BLADE FOR A TURO MACHINE, BLADE ASSEMBLY, GAS TURBINE, AND METHOD FOR MANUFACTURING A BLADE FOR A TURBO MACHINE
A blade for turbo machine, in particular for a gas turbine, includes an airfoil body extending in a radial direction between a root end and a tip end, the air foil body comprising an inner cavity or void that extends from the root end in the radial direction, a root body integrally formed with the a...
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| creator | BEAUMONT, Wade HOFFMANN, Willy H KRUECKELS, Joerg TSYPKAYKIN, Igor MARTIN, Stafan Emanuel |
| description | A blade for turbo machine, in particular for a gas turbine, includes an airfoil body extending in a radial direction between a root end and a tip end, the air foil body comprising an inner cavity or void that extends from the root end in the radial direction, a root body integrally formed with the airfoil body and extending from the root end of the air foil body to a bottom end in the radial direction, the root body comprising a receiving slot extending from the bottom end in the radial direction and opening into the inner void of the air foil body, and an insert positioned within the receiving slot of the root body, the insert comprising a plurality of through holes extending in the radial direction to form a fluid connection to the inner void. |
| format | Patent |
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HOFFMANN, Willy H ; KRUECKELS, Joerg ; TSYPKAYKIN, Igor ; MARTIN, Stafan Emanuel</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4112881B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BEAUMONT, Wade</creatorcontrib><creatorcontrib>HOFFMANN, Willy H</creatorcontrib><creatorcontrib>KRUECKELS, Joerg</creatorcontrib><creatorcontrib>TSYPKAYKIN, Igor</creatorcontrib><creatorcontrib>MARTIN, Stafan Emanuel</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BEAUMONT, Wade</au><au>HOFFMANN, Willy H</au><au>KRUECKELS, Joerg</au><au>TSYPKAYKIN, Igor</au><au>MARTIN, Stafan Emanuel</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>BLADE FOR A TURO MACHINE, BLADE ASSEMBLY, GAS TURBINE, AND METHOD FOR MANUFACTURING A BLADE FOR A TURBO MACHINE</title><date>2024-08-21</date><risdate>2024</risdate><abstract>A blade for turbo machine, in particular for a gas turbine, includes an airfoil body extending in a radial direction between a root end and a tip end, the air foil body comprising an inner cavity or void that extends from the root end in the radial direction, a root body integrally formed with the airfoil body and extending from the root end of the air foil body to a bottom end in the radial direction, the root body comprising a receiving slot extending from the bottom end in the radial direction and opening into the inner void of the air foil body, and an insert positioned within the receiving slot of the root body, the insert comprising a plurality of through holes extending in the radial direction to form a fluid connection to the inner void.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | BLADE FOR A TURO MACHINE, BLADE ASSEMBLY, GAS TURBINE, AND METHOD FOR MANUFACTURING A BLADE FOR A TURBO MACHINE |
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