METHOD FOR PRODUCING A HOLLOW FAN BLADE

A method for manufacturing a hollow fan blade of a titanium alloy, said blade consisting of skins and a filler forming stiffeners, comprises the step of working skin workpieces with a preformed blade root portion, during which working on surfaces of the skin workpieces, areas to be bonded to a fille...

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Hauptverfasser: KOKSHAROV, NIKOLAY LEONIDOVICH, MULYUKOV, RADIK RAFIKOVICH, SAIRANOV, AZAT NAILIEVICH, LUTFULLIN, RAMIL YAVATOVICH, KLIMOV, VALERY NIKOLAEVICH, ANDREYCHENKO, IGOR LEONARDOVICH, MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH, SAFIULLIN, RINAT VLADIKOVICH, RUDENKO, OLEG ALEXANDROVICH, MOROZOV, MIKHAIL ALEXANDROVICH, KHARIN, SERGEY ALEXANDROVICH, DONGAUZER, KONSTANTIN ALEXANDROVICH, KRUGLOV, ALEXEY ANATOLIEVICH
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Sprache:eng ; fre ; ger
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creator KOKSHAROV, NIKOLAY LEONIDOVICH
MULYUKOV, RADIK RAFIKOVICH
SAIRANOV, AZAT NAILIEVICH
LUTFULLIN, RAMIL YAVATOVICH
KLIMOV, VALERY NIKOLAEVICH
ANDREYCHENKO, IGOR LEONARDOVICH
MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH
SAFIULLIN, RINAT VLADIKOVICH
RUDENKO, OLEG ALEXANDROVICH
MOROZOV, MIKHAIL ALEXANDROVICH
KHARIN, SERGEY ALEXANDROVICH
DONGAUZER, KONSTANTIN ALEXANDROVICH
KRUGLOV, ALEXEY ANATOLIEVICH
description A method for manufacturing a hollow fan blade of a titanium alloy, said blade consisting of skins and a filler forming stiffeners, comprises the step of working skin workpieces with a preformed blade root portion, during which working on surfaces of the skin workpieces, areas to be bonded to a filler workpiece are shaped in the form of projections with a surface flat in a cross-section, and areas to be not bonded to the filler workpiece are shaped in the form of recesses, respectively, wherein at least a part of a surface of recesses opposite to projections in a stack assembled for diffusion welding is made flat in a cross-section, and also comprises the steps of: applying a bond preventing coating onto surfaces of workpiece areas to be not bonded; assembling the skin and filler workpieces into a stack; diffusion welding the skin and filler workpieces; forming stiffeners by superplastic forming, the method further comprises the step of providing the skin and filler workpieces with an aerodynamic profile by applying a deforming load thereto, including forming a pressure face and a suction face of the blade and twisting its airfoil. The method is characterized in that said projections and recesses are made on the surfaces of the skin workpieces prior to providing them with the aerodynamic profile, while the step of providing the workpieces with the aerodynamic profile is performed after diffusion welding. The method is particularly applicable to aircraft engine building.
