FIELD: machine building.
SUBSTANCE: jacket contains stationary coaxial circular rail projecting from external surface of this jacket. Also, at least three movable parts spaced one from another in circumferential direction can travel along this rail. Each movable part is connected with the driven ring by means of a radial guiding structure. For each movable part the radial guiding structure contains an element in form of a rod installed in radial direction into an orifice made in the said ring. The rod-shaped element is secured on the movable part. Another invention of the group refers to a compressor equipped with at least one above said row of the blades of the straightening device with alternate angles of assembly. One more invention refers to the gas-turbine motor incorporating the said compressor.
EFFECT: upgraded quality of centring driven ring relative to jacket under effects of high temperature.
16 cl, 8 dwg
| Title |
Year |
Author |
Number |
| LINE OF FLOW-STRAIGHTENING GRID VANES DRIVEN BY ROTARY RING DRIVEN BY ELECTRICAL ACTUATORS, COMPRESSOR INCORPORATING SAID LINE OF VANES AND TURBOJET ENGINE COMPRISING SUCH COMPRESSOR |
2005 |
|
RU2397331C2 |
| BIROTARY COMPRESSOR OF GAS TURBINE ENGINE |
2017 |
|
RU2659841C1 |
| AIR BLEED DEVICE, COMPRESSOR STAGE WITH SAID DEVICE, COMPRESSOR WITH SAID STAGE, AND TURBOJET WITH SAID COMPRESSOR |
2008 |
- Deren Zhaki
- Russelehn Stefan
|
RU2467209C2 |
| STRUCTURAL ROW OF VERTICAL ELECTRICALLY DRIVEN OIL PUMPS |
2011 |
- Valjukhov Sergej Georgievich
- Zhitenev Aleksej Ivanovich
- Zhitenev Sergej Vjacheslavovich
- Pechkurov Sergej Vladimirovich
- Selivanov Nikolaj Pavlovich
|
RU2472039C1 |
| GUIDING UNIT FOR BLADE WITH ADJUSTABLE SETTING ANGLE |
2004 |
- Debeneks P'Er
- Bromann Alen
- Bjuffenuar Fransua
|
RU2342540C2 |
| COMPRESSOR ROTOR PART, IMPROVED COUPLING BETWEEN DISKS WITH SYSTEMS OF BLADES ON COMPRESSOR ROTOR LINE, TURBOMACHINE AND METHOD OF MOUNTING OF SAID COUPLING (VERSIONS) |
2004 |
- Ehskjur Did'E Rene Andre
- Mirokur Zherar Gabriel'
- Soniak Fransis Zhill' Bazil'
- Boston Ehrik Zhak
- Ode Zhak Rober
- Burzhua Mari-Frans
- Dao Daniel'
|
RU2279571C2 |
| CLAMP FOR BLADE WITH T-SHAPE FASTENER, APPROPRIATE COMPRESSOR DISC, COMPRESSOR AND TURBO MACHINE |
2009 |
- Bel'Mont Oliv'E
- Bosko Frank Ehmmanjuehl'
|
RU2515572C2 |
| RECONDITIONING OF COMPRESSOR BLADES BY COLD FORMING |
2010 |
- Bertoli,Vinchentso
- De Sanktis,Serzh
- Zhijusti,Stefan,Rene,Zhjul'En
- Mon,Klod,Marsel'
|
RU2538145C2 |
| SYSTEM TO CONTROL TURBOJET ENGINE STATOR VANES WITH VARIABLE MOUNTING ANGLE |
2006 |
|
RU2396438C2 |
| AIRCRAFT ENGINE COMPRESSOR STRAIGHTENING BLADE DEVICE WITH THE GLUED BLADES |
2004 |
- Mon Klod Marsel'
- Andrie Sandra
- Zhirar Manjuehl'
- Ribassen Fransua P'Er Zhorzh Moris
|
RU2317448C2 |
