Heat Resisting Metals for Gas Turbine Parts (N-102) - Chromium- Base Alloys
Results of a 42-month search for heat resistant metals for gas turbine blades which ended in the development of a new series of alloys of which the principal element of the series is chromium. The chromium rich portions of thirteen binary and nine ternary systems of chromium have been surveyed. Meth...
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description | Results of a 42-month search for heat resistant metals for gas turbine blades which ended in the development of a new series of alloys of which the principal element of the series is chromium. The chromium rich portions of thirteen binary and nine ternary systems of chromium have been surveyed. Methods of melting, purifying, casting, and machining the alloys have been devised. Stress-rupture properties of certain of the chromium-based alloys are superior to those of all other materials known to have been tested. |
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The chromium rich portions of thirteen binary and nine ternary systems of chromium have been surveyed. Methods of melting, purifying, casting, and machining the alloys have been devised. Stress-rupture properties of certain of the chromium-based alloys are superior to those of all other materials known to have been tested.</description><language>eng</language><subject>ATI COLLECTION ; ATI-8908 ; CHROMIUM ALLOYS ; GAS TURBINES ; HEAT RESISTANT METALS ; Jet and Gas Turbine Engines ; Properties of Metals and Alloys</subject><creationdate>1945</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27546,27547</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADB808050$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Parke, Robert M</creatorcontrib><creatorcontrib>Herzig, Alvin J</creatorcontrib><creatorcontrib>CLIMAX MOLYBDENUM CO OF MICHIGAN DETROIT</creatorcontrib><title>Heat Resisting Metals for Gas Turbine Parts (N-102) - Chromium- Base Alloys</title><description>Results of a 42-month search for heat resistant metals for gas turbine blades which ended in the development of a new series of alloys of which the principal element of the series is chromium. The chromium rich portions of thirteen binary and nine ternary systems of chromium have been surveyed. Methods of melting, purifying, casting, and machining the alloys have been devised. Stress-rupture properties of certain of the chromium-based alloys are superior to those of all other materials known to have been tested.</description><subject>ATI COLLECTION</subject><subject>ATI-8908</subject><subject>CHROMIUM ALLOYS</subject><subject>GAS TURBINES</subject><subject>HEAT RESISTANT METALS</subject><subject>Jet and Gas Turbine Engines</subject><subject>Properties of Metals and Alloys</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1945</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZPD2SE0sUQhKLc4sLsnMS1fwTS1JzClWSMsvUnBPLFYIKS1KysxLVQhILCopVtDw0zU0MNJU0FVwzijKz80szdVVcEosTlVwzMnJryzmYWBNA2pO5YXS3Awybq4hzh66KSWZyfEg81NL4h1dnCwMLAxMDYwJSAMAAxQviw</recordid><startdate>19451128</startdate><enddate>19451128</enddate><creator>Parke, Robert M</creator><creator>Herzig, Alvin J</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19451128</creationdate><title>Heat Resisting Metals for Gas Turbine Parts (N-102) - Chromium- Base Alloys</title><author>Parke, Robert M ; Herzig, Alvin J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADB8080503</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1945</creationdate><topic>ATI COLLECTION</topic><topic>ATI-8908</topic><topic>CHROMIUM ALLOYS</topic><topic>GAS TURBINES</topic><topic>HEAT RESISTANT METALS</topic><topic>Jet and Gas Turbine Engines</topic><topic>Properties of Metals and Alloys</topic><toplevel>online_resources</toplevel><creatorcontrib>Parke, Robert M</creatorcontrib><creatorcontrib>Herzig, Alvin J</creatorcontrib><creatorcontrib>CLIMAX MOLYBDENUM CO OF MICHIGAN DETROIT</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Parke, Robert M</au><au>Herzig, Alvin J</au><aucorp>CLIMAX MOLYBDENUM CO OF MICHIGAN DETROIT</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Heat Resisting Metals for Gas Turbine Parts (N-102) - Chromium- Base Alloys</btitle><date>1945-11-28</date><risdate>1945</risdate><abstract>Results of a 42-month search for heat resistant metals for gas turbine blades which ended in the development of a new series of alloys of which the principal element of the series is chromium. The chromium rich portions of thirteen binary and nine ternary systems of chromium have been surveyed. Methods of melting, purifying, casting, and machining the alloys have been devised. Stress-rupture properties of certain of the chromium-based alloys are superior to those of all other materials known to have been tested.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | ATI COLLECTION ATI-8908 CHROMIUM ALLOYS GAS TURBINES HEAT RESISTANT METALS Jet and Gas Turbine Engines Properties of Metals and Alloys |
title | Heat Resisting Metals for Gas Turbine Parts (N-102) - Chromium- Base Alloys |
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