FIELD: engines and pumps.
SUBSTANCE: group of inventions refers to attachment system of end of shaft (14) of gas-turbine engine installed inside sleeve (15) fixed on support bearing (3). The above system includes nut (16) and differs by the fact that nut (16) includes the first thread (16f1) by means of which it is screwed into they above shaft (14), containing thread (14f), and the second thread (16f2) by means of which it is screwed into the above sleeve (15). Preferably, pitch of thread (16f1, 16f2) of nut (16) has in one thread the opposite direction relative to the other thread in order to obtain coupling nut.
EFFECT: group of inventions allows providing the erection and removal of rotor shaft on the turbine rear wall.
8 cl, 8 dwg
Title |
Year |
Author |
Number |
SHAFT END FIXING SYSTEM, COMPRESSOR SHAFT ERECTION METHOD, GAS TURBINE ENGINE COMPRESSOR AND GAS TURBINE ENGINE |
2007 |
- Servan Rezhi Ehzhen Ehnri
|
RU2436977C2 |
FRONT PART OF AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE AND AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE |
2015 |
- Nowakowski, Nathalie
- Vincent, Thomas, Alain, Christian
|
RU2686248C2 |
GAS TURBINE PLANT AND ITS DISMANTLING METHOD |
2015 |
- Curlier, Augustin
- Lemarchand, Kevin, Morgane
- Nowakowski, Nathalie
- Vincent, Thomas, Alain, Christian
|
RU2689258C2 |
INSTALLATION OF SHAFT INTO BEARING WITH SELF-REMOVABLE NUT |
2008 |
|
RU2468213C2 |
ASSEMBLY FOR AIRCRAFT GAS-TURBINE ENGINE AND METHOD OF ITS MOUNTING |
2015 |
- Lemarchand, Kevin, Morgane
|
RU2673027C2 |
AVIATION GAS-TURBINE ENGINE WITH AT LEAST TWO CASES AND WITH POWER TAKEOFF |
2019 |
- Charier, Gilles, Alain, Marie
- Frantz, Caroline, Marie
- Guillotel, Loic, Paul, Yves
- Millier, Vincent, Francois, Georges
|
RU2788264C2 |
SEALED FRONT CHAMBER DURING MODULAR DISMANTLING OF TURBOJET WITH REDUCTION GEAR |
2014 |
- Bro Mishel Zhilber Rolan
- Novakovski Natali
|
RU2674837C1 |
MODULAR ENGINE, SUCH AS JET ENGINE, WITH SPEED REDUCTION GEAR |
2014 |
- Bro Mishel Zhilber Rolan
- Novakovski Natali
|
RU2674098C1 |
DEVICE FOR GENERATION OF ELECTRIC ENERGY IN TWO-SHAFT GAS TURBINE ENGINE |
2008 |
- Kolin Antuan
- Lebrehn Arno
- Barzhon Zhill'
|
RU2472002C2 |
DEVICE FOR MECHANICAL POWER TALE-OFF BETWEEN HIGH-PRESSURE AND LOW-PRESSURE SHAFTS OF TWO-SHAFT GAS TURBINE ENGINE |
2006 |
- Line Jug Anri Rajmon
- Mushnino Siril Frank
- Pettinotti Serzh Dominik
|
RU2407903C2 |