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fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2368651A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2368651A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2368651A13</originalsourceid><addsrcrecordid>eNrjZFD3dQ3x8HdRcPMPUggI8ncJdfb0c1dwVPDw9_HxD1dwc_RTcPJxdHHlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgFGxmYWZqaGjobGRCgBAHnjIwo</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD FOR PRODUCING A HOLLOW FAN BLADE</title><source>esp@cenet</source><creator>KOKSHAROV, NIKOLAY LEONIDOVICH ; MULYUKOV, RADIK RAFIKOVICH ; SAIRANOV, AZAT NAILIEVICH ; LUTFULLIN, RAMIL YAVATOVICH ; KLIMOV, VALERY NIKOLAEVICH ; ANDREYCHENKO, IGOR LEONARDOVICH ; MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH ; SAFIULLIN, RINAT VLADIKOVICH ; RUDENKO, OLEG ALEXANDROVICH ; MOROZOV, MIKHAIL ALEXANDROVICH ; KHARIN, SERGEY ALEXANDROVICH ; DONGAUZER, KONSTANTIN ALEXANDROVICH ; KRUGLOV, ALEXEY ANATOLIEVICH</creator><creatorcontrib>KOKSHAROV, NIKOLAY LEONIDOVICH ; MULYUKOV, RADIK RAFIKOVICH ; SAIRANOV, AZAT NAILIEVICH ; LUTFULLIN, RAMIL YAVATOVICH ; KLIMOV, VALERY NIKOLAEVICH ; ANDREYCHENKO, IGOR LEONARDOVICH ; MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH ; SAFIULLIN, RINAT VLADIKOVICH ; RUDENKO, OLEG ALEXANDROVICH ; MOROZOV, MIKHAIL ALEXANDROVICH ; KHARIN, SERGEY ALEXANDROVICH ; DONGAUZER, KONSTANTIN ALEXANDROVICH ; KRUGLOV, ALEXEY ANATOLIEVICH</creatorcontrib><description>A method for manufacturing a hollow fan blade of a titanium alloy, said blade consisting of skins and a filler forming stiffeners, comprises the step of working skin workpieces with a preformed blade root portion, during which working on surfaces of the skin workpieces, areas to be bonded to a filler workpiece are shaped in the form of projections with a surface flat in a cross-section, and areas to be not bonded to the filler workpiece are shaped in the form of recesses, respectively, wherein at least a part of a surface of recesses opposite to projections in a stack assembled for diffusion welding is made flat in a cross-section, and also comprises the steps of: applying a bond preventing coating onto surfaces of workpiece areas to be not bonded; assembling the skin and filler workpieces into a stack; diffusion welding the skin and filler workpieces; forming stiffeners by superplastic forming, the method further comprises the step of providing the skin and filler workpieces with an aerodynamic profile by applying a deforming load thereto, including forming a pressure face and a suction face of the blade and twisting its airfoil. The method is characterized in that said projections and recesses are made on the surfaces of the skin workpieces prior to providing them with the aerodynamic profile, while the step of providing the workpieces with the aerodynamic profile is performed after diffusion welding. The method is particularly applicable to aircraft engine building.</description><language>eng ; fre ; ger</language><subject>BLASTING ; CLADDING OR PLATING BY SOLDERING OR WELDING ; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ; COMBINED OPERATIONS ; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ; 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 ; MACHINE TOOLS ; MACHINES OR ENGINES IN GENERAL ; MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS ; MECHANICAL ENGINEERING ; MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; OTHER WORKING OF METAL ; PERFORMING OPERATIONS ; PUNCHING METAL ; 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 ; TRANSPORTING ; UNIVERSAL MACHINE TOOLS ; WEAPONS ; WELDING ; WORKING BY LASER BEAM ; WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL</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&amp;date=20110928&amp;DB=EPODOC&amp;CC=EP&amp;NR=2368651A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20110928&amp;DB=EPODOC&amp;CC=EP&amp;NR=2368651A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KOKSHAROV, NIKOLAY LEONIDOVICH</creatorcontrib><creatorcontrib>MULYUKOV, RADIK RAFIKOVICH</creatorcontrib><creatorcontrib>SAIRANOV, AZAT NAILIEVICH</creatorcontrib><creatorcontrib>LUTFULLIN, RAMIL YAVATOVICH</creatorcontrib><creatorcontrib>KLIMOV, VALERY NIKOLAEVICH</creatorcontrib><creatorcontrib>ANDREYCHENKO, IGOR LEONARDOVICH</creatorcontrib><creatorcontrib>MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH</creatorcontrib><creatorcontrib>SAFIULLIN, RINAT VLADIKOVICH</creatorcontrib><creatorcontrib>RUDENKO, OLEG