EA201200836A1 - RADIAL AXIAL HYDRO-TURBINE RADIATOR DEVICE OF THE WORKING WHEEL - Google Patents
RADIAL AXIAL HYDRO-TURBINE RADIATOR DEVICE OF THE WORKING WHEELInfo
- Publication number
- EA201200836A1 EA201200836A1 EA201200836A EA201200836A EA201200836A1 EA 201200836 A1 EA201200836 A1 EA 201200836A1 EA 201200836 A EA201200836 A EA 201200836A EA 201200836 A EA201200836 A EA 201200836A EA 201200836 A1 EA201200836 A1 EA 201200836A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- rim
- hub
- section
- blade
- thickness
- Prior art date
Links
- 238000010276 construction Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 230000002265 prevention Effects 0.000 abstract 1
- 238000000926 separation method Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/12—Blades; Blade-carrying rotors
- F03B3/121—Blades, their form or construction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/301—Cross-section characteristics
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Hydraulic Turbines (AREA)
Abstract
Изобретение относится к области гидротурбостроения и может быть использовано при разработке рабочих колес радиально-осевых гидротурбин. Лопаточный аппарат рабочего колеса радиально-осевой гидротурбины содержит обод, ступицу и лопасти, каждая из которых соединена с ободом и ступицей и выполнена с входной и выходной кромками изогнутого профиля и плавно изменяющейся толщиной в направлении от входной кромки к выходной и от ступицы к ободу. Лопасти лопаточного аппарата выполнены с утолщенной частью вблизи входной кромки, причем максимальная толщина лопасти в сечении ее ступицей больше максимальной толщины лопасти в сечении ее ободом. Определены оптимальные интервалы значений параметров: максимальной толщины сечения лопасти ступицей, максимальной толщины сечения лопасти ободом, а также мест их расположения вдоль распрямленной срединной линии соответствующего сечения. Технический результат: предотвращение отрыва потока за входными кромками лопастей при работе гидротурбины на режимах с повышенными напорами и режимах с частичными нагрузками во всем диапазоне рабочих напоров.The invention relates to the field of hydraulic turbine construction and can be used in the development of impellers of radial-axial hydraulic turbines. The vane of the impeller of a radial-axial hydraulic turbine contains a rim, a hub and blades, each of which is connected to the rim and a hub and is made with an inlet and outlet edges of a curved profile and a smoothly varying thickness in the direction from the inlet edge to the outlet and from the hub to the rim. The blades of the blade apparatus are made with a thickened part near the leading edge, and the maximum blade thickness in its hub section is greater than the maximum blade thickness in its rim section. The optimal intervals of parameter values have been determined: the maximum thickness of the blade section with the hub, the maximum thickness of the blade section with the rim, as well as their locations along the straightened midline of the corresponding section. EFFECT: prevention of flow separation behind the leading edges of the blades during operation of the hydraulic turbine in modes with increased heads and modes with partial loads in the entire range of operating heads.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009147213/06A RU2422670C1 (en) | 2009-12-09 | 2009-12-09 | Blade system of impeller of radial axial hydraulic turbine |
| PCT/RU2010/000745 WO2011071420A1 (en) | 2009-12-09 | 2010-12-06 | Vane apparatus of an impeller of a radial/axial hydroturbine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EA201200836A1 true EA201200836A1 (en) | 2012-11-30 |
| EA019417B1 EA019417B1 (en) | 2014-03-31 |
Family
ID=44145773
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EA201200836A EA019417B1 (en) | 2009-12-09 | 2010-12-06 | Vane apparatus of an impeller of a radial/axial hydroturbine |
Country Status (3)
| Country | Link |
|---|---|
| EA (1) | EA019417B1 (en) |
| RU (1) | RU2422670C1 (en) |
