GAS TURBINE BLADE WITH INTEGRATED PYROMETER PROBE
Diese Erfindung betrifft eine Gasturbinenschaufel (10), welche bei regulärer Benutzung eine Saugseite (11) wie auch eine Druckseite (12) hat, und welche weiterhin wenigstens eine innerlich angeordnete Kammer (15) aufweist, die dazu ausgebildet ist, bei regulärer Benutzung ein Kühlfluid (16) zu leite...
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| creator | Dahlke, Stefan Ehrlich, Tom |
| description | Diese Erfindung betrifft eine Gasturbinenschaufel (10), welche bei regulärer Benutzung eine Saugseite (11) wie auch eine Druckseite (12) hat, und welche weiterhin wenigstens eine innerlich angeordnete Kammer (15) aufweist, die dazu ausgebildet ist, bei regulärer Benutzung ein Kühlfluid (16) zu leiten, wobei in die wenigstens eine Kammer (15) eine Pyrometersonde (20) so integriert ist, dass ein Messabschnitt (21) der Pyrometersonde (20) an einer Öffnung (17) auf einer der beiden Seiten (11, 12) der Gasturbinenschaufel (10) angeordnet ist, so dass über die Öffnung (17) elektromagnetische Strahlung aus der Umgebung dem Messabschnitt (21) zuführbar ist.
This invention relates to a gas turbine blade (10), which has a suction side (11) and a pressure side (12) during regular use and which also has at least one internally arranged chamber (15), which is designed to conduct a cooling fluid (16) during regular use, wherein a pyrometer probe (20) is integrated into the at least one chamber (15) in such a way that a measuring section (21) of the pyrometer probe (20) is arranged at an opening (17) on one of the two sides (11, 12) of the gas turbine blade (10) such that electromagnetic radiation can be fed from the surroundings to the measuring section (21) via the opening (17). |
| format | Patent |
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This invention relates to a gas turbine blade (10), which has a suction side (11) and a pressure side (12) during regular use and which also has at least one internally arranged chamber (15), which is designed to conduct a cooling fluid (16) during regular use, wherein a pyrometer probe (20) is integrated into the at least one chamber (15) in such a way that a measuring section (21) of the pyrometer probe (20) is arranged at an opening (17) on one of the two sides (11, 12) of the gas turbine blade (10) such that electromagnetic radiation can be fed from the surroundings to the measuring section (21) via the opening (17).</description><language>eng ; fre ; ger</language><subject>BLASTING ; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ; COLORIMETRY ; ENGINE PLANTS IN GENERAL ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT,POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED,VISIBLE OR ULTRA-VIOLET LIGHT ; MEASURING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PHYSICS ; RADIATION PYROMETRY ; 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 ; WEAPONS</subject><creationdate>2018</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&date=20180620&DB=EPODOC&CC=EP&NR=3336497A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180620&DB=EPODOC&CC=EP&NR=3336497A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Dahlke, Stefan</creatorcontrib><creatorcontrib>Ehrlich, Tom</creatorcontrib><title>GAS TURBINE BLADE WITH INTEGRATED PYROMETER PROBE</title><description>Diese Erfindung betrifft eine Gasturbinenschaufel (10), welche bei regulärer Benutzung eine Saugseite (11) wie auch eine Druckseite (12) hat, und welche weiterhin wenigstens eine innerlich angeordnete Kammer (15) aufweist, die dazu ausgebildet ist, bei regulärer Benutzung ein Kühlfluid (16) zu leiten, wobei in die wenigstens eine Kammer (15) eine Pyrometersonde (20) so integriert ist, dass ein Messabschnitt (21) der Pyrometersonde (20) an einer Öffnung (17) auf einer der beiden Seiten (11, 12) der Gasturbinenschaufel (10) angeordnet ist, so dass über die Öffnung (17) elektromagnetische Strahlung aus der Umgebung dem Messabschnitt (21) zuführbar ist.
This invention relates to a gas turbine blade (10), which has a suction side (11) and a pressure side (12) during regular use and which also has at least one internally arranged chamber (15), which is designed to conduct a cooling fluid (16) during regular use, wherein a pyrometer probe (20) is integrated into the at least one chamber (15) in such a way that a measuring section (21) of the pyrometer probe (20) is arranged at an opening (17) on one of the two sides (11, 12) of the gas turbine blade (10) such that electromagnetic radiation can be fed from the surroundings to the measuring section (21) via the opening (17).</description><subject>BLASTING</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</subject><subject>COLORIMETRY</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>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT,POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED,VISIBLE OR ULTRA-VIOLET LIGHT</subject><subject>MEASURING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PHYSICS</subject><subject>RADIATION PYROMETRY</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>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB0dwxWCAkNcvL0c1Vw8nF0cVUI9wzxUPD0C3F1D3IMcXVRCIgM8vd1DXENUggI8ndy5WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxsbGZiaW5o6GxkQoAQAFAiY0</recordid><startdate>20180620</startdate><enddate>20180620</enddate><creator>Dahlke, Stefan</creator><creator>Ehrlich, Tom</creator><scope>EVB</scope></search><sort><creationdate>20180620</creationdate><title>GAS TURBINE BLADE WITH INTEGRATED PYROMETER PROBE</title><author>Dahlke, Stefan ; Ehrlich, Tom</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3336497A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>BLASTING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COLORIMETRY</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>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT,POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED,VISIBLE OR ULTRA-VIOLET LIGHT</topic><topic>MEASURING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PHYSICS</topic><topic>RADIATION PYROMETRY</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>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Dahlke, Stefan</creatorcontrib><creatorcontrib>Ehrlich, Tom</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Dahlke, Stefan</au><au>Ehrlich, Tom</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE BLADE WITH INTEGRATED PYROMETER PROBE</title><date>2018-06-20</date><risdate>2018</risdate><abstract>Diese Erfindung betrifft eine Gasturbinenschaufel (10), welche bei regulärer Benutzung eine Saugseite (11) wie auch eine Druckseite (12) hat, und welche weiterhin wenigstens eine innerlich angeordnete Kammer (15) aufweist, die dazu ausgebildet ist, bei regulärer Benutzung ein Kühlfluid (16) zu leiten, wobei in die wenigstens eine Kammer (15) eine Pyrometersonde (20) so integriert ist, dass ein Messabschnitt (21) der Pyrometersonde (20) an einer Öffnung (17) auf einer der beiden Seiten (11, 12) der Gasturbinenschaufel (10) angeordnet ist, so dass über die Öffnung (17) elektromagnetische Strahlung aus der Umgebung dem Messabschnitt (21) zuführbar ist.
This invention relates to a gas turbine blade (10), which has a suction side (11) and a pressure side (12) during regular use and which also has at least one internally arranged chamber (15), which is designed to conduct a cooling fluid (16) during regular use, wherein a pyrometer probe (20) is integrated into the at least one chamber (15) in such a way that a measuring section (21) of the pyrometer probe (20) is arranged at an opening (17) on one of the two sides (11, 12) of the gas turbine blade (10) such that electromagnetic radiation can be fed from the surroundings to the measuring section (21) via the opening (17).</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COLORIMETRY ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT,POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED,VISIBLE OR ULTRA-VIOLET LIGHT MEASURING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS RADIATION PYROMETRY 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 WEAPONS |
| title | GAS TURBINE BLADE WITH INTEGRATED PYROMETER PROBE |
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