Multi-part dovetail repair broach assembly and methods of use
The present invention relates to a broach assembly for cutting surfaces in a slot and particularly relates to a broach assembly for use in a turbine for cutting active surfaces of dovetail slots and methods of cutting the slots. The broach assembly includes alternate spacers and cutters arranged in...
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creator | Nolan, John Francis Pollock, Ralph Arnold Fischer, Todd Joseph |
description | The present invention relates to a broach assembly for cutting surfaces in a slot and particularly relates to a broach assembly for use in a turbine for cutting active surfaces of dovetail slots and methods of cutting the slots.
The broach assembly includes alternate spacers and cutters arranged in a sub-assembly having a lead at a leading end and a lag at a trailing end. The cutters have side margins in excess of the margins of the spacers for cutting material from the dovetail slots of the turbine wheel as the broach assembly passes through the slots. The bottom or apices of each spacer and cutter are tapered to form a continuously tapered surface along the bottom of the broach assembly. Upon passing the broach assembly through the slot, the assembly is progressively displaced in a radial outward direction to progressively cut the active dovetail slot surfaces. Shims may be disposed in the bottom of the slot to further displace the broach assembly radially outwardly in multiple passes. |
format | Patent |
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The broach assembly includes alternate spacers and cutters arranged in a sub-assembly having a lead at a leading end and a lag at a trailing end. The cutters have side margins in excess of the margins of the spacers for cutting material from the dovetail slots of the turbine wheel as the broach assembly passes through the slots. The bottom or apices of each spacer and cutter are tapered to form a continuously tapered surface along the bottom of the broach assembly. Upon passing the broach assembly through the slot, the assembly is progressively displaced in a radial outward direction to progressively cut the active dovetail slot surfaces. Shims may be disposed in the bottom of the slot to further displace the broach assembly radially outwardly in multiple passes.</description><language>eng</language><creationdate>2004</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6676336$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,776,798,881,64012</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6676336$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Nolan, John Francis</creatorcontrib><creatorcontrib>Pollock, Ralph Arnold</creatorcontrib><creatorcontrib>Fischer, Todd Joseph</creatorcontrib><creatorcontrib>General Electric Company</creatorcontrib><title>Multi-part dovetail repair broach assembly and methods of use</title><description>The present invention relates to a broach assembly for cutting surfaces in a slot and particularly relates to a broach assembly for use in a turbine for cutting active surfaces of dovetail slots and methods of cutting the slots.
The broach assembly includes alternate spacers and cutters arranged in a sub-assembly having a lead at a leading end and a lag at a trailing end. The cutters have side margins in excess of the margins of the spacers for cutting material from the dovetail slots of the turbine wheel as the broach assembly passes through the slots. The bottom or apices of each spacer and cutter are tapered to form a continuously tapered surface along the bottom of the broach assembly. Upon passing the broach assembly through the slot, the assembly is progressively displaced in a radial outward direction to progressively cut the active dovetail slot surfaces. Shims may be disposed in the bottom of the slot to further displace the broach assembly radially outwardly in multiple passes.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2004</creationdate><recordtype>patent</recordtype><sourceid>EFH</sourceid><recordid>eNrjZLD1Lc0pydQtSCwqUUjJL0stSczMUShKLUjMLFJIKspPTM5QSCwuTs1NyqlUSMxLUchNLcnITylWyE9TKC1O5WFgTUvMKU7lhdLcDApuriHOHrqlxQWJJal5JcXx6UWJIMrAzMzczNjYzJgIJQDlVTD-</recordid><startdate>20040113</startdate><enddate>20040113</enddate><creator>Nolan, John Francis</creator><creator>Pollock, Ralph Arnold</creator><creator>Fischer, Todd Joseph</creator><scope>EFH</scope></search><sort><creationdate>20040113</creationdate><title>Multi-part dovetail repair broach assembly and methods of use</title><author>Nolan, John Francis ; Pollock, Ralph Arnold ; Fischer, Todd Joseph</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_066763363</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2004</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Nolan, John Francis</creatorcontrib><creatorcontrib>Pollock, Ralph Arnold</creatorcontrib><creatorcontrib>Fischer, Todd Joseph</creatorcontrib><creatorcontrib>General Electric Company</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Nolan, John Francis</au><au>Pollock, Ralph Arnold</au><au>Fischer, Todd Joseph</au><aucorp>General Electric Company</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Multi-part dovetail repair broach assembly and methods of use</title><date>2004-01-13</date><risdate>2004</risdate><abstract>The present invention relates to a broach assembly for cutting surfaces in a slot and particularly relates to a broach assembly for use in a turbine for cutting active surfaces of dovetail slots and methods of cutting the slots.
The broach assembly includes alternate spacers and cutters arranged in a sub-assembly having a lead at a leading end and a lag at a trailing end. The cutters have side margins in excess of the margins of the spacers for cutting material from the dovetail slots of the turbine wheel as the broach assembly passes through the slots. The bottom or apices of each spacer and cutter are tapered to form a continuously tapered surface along the bottom of the broach assembly. Upon passing the broach assembly through the slot, the assembly is progressively displaced in a radial outward direction to progressively cut the active dovetail slot surfaces. Shims may be disposed in the bottom of the slot to further displace the broach assembly radially outwardly in multiple passes.</abstract><oa>free_for_read</oa></addata></record> |
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title | Multi-part dovetail repair broach assembly and methods of use |
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