IN2014DE03228A - - Google Patents
Info
- Publication number
- IN2014DE03228A IN2014DE03228A IN3228DE2014A IN2014DE03228A IN 2014DE03228 A IN2014DE03228 A IN 2014DE03228A IN 3228DE2014 A IN3228DE2014 A IN 3228DE2014A IN 2014DE03228 A IN2014DE03228 A IN 2014DE03228A
- Authority
- IN
- India
- Prior art keywords
- outer ring
- diaphragm outer
- rotor
- shroud
- extended
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/02—Arrangement of sensing elements
- F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/145—Means for influencing boundary layers or secondary circulations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/28—Arrangement of seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/31—Application in turbines in steam turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/40—Movement of components
- F05D2250/41—Movement of components with one degree of freedom
- F05D2250/411—Movement of components with one degree of freedom in rotation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
An axial turbine includes a plurality of ribs provided in such a way as to be sandwiched between the diaphragm outer ring and the axial seal fin in the gap between the shroud and the diaphragm outer ring, the ribs being extended from the diaphragm outer ring toward the shroud in the radial direction of the rotor and in the direction of the rotation axis thereof, and a guide plate provided in such a way as to be present along the axial seal fin and a face of the diaphragm outer ring, opposed to the rotor, so as to be extended in the rotation radial direction of the rotor.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2013232039A JP2015094220A (en) | 2013-11-08 | 2013-11-08 | Axial flow turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
IN2014DE03228A true IN2014DE03228A (en) | 2015-07-17 |
Family
ID=51868085
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN3228DE2014 IN2014DE03228A (en) | 2013-11-08 | 2014-11-07 |
Country Status (6)
Country | Link |
---|---|
US (1) | US20150132114A1 (en) |
EP (1) | EP2871324A3 (en) |
JP (1) | JP2015094220A (en) |
KR (1) | KR101660120B1 (en) |
CN (1) | CN104632296B (en) |
IN (1) | IN2014DE03228A (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201519869D0 (en) * | 2015-11-11 | 2015-12-23 | Rolls Royce Plc | Shrouded turbine blade |
JP6638938B2 (en) * | 2016-03-25 | 2020-02-05 | 三菱日立パワーシステムズ株式会社 | Rotating machinery |
EP3404213A1 (en) * | 2017-05-15 | 2018-11-21 | Siemens Aktiengesellschaft | Sealing device for a turbo-engine |
CN106996389B (en) * | 2017-05-26 | 2020-06-26 | 西安理工大学 | Short-distance inducer without blade top clearance cavitation |
JP6930896B2 (en) * | 2017-10-31 | 2021-09-01 | 三菱重工業株式会社 | Turbines and blades |
JP7145774B2 (en) * | 2019-01-31 | 2022-10-03 | 三菱重工業株式会社 | rotating machinery |
JP7267022B2 (en) * | 2019-01-31 | 2023-05-01 | 三菱重工業株式会社 | rotating machinery |
JP7145775B2 (en) * | 2019-01-31 | 2022-10-03 | 三菱重工業株式会社 | rotating machinery |
JP7356285B2 (en) * | 2019-07-31 | 2023-10-04 | 三菱重工業株式会社 | axial flow turbine |
CN110863863A (en) * | 2019-11-29 | 2020-03-06 | 四川大学 | Moving blade retaining ring structure with grate tooth sealing for gas turbine |
CN114934813B (en) * | 2022-04-28 | 2023-12-01 | 西北工业大学 | Partial inlet axial flow impulse turbine and active control method for clearance loss of blade tip of partial inlet axial flow impulse turbine |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS578302A (en) * | 1980-06-19 | 1982-01-16 | Hitachi Ltd | Internal stage structure of multistage axial-flow machine |
JPS6123804A (en) * | 1984-07-10 | 1986-02-01 | Hitachi Ltd | Turbine stage structure |
JP2006104952A (en) * | 2004-09-30 | 2006-04-20 | Toshiba Corp | Swirling flow preventive device of fluid machine |
JP2006138259A (en) * | 2004-11-12 | 2006-06-01 | Mitsubishi Heavy Ind Ltd | Axial flow turbine |
EP1767746A1 (en) * | 2005-09-22 | 2007-03-28 | Siemens Aktiengesellschaft | Turbine blade/vane and turbine section comprising a plurality of such turbine blades/vanes |
US20080118350A1 (en) * | 2006-11-16 | 2008-05-22 | General Electric | Turbine seal guards |
EP2096262A1 (en) * | 2008-02-26 | 2009-09-02 | Siemens Aktiengesellschaft | Axial flow turbine with low shroud leakage losses |
JP5591042B2 (en) * | 2010-09-17 | 2014-09-17 | 三菱重工業株式会社 | Turbine |
JP2011106474A (en) * | 2011-03-04 | 2011-06-02 | Toshiba Corp | Axial flow turbine stage and axial flow turbine |
US20130230379A1 (en) * | 2012-03-01 | 2013-09-05 | General Electric Company | Rotating turbomachine component having a tip leakage flow guide |
JP5985351B2 (en) * | 2012-10-25 | 2016-09-06 | 三菱日立パワーシステムズ株式会社 | Axial flow turbine |
-
2013
- 2013-11-08 JP JP2013232039A patent/JP2015094220A/en not_active Abandoned
-
2014
- 2014-11-06 KR KR1020140153712A patent/KR101660120B1/en active IP Right Grant
- 2014-11-06 CN CN201410637747.8A patent/CN104632296B/en not_active Expired - Fee Related
- 2014-11-07 IN IN3228DE2014 patent/IN2014DE03228A/en unknown
- 2014-11-07 US US14/535,362 patent/US20150132114A1/en not_active Abandoned
- 2014-11-07 EP EP14192274.0A patent/EP2871324A3/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
CN104632296A (en) | 2015-05-20 |
US20150132114A1 (en) | 2015-05-14 |
EP2871324A3 (en) | 2015-06-17 |
KR20150053714A (en) | 2015-05-18 |
JP2015094220A (en) | 2015-05-18 |
KR101660120B1 (en) | 2016-09-26 |
CN104632296B (en) | 2016-09-28 |
EP2871324A2 (en) | 2015-05-13 |
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