FIELD: transportation.
SUBSTANCE: control device of gas flow in a channel comprises a plurality of turning blades (27, 28). The rotation axes of the first and the second adjacent blades (27, 28) are spaced apart so that the rear edge (47) of the first blade (27) overlaps the front edge (48) of the second blade (28), when the first and the second adjacent blades (27, 28) are in the first mutual extreme position for substantial restriction of the gas flow in the channel. The second blade (28) has a recess (49) of such shape that the rear edge (47) of the first blade (27) at least partially enters the recess, when the first and the second adjacent blades (27, 28) are in the first mutual extreme position, so that the recess (49) in the second blade (28) and the rear edge (47) of the first blade (27) are made with the possibility to form a substantially constant gap between the opposed mutually facing surfaces in the blades (27, 28) position within tolerance, when the first and the second blades are in the first mutual extreme position.
EFFECT: providing the reliable operation of the device.
27 cl, 11 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBINE NOZZLE ASSEMBLY WITH VARIABLE GEOMETRY AND METHOD FOR OPERATION THEREOF | 2015 |
|
RU2709901C2 |
TURBO-SUPERCHARGER | 1990 |
|
RU2011850C1 |
DEVICE FOR INCREASING BRAKE POWER OF VEHICLE MULTICYLINDER COMBUSTION ENGINE IN ENGINE BRAKING MODE | 2006 |
|
RU2404367C2 |
TURBINE EFFICIENCY CONTROL PROCEDURE AND DEVICE | 2009 |
|
RU2544640C2 |
METHOD FOR OPERATING ENGINE SYSTEM (OPTIONS) AND ENGINE SYSTEM | 2015 |
|
RU2681547C2 |
AXIAL GAS TURBINE | 2010 |
|
RU2543101C2 |
AXIAL GAS TURBINE | 2010 |
|
RU2547542C2 |
METHOD (OPTIONS) AND SYSTEM FOR ENGINE | 2017 |
|
RU2683344C2 |
CENTRIFUGAL NOZZLE WITH PROJECTING PARTS | 2012 |
|
RU2550370C2 |
GAS TRANSFER UNIT | 2020 |
|
RU2735881C1 |
Authors
Dates
2017-06-06—Published
2012-06-19—Filed