FIELD: turbines. SUBSTANCE: toroidal turbine intended for operation as a small-sized turbodrive uses body 1 and impeller 2 embracing it with a clearance, both of them for toroidal working passage 3 of two semi-oval sections. The impeller carries blades. Installed on the body is a separator with helical groove 10 with inlet (6) and outlet (7) connections located on its both sides. Inlet connection 6 communicates with the working passage by means of a nozzle with a square exit section, and outlet connection 7 - by means of window 11. The nozzle exit section is shifted relative to the plane of impeller rotation passing through the smaller axes of the groove semi-oval generating lines. Sealing on the impeller end surfaces is made as a labyrinth of annular lugs 12 and grooves; an the side of the heavy-duty surfaces lugs 13 with radial kerfs face the impeller grooves. EFFECT: enhanced turbine efficiency due to improved organization of flow and reduced leakages. 28 cl, 21 dwg
Title | Year | Author | Number |
---|---|---|---|
TOROIDAL TURBINE | 1997 |
|
RU2133381C1 |
TOROIDAL TURBINE | 2001 |
|
RU2193090C1 |
SCREW STEAM ENGINE | 1997 |
|
RU2168023C1 |
COOLING SYSTEM OF GAS-TURBINE ENGINE IMPELLER | 2012 |
|
RU2490473C1 |
BLADELESS NOZZLE SET FOR AIRCRAFT GAS-TURBINE ENGINE | 1999 |
|
RU2164603C1 |
TURBINE ASSEMBLY OF TURBO-PUMP UNIT | 2013 |
|
RU2511964C1 |
SCREW-ROTOR STEAM MACHINE | 1995 |
|
RU2118460C1 |
POWER PLANT WITH STEAM SCREW ENGINE | 1997 |
|
RU2127812C1 |
TURBO-PUMP UNIT, AND COLD, HOT AND INDUSTRIAL WATER PUMPING METHOD | 2013 |
|
RU2511983C1 |
TURBO-PUMP UNIT, AND COLD, HOT AND INDUSTRIAL WATER PUMPING METHOD | 2013 |
|
RU2511963C1 |
Authors
Dates
1999-02-20—Published
1997-03-19—Filed