Drive mechanism for e.g. fixed wing aircraft, has lifting drive turbine actuated by exhaust gas stream of radiation jet engine, and device increasing exhaust gas temperature of burners and arranged in section of exhaust gas channel
The mechanism has a lifting drive turbine actuated by an exhaust gas stream of a radiation jet engine (2), which is designed as a two stream or multi-stream-turbo fan jet engine. A device is provided for increasing exhaust gas temperature of burners and arranged in a section of an exhaust gas channe...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; ger |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | JUDAS, MICHAEL WEDEKIND, GERHARD BICHLER, BARTHOLOMAEUS |
| description | The mechanism has a lifting drive turbine actuated by an exhaust gas stream of a radiation jet engine (2), which is designed as a two stream or multi-stream-turbo fan jet engine. A device is provided for increasing exhaust gas temperature of burners and arranged in a section of an exhaust gas channel (40). The exhaust gas channel system exhibits a shear exhaust gas-discharge channel (46) that is directed rearwards, and a stroke exhaust gas-discharge channel (48) that is directed downwards. A lifting blower is displaced in rotation at the shaft by the lifting drive turbine. An independent claim is also included for a method for increasing surge of a radiation jet engine in a perpendicular startable aircraft.
Eine Antriebseinheit für ein senkrecht startendes Luftfahrzeug (1) mit zumindest einem Strahltriebwerk (2) für den Schubantrieb und zumindest einem Bläsertriebwerk (3) für den Hubantrieb, wobei das Bläsertriebwerk (3) ein Hubgebläse (30) aufweist, welches mittels einer vom Strahltriebwerk (2) antreibbaren Hubantriebsturbine (50) über eine Welle (52) in Rotation versetzbar ist, zeichnet sich dadurch aus, dass die Hubantriebsturbine (50) vom Abgasstrom des Strahltriebwerks (2) betätigt wird und dass das Strahltriebwerk (2) im Bereich des Abgasauslasses (40) eine Vorrichtung (6) zur Erhöhung der Abgastemperatur aufweist, die bedarfsweise die Temperatur des Abgasstroms erhöht. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_DE102009048201A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>DE102009048201A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_DE102009048201A13</originalsourceid><addsrcrecordid>eNqNj7FOw1AMRbMwIOAfvLCVKikdYES0iA9gr9yX-xKjxIn8nFK-mN_gJWLoyGTJOudYvi5-diYnUI_QskrqKQ5GWDdrinJGTV-iDbFYMI6-opYTdRJ93taL6ZMdRUEcfGLPxvGbcG55Sk5NppMbuKchknEt7DIofcIJ2mRtRaw11ThJAImGzKa5fVlw9COM8yHMmeNkCkuLyGasTT4qSglhiWfk0p7_UnS3xVXkLuHub94U92_7j9f3B4zDAWnkAIUfdvuq3JTlc7l92pTVS_X4X-4XYhBwTg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Drive mechanism for e.g. fixed wing aircraft, has lifting drive turbine actuated by exhaust gas stream of radiation jet engine, and device increasing exhaust gas temperature of burners and arranged in section of exhaust gas channel</title><source>esp@cenet</source><creator>JUDAS, MICHAEL ; WEDEKIND, GERHARD ; BICHLER, BARTHOLOMAEUS</creator><creatorcontrib>JUDAS, MICHAEL ; WEDEKIND, GERHARD ; BICHLER, BARTHOLOMAEUS</creatorcontrib><description>The mechanism has a lifting drive turbine actuated by an exhaust gas stream of a radiation jet engine (2), which is designed as a two stream or multi-stream-turbo fan jet engine. A device is provided for increasing exhaust gas temperature of burners and arranged in a section of an exhaust gas channel (40). The exhaust gas channel system exhibits a shear exhaust gas-discharge channel (46) that is directed rearwards, and a stroke exhaust gas-discharge channel (48) that is directed downwards. A lifting blower is displaced in rotation at the shaft by the lifting drive turbine. An independent claim is also included for a method for increasing surge of a radiation jet engine in a perpendicular startable aircraft.
Eine Antriebseinheit für ein senkrecht startendes Luftfahrzeug (1) mit zumindest einem Strahltriebwerk (2) für den Schubantrieb und zumindest einem Bläsertriebwerk (3) für den Hubantrieb, wobei das Bläsertriebwerk (3) ein Hubgebläse (30) aufweist, welches mittels einer vom Strahltriebwerk (2) antreibbaren Hubantriebsturbine (50) über eine Welle (52) in Rotation versetzbar ist, zeichnet sich dadurch aus, dass die Hubantriebsturbine (50) vom Abgasstrom des Strahltriebwerks (2) betätigt wird und dass das Strahltriebwerk (2) im Bereich des Abgasauslasses (40) eine Vorrichtung (6) zur Erhöhung der Abgastemperatur aufweist, die bedarfsweise die Temperatur des Abgasstroms erhöht.</description><language>eng ; ger</language><subject>AEROPLANES ; AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; GAS-TURBINE PLANTS ; HEATING ; HELICOPTERS ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2011</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=20110428&DB=EPODOC&CC=DE&NR=102009048201A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20110428&DB=EPODOC&CC=DE&NR=102009048201A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JUDAS, MICHAEL</creatorcontrib><creatorcontrib>WEDEKIND, GERHARD</creatorcontrib><creatorcontrib>BICHLER, BARTHOLOMAEUS</creatorcontrib><title>Drive mechanism for e.g. fixed wing aircraft, has lifting drive turbine actuated by exhaust gas stream of radiation jet engine, and device increasing exhaust gas temperature of burners and arranged in section of exhaust gas channel</title><description>The mechanism has a lifting drive turbine actuated by an exhaust gas stream of a radiation jet engine (2), which is designed as a two stream or multi-stream-turbo fan jet engine. A device is provided for increasing exhaust gas temperature of burners and arranged in a section of an exhaust gas channel (40). The exhaust gas channel system exhibits a shear exhaust gas-discharge channel (46) that is directed rearwards, and a stroke exhaust gas-discharge channel (48) that is directed downwards. A lifting blower is displaced in rotation at the shaft by the lifting drive turbine. An independent claim is also included for a method for increasing surge of a radiation jet engine in a perpendicular startable aircraft.
