TURBOFAN CASE AND METHOD OF MAKING
A casing for a gas turbine includes a fan case, an intermediate case and a gas generator case integrated with one another. In another aspect, the casing provides a construction including several aspects which improve structural efficiency, such as a semi-monocoque construction, improved strut design...
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| creator | LOBO, KEVIN WEINBERG, MAURICE LIU, QUANTAL ELEFTHERIOU, ANDREAS |
| description | A casing for a gas turbine includes a fan case, an intermediate case and a gas generator case integrated with one another. In another aspect, the casing provides a construction including several aspects which improve structural efficiency, such as a semi-monocoque construction, improved strut design, etc. Improved load paths and means for transmitting loads in the engine case are also disclosed.
L'enveloppe d'une turbine à gaz comprend le carter du ventilateur, le carter intermédiaire et le carter du générateur de gaz, ces trois éléments étant emboîtés les uns dans les autres. Dans un autre mode de réalisation, l'enveloppe est configurée différemment afin d'inclure plusieurs aspects qui améliorent l'efficacité structurelle, comme une configuration en semi-monocoque ou une conception en caisson améliorée. Les chemins de charge améliorés et les moyens de transmettre les charges dans le carter de moteur sont également fournis. |
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L'enveloppe d'une turbine à gaz comprend le carter du ventilateur, le carter intermédiaire et le carter du générateur de gaz, ces trois éléments étant emboîtés les uns dans les autres. Dans un autre mode de réalisation, l'enveloppe est configurée différemment afin d'inclure plusieurs aspects qui améliorent l'efficacité structurelle, comme une configuration en semi-monocoque ou une conception en caisson améliorée. Les chemins de charge améliorés et les moyens de transmettre les charges dans le carter de moteur sont également fournis.</description><language>eng ; fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2013</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=20130409&DB=EPODOC&CC=CA&NR=2776254C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130409&DB=EPODOC&CC=CA&NR=2776254C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LOBO, KEVIN</creatorcontrib><creatorcontrib>WEINBERG, MAURICE</creatorcontrib><creatorcontrib>LIU, QUANTAL</creatorcontrib><creatorcontrib>ELEFTHERIOU, ANDREAS</creatorcontrib><title>TURBOFAN CASE AND METHOD OF MAKING</title><description>A casing for a gas turbine includes a fan case, an intermediate case and a gas generator case integrated with one another. In another aspect, the casing provides a construction including several aspects which improve structural efficiency, such as a semi-monocoque construction, improved strut design, etc. Improved load paths and means for transmitting loads in the engine case are also disclosed.
L'enveloppe d'une turbine à gaz comprend le carter du ventilateur, le carter intermédiaire et le carter du générateur de gaz, ces trois éléments étant emboîtés les uns dans les autres. Dans un autre mode de réalisation, l'enveloppe est configurée différemment afin d'inclure plusieurs aspects qui améliorent l'efficacité structurelle, comme une configuration en semi-monocoque ou une conception en caisson améliorée. Les chemins de charge améliorés et les moyens de transmettre les charges dans le carter de moteur sont également fournis.</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>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAKCQ1y8ndz9FNwdgx2VXD0c1HwdQ3x8HdR8HdT8HX09vRz52FgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8c6ORubmZkamJs7GhFUAAIylIS4</recordid><startdate>20130409</startdate><enddate>20130409</enddate><creator>LOBO, KEVIN</creator><creator>WEINBERG, MAURICE</creator><creator>LIU, QUANTAL</creator><creator>ELEFTHERIOU, ANDREAS</creator><scope>EVB</scope></search><sort><creationdate>20130409</creationdate><title>TURBOFAN CASE AND METHOD OF MAKING</title><author>LOBO, KEVIN ; WEINBERG, MAURICE ; LIU, QUANTAL ; ELEFTHERIOU, ANDREAS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2776254C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2013</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>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>LOBO, KEVIN</creatorcontrib><creatorcontrib>WEINBERG, MAURICE</creatorcontrib><creatorcontrib>LIU, QUANTAL</creatorcontrib><creatorcontrib>ELEFTHERIOU, ANDREAS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LOBO, KEVIN</au><au>WEINBERG, MAURICE</au><au>LIU, QUANTAL</au><au>ELEFTHERIOU, ANDREAS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBOFAN CASE AND METHOD OF MAKING</title><date>2013-04-09</date><risdate>2013</risdate><abstract>A casing for a gas turbine includes a fan case, an intermediate case and a gas generator case integrated with one another. In another aspect, the casing provides a construction including several aspects which improve structural efficiency, such as a semi-monocoque construction, improved strut design, etc. Improved load paths and means for transmitting loads in the engine case are also disclosed.
L'enveloppe d'une turbine à gaz comprend le carter du ventilateur, le carter intermédiaire et le carter du générateur de gaz, ces trois éléments étant emboîtés les uns dans les autres. Dans un autre mode de réalisation, l'enveloppe est configurée différemment afin d'inclure plusieurs aspects qui améliorent l'efficacité structurelle, comme une configuration en semi-monocoque ou une conception en caisson améliorée. Les chemins de charge améliorés et les moyens de transmettre les charges dans le carter de moteur sont également fournis.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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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 GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | TURBOFAN CASE AND METHOD OF MAKING |
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