FIELD: turbojet engine.
SUBSTANCE: double-flow turbojet engine contains the intermediate jacket, with installed drive shaft of transfer gearbox in its radial arm designed to auxiliary drives. The drive shaft of output transfer gearbox is connected on its first end with the mechanical transfer mechanism placed on the drive shaft of the turbojet engine, and on the second end with the mechanical transmission to the abovementioned gearbox. The drive shaft of output transfer gearbox has a conic gearwheel between two ends of this shaft and allows providing mechanical linkage with additional auxiliary equipment. The drive shaft of output transfer gearbox in combination with the abovementioned gearwheel is encased forming an oil circuit, sealed in relation to the radial arm.
EFFECT: allows limiting a inflammable area at the expense oil leak elimination.
16 cl, 6 dwg
