METHOD OF MANUFACTURING AN ACTUATOR ASSEMBLY COMPONENT AND METHOD OF VERIFYING SURFACE FINISH
A method of manufacturing an actuator assembly component is provided. The method includes tumble polishing the actuator assembly component. The method also includes taking at least one bearing ratio measurement along a portion of a surface of the actuator assembly component. The method further inclu...
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| creator | CHODAKOWSKI, Pawel P BANNON, David G |
| description | A method of manufacturing an actuator assembly component is provided. The method includes tumble polishing the actuator assembly component. The method also includes taking at least one bearing ratio measurement along a portion of a surface of the actuator assembly component. The method further includes comparing the at least one bearing ratio measurement to a minimum bearing ratio value to verify that the actuator assembly component has been tumble polished. |
| format | Patent |
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The method includes tumble polishing the actuator assembly component. The method also includes taking at least one bearing ratio measurement along a portion of a surface of the actuator assembly component. The method further includes comparing the at least one bearing ratio measurement to a minimum bearing ratio value to verify that the actuator assembly component has been tumble polished.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; DRESSING OR CONDITIONING OF ABRADING SURFACES ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS ; FLYING SUITS ; GRINDING ; MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING ; MEASURING ; MEASURING ANGLES ; MEASURING AREAS ; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS ; MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; POLISHING ; TESTING ; TRANSPORTING</subject><creationdate>2017</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=20170503&DB=EPODOC&CC=EP&NR=3162500A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170503&DB=EPODOC&CC=EP&NR=3162500A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CHODAKOWSKI, Pawel P</creatorcontrib><creatorcontrib>BANNON, David G</creatorcontrib><title>METHOD OF MANUFACTURING AN ACTUATOR ASSEMBLY COMPONENT AND METHOD OF VERIFYING SURFACE FINISH</title><description>A method of manufacturing an actuator assembly component is provided. The method includes tumble polishing the actuator assembly component. The method also includes taking at least one bearing ratio measurement along a portion of a surface of the actuator assembly component. The method further includes comparing the at least one bearing ratio measurement to a minimum bearing ratio value to verify that the actuator assembly component has been tumble polished.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DRESSING OR CONDITIONING OF ABRADING SURFACES</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS</subject><subject>FLYING SUITS</subject><subject>GRINDING</subject><subject>MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING</subject><subject>MEASURING</subject><subject>MEASURING ANGLES</subject><subject>MEASURING AREAS</subject><subject>MEASURING IRREGULARITIES OF SURFACES OR CONTOURS</subject><subject>MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>POLISHING</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZIj1dQ3x8HdR8HdT8HX0C3VzdA4JDfL0c1dw9FMAsR1D_IMUHIODXX2dfCIVnP19A_z9XP1CgNIuCgitYa5Bnm6RIG3BoUFAM1wV3Dz9PIM9eBhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJvGuAsaGZkamBgaOhMRFKAIXZMiM</recordid><startdate>20170503</startdate><enddate>20170503</enddate><creator>CHODAKOWSKI, Pawel P</creator><creator>BANNON, David G</creator><scope>EVB</scope></search><sort><creationdate>20170503</creationdate><title>METHOD OF MANUFACTURING AN ACTUATOR ASSEMBLY COMPONENT AND METHOD OF VERIFYING SURFACE FINISH</title><author>CHODAKOWSKI, Pawel P ; BANNON, David G</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3162500A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DRESSING OR CONDITIONING OF ABRADING SURFACES</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS</topic><topic>FLYING SUITS</topic><topic>GRINDING</topic><topic>MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING</topic><topic>MEASURING</topic><topic>MEASURING ANGLES</topic><topic>MEASURING AREAS</topic><topic>MEASURING IRREGULARITIES OF SURFACES OR CONTOURS</topic><topic>MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>POLISHING</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>CHODAKOWSKI, Pawel P</creatorcontrib><creatorcontrib>BANNON, David G</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CHODAKOWSKI, Pawel P</au><au>BANNON, David G</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD OF MANUFACTURING AN ACTUATOR ASSEMBLY COMPONENT AND METHOD OF VERIFYING SURFACE FINISH</title><date>2017-05-03</date><risdate>2017</risdate><abstract>A method of manufacturing an actuator assembly component is provided. The method includes tumble polishing the actuator assembly component. The method also includes taking at least one bearing ratio measurement along a portion of a surface of the actuator assembly component. The method further includes comparing the at least one bearing ratio measurement to a minimum bearing ratio value to verify that the actuator assembly component has been tumble polished.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DRESSING OR CONDITIONING OF ABRADING SURFACES EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS FLYING SUITS GRINDING MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING MEASURING MEASURING ANGLES MEASURING AREAS MEASURING IRREGULARITIES OF SURFACES OR CONTOURS MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS PARACHUTES PERFORMING OPERATIONS PHYSICS POLISHING TESTING TRANSPORTING |
| title | METHOD OF MANUFACTURING AN ACTUATOR ASSEMBLY COMPONENT AND METHOD OF VERIFYING SURFACE FINISH |
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