FEDERELEMENTE AUS KERAMISCHEN FASERN
Die vorliegende Erfindung betrifft ein Federelement für Hochtemperaturanwendungen, insbesondere für Strömungsmaschinen, wie Gasturbinen oder Flugtriebwerke, sowie entsprechende Strömungsmaschinen, wobei das Federelement eine Vielzahl von keramischen Fasern umfasst, die mindestens ein Faserelement (4...
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| creator | Sikorski, Siegfried Hofmann, Severin Heller, Lothar |
| description | Die vorliegende Erfindung betrifft ein Federelement für Hochtemperaturanwendungen, insbesondere für Strömungsmaschinen, wie Gasturbinen oder Flugtriebwerke, sowie entsprechende Strömungsmaschinen, wobei das Federelement eine Vielzahl von keramischen Fasern umfasst, die mindestens ein Faserelement (4,5) bilden, wobei das Federelement zwei oder mehr Basiselemente (2,3) aufweist, zwischen denen das mindestens eine Faserelement zumindest teilweise angeordnet ist.
The invention relates to a spring element for high-temperature applications, in particular for continuous-flow machines, such as gas turbines or aircraft engines, as well as corresponding continuous-flow machines, wherein the spring element comprises a plurality of ceramic fibres forming at least one fibre element (4, 5), wherein the spring element has one, two or more base elements (2, 3) on which or between which at least parts of the at least one fibre element are arranged. |
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The invention relates to a spring element for high-temperature applications, in particular for continuous-flow machines, such as gas turbines or aircraft engines, as well as corresponding continuous-flow machines, wherein the spring element comprises a plurality of ceramic fibres forming at least one fibre element (4, 5), wherein the spring element has one, two or more base elements (2, 3) on which or between which at least parts of the at least one fibre element are arranged.</description><language>ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; GAS-TURBINE PLANTS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MEANS FOR DAMPING VIBRATION ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; SHOCK-ABSORBERS ; SPRINGS ; STEAM ENGINES ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2021</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=20210318&DB=EPODOC&CC=DE&NR=102019214231A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210318&DB=EPODOC&CC=DE&NR=102019214231A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Sikorski, Siegfried</creatorcontrib><creatorcontrib>Hofmann, Severin</creatorcontrib><creatorcontrib>Heller, Lothar</creatorcontrib><title>FEDERELEMENTE AUS KERAMISCHEN FASERN</title><description>Die vorliegende Erfindung betrifft ein Federelement für Hochtemperaturanwendungen, insbesondere für Strömungsmaschinen, wie Gasturbinen oder Flugtriebwerke, sowie entsprechende Strömungsmaschinen, wobei das Federelement eine Vielzahl von keramischen Fasern umfasst, die mindestens ein Faserelement (4,5) bilden, wobei das Federelement zwei oder mehr Basiselemente (2,3) aufweist, zwischen denen das mindestens eine Faserelement zumindest teilweise angeordnet ist.
The invention relates to a spring element for high-temperature applications, in particular for continuous-flow machines, such as gas turbines or aircraft engines, as well as corresponding continuous-flow machines, wherein the spring element comprises a plurality of ceramic fibres forming at least one fibre element (4, 5), wherein the spring element has one, two or more base elements (2, 3) on which or between which at least parts of the at least one fibre element are arranged.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MEANS FOR DAMPING VIBRATION</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>SHOCK-ABSORBERS</subject><subject>SPRINGS</subject><subject>STEAM ENGINES</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBxc3VxDXL1cfV19QtxVXAMDVbwdg1y9PUMdvZw9VNwcwx2DfLjYWBNS8wpTuWF0twMqm6uIc4euqkF-fGpxQWJyal5qSXxLq6GBkYGhpZGhiZGxoaOhsbEqgMAhegkYA</recordid><startdate>20210318</startdate><enddate>20210318</enddate><creator>Sikorski, Siegfried</creator><creator>Hofmann, Severin</creator><creator>Heller, Lothar</creator><scope>EVB</scope></search><sort><creationdate>20210318</creationdate><title>FEDERELEMENTE AUS KERAMISCHEN FASERN</title><author>Sikorski, Siegfried ; Hofmann, Severin ; Heller, Lothar</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE102019214231A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>2021</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MEANS FOR DAMPING VIBRATION</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>SHOCK-ABSORBERS</topic><topic>SPRINGS</topic><topic>STEAM ENGINES</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Sikorski, Siegfried</creatorcontrib><creatorcontrib>Hofmann, Severin</creatorcontrib><creatorcontrib>Heller, Lothar</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Sikorski, Siegfried</au><au>Hofmann, Severin</au><au>Heller, Lothar</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>FEDERELEMENTE AUS KERAMISCHEN FASERN</title><date>2021-03-18</date><risdate>2021</risdate><abstract>Die vorliegende Erfindung betrifft ein Federelement für Hochtemperaturanwendungen, insbesondere für Strömungsmaschinen, wie Gasturbinen oder Flugtriebwerke, sowie entsprechende Strömungsmaschinen, wobei das Federelement eine Vielzahl von keramischen Fasern umfasst, die mindestens ein Faserelement (4,5) bilden, wobei das Federelement zwei oder mehr Basiselemente (2,3) aufweist, zwischen denen das mindestens eine Faserelement zumindest teilweise angeordnet ist.
The invention relates to a spring element for high-temperature applications, in particular for continuous-flow machines, such as gas turbines or aircraft engines, as well as corresponding continuous-flow machines, wherein the spring element comprises a plurality of ceramic fibres forming at least one fibre element (4, 5), wherein the spring element has one, two or more base elements (2, 3) on which or between which at least parts of the at least one fibre element are arranged.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES SHOCK-ABSORBERS SPRINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS |
| title | FEDERELEMENTE AUS KERAMISCHEN FASERN |
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