ALEXANDROVICH</creatorcontrib><creatorcontrib>MOROZOV, MIKHAIL ALEXANDROVICH</creatorcontrib><creatorcontrib>KHARIN, SERGEY ALEXANDROVICH</creatorcontrib><creatorcontrib>DONGAUZER, KONSTANTIN ALEXANDROVICH</creatorcontrib><creatorcontrib>KRUGLOV, ALEXEY ANATOLIEVICH</creatorcontrib><title>METHOD FOR PRODUCING A HOLLOW FAN BLADE</title><description>A method for manufacturing a hollow fan blade of a titanium alloy, said blade consisting of skins and a filler forming stiffeners, comprises the step of working skin workpieces with a preformed blade root portion, during which working on surfaces of the skin workpieces, areas to be bonded to a filler workpiece are shaped in the form of projections with a surface flat in a cross-section, and areas to be not bonded to the filler workpiece are shaped in the form of recesses, respectively, wherein at least a part of a surface of recesses opposite to projections in a stack assembled for diffusion welding is made flat in a cross-section, and also comprises the steps of: applying a bond preventing coating onto surfaces of workpiece areas to be not bonded; assembling the skin and filler workpieces into a stack; diffusion welding the skin and filler workpieces; forming stiffeners by superplastic forming, the method further comprises the step of providing the skin and filler workpieces with an aerodynamic profile by applying a deforming load thereto, including forming a pressure face and a suction face of the blade and twisting its airfoil. The method is characterized in that said projections and recesses are made on the surfaces of the skin workpieces prior to providing them with the aerodynamic profile, while the step of providing the workpieces with the aerodynamic profile is performed after diffusion welding. The method is particularly applicable to aircraft engine building.</description><subject>BLASTING</subject><subject>CLADDING OR PLATING BY SOLDERING OR WELDING</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</subject><subject>COMBINED OPERATIONS</subject><subject>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</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>MACHINE TOOLS</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS</subject><subject>MECHANICAL ENGINEERING</subject><subject>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>OTHER WORKING OF METAL</subject><subject>PERFORMING OPERATIONS</subject><subject>PUNCHING METAL</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>TRANSPORTING</subject><subject>UNIVERSAL MACHINE TOOLS</subject><subject>WEAPONS</subject><subject>WELDING</subject><subject>WORKING BY LASER BEAM</subject><subject>WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFD3dQ3x8HdRcPMPUggI8ncJdfb0c1dwVPDw9_HxD1dwc_RTcPJxdHHlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgFGxmYWZqaGjobGRCgBAHnjIwo</recordid><startdate>20110928</startdate><enddate>20110928</enddate><creator>KOKSHAROV, NIKOLAY LEONIDOVICH</creator><creator>MULYUKOV, RADIK RAFIKOVICH</creator><creator>SAIRANOV, AZAT NAILIEVICH</creator><creator>LUTFULLIN, RAMIL YAVATOVICH</creator><creator>KLIMOV, VALERY NIKOLAEVICH</creator><creator>ANDREYCHENKO, IGOR LEONARDOVICH</creator><creator>MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH</creator><creator>SAFIULLIN, RINAT VLADIKOVICH</creator><creator>RUDENKO, OLEG ALEXANDROVICH</creator><creator>MOROZOV, MIKHAIL ALEXANDROVICH</creator><creator>KHARIN, SERGEY ALEXANDROVICH</creator><creator>DONGAUZER, KONSTANTIN ALEXANDROVICH</creator><creator>KRUGLOV, ALEXEY ANATOLIEVICH</creator><scope>EVB</scope></search><sort><creationdate>20110928</creationdate><title>METHOD FOR PRODUCING A HOLLOW FAN BLADE</title><author>KOKSHAROV, NIKOLAY LEONIDOVICH ; MULYUKOV, RADIK RAFIKOVICH ; SAIRANOV, AZAT NAILIEVICH ; LUTFULLIN, RAMIL YAVATOVICH ; KLIMOV, VALERY NIKOLAEVICH ; ANDREYCHENKO, IGOR LEONARDOVICH ; MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH ; SAFIULLIN, RINAT VLADIKOVICH ; RUDENKO, OLEG ALEXANDROVICH ; MOROZOV, MIKHAIL ALEXANDROVICH ; KHARIN, SERGEY ALEXANDROVICH ; DONGAUZER, KONSTANTIN ALEXANDROVICH ; KRUGLOV, ALEXEY ANATOLIEVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2368651A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2011</creationdate><topic>BLASTING</topic><topic>CLADDING OR PLATING BY SOLDERING OR WELDING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COMBINED OPERATIONS</topic><topic>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</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>MACHINE