RU2009148541A - RADIAL Vortex Turbo Machine - Google Patents
RADIAL Vortex Turbo Machine Download PDFInfo
- Publication number
- RU2009148541A RU2009148541A RU2009148541/06A RU2009148541A RU2009148541A RU 2009148541 A RU2009148541 A RU 2009148541A RU 2009148541/06 A RU2009148541/06 A RU 2009148541/06A RU 2009148541 A RU2009148541 A RU 2009148541A RU 2009148541 A RU2009148541 A RU 2009148541A
- Authority
- RU
- Russia
- Prior art keywords
- trailing edge
- scapula
- tangent
- blade
- region
- Prior art date
Links
- 210000001991 scapula Anatomy 0.000 claims abstract 4
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Радиальная вихревая турбомашина, содержащая спиральный корпус, рабочее колесо с несущим, покрывным дисками и с расположенными между ними лопатками, имеющими в области задней кромки продольный и дополнительный выступы, отличающаяся тем, что указанные выступы совмещены в области задней кромки лопатки, образуя кольцевую цилиндрическую камеру с тангенциальным входным каналом и перфорированной обечайкой, закрепленную на несущем и покрывном дисках, параллельно задней кромки лопатки таким образом, что касательная к ней по линии пересечения плоскости, проходящей через ось камеры и заднюю кромку лопатки, параллельна касательной к тыльной и рабочей поверхностям лопаток в ее задней кромке. A radial vortex turbomachine containing a spiral casing, an impeller with a bearing, cover discs and blades located between them, having longitudinal and additional protrusions in the region of the trailing edge, characterized in that said protrusions are aligned in the region of the trailing edge of the blade, forming an annular cylindrical chamber with tangential inlet channel and perforated shell mounted on the carrier and cover disks parallel to the trailing edge of the blade so that it is tangent to it along the line of intersection the plane passing through the axis of the chamber and the trailing edge of the scapula is parallel to the tangent to the back and working surfaces of the scapula in its trailing edge.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009148541/06A RU2430274C1 (en) | 2009-12-25 | 2009-12-25 | Radial-swirl turbo-machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009148541/06A RU2430274C1 (en) | 2009-12-25 | 2009-12-25 | Radial-swirl turbo-machine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2009148541A true RU2009148541A (en) | 2011-06-27 |
| RU2430274C1 RU2430274C1 (en) | 2011-09-27 |
Family
ID=44738867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2009148541/06A RU2430274C1 (en) | 2009-12-25 | 2009-12-25 | Radial-swirl turbo-machine |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2430274C1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2525762C1 (en) * | 2013-05-20 | 2014-08-20 | ФГБОУ ВПО "Уральский государственный горный университет" | Radially-vortex turbomachine |
| RU2563044C1 (en) * | 2014-06-16 | 2015-09-20 | ФГБОУ ВПО "Уральский государственный горный университет" | Centrifugal fan impeller |
| RU2557818C1 (en) * | 2014-07-21 | 2015-07-27 | Общество с ограниченной ответственностью "ГрандАэро" | Radial-swirl turbo-machine |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2009379C1 (en) * | 1991-12-23 | 1994-03-15 | Научно-исследовательское, испытательное и проектное предприятие вентиляторостроения "Турмаш" | Centrifugal fan impeller |
| RU2067694C1 (en) * | 1992-12-08 | 1996-10-10 | Научно-исследовательское, испытательное и проектное предприятие вентиляторостроения "Турмаш" | Working wheel of centrifugal fan |
| JP2009133267A (en) * | 2007-11-30 | 2009-06-18 | Mitsubishi Heavy Ind Ltd | Impeller of compressor |
| RU2390658C2 (en) * | 2008-04-02 | 2010-05-27 | Государственное образовательное учреждение высшего профессионального образования "Уральский государственный горный университет" | Centrifugal fan impeller |
-
2009
- 2009-12-25 RU RU2009148541/06A patent/RU2430274C1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2430274C1 (en) | 2011-09-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2011138200A (en) | TURBOCHARGER VELVET EROSION INDICATOR | |
| EA201071359A1 (en) | WORKING WHEEL OF SLIM PUMP | |
| UA92141C2 (en) | Centrifugal fan | |
| RU2014145610A (en) | TURBINE HUB WITH SURFACE SURFACE AND TURBOCHARGER CONTAINING SUCH HUB | |
| RU2014117435A (en) | AXIAL TURBO MACHINE STATOR WITH ELERONS IN TROUSERS TAILS | |
| EA201400072A1 (en) | WORKING WHEEL OF CENTRIFUGAL PUMP AND ITS COMBINATION WITH INTERNAL DEPOSIT (OPTIONS) | |
| EP2096319A3 (en) | Centrifugal compressor | |
| RU2014145472A (en) | TURBOCHARGER BLADE WITH RELIEF ON EDGE PROFILE AND TURBOCHARGER CONTAINING SUCH SHOVEL | |
| MX2011012560A (en) | Direct-connection low-speed small mixed-flow hydroturbine for hydrodynamic energy-saving cooling tower. | |
| RU2013158435A (en) | MULTI-STAGE CENTRIFUGAL TURBO MACHINE | |
| RU2014145575A (en) | TURBOCHARGER CASING WITH CROSS grooves AND TURBOCHARGER WITH SUCH CASING | |
| RU2009133483A (en) | ROTATING SHOVEL OF STEAM TURBINE FOR LOW PRESSURE SECTION OF STEAM TURBINE ENGINE | |
| MX2016005523A (en) | Centrifugal compressor impeller with blades having an s-shaped trailing edge. | |
| RU2013102076A (en) | COMPRESSOR AND GAS TURBINE ENGINE WITH OPTIMIZED USEFUL EFFICIENCY | |
| RU2009148541A (en) | RADIAL Vortex Turbo Machine | |
| RU2013158608A (en) | SCREW LIQUID RING PUMP WITH INTEGRATED GRINDER | |
| RU2011135908A (en) | SUPERSONIC COMPRESSOR ROTOR AND SUPERSONIC COMPRESSOR UNIT | |
| RU2014118768A (en) | TURBO MACHINE STATOR BLADE CONTAINING A CONVEX SECTION | |
| BRPI0518716A2 (en) | centrifugal fan | |
| RU2013156047A (en) | METHOD FOR SCATTERING THE STAGE OF COMPRESSION OF A GAS TURBINE ENGINE AND THE SCATTERING STAGE FOR APPLICATION | |
| TW200736490A (en) | A structure of the radial turbine wheel | |
| RU2008115661A (en) | TWO FLOW CYLINDER OF A STEAM TURBINE INSTALLATION | |
| RU2525762C1 (en) | Radially-vortex turbomachine | |
| RU2010153329A (en) | GAS TURBINE ENGINE COMPRESSOR COVER CONTAINING AXIAL STOP | |
| JP2015075013A (en) | Centrifugal compressor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20131226 |