Method for setting up and controlling confinement media flow in laser shock peening

A method for setting up a transparent confinement media nozzle (123) for flowing the confinement media (121) during laser shock peening (LSP) of a work piece (108) includes the following steps: Step A) flowing a confinement media (121) and setting a flow rate of the confinement media through a confi...

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Hauptverfasser: LAWRENCE, WAYNE LEE, KLAASSEN, RICHARD EUGENE
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Sprache:eng ; fre ; ger
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KLAASSEN, RICHARD EUGENE
description A method for setting up a transparent confinement media nozzle (123) for flowing the confinement media (121) during laser shock peening (LSP) of a work piece (108) includes the following steps: Step A) flowing a confinement media (121) and setting a flow rate of the confinement media through a confinement media flow nozzle (123); Step B) positioning the nozzle (123) to flow the confinement media through the nozzle (123) and onto the correlation surface (154); and Step C) measuring a confinement media layer thickness (T) on the correlation surface (154) using an ultrasonic transducer (20) attached to a side (148) of the test piece opposite that of the correlation surface (154). One embodiment of the invention employs the work piece (108) as the test piece and the correlation surface (154) is a first laser shock peening surface (154) on a first side of the work piece (108). Further embodiments includes Step D) comparing the measured and recorded confinement media layer thickness (T) from Step C) against a predetermined value or range of values for confinement media layer thickness (T) and Step E) determining whether to reset the confinement media flow rate and/or nozzle position or proceeding with the laser shock peening (LSP) of the work piece (108) with the confinement media flow rate and nozzle position set in Step A) based on the comparison in Step D).
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One embodiment of the invention employs the work piece (108) as the test piece and the correlation surface (154) is a first laser shock peening surface (154) on a first side of the work piece (108). Further embodiments includes Step D) comparing the measured and recorded confinement media layer thickness (T) from Step C) against a predetermined value or range of values for confinement media layer thickness (T) and Step E) determining whether to reset the confinement media flow rate and/or nozzle position or proceeding with the laser shock peening (LSP) of the work piece (108) with the confinement media flow rate and nozzle position set in Step A) based on the comparison in Step D).</description><edition>7</edition><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; CHEMISTRY ; CLADDING OR PLATING BY SOLDERING OR WELDING ; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; 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 ; INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES ; LIGHTING ; MACHINE TOOLS ; MACHINES OR ENGINES IN GENERAL ; MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS ; MEASURING ; MEASURING ANGLES ; MEASURING AREAS ; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS ; MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS ; MECHANICAL ENGINEERING ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; METALLURGY ; METALLURGY OF IRON ; MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; PHYSICS ; SOLDERING OR UNSOLDERING ; STEAM ENGINES ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE ; TESTING ; TRANSPORTING ; WEAPONS ; WELDING ; WORKING BY LASER BEAM</subject><creationdate>2004</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&amp;date=20040623&amp;DB=EPODOC&amp;CC=EP&amp;NR=1081239B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20040623&amp;DB=EPODOC&amp;CC=EP&amp;NR=1081239B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LAWRENCE, WAYNE LEE</creatorcontrib><creatorcontrib>KLAASSEN, RICHARD EUGENE</creatorcontrib><title>Method for setting up and controlling confinement media flow in laser shock peening</title><description>A method for setting up a transparent confinement media nozzle (123) for flowing the confinement media (121) during laser shock peening (LSP) of a work piece (108) includes the following steps: Step A) flowing a confinement media (121) and setting a flow rate of the confinement media through a confinement media flow nozzle (123); Step B) positioning the nozzle (123) to flow the confinement media through the nozzle (123) and onto the correlation surface (154); and Step C) measuring a confinement media layer thickness (T) on the correlation surface (154) using an ultrasonic transducer (20) attached to a side (148) of the test piece opposite that of the correlation surface (154). One embodiment of the invention employs the work piece (108) as the test piece and the correlation surface (154) is a first laser shock peening surface (154) on a first side of the work piece (108). Further embodiments includes Step D) comparing the measured and recorded confinement media layer thickness (T) from Step C) against a predetermined value or range of values for confinement media layer thickness (T) and Step E) determining whether to reset the confinement media flow rate and/or nozzle position or proceeding with the laser shock peening (LSP) of the work piece (108) with the confinement media flow rate and nozzle position set in Step A) based on the comparison in Step D).