FIELD: mechanical engineering.
SUBSTANCE: device comprises sealing spacers and clutch interposed between the spacers. The clutch is conical and bears on the transverse link of the outer shaft line for permitting access to the mounting nut of the front end through the space between the shaft lines, which allows the nut be screwed out and the outer shaft line to be dismounted.
EFFECT: simplified mounting.
3 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
SEALED FRONT CHAMBER DURING MODULAR DISMANTLING OF TURBOJET WITH REDUCTION GEAR | 2014 |
|
RU2674837C1 |
GAS TURBINE ENGINE WITH AUXILIARY EQUIPMENT UNIT GEARING DRIVE, AND METHOD OF MOUNTING SAID ENGINE | 2008 |
|
RU2476701C2 |
DOUBLE-FLOW TURBOJET ENGINE WITH THE INTERMEDIATE JACKET, WITH THE DRIVE SHAFT OF TRANSFER GEARBOX FOR TURBOJET ENGINE ACCESSORY DRIVE | 2007 |
|
RU2442000C2 |
AVIATION GAS-TURBINE ENGINE WITH AT LEAST TWO CASES AND WITH POWER TAKEOFF | 2019 |
|
RU2788264C2 |
FRONT PART OF AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE AND AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE | 2015 |
|
RU2686248C2 |
ASSEMBLY FOR AIRCRAFT GAS-TURBINE ENGINE AND METHOD OF ITS MOUNTING | 2015 |
|
RU2673027C2 |
RPM GEARBOX WITH FLEXIBLE JOINT BETWEEN SATELLITE RACE AND FIXED BRACKET | 2004 |
|
RU2332598C2 |
FAN MODULE WITH VARIABLE ANGLE BLADES | 2019 |
|
RU2794134C2 |
ATTACHMENT SYSTEM OF ENGINE SHAFT BY MEANS OF COUPLING NUT, INSTALLATION METHOD OF SHAFT, COMPRESSOR OF GAS-TURBINE ENGINE, DOUBLE-FLOW GAS-TURBINE ENGINE | 2007 |
|
RU2431063C2 |
ROTOR DISK OF GAS-TURBINE ENGINE (VERSIONS) | 2001 |
|
RU2281420C2 |
Authors
Dates
2007-03-10—Published
2002-05-02—Filed