Superior Fatigue Properties for Blended Elemental P/M Ti-6Al-4V
Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Abkowitz, Stanley [verfasserIn] |
|---|
| Format: |
E-Artikel |
|---|---|
| Sprache: |
Englisch |
| Erschienen: |
1986 |
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| Schlagwörter: |
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| Anmerkung: |
© TMS 1986 |
|---|
| Übergeordnetes Werk: |
Enthalten in: JOM - New York, NY : Springer Science + Business Media, 1989, 38(1986), 8 vom: Aug., Seite 36-39 |
|---|---|
| Übergeordnetes Werk: |
volume:38 ; year:1986 ; number:8 ; month:08 ; pages:36-39 |
| Links: |
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| DOI / URN: |
10.1007/BF03257786 |
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| 520 | |a Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. | ||
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10.1007/BF03257786 doi (DE-627)SPR022683518 (SPR)BF03257786-e DE-627 ger DE-627 rakwb eng Abkowitz, Stanley verfasserin aut Superior Fatigue Properties for Blended Elemental P/M Ti-6Al-4V 1986 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © TMS 1986 Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. Fatigue (dpeaa)DE-He213 Fatigue Performance (dpeaa)DE-He213 Titanium Sponge (dpeaa)DE-He213 Prealloyed Powder (dpeaa)DE-He213 Blended Elemental (dpeaa)DE-He213 Rowell, David aut Enthalten in JOM New York, NY : Springer Science + Business Media, 1989 38(1986), 8 vom: Aug., Seite 36-39 (DE-627)31368197X (DE-600)2002726-6 1543-1851 nnns volume:38 year:1986 number:8 month:08 pages:36-39 https://dx.doi.org/10.1007/BF03257786 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER AR 38 1986 8 08 36-39 |
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10.1007/BF03257786 doi (DE-627)SPR022683518 (SPR)BF03257786-e DE-627 ger DE-627 rakwb eng Abkowitz, Stanley verfasserin aut Superior Fatigue Properties for Blended Elemental P/M Ti-6Al-4V 1986 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © TMS 1986 Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. Fatigue (dpeaa)DE-He213 Fatigue Performance (dpeaa)DE-He213 Titanium Sponge (dpeaa)DE-He213 Prealloyed Powder (dpeaa)DE-He213 Blended Elemental (dpeaa)DE-He213 Rowell, David aut Enthalten in JOM New York, NY : Springer Science + Business Media, 1989 38(1986), 8 vom: Aug., Seite 36-39 (DE-627)31368197X (DE-600)2002726-6 1543-1851 nnns volume:38 year:1986 number:8 month:08 pages:36-39 https://dx.doi.org/10.1007/BF03257786 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER AR 38 1986 8 08 36-39 |
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10.1007/BF03257786 doi (DE-627)SPR022683518 (SPR)BF03257786-e DE-627 ger DE-627 rakwb eng Abkowitz, Stanley verfasserin aut Superior Fatigue Properties for Blended Elemental P/M Ti-6Al-4V 1986 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © TMS 1986 Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. Fatigue (dpeaa)DE-He213 Fatigue Performance (dpeaa)DE-He213 Titanium Sponge (dpeaa)DE-He213 Prealloyed Powder (dpeaa)DE-He213 Blended Elemental (dpeaa)DE-He213 Rowell, David aut Enthalten in JOM New York, NY : Springer Science + Business Media, 1989 38(1986), 8 vom: Aug., Seite 36-39 (DE-627)31368197X (DE-600)2002726-6 1543-1851 nnns volume:38 year:1986 number:8 month:08 pages:36-39 https://dx.doi.org/10.1007/BF03257786 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER AR 38 1986 8 08 36-39 |
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10.1007/BF03257786 doi (DE-627)SPR022683518 (SPR)BF03257786-e DE-627 ger DE-627 rakwb eng Abkowitz, Stanley verfasserin aut Superior Fatigue Properties for Blended Elemental P/M Ti-6Al-4V 1986 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © TMS 1986 Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. Fatigue (dpeaa)DE-He213 Fatigue Performance (dpeaa)DE-He213 Titanium Sponge (dpeaa)DE-He213 Prealloyed Powder (dpeaa)DE-He213 Blended Elemental (dpeaa)DE-He213 Rowell, David aut Enthalten in JOM New York, NY : Springer Science + Business Media, 1989 38(1986), 8 vom: Aug., Seite 36-39 (DE-627)31368197X (DE-600)2002726-6 1543-1851 nnns volume:38 year:1986 number:8 month:08 pages:36-39 https://dx.doi.org/10.1007/BF03257786 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER AR 38 1986 8 08 36-39 |
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10.1007/BF03257786 doi (DE-627)SPR022683518 (SPR)BF03257786-e DE-627 ger DE-627 rakwb eng Abkowitz, Stanley verfasserin aut Superior Fatigue Properties for Blended Elemental P/M Ti-6Al-4V 1986 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © TMS 1986 Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. Fatigue (dpeaa)DE-He213 Fatigue Performance (dpeaa)DE-He213 Titanium Sponge (dpeaa)DE-He213 Prealloyed Powder (dpeaa)DE-He213 Blended Elemental (dpeaa)DE-He213 Rowell, David aut Enthalten in JOM New York, NY : Springer Science + Business Media, 1989 38(1986), 8 vom: Aug., Seite 36-39 (DE-627)31368197X (DE-600)2002726-6 1543-1851 nnns volume:38 year:1986 number:8 month:08 pages:36-39 https://dx.doi.org/10.1007/BF03257786 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER AR 38 1986 8 08 36-39 |
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Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. © TMS 1986 |
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Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. © TMS 1986 |
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Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications. © TMS 1986 |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR022683518</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230330070255.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">201006s1986 xx |||||o 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/BF03257786</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR022683518</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)BF03257786-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Abkowitz, Stanley</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Superior Fatigue Properties for Blended Elemental P/M Ti-6Al-4V</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">1986</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© TMS 1986</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract This report represents the successful culmination of many years of developmental work with blended elemental (BE) P/M titanium alloys. Although the appreciable cost savings possible through utilization of cold isostatically pressed near-net shape titanium components has been recognized for several years, applications have been somewhat limited by the less than optimal fatigue performance of these P/M alloys. The recent completion of fatigue testing on reduced chloride P/M Ti-6Al-4V alloys has demonstrated the achievement of wrought equivalent fatigue properties. This data supplements the wrought equivalent tensile properties previously achieved. By virtue of these advances, cost effective blended elemental titanium components can now satisfy the most demanding requirements in industrial and aerospace applications.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Fatigue</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Fatigue Performance</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Titanium Sponge</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Prealloyed Powder</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Blended Elemental</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Rowell, David</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">JOM</subfield><subfield code="d">New York, NY : Springer Science + Business Media, 1989</subfield><subfield code="g">38(1986), 8 vom: Aug., Seite 36-39</subfield><subfield code="w">(DE-627)31368197X</subfield><subfield code="w">(DE-600)2002726-6</subfield><subfield code="x">1543-1851</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:38</subfield><subfield code="g">year:1986</subfield><subfield code="g">number:8</subfield><subfield code="g">month:08</subfield><subfield code="g">pages:36-39</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://dx.doi.org/10.1007/BF03257786</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_SPRINGER</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">38</subfield><subfield code="j">1986</subfield><subfield code="e">8</subfield><subfield code="c">08</subfield><subfield code="h">36-39</subfield></datafield></record></collection>
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