</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>CHEMISTRY</subject><subject>CLADDING OR PLATING BY SOLDERING OR WELDING</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS</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>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES</subject><subject>LIGHTING</subject><subject>MACHINE TOOLS</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS</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>MECHANICAL ENGINEERING</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>METALLURGY</subject><subject>METALLURGY OF IRON</subject><subject>MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>SOLDERING OR UNSOLDERING</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>TESTING</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><subject>WELDING</subject><subject>WORKING BY LASER BEAM</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2004</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNizEKAjEQRbexEPUOcwHBuI22yoqNIGi_hOTHDWZnwmbE6xvBA1j9x-P9eXO7QAfxFGSiAtXID3plsuzJCeskKX1V5RAZI1hphI-WQpI3RaZkC-p1EPekDHCtl80s2FSw-u2ioVN3P57XyNKjZOvA0L67ms3ObNv9wbR_JB_jNjf3</recordid><startdate>20040623</startdate><enddate>20040623</enddate><creator>LAWRENCE, WAYNE LEE</creator><creator>KLAASSEN, RICHARD EUGENE</creator><scope>EVB</scope></search><sort><creationdate>20040623</creationdate><title>Method for setting up and controlling confinement media flow in laser shock peening</title><author>LAWRENCE, WAYNE LEE ; KLAASSEN, RICHARD EUGENE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP1081239B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2004</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>CHEMISTRY</topic><topic>CLADDING OR PLATING BY SOLDERING OR WELDING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS</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>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES</topic><topic>LIGHTING</topic><topic>MACHINE TOOLS</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS</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>MECHANICAL ENGINEERING</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>METALLURGY</topic><topic>METALLURGY OF IRON</topic><topic>MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>SOLDERING OR UNSOLDERING</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>TESTING</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><topic>WELDING</topic><topic>WORKING BY LASER BEAM</topic><toplevel>online_resources</toplevel><creatorcontrib>LAWRENCE, WAYNE LEE</creatorcontrib><creatorcontrib>KLAASSEN, RICHARD EUGENE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LAWRENCE, WAYNE LEE</au><au>KLAASSEN, RICHARD EUGENE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method for setting up and controlling confinement media flow in laser shock peening</title><date>2004-06-23</date><risdate>2004</risdate><abstract>A method for setting up a transparent confinement media nozzle (123) for flowing the confinement media (121) during laser shock peening (LSP) of a work piece (108) includes the following steps: Step A) flowing a confinement media (121) and setting a flow rate of the confinement media through a confinement media flow nozzle (123); Step B) positioning the nozzle (123) to flow the confinement media through the nozzle (123) and onto the correlation surface (154); and Step C) measuring a confinement media layer thickness (T) on the correlation surface (154) using an ultrasonic transducer (20) attached to a side (148) of the test piece opposite that of the correlation surface (154). One embodiment of the invention employs the work piece (108) as the test piece and the correlation surface (154) is a first laser shock peening surface (154) on a first side of the work piece (108). Further embodiments includes Step D) comparing the measured and recorded confinement media layer thickness (T) from Step C) against a predetermined value or range of values for confinement media layer thickness (T) and Step E) determining whether to reset the confinement media flow rate and/or nozzle position or proceeding with the laser shock peening (LSP) of the work piece (108) with the confinement media flow rate and nozzle position set in Step A) based on the comparison in Step D).</abstract><edition>7</edition><oa>free_for_read</oa></addata></record>
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
CHEMISTRY
CLADDING OR PLATING BY SOLDERING OR WELDING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES
LIGHTING
MACHINE TOOLS
MACHINES OR ENGINES IN GENERAL
MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS
MEASURING
MEASURING ANGLES
MEASURING AREAS
MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
MEASURING LENGTH, THICKNESS OR SIMILAR LINEARDIMENSIONS
MECHANICAL ENGINEERING
METAL-WORKING NOT OTHERWISE PROVIDED FOR
METALLURGY
METALLURGY OF IRON
MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PERFORMING OPERATIONS
PHYSICS
SOLDERING OR UNSOLDERING
STEAM ENGINES
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
TESTING
TRANSPORTING
WEAPONS
WELDING
WORKING BY LASER BEAM
title Method for setting up and controlling confinement media flow in laser shock peening
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