COMBUSTOR LINER
PURPOSE: To raise film cooling capacity by having a suitable porous film cooling hole pattern consisting of a plurality of small film cooling holes which leans downward from high temperature side to low temperature side and are isolated densely from one another. CONSTITUTION: A suitable cooling hole...
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| creator | ERIASU HARII RANPUSU |
| description | PURPOSE: To raise film cooling capacity by having a suitable porous film cooling hole pattern consisting of a plurality of small film cooling holes which leans downward from high temperature side to low temperature side and are isolated densely from one another. CONSTITUTION: A suitable cooling hole pattern consists of many small film cooling holes 80, and these cooling holes 80 inclines acutely in the downstream direction from the high temperature side 61 of liners 48 and 50 to the low temperature side 57, and are isolated densely from one another. That is, for example, these cooling holes 80 have diameters of about twenty mill and tilt angles of about 20 deg., and are densely isolated from one another at intervals 6.5 to 7.5 times the diameter of the hole 80, and the holes 80 in the rows adjoining each other in axial direction are slid from each other in circumferential direction by about half the angle between the holes 80 adjoining each other in circumferential direction, which raises the equality of a cooling film more. Hereby, this liner can raise the film cooling effect. |
| format | Patent |
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CONSTITUTION: A suitable cooling hole pattern consists of many small film cooling holes 80, and these cooling holes 80 inclines acutely in the downstream direction from the high temperature side 61 of liners 48 and 50 to the low temperature side 57, and are isolated densely from one another. That is, for example, these cooling holes 80 have diameters of about twenty mill and tilt angles of about 20 deg., and are densely isolated from one another at intervals 6.5 to 7.5 times the diameter of the hole 80, and the holes 80 in the rows adjoining each other in axial direction are slid from each other in circumferential direction by about half the angle between the holes 80 adjoining each other in circumferential direction, which raises the equality of a cooling film more. Hereby, this liner can raise the film cooling effect.</description><language>eng</language><subject>BLASTING ; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; ENGINE PLANTS IN GENERAL ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; 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</subject><creationdate>1993</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=19930406&DB=EPODOC&CC=JP&NR=H0587339A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19930406&DB=EPODOC&CC=JP&NR=H0587339A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ERIASU HARII RANPUSU</creatorcontrib><title>COMBUSTOR LINER</title><description>PURPOSE: To raise film cooling capacity by having a suitable porous film cooling hole pattern consisting of a plurality of small film cooling holes which leans downward from high temperature side to low temperature side and are isolated densely from one another. CONSTITUTION: A suitable cooling hole pattern consists of many small film cooling holes 80, and these cooling holes 80 inclines acutely in the downstream direction from the high temperature side 61 of liners 48 and 50 to the low temperature side 57, and are isolated densely from one another. That is, for example, these cooling holes 80 have diameters of about twenty mill and tilt angles of about 20 deg., and are densely isolated from one another at intervals 6.5 to 7.5 times the diameter of the hole 80, and the holes 80 in the rows adjoining each other in axial direction are slid from each other in circumferential direction by about half the angle between the holes 80 adjoining each other in circumferential direction, which raises the equality of a cooling film more. Hereby, this liner can raise the film cooling effect.</description><subject>BLASTING</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</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>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</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>STEAM ENGINES</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1993</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOB39vd1Cg0O8Q9S8PH0cw3iYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxXgEeBqYW5sbGlo7GRCgBAL87HTQ</recordid><startdate>19930406</startdate><enddate>19930406</enddate><creator>ERIASU HARII RANPUSU</creator><scope>EVB</scope></search><sort><creationdate>19930406</creationdate><title>COMBUSTOR LINER</title><author>ERIASU HARII RANPUSU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JPH0587339A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1993</creationdate><topic>BLASTING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</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>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</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>STEAM ENGINES</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ERIASU HARII RANPUSU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ERIASU HARII RANPUSU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMBUSTOR LINER</title><date>1993-04-06</date><risdate>1993</risdate><abstract>PURPOSE: To raise film cooling capacity by having a suitable porous film cooling hole pattern consisting of a plurality of small film cooling holes which leans downward from high temperature side to low temperature side and are isolated densely from one another. CONSTITUTION: A suitable cooling hole pattern consists of many small film cooling holes 80, and these cooling holes 80 inclines acutely in the downstream direction from the high temperature side 61 of liners 48 and 50 to the low temperature side 57, and are isolated densely from one another. That is, for example, these cooling holes 80 have diameters of about twenty mill and tilt angles of about 20 deg., and are densely isolated from one another at intervals 6.5 to 7.5 times the diameter of the hole 80, and the holes 80 in the rows adjoining each other in axial direction are slid from each other in circumferential direction by about half the angle between the holes 80 adjoining each other in circumferential direction, which raises the equality of a cooling film more. Hereby, this liner can raise the film cooling effect.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS 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 | COMBUSTOR LINER |
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