TURBOMACHINE BLADE WITH FLUIDICALLY COOLED SHROUD
OF THE DISCLOSURE TURBOMACHINE BLADE WITH FLUIDICALLY COOLED SHROUD THE INVENTION RELATES TO A TURBOMACHINE BLADE (10) , IN PARTICULAR A TURBINE BLADE OF A GAS TURBINE. THE 5 TURBOMACHINE BLADE (10) DESIGNED ACCORDING TO THE INVENTION COMPRISES A BLADE ROOT (11) WITH A COOLING- FLUID FEED (12), A BL...
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| creator | REMIGI TSCHUOR HEINZ NEUHOFF |
| description | OF THE DISCLOSURE TURBOMACHINE BLADE WITH FLUIDICALLY COOLED SHROUD THE INVENTION RELATES TO A TURBOMACHINE BLADE (10) , IN PARTICULAR A TURBINE BLADE OF A GAS TURBINE. THE 5 TURBOMACHINE BLADE (10) DESIGNED ACCORDING TO THE INVENTION COMPRISES A BLADE ROOT (11) WITH A COOLING- FLUID FEED (12), A BLADE TIP (13) WHICH IS FORMED WITH A SHROUD ELEMENT (14) . AT LEAST ONE THROUGHF LOW PASSAGE (-19A) WHICH EXTENDS IN THE BLADE LONGITUDINAL DIRECTION 10 IS ARRANGED INSIDE THE AIRFOIL (15) . A SHROUD COOLING PASSAGE (22) IS FORMED IN THE SHROUD ELEMENT AT LEAST ALONG A SECTION OF THE LATTER, THIS SHROUD COOLING PASSAGE (22) BEING CONNECTED VIA AN OPENING (23, 24) TO THE THROUGHFLOW PASSAGE (19A), AND A COOLING FLUID 15 FLOWING THROUGH THIS SHROUD COOLING PASSAGE (22) DURING OPERATION OF THE T-URBOMACHINE BLADE. AT LEAST ONE FLOW- GUIDING ELEMENT (30, 31-DL - 31-D1L, 31-SL - 31-SI2, 32) FOR GUIDING AT LEAST SOME OF THE COOLING-FLUID FLOW FLOWING THROUGH THE SHROUD COOLING PASSAGE IS ARRANGED 20 IN THE SHROUD COOLING PASSAGE AND/OR IN AN INFLOW OR OUTFLOW CO OR FROM THE SHROUD COOLING PASSAGE. (PIGURE 4) 25 D @O 9 2 |
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THE 5 TURBOMACHINE BLADE (10) DESIGNED ACCORDING TO THE INVENTION COMPRISES A BLADE ROOT (11) WITH A COOLING- FLUID FEED (12), A BLADE TIP (13) WHICH IS FORMED WITH A SHROUD ELEMENT (14) . AT LEAST ONE THROUGHF LOW PASSAGE (-19A) WHICH EXTENDS IN THE BLADE LONGITUDINAL DIRECTION 10 IS ARRANGED INSIDE THE AIRFOIL (15) . A SHROUD COOLING PASSAGE (22) IS FORMED IN THE SHROUD ELEMENT AT LEAST ALONG A SECTION OF THE LATTER, THIS SHROUD COOLING PASSAGE (22) BEING CONNECTED VIA AN OPENING (23, 24) TO THE THROUGHFLOW PASSAGE (19A), AND A COOLING FLUID 15 FLOWING THROUGH THIS SHROUD COOLING PASSAGE (22) DURING OPERATION OF THE T-URBOMACHINE BLADE. AT LEAST ONE FLOW- GUIDING ELEMENT (30, 31-DL - 31-D1L, 31-SL - 31-SI2, 32) FOR GUIDING AT LEAST SOME OF THE COOLING-FLUID FLOW FLOWING THROUGH THE SHROUD COOLING PASSAGE IS ARRANGED 20 IN THE SHROUD COOLING PASSAGE AND/OR IN AN INFLOW OR OUTFLOW CO OR FROM THE SHROUD COOLING PASSAGE. 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THE 5 TURBOMACHINE BLADE (10) DESIGNED ACCORDING TO THE INVENTION COMPRISES A BLADE ROOT (11) WITH A COOLING- FLUID FEED (12), A BLADE TIP (13) WHICH IS FORMED WITH A SHROUD ELEMENT (14) . AT LEAST ONE THROUGHF LOW PASSAGE (-19A) WHICH EXTENDS IN THE BLADE LONGITUDINAL DIRECTION 10 IS ARRANGED INSIDE THE AIRFOIL (15) . A SHROUD COOLING PASSAGE (22) IS FORMED IN THE SHROUD ELEMENT AT LEAST ALONG A SECTION OF THE LATTER, THIS SHROUD COOLING PASSAGE (22) BEING CONNECTED VIA AN OPENING (23, 24) TO THE THROUGHFLOW PASSAGE (19A), AND A COOLING FLUID 15 FLOWING THROUGH THIS SHROUD COOLING PASSAGE (22) DURING OPERATION OF THE T-URBOMACHINE BLADE. AT LEAST ONE FLOW- GUIDING ELEMENT (30, 31-DL - 31-D1L, 31-SL - 31-SI2, 32) FOR GUIDING AT LEAST SOME OF THE COOLING-FLUID FLOW FLOWING THROUGH THE SHROUD COOLING PASSAGE IS ARRANGED 20 IN THE SHROUD COOLING PASSAGE AND/OR IN AN INFLOW OR OUTFLOW CO OR FROM THE SHROUD COOLING PASSAGE. 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THE 5 TURBOMACHINE BLADE (10) DESIGNED ACCORDING TO THE INVENTION COMPRISES A BLADE ROOT (11) WITH A COOLING- FLUID FEED (12), A BLADE TIP (13) WHICH IS FORMED WITH A SHROUD ELEMENT (14) . AT LEAST ONE THROUGHF LOW PASSAGE (-19A) WHICH EXTENDS IN THE BLADE LONGITUDINAL DIRECTION 10 IS ARRANGED INSIDE THE AIRFOIL (15) . A SHROUD COOLING PASSAGE (22) IS FORMED IN THE SHROUD ELEMENT AT LEAST ALONG A SECTION OF THE LATTER, THIS SHROUD COOLING PASSAGE (22) BEING CONNECTED VIA AN OPENING (23, 24) TO THE THROUGHFLOW PASSAGE (19A), AND A COOLING FLUID 15 FLOWING THROUGH THIS SHROUD COOLING PASSAGE (22) DURING OPERATION OF THE T-URBOMACHINE BLADE. AT LEAST ONE FLOW- GUIDING ELEMENT (30, 31-DL - 31-D1L, 31-SL - 31-SI2, 32) FOR GUIDING AT LEAST SOME OF THE COOLING-FLUID FLOW FLOWING THROUGH THE SHROUD COOLING PASSAGE IS ARRANGED 20 IN THE SHROUD COOLING PASSAGE AND/OR IN AN INFLOW OR OUTFLOW CO OR FROM THE SHROUD COOLING PASSAGE. (PIGURE 4) 25 D @O 9 2</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS |
| title | TURBOMACHINE BLADE WITH FLUIDICALLY COOLED SHROUD |
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