| WO (1) | WO2011071420A1 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2717461T3 (en) | 2011-10-23 | 2019-06-21 | Andritz Hydro Canada Inc | Compact blade for Francis turbine impeller and method for configuring the impeller |
| CN112329128B (en) * | 2020-09-03 | 2022-11-29 | 中国人民解放军海军工程大学 | A hydraulic model and design method of marine high-speed pump spray with fine blade load control |
| CN117236228B (en) * | 2023-11-13 | 2024-02-02 | 山东省科学院海洋仪器仪表研究所 | An optimization method for tidal energy turbine blades |
| CN119761262B (en) * | 2025-03-05 | 2025-05-13 | 中铁水利水电规划设计集团有限公司 | Operation evaluation method and system for ultra-large bulb through-flow turbine generator set |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1249189A1 (en) * | 1985-04-25 | 1986-08-07 | Производственное Объединение Атомного Турбостроения "Харьковский Турбинный Завод" Им.С.М.Кирова | Blade of radial axial-flow hydraulic machine impeller |
| SU1659679A1 (en) * | 1988-02-08 | 1991-06-30 | Производственное Объединение Атомного Турбостроения "Харьковский Турбинный Завод" Им.С.М.Кирова | Francis turbine wheel |
| US6155783A (en) * | 1998-05-20 | 2000-12-05 | Voith Siemens Hydro Power Generation, Inc. | Hollow blade for hydraulic turbine or pump |
| FR2844560B1 (en) * | 2002-09-13 | 2006-01-27 | Alstom Switzerland Ltd | FRANCIS-TYPE WHEEL AND HYDRAULIC MACHINE EQUIPPED WITH SUCH A WHEEL |
| JP2009091992A (en) * | 2007-10-09 | 2009-04-30 | Toshiba Corp | Francis turbine runner |
| NO20081661A (en) * | 2008-04-03 | 2009-08-03 | Hermond Brekke | Impeller for hydraulic flow machine. |
-
2009
- 2009-12-09 RU RU2009147213/06A patent/RU2422670C1/en active
-
2010
- 2010-12-06 WO PCT/RU2010/000745 patent/WO2011071420A1/en not_active Ceased
- 2010-12-06 EA EA201200836A patent/EA019417B1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| WO2011071420A1 (en) | 2011-06-16 |
| EA019417B1 (en) | 2014-03-31 |
| RU2422670C1 (en) | 2011-06-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ATE521812T1 (en) | HOUSING FOR A MOVING IMPELLER OF A TURBO MACHINE | |
| EP2518326A3 (en) | Centrifugal compressor assembly with stator vane row | |
| RU2014117435A (en) | AXIAL TURBO MACHINE STATOR WITH ELERONS IN TROUSERS TAILS | |
| EP2423510A3 (en) | Turbomachine with mixed-flow stage and method | |
| RU2011135181A (en) | ROTARY SHOVEL (OPTIONS) AND TURBO INSTALLATION | |
| MX2010003201A (en) | Airfoil diffuser for a centrifugal compressor. | |
| CN102099547A (en) | Axial turbo engine with low gap losses | |
| RU2013110571A (en) | RADIAL DIFFUSER BLADE FOR CENTRIFUGAL COMPRESSORS | |
| EP2775119A3 (en) | Compressor shroud reverse bleed holes | |
| MY155494A (en) | Direct-connected low-speed small mixed flow type water turbine applied in hydrodynamic energy-saving cooling tower | |
| EP2657532A3 (en) | Twisted variable inlet guide vane | |
| CN106194821A (en) | Centrifugal hydraulic turbine impeller and design method thereof | |
| EP2484913A3 (en) | A turbomachine comprising an annular casing and a bladed rotor | |
| WO2011102746A3 (en) | Turbine with radial inlet and outlet rotor for use in bidirectional flows | |
| RU2015137073A (en) | CENTRIFUGAL COMPRESSOR STEP | |
| EP2431577A3 (en) | Axial flow compressor, gas turbine system having the axial flow compressor and method of modifying the axial flow compressor | |
| RU2013158435A (en) | MULTI-STAGE CENTRIFUGAL TURBO MACHINE | |
| RU2010111039A (en) | SHOVEL FOR STEAM TURBINE WITH PROFILE PART LENGTH AT LEAST ABOUT 52 inches (132 cm) AND STEAM TURBINE WITH SUCH SHOVELS | |
| EA201200836A1 (en) | RADIAL AXIAL HYDRO-TURBINE RADIATOR DEVICE OF THE WORKING WHEEL | |
| WO2013180897A3 (en) | Gas turbine engine compressor stator seal | |
| RU2011153687A (en) | CENTRIFUGAL PORCH OF THE COMPRESSOR | |
| US9316103B2 (en) | Blading | |
| RU2011146094A (en) | CASING DIFFUSER FOR WORKING STEAM (OPTIONS) | |
| RU2010128086A (en) | HYDROPULSOR | |
| RU2017110166A (en) | CONTROLLED COMPRESSOR FLOW WITH REGULATED PRESSURE FOR THE GAS-TURBINE ENGINE |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AM BY MD RU |
|
| MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AZ TM |