AIR INTAKE SYSTEM
The present invention provides an air intake system (10) comprising an air duct (2) suitable for providing airflow to the inside of an aircraft (18), preferably to an auxiliary power unit; an inlet (1) arranged at one end of the air duct (2); a skin (3) surrounding the inlet; a plurality of slots (4...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; 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 | CASADO MONTERO, Carlos FERNÁNDEZ LÓPEZ, Pio |
| description | The present invention provides an air intake system (10) comprising an air duct (2) suitable for providing airflow to the inside of an aircraft (18), preferably to an auxiliary power unit; an inlet (1) arranged at one end of the air duct (2); a skin (3) surrounding the inlet; a plurality of slots (4) arranged on the skin; driving means (16, 17), a flap door (5) connected to a driving means, a plurality of fins (6) connected to the driving means; wherein the driving means is configured for moving the flap door between at least two positions, said positions being a closed position wherein the flap door closes the inlet, and an opened position wherein the flap door is driven away from said closed position, and wherein the driving means is also configured for moving the plurality of fins in such a way that the plurality of fins protrudes through the slots |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3587273B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3587273B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3587273B13</originalsourceid><addsrcrecordid>eNrjZBB09AxS8PQLcfR2VQiODA5x9eVhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcamFuZG5sZOhsZEKAEA4zIdZQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIR INTAKE SYSTEM</title><source>esp@cenet</source><creator>CASADO MONTERO, Carlos ; FERNÁNDEZ LÓPEZ, Pio</creator><creatorcontrib>CASADO MONTERO, Carlos ; FERNÁNDEZ LÓPEZ, Pio</creatorcontrib><description>The present invention provides an air intake system (10) comprising an air duct (2) suitable for providing airflow to the inside of an aircraft (18), preferably to an auxiliary power unit; an inlet (1) arranged at one end of the air duct (2); a skin (3) surrounding the inlet; a plurality of slots (4) arranged on the skin; driving means (16, 17), a flap door (5) connected to a driving means, a plurality of fins (6) connected to the driving means; wherein the driving means is configured for moving the flap door between at least two positions, said positions being a closed position wherein the flap door closes the inlet, and an opened position wherein the flap door is driven away from said closed position, and wherein the driving means is also configured for moving the plurality of fins in such a way that the plurality of fins protrudes through the slots</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEATING ; HELICOPTERS ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2023</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=20231011&DB=EPODOC&CC=EP&NR=3587273B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231011&DB=EPODOC&CC=EP&NR=3587273B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CASADO MONTERO, Carlos</creatorcontrib><creatorcontrib>FERNÁNDEZ LÓPEZ, Pio</creatorcontrib><title>AIR INTAKE SYSTEM</title><description>The present invention provides an air intake system (10) comprising an air duct (2) suitable for providing airflow to the inside of an aircraft (18), preferably to an auxiliary power unit; an inlet (1) arranged at one end of the air duct (2); a skin (3) surrounding the inlet; a plurality of slots (4) arranged on the skin; driving means (16, 17), a flap door (5) connected to a driving means, a plurality of fins (6) connected to the driving means; wherein the driving means is configured for moving the flap door between at least two positions, said positions being a closed position wherein the flap door closes the inlet, and an opened position wherein the flap door is driven away from said closed position, and wherein the driving means is also configured for moving the plurality of fins in such a way that the plurality of fins protrudes through the slots</description><subject>AEROPLANES</subject><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN 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>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBB09AxS8PQLcfR2VQiODA5x9eVhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcamFuZG5sZOhsZEKAEA4zIdZQ</recordid><startdate>20231011</startdate><enddate>20231011</enddate><creator>CASADO MONTERO, Carlos</creator><creator>FERNÁNDEZ LÓPEZ, Pio</creator><scope>EVB</scope></search><sort><creationdate>20231011</creationdate><title>AIR INTAKE SYSTEM</title><author>CASADO MONTERO, Carlos ; FERNÁNDEZ LÓPEZ, Pio</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3587273B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN 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>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>CASADO MONTERO, Carlos</creatorcontrib><creatorcontrib>FERNÁNDEZ LÓPEZ, Pio</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CASADO MONTERO, Carlos</au><au>FERNÁNDEZ LÓPEZ, Pio</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIR INTAKE SYSTEM</title><date>2023-10-11</date><risdate>2023</risdate><abstract>The present invention provides an air intake system (10) comprising an air duct (2) suitable for providing airflow to the inside of an aircraft (18), preferably to an auxiliary power unit; an inlet (1) arranged at one end of the air duct (2); a skin (3) surrounding the inlet; a plurality of slots (4) arranged on the skin; driving means (16, 17), a flap door (5) connected to a driving means, a plurality of fins (6) connected to the driving means; wherein the driving means is configured for moving the flap door between at least two positions, said positions being a closed position wherein the flap door closes the inlet, and an opened position wherein the flap door is driven away from said closed position, and wherein the driving means is also configured for moving the plurality of fins in such a way that the plurality of fins protrudes through the slots</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP3587273B1 |
| source | esp@cenet |
| subjects | AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | AIR INTAKE SYSTEM |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-25T18%3A04%3A46IST&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=CASADO%20MONTERO,%20Carlos&rft.date=2023-10-11&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3587273B1%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 |