TURBINE BLADE AND GAS TURBINE WITH THIS BLADE
FIELD: machine building. ^ SUBSTANCE: turbine blade incorporates an edge and a platform arranged along the blade axis, the said platform being made on the blade edge base and crossing the blade axis. The platform is formed by the first spring-flexible sheet part fitting partially tightly on the thru...
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| creator | BOLMS KHANS-TOMAS LERNER KRISTIAN BAL'DAUF SHTEFAN KHENDLER MIKHEL |
| description | FIELD: machine building. ^ SUBSTANCE: turbine blade incorporates an edge and a platform arranged along the blade axis, the said platform being made on the blade edge base and crossing the blade axis. The platform is formed by the first spring-flexible sheet part fitting partially tightly on the thrust block furnished on the blade edge. The aforesaid part fits tightly on the following thrust block arranged on the adjacent turbine blade. The second invention of the set covers the gas turbine incorporating a flowing channel arranged along its axis and furnished with annular crosswise section for working medium and a second blades rim arranged after the first one along the turbine axis. The aforesaid rim incorporates a set of circular turbine blades entering radially the turbine blade flowing channel protected by this invention. ^ EFFECT: simple and reliable sealing of blade-to-blade allowing a relative motion of adjacent blades edges. ^ 14 cl, 2 dwg |
| format | Patent |
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The platform is formed by the first spring-flexible sheet part fitting partially tightly on the thrust block furnished on the blade edge. The aforesaid part fits tightly on the following thrust block arranged on the adjacent turbine blade. The second invention of the set covers the gas turbine incorporating a flowing channel arranged along its axis and furnished with annular crosswise section for working medium and a second blades rim arranged after the first one along the turbine axis. The aforesaid rim incorporates a set of circular turbine blades entering radially the turbine blade flowing channel protected by this invention. ^ EFFECT: simple and reliable sealing of blade-to-blade allowing a relative motion of adjacent blades edges. ^ 14 cl, 2 dwg</description><language>eng ; rus</language><subject>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</subject><creationdate>2008</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20080827&DB=EPODOC&CC=RU&NR=2332575C2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20080827&DB=EPODOC&CC=RU&NR=2332575C2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BOLMS KHANS-TOMAS</creatorcontrib><creatorcontrib>LERNER KRISTIAN</creatorcontrib><creatorcontrib>BAL'DAUF SHTEFAN</creatorcontrib><creatorcontrib>KHENDLER MIKHEL</creatorcontrib><title>TURBINE BLADE AND GAS TURBINE WITH THIS BLADE</title><description>FIELD: machine building. ^ SUBSTANCE: turbine blade incorporates an edge and a platform arranged along the blade axis, the said platform being made on the blade edge base and crossing the blade axis. The platform is formed by the first spring-flexible sheet part fitting partially tightly on the thrust block furnished on the blade edge. The aforesaid part fits tightly on the following thrust block arranged on the adjacent turbine blade. The second invention of the set covers the gas turbine incorporating a flowing channel arranged along its axis and furnished with annular crosswise section for working medium and a second blades rim arranged after the first one along the turbine axis. 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The platform is formed by the first spring-flexible sheet part fitting partially tightly on the thrust block furnished on the blade edge. The aforesaid part fits tightly on the following thrust block arranged on the adjacent turbine blade. The second invention of the set covers the gas turbine incorporating a flowing channel arranged along its axis and furnished with annular crosswise section for working medium and a second blades rim arranged after the first one along the turbine axis. The aforesaid rim incorporates a set of circular turbine blades entering radially the turbine blade flowing channel protected by this invention. ^ EFFECT: simple and reliable sealing of blade-to-blade allowing a relative motion of adjacent blades edges. ^ 14 cl, 2 dwg</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; rus |
| recordid | cdi_epo_espacenet_RU2332575C2 |
| source | esp@cenet |
| 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 | TURBINE BLADE AND GAS TURBINE WITH THIS BLADE |
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