PATCH RING SEGMENT FOR TURBOMACHINE COMPRESSOR
PROBLEM TO BE SOLVED: To provide a turbomachine for preventing an edge part of a patch ring segment from bending in a flow path and contacting a rotor blade.SOLUTION: The patch ring segment 46 is mounted to an inner surface of a compressor casing 12 spaced away from a tip portion of the rotating rot...
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| creator | MOREE JEFFREY CRAIG MEMMER JOHN DAVID |
| description | PROBLEM TO BE SOLVED: To provide a turbomachine for preventing an edge part of a patch ring segment from bending in a flow path and contacting a rotor blade.SOLUTION: The patch ring segment 46 is mounted to an inner surface of a compressor casing 12 spaced away from a tip portion of the rotating rotor blade 25. At least one patch ring segment 46 includes a body 80 having a first end 82 that extends to a second end 83 through a surface portion 84. A first wall member 90 extends from the first end 82 and a second wall member 92 extends from the second end 83. The first and second wall members 90, 92 include in-turned sections 94, 96 that define a C-shaped cross-section of the at least one patch ring segment 46. |
| format | Patent |
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At least one patch ring segment 46 includes a body 80 having a first end 82 that extends to a second end 83 through a surface portion 84. A first wall member 90 extends from the first end 82 and a second wall member 92 extends from the second end 83. The first and second wall members 90, 92 include in-turned sections 94, 96 that define a C-shaped cross-section of the at least one patch ring segment 46.</description><language>eng</language><subject>BLASTING ; 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 ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION ; TECHNICAL SUBJECTS COVERED BY FORMER USPC ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; WEAPONS</subject><creationdate>2011</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=20111215&DB=EPODOC&CC=JP&NR=2011252496A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25566,76549</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20111215&DB=EPODOC&CC=JP&NR=2011252496A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MOREE JEFFREY CRAIG</creatorcontrib><creatorcontrib>MEMMER JOHN DAVID</creatorcontrib><title>PATCH RING SEGMENT FOR TURBOMACHINE COMPRESSOR</title><description>PROBLEM TO BE SOLVED: To provide a turbomachine for preventing an edge part of a patch ring segment from bending in a flow path and contacting a rotor blade.SOLUTION: The patch ring segment 46 is mounted to an inner surface of a compressor casing 12 spaced away from a tip portion of the rotating rotor blade 25. At least one patch ring segment 46 includes a body 80 having a first end 82 that extends to a second end 83 through a surface portion 84. A first wall member 90 extends from the first end 82 and a second wall member 92 extends from the second end 83. The first and second wall members 90, 92 include in-turned sections 94, 96 that define a C-shaped cross-section of the at least one patch ring segment 46.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</subject><subject>HEATING</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNALcAxx9lAI8vRzVwh2dfd19QtRcPMPUggJDXLy93V09vD0c1Vw9vcNCHINDvYP4mFgTUvMKU7lhdLcDEpurkADdFML8uNTiwsSk1PzUkvivQKMDAwNjUyNTCzNHI2JUgQANz4mUQ</recordid><startdate>20111215</startdate><enddate>20111215</enddate><creator>MOREE JEFFREY CRAIG</creator><creator>MEMMER JOHN DAVID</creator><scope>EVB</scope></search><sort><creationdate>20111215</creationdate><title>PATCH RING SEGMENT FOR TURBOMACHINE COMPRESSOR</title><author>MOREE JEFFREY CRAIG ; MEMMER JOHN DAVID</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2011252496A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2011</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>HEATING</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</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>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>STEAM ENGINES</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>MOREE JEFFREY CRAIG</creatorcontrib><creatorcontrib>MEMMER JOHN DAVID</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MOREE JEFFREY CRAIG</au><au>MEMMER JOHN DAVID</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PATCH RING SEGMENT FOR TURBOMACHINE COMPRESSOR</title><date>2011-12-15</date><risdate>2011</risdate><abstract>PROBLEM TO BE SOLVED: To provide a turbomachine for preventing an edge part of a patch ring segment from bending in a flow path and contacting a rotor blade.SOLUTION: The patch ring segment 46 is mounted to an inner surface of a compressor casing 12 spaced away from a tip portion of the rotating rotor blade 25. At least one patch ring segment 46 includes a body 80 having a first end 82 that extends to a second end 83 through a surface portion 84. A first wall member 90 extends from the first end 82 and a second wall member 92 extends from the second end 83. The first and second wall members 90, 92 include in-turned sections 94, 96 that define a C-shaped cross-section of the at least one patch ring segment 46.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | BLASTING 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 NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS WEAPONS |
| title | PATCH RING SEGMENT FOR TURBOMACHINE COMPRESSOR |
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