОДЕРЖАЩИЙ ЛОПАТКУ

摘要

The vane (2) has radial sections carried orthogonal to its stacking axis, where each radial section has points with Cartesian coordinates (X, Y, Z). The coordinate (Z) corresponds to a distance between a related radial section and a rotational axis of a turbo machine. The coordinates (X, Y) correspond to coordinates in a plane comprising the related section of points. Values of the coordinate (X) increase in a gas flow direction of the turbo machine, and an origin of the axis of the coordinate (X) is located at its intersection with the axis of the coordinate (Z).