TOOLS</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS</topic><topic>MECHANICAL ENGINEERING</topic><topic>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>OTHER WORKING OF METAL</topic><topic>PERFORMING OPERATIONS</topic><topic>PUNCHING METAL</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>TRANSPORTING</topic><topic>UNIVERSAL MACHINE TOOLS</topic><topic>WEAPONS</topic><topic>WELDING</topic><topic>WORKING BY LASER BEAM</topic><topic>WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL</topic><toplevel>online_resources</toplevel><creatorcontrib>KOKSHAROV, NIKOLAY LEONIDOVICH</creatorcontrib><creatorcontrib>MULYUKOV, RADIK RAFIKOVICH</creatorcontrib><creatorcontrib>SAIRANOV, AZAT NAILIEVICH</creatorcontrib><creatorcontrib>LUTFULLIN, RAMIL YAVATOVICH</creatorcontrib><creatorcontrib>KLIMOV, VALERY NIKOLAEVICH</creatorcontrib><creatorcontrib>ANDREYCHENKO, IGOR LEONARDOVICH</creatorcontrib><creatorcontrib>MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH</creatorcontrib><creatorcontrib>SAFIULLIN, RINAT VLADIKOVICH</creatorcontrib><creatorcontrib>RUDENKO, OLEG ALEXANDROVICH</creatorcontrib><creatorcontrib>MOROZOV, MIKHAIL ALEXANDROVICH</creatorcontrib><creatorcontrib>KHARIN, SERGEY ALEXANDROVICH</creatorcontrib><creatorcontrib>DONGAUZER, KONSTANTIN ALEXANDROVICH</creatorcontrib><creatorcontrib>KRUGLOV, ALEXEY ANATOLIEVICH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KOKSHAROV, NIKOLAY LEONIDOVICH</au><au>MULYUKOV, RADIK RAFIKOVICH</au><au>SAIRANOV, AZAT NAILIEVICH</au><au>LUTFULLIN, RAMIL YAVATOVICH</au><au>KLIMOV, VALERY NIKOLAEVICH</au><au>ANDREYCHENKO, IGOR LEONARDOVICH</au><au>MUKHAMETRAKHIMOV, MINNAUL KHIDIYATOVICH</au><au>SAFIULLIN, RINAT VLADIKOVICH</au><au>RUDENKO, OLEG ALEXANDROVICH</au><au>MOROZOV, MIKHAIL ALEXANDROVICH</au><au>KHARIN, SERGEY ALEXANDROVICH</au><au>DONGAUZER, KONSTANTIN ALEXANDROVICH</au><au>KRUGLOV, ALEXEY ANATOLIEVICH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD FOR PRODUCING A HOLLOW FAN BLADE</title><date>2011-09-28</date><risdate>2011</risdate><abstract>A method for manufacturing a hollow fan blade of a titanium alloy, said blade consisting of skins and a filler forming stiffeners, comprises the step of working skin workpieces with a preformed blade root portion, during which working on surfaces of the skin workpieces, areas to be bonded to a filler workpiece are shaped in the form of projections with a surface flat in a cross-section, and areas to be not bonded to the filler workpiece are shaped in the form of recesses, respectively, wherein at least a part of a surface of recesses opposite to projections in a stack assembled for diffusion welding is made flat in a cross-section, and also comprises the steps of: applying a bond preventing coating onto surfaces of workpiece areas to be not bonded; assembling the skin and filler workpieces into a stack; diffusion welding the skin and filler workpieces; forming stiffeners by superplastic forming, the method further comprises the step of providing the skin and filler workpieces with an aerodynamic profile by applying a deforming load thereto, including forming a pressure face and a suction face of the blade and twisting its airfoil. The method is characterized in that said projections and recesses are made on the surfaces of the skin workpieces prior to providing them with the aerodynamic profile, while the step of providing the workpieces with the aerodynamic profile is performed after diffusion welding. The method is particularly applicable to aircraft engine building.</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
CLADDING OR PLATING BY SOLDERING OR WELDING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBINED OPERATIONS
CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING
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
MACHINE TOOLS
MACHINES OR ENGINES IN GENERAL
MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS
MECHANICAL ENGINEERING
MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL
METAL-WORKING NOT OTHERWISE PROVIDED FOR
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
OTHER WORKING OF METAL
PERFORMING OPERATIONS
PUNCHING METAL
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
TRANSPORTING
UNIVERSAL MACHINE TOOLS
WEAPONS
WELDING
WORKING BY LASER BEAM
WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL
title METHOD FOR PRODUCING A HOLLOW FAN BLADE
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