CONTROLLED JET NOZZLE OF AVIATION GAS-TURBINE ENGINE

摘要

A controlled jet nozzle of aviation gas-turbine engine has coaxial outer and inner folds connected in hinged way to power support sections of the motor and to each other – with levers with hinges. The inner folds at their input are hinged on support body of afterburner chamber and connected to three-hinge lever. Each rod of hydro-drive and three-hinge lever are directly connected to each other by common hinge. With one more hinge each of those three-hinge levers is fixed directly on support body of afterburner chamber. In outlet cavity between those each outer and inner folds are placed additional con-rods hinged to the both of those.