СТАТОР КОМПРЕССОРА ГАЗОТУРБИННОГО ДВИГАТЕЛЯ

摘要

FIELD: stators of gas-turbine engine for aircraft and ground employment. ^ SUBSTANCE: proposed stator has inner body connected with outer body by means of two flexible members and blowing cavity which is bounded by flexible member, taper and cylindrical perforated partitions; I/h=0.1-1.5, where I is distance between taper partition and other flexible member and h is distance between cylindrical perforated partition and outer surface of inner body. ^ EFFECT: enhanced reliability and economical efficiency due to enhanced efficiency of radial clearance control system. ^ 2 dwg