TURBOJET WITH STEP-DOWN MECHANISM
Turbojet engine includes a fan, a compressor, a combustion chamber, and a turbine configured to rotatably drive the fan via a first reduction gear and the compressor via a second reduction gear, in which an outlet of the first reduction gear is rotatably coupled to an inlet of the second reduction g...
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creator | LEMARCHAND, Kévin, Morgane TANTOT, Nicolas, Jérôme, Jean CHARIER, Gilles, Alain, Marie VLASTUIN, Jonathan, Evert NOWAKOWSKI, Nathalie YESILCIMEN, Henri |
description | Turbojet engine includes a fan, a compressor, a combustion chamber, and a turbine configured to rotatably drive the fan via a first reduction gear and the compressor via a second reduction gear, in which an outlet of the first reduction gear is rotatably coupled to an inlet of the second reduction gear by a reduction shaft, the reduction shaft being supported by a bearing arranged between the first reduction gear and the second reduction gear. |
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fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2022</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=20221026&DB=EPODOC&CC=EP&NR=3853456B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221026&DB=EPODOC&CC=EP&NR=3853456B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEMARCHAND, Kévin, Morgane</creatorcontrib><creatorcontrib>TANTOT, Nicolas, Jérôme, Jean</creatorcontrib><creatorcontrib>CHARIER, Gilles, Alain, Marie</creatorcontrib><creatorcontrib>VLASTUIN, Jonathan, Evert</creatorcontrib><creatorcontrib>NOWAKOWSKI, Nathalie</creatorcontrib><creatorcontrib>YESILCIMEN, Henri</creatorcontrib><title>TURBOJET WITH STEP-DOWN MECHANISM</title><description>Turbojet engine includes a fan, a compressor, a combustion chamber, and a turbine configured to rotatably drive the fan via a first reduction gear and the compressor via a second reduction gear, in which an outlet of the first reduction gear is rotatably coupled to an inlet of the second reduction gear by a reduction shaft, the reduction shaft being supported by a bearing arranged between the first reduction gear and the second reduction gear.</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>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>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAMCQ1y8vdyDVEI9wzxUAgOcQ3QdfEP91PwdXX2cPTzDPblYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGFqbGJqZmTobGRCgBAOYCIfc</recordid><startdate>20221026</startdate><enddate>20221026</enddate><creator>LEMARCHAND, Kévin, Morgane</creator><creator>TANTOT, Nicolas, Jérôme, Jean</creator><creator>CHARIER, Gilles, Alain, Marie</creator><creator>VLASTUIN, Jonathan, Evert</creator><creator>NOWAKOWSKI, Nathalie</creator><creator>YESILCIMEN, Henri</creator><scope>EVB</scope></search><sort><creationdate>20221026</creationdate><title>TURBOJET WITH STEP-DOWN MECHANISM</title><author>LEMARCHAND, Kévin, Morgane ; 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language | eng ; fre ; ger |
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subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | TURBOJET WITH STEP-DOWN MECHANISM |
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