RU2010132943A - GUIDELINE TURNING MECHANISM - Google Patents
GUIDELINE TURNING MECHANISM Download PDFInfo
- Publication number
- RU2010132943A RU2010132943A RU2010132943/06A RU2010132943A RU2010132943A RU 2010132943 A RU2010132943 A RU 2010132943A RU 2010132943/06 A RU2010132943/06 A RU 2010132943/06A RU 2010132943 A RU2010132943 A RU 2010132943A RU 2010132943 A RU2010132943 A RU 2010132943A
- Authority
- RU
- Russia
- Prior art keywords
- turbine
- compressor
- shaft
- hydraulic drive
- levers
- Prior art date
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- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Механизм поворота направляющих лопаток осевой турбины (компрессора), содержащий корпус турбины с установленной в него обоймой с поворотными лопатками, закрепленными на их цапфах рычагами, соединенными подвижно с кольцом, опирающимся на обойму, расположенные с двух сторон корпуса турбины (компрессора) механизмы, включающие вал, установленный во втулке прикрепленной к корпусу турбины, рычаги на концах вала, соединенные шарнирно с одного конца с кольцом и гидроприводом с другого конца, отличающийся тем, что на одном из гидроприводов установлен золотник, через который подается масло из системы управления турбиной в его напорную полость, соединенную трубой с напорной полостью второго гидропривода. The mechanism of rotation of the guide vanes of the axial turbine (compressor), comprising a turbine housing with a cage installed in it with rotary blades, levers fixed on their pins, movably connected to a ring resting on the cage located on both sides of the turbine (compressor) casing, mechanisms including a shaft installed in the sleeve attached to the turbine body, levers at the ends of the shaft, pivotally connected at one end with a ring and hydraulic drive at the other end, characterized in that one of the hydraulic drives is installed flax spool, through which oil is supplied from a turbine control system in its pressure chamber connected with the discharge pipe of the second cavity of the hydraulic drive.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010132943/06A RU2465465C2 (en) | 2010-08-05 | 2010-08-05 | Guide vane turning mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010132943/06A RU2465465C2 (en) | 2010-08-05 | 2010-08-05 | Guide vane turning mechanism |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2010132943A true RU2010132943A (en) | 2012-02-20 |
RU2465465C2 RU2465465C2 (en) | 2012-10-27 |
Family
ID=45854175
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2010132943/06A RU2465465C2 (en) | 2010-08-05 | 2010-08-05 | Guide vane turning mechanism |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2465465C2 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU896242A1 (en) * | 1979-10-10 | 1982-01-07 | Производственное объединение "Турбомоторный завод" | Mechanism for adjusting the stator blades of axial turbomachine |
SU1198258A1 (en) * | 1984-03-29 | 1985-12-15 | Университет дружбы народов им.Патриса Лумумбы | Mechanism of turning vanes of centrifugal compressor diffuser |
FR2856424B1 (en) * | 2003-06-20 | 2005-09-23 | Snecma Moteurs | DEVICE FOR VARIABLE SETTING OF TWO FLOORS OF BLADES FIXED ON A TURBOJETACTOR |
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2010
- 2010-08-05 RU RU2010132943/06A patent/RU2465465C2/en active
Also Published As
Publication number | Publication date |
---|---|
RU2465465C2 (en) | 2012-10-27 |
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