PULSAR PLATE MOUNTING STRUCTURE
PROBLEM TO BE SOLVED: To suppress stress concentration in the vicinity of fastening members in a structure where a disk-like pulsar plate is fastened to a mounting surface formed of a crank web and a counter weight and orthogonal to a crank axial line by at least three fastening members.SOLUTION: A...
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| creator | FUJII KINYA NAGAO HIROYUKI |
| description | PROBLEM TO BE SOLVED: To suppress stress concentration in the vicinity of fastening members in a structure where a disk-like pulsar plate is fastened to a mounting surface formed of a crank web and a counter weight and orthogonal to a crank axial line by at least three fastening members.SOLUTION: A pulsar plate 7 includes a plate-like inner circumferential side portion 12 where an insertion hole 11 is formed, and a plate-like outer circumferential side portion 14 continuously provided via an annular step part 13. In the annular step part 13, a protruding part 13b is formed which protrudes to the outside in a radial direction partially in a circumferential direction. The protruding part 13b is provided in a position overlapped in a circumferential direction with at least one (first insertion hole 11a) of two insertion holes 11a, 11b which are provided to be adjacent to both circumferential ends 5b of an end face 5a of the counter weight 5. |
| format | Patent |
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In the annular step part 13, a protruding part 13b is formed which protrudes to the outside in a radial direction partially in a circumferential direction. The protruding part 13b is provided in a position overlapped in a circumferential direction with at least one (first insertion hole 11a) of two insertion holes 11a, 11b which are provided to be adjacent to both circumferential ends 5b of an end face 5a of the counter weight 5.</description><language>eng</language><subject>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS ; BEARINGS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING COMBUSTION ENGINES ; ELEMENTS OR CRANKSHAFT MECHANISMS ; ENGINEERING ELEMENTS AND UNITS ; FLEXIBLE SHAFTS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MEASURING ; MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE ; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR ; MECHANICAL ENGINEERING ; PHYSICS ; ROTARY BODIES OTHER THAN GEARING ELEMENTS ; SHAFTS ; TARIFF METERING APPARATUS ; TESTING ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2013</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=20131209&DB=EPODOC&CC=JP&NR=2013245583A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20131209&DB=EPODOC&CC=JP&NR=2013245583A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FUJII KINYA</creatorcontrib><creatorcontrib>NAGAO HIROYUKI</creatorcontrib><title>PULSAR PLATE MOUNTING STRUCTURE</title><description>PROBLEM TO BE SOLVED: To suppress stress concentration in the vicinity of fastening members in a structure where a disk-like pulsar plate is fastened to a mounting surface formed of a crank web and a counter weight and orthogonal to a crank axial line by at least three fastening members.SOLUTION: A pulsar plate 7 includes a plate-like inner circumferential side portion 12 where an insertion hole 11 is formed, and a plate-like outer circumferential side portion 14 continuously provided via an annular step part 13. In the annular step part 13, a protruding part 13b is formed which protrudes to the outside in a radial direction partially in a circumferential direction. The protruding part 13b is provided in a position overlapped in a circumferential direction with at least one (first insertion hole 11a) of two insertion holes 11a, 11b which are provided to be adjacent to both circumferential ends 5b of an end face 5a of the counter weight 5.</description><subject>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS</subject><subject>BEARINGS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING COMBUSTION ENGINES</subject><subject>ELEMENTS OR CRANKSHAFT MECHANISMS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>FLEXIBLE SHAFTS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MEASURING</subject><subject>MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE</subject><subject>MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR</subject><subject>MECHANICAL ENGINEERING</subject><subject>PHYSICS</subject><subject>ROTARY BODIES OTHER THAN GEARING ELEMENTS</subject><subject>SHAFTS</subject><subject>TARIFF METERING APPARATUS</subject><subject>TESTING</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJAPCPUJdgxSCPBxDHFV8PUP9Qvx9HNXCA4JCnUOCQ1y5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8V4BRgaGxkYmpqYWxo7GRCkCADlbIms</recordid><startdate>20131209</startdate><enddate>20131209</enddate><creator>FUJII KINYA</creator><creator>NAGAO HIROYUKI</creator><scope>EVB</scope></search><sort><creationdate>20131209</creationdate><title>PULSAR PLATE MOUNTING STRUCTURE</title><author>FUJII KINYA ; NAGAO HIROYUKI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2013245583A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2013</creationdate><topic>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS</topic><topic>BEARINGS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING COMBUSTION ENGINES</topic><topic>ELEMENTS OR CRANKSHAFT MECHANISMS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>FLEXIBLE SHAFTS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MEASURING</topic><topic>MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE</topic><topic>MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR</topic><topic>MECHANICAL ENGINEERING</topic><topic>PHYSICS</topic><topic>ROTARY BODIES OTHER THAN GEARING ELEMENTS</topic><topic>SHAFTS</topic><topic>TARIFF METERING APPARATUS</topic><topic>TESTING</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>FUJII KINYA</creatorcontrib><creatorcontrib>NAGAO HIROYUKI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FUJII KINYA</au><au>NAGAO HIROYUKI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PULSAR PLATE MOUNTING STRUCTURE</title><date>2013-12-09</date><risdate>2013</risdate><abstract>PROBLEM TO BE SOLVED: To suppress stress concentration in the vicinity of fastening members in a structure where a disk-like pulsar plate is fastened to a mounting surface formed of a crank web and a counter weight and orthogonal to a crank axial line by at least three fastening members.SOLUTION: A pulsar plate 7 includes a plate-like inner circumferential side portion 12 where an insertion hole 11 is formed, and a plate-like outer circumferential side portion 14 continuously provided via an annular step part 13. In the annular step part 13, a protruding part 13b is formed which protrudes to the outside in a radial direction partially in a circumferential direction. The protruding part 13b is provided in a position overlapped in a circumferential direction with at least one (first insertion hole 11a) of two insertion holes 11a, 11b which are provided to be adjacent to both circumferential ends 5b of an end face 5a of the counter weight 5.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS BEARINGS BLASTING COMBUSTION ENGINES CONTROLLING COMBUSTION ENGINES ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MEASURING MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR MECHANICAL ENGINEERING PHYSICS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS TARIFF METERING APPARATUS TESTING THERMAL INSULATION IN GENERAL WEAPONS |
| title | PULSAR PLATE MOUNTING STRUCTURE |
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