Eine Antriebseinheit für ein senkrecht startendes Luftfahrzeug (1) mit zumindest einem Strahltriebwerk (2) für den Schubantrieb und zumindest einem Bläsertriebwerk (3) für den Hubantrieb, wobei das Bläsertriebwerk (3) ein Hubgebläse (30) aufweist, welches mittels einer vom Strahltriebwerk (2) antreibbaren Hubantriebsturbine (50) über eine Welle (52) in Rotation versetzbar ist, zeichnet sich dadurch aus, dass die Hubantriebsturbine (50) vom Abgasstrom des Strahltriebwerks (2) betätigt wird und dass das Strahltriebwerk (2) im Bereich des Abgasauslasses (40) eine Vorrichtung (6) zur Erhöhung der Abgastemperatur aufweist, die bedarfsweise die Temperatur des Abgasstroms erhöht.</description><subject>AEROPLANES</subject><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNj7FOw1AMRbMwIOAfvLCVKikdYES0iA9gr9yX-xKjxIn8nFK-mN_gJWLoyGTJOudYvi5-diYnUI_QskrqKQ5GWDdrinJGTV-iDbFYMI6-opYTdRJ93taL6ZMdRUEcfGLPxvGbcG55Sk5NppMbuKchknEt7DIofcIJ2mRtRaw11ThJAImGzKa5fVlw9COM8yHMmeNkCkuLyGasTT4qSglhiWfk0p7_UnS3xVXkLuHub94U92_7j9f3B4zDAWnkAIUfdvuq3JTlc7l92pTVS_X4X-4XYhBwTg</recordid><startdate>20110428</startdate><enddate>20110428</enddate><creator>JUDAS, MICHAEL</creator><creator>WEDEKIND, GERHARD</creator><creator>BICHLER, BARTHOLOMAEUS</creator><scope>EVB</scope></search><sort><creationdate>20110428</creationdate><title>Drive mechanism for e.g. fixed wing aircraft, has lifting drive turbine actuated by exhaust gas stream of radiation jet engine, and device increasing exhaust gas temperature of burners and arranged in section of exhaust gas channel</title><author>JUDAS, MICHAEL ; WEDEKIND, GERHARD ; BICHLER, BARTHOLOMAEUS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE102009048201A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; ger</language><creationdate>2011</creationdate><topic>AEROPLANES</topic><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>JUDAS, MICHAEL</creatorcontrib><creatorcontrib>WEDEKIND, GERHARD</creatorcontrib><creatorcontrib>BICHLER, BARTHOLOMAEUS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JUDAS, MICHAEL</au><au>WEDEKIND, GERHARD</au><au>BICHLER, BARTHOLOMAEUS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Drive mechanism for e.g. fixed wing aircraft, has lifting drive turbine actuated by exhaust gas stream of radiation jet engine, and device increasing exhaust gas temperature of burners and arranged in section of exhaust gas channel</title><date>2011-04-28</date><risdate>2011</risdate><abstract>The mechanism has a lifting drive turbine actuated by an exhaust gas stream of a radiation jet engine (2), which is designed as a two stream or multi-stream-turbo fan jet engine. A device is provided for increasing exhaust gas temperature of burners and arranged in a section of an exhaust gas channel (40). The exhaust gas channel system exhibits a shear exhaust gas-discharge channel (46) that is directed rearwards, and a stroke exhaust gas-discharge channel (48) that is directed downwards. A lifting blower is displaced in rotation at the shaft by the lifting drive turbine. An independent claim is also included for a method for increasing surge of a radiation jet engine in a perpendicular startable aircraft.
Eine Antriebseinheit für ein senkrecht startendes Luftfahrzeug (1) mit zumindest einem Strahltriebwerk (2) für den Schubantrieb und zumindest einem Bläsertriebwerk (3) für den Hubantrieb, wobei das Bläsertriebwerk (3) ein Hubgebläse (30) aufweist, welches mittels einer vom Strahltriebwerk (2) antreibbaren Hubantriebsturbine (50) über eine Welle (52) in Rotation versetzbar ist, zeichnet sich dadurch aus, dass die Hubantriebsturbine (50) vom Abgasstrom des Strahltriebwerks (2) betätigt wird und dass das Strahltriebwerk (2) im Bereich des Abgasauslasses (40) eine Vorrichtung (6) zur Erhöhung der Abgastemperatur aufweist, die bedarfsweise die Temperatur des Abgasstroms erhöht.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; ger |
| recordid | cdi_epo_espacenet_DE102009048201A1 |
| source | esp@cenet |
| subjects | AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | Drive mechanism for e.g. fixed wing aircraft, has lifting drive turbine actuated by exhaust gas stream of radiation jet engine, and device increasing exhaust gas temperature of burners and arranged in section of exhaust gas channel |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T16%3A12%3A13IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=JUDAS,%20MICHAEL&rft.date=2011-04-28&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EDE102009048201A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |