Rotary wing assembly with adjustable pitch angle for aircraft engine
An engine for an aircraft. The engine includes a rotary wing assembly, at least one actuator, a torque generating system, and a controller. The rotary wing assembly includes an axis of rotation and a plurality of rotary wings configured to rotate about the axis of rotation in a plane of rotation. Th...
Gespeichert in:
| Hauptverfasser: | , , , , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| 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 | YADAV ABHIJIT PAIYOR, NARAYANAN GOVDAN, ABSHEK BRYANT GARY W SURESH BALARAJU RICARDO HERNANDEZ PANDLI ALKOS ILYA CHAKRABARTI, SURYAGYA DAGUETTE NICHOLAS M RAJPUT, ASHISH KAKARLA, AMANATH |
| description | An engine for an aircraft. The engine includes a rotary wing assembly, at least one actuator, a torque generating system, and a controller. The rotary wing assembly includes an axis of rotation and a plurality of rotary wings configured to rotate about the axis of rotation in a plane of rotation. The at least one actuator is operable to vary a plane of rotation of the plurality of rotary wings. The torque generating system is coupled to the rotating wing assembly and is configured to rotate the rotating wing assembly about a rotational axis of the rotating wing assembly. The controller is configured to determine that the aircraft has an angle of attack and to operate the at least one actuator to vary a plane of rotation of the plurality of rotary airfoils based on the angle of attack.
一种用于飞行器的发动机。该发动机包括旋转翼型件组件、至少一个致动器、扭矩产生系统和控制器。旋转翼型件组件包括旋转轴线和多个旋转翼型件，多个旋转翼型件被构造成在旋转平面中围绕旋转轴线旋转。至少一个致动器能够操作，以改变多个旋转翼型件的旋转平面。扭矩产生系统联接到旋转翼型件组件，并且被构造成使旋转翼型件组件围绕旋转翼型件组件的旋转轴线旋转。控制器被构造成确定飞行器具有迎角，并且操作至少一个致动器，以基于迎角，改变多个旋转翼型件的旋转平面。 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN117287305A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN117287305A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN117287305A3</originalsourceid><addsrcrecordid>eNrjZHAJyi9JLKpUKM_MS1dILC5OzU3KAfFKMhQSU7JKi0sSk3JSFQoyS5KBAnnpQHZafpFCYmZRclFiWolCal56Zl4qDwNrWmJOcSovlOZmUHRzDXH20E0tyI9PLS5ITE7NSy2Jd_YzNDQ3sjA3NjB1NCZGDQDHKDLo</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Rotary wing assembly with adjustable pitch angle for aircraft engine</title><source>esp@cenet</source><creator>YADAV ABHIJIT ; PAIYOR, NARAYANAN ; GOVDAN, ABSHEK ; BRYANT GARY W ; SURESH BALARAJU ; RICARDO HERNANDEZ PANDLI ; ALKOS ILYA ; CHAKRABARTI, SURYAGYA ; DAGUETTE NICHOLAS M ; RAJPUT, ASHISH ; KAKARLA, AMANATH</creator><creatorcontrib>YADAV ABHIJIT ; PAIYOR, NARAYANAN ; GOVDAN, ABSHEK ; BRYANT GARY W ; SURESH BALARAJU ; RICARDO HERNANDEZ PANDLI ; ALKOS ILYA ; CHAKRABARTI, SURYAGYA ; DAGUETTE NICHOLAS M ; RAJPUT, ASHISH ; KAKARLA, AMANATH</creatorcontrib><description>An engine for an aircraft. The engine includes a rotary wing assembly, at least one actuator, a torque generating system, and a controller. The rotary wing assembly includes an axis of rotation and a plurality of rotary wings configured to rotate about the axis of rotation in a plane of rotation. The at least one actuator is operable to vary a plane of rotation of the plurality of rotary wings. The torque generating system is coupled to the rotating wing assembly and is configured to rotate the rotating wing assembly about a rotational axis of the rotating wing assembly. The controller is configured to determine that the aircraft has an angle of attack and to operate the at least one actuator to vary a plane of rotation of the plurality of rotary airfoils based on the angle of attack.
一种用于飞行器的发动机。该发动机包括旋转翼型件组件、至少一个致动器、扭矩产生系统和控制器。旋转翼型件组件包括旋转轴线和多个旋转翼型件，多个旋转翼型件被构造成在旋转平面中围绕旋转轴线旋转。至少一个致动器能够操作，以改变多个旋转翼型件的旋转平面。扭矩产生系统联接到旋转翼型件组件，并且被构造成使旋转翼型件组件围绕旋转翼型件组件的旋转轴线旋转。控制器被构造成确定飞行器具有迎角，并且操作至少一个致动器，以基于迎角，改变多个旋转翼型件的旋转平面。</description><language>chi ; eng</language><subject>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 ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT PUMPS ; PARACHUTES ; PERFORMING OPERATIONS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; 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=20231226&DB=EPODOC&CC=CN&NR=117287305A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231226&DB=EPODOC&CC=CN&NR=117287305A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YADAV ABHIJIT</creatorcontrib><creatorcontrib>PAIYOR, NARAYANAN</creatorcontrib><creatorcontrib>GOVDAN, ABSHEK</creatorcontrib><creatorcontrib>BRYANT GARY W</creatorcontrib><creatorcontrib>SURESH BALARAJU</creatorcontrib><creatorcontrib>RICARDO HERNANDEZ PANDLI</creatorcontrib><creatorcontrib>ALKOS ILYA</creatorcontrib><creatorcontrib>CHAKRABARTI, SURYAGYA</creatorcontrib><creatorcontrib>DAGUETTE NICHOLAS M</creatorcontrib><creatorcontrib>RAJPUT, ASHISH</creatorcontrib><creatorcontrib>KAKARLA, AMANATH</creatorcontrib><title>Rotary wing assembly with adjustable pitch angle for aircraft engine</title><description>An engine for an aircraft. The engine includes a rotary wing assembly, at least one actuator, a torque generating system, and a controller. The rotary wing assembly includes an axis of rotation and a plurality of rotary wings configured to rotate about the axis of rotation in a plane of rotation. The at least one actuator is operable to vary a plane of rotation of the plurality of rotary wings. The torque generating system is coupled to the rotating wing assembly and is configured to rotate the rotating wing assembly about a rotational axis of the rotating wing assembly. The controller is configured to determine that the aircraft has an angle of attack and to operate the at least one actuator to vary a plane of rotation of the plurality of rotary airfoils based on the angle of attack.
一种用于飞行器的发动机。该发动机包括旋转翼型件组件、至少一个致动器、扭矩产生系统和控制器。旋转翼型件组件包括旋转轴线和多个旋转翼型件，多个旋转翼型件被构造成在旋转平面中围绕旋转轴线旋转。至少一个致动器能够操作，以改变多个旋转翼型件的旋转平面。扭矩产生系统联接到旋转翼型件组件，并且被构造成使旋转翼型件组件围绕旋转翼型件组件的旋转轴线旋转。控制器被构造成确定飞行器具有迎角，并且操作至少一个致动器，以基于迎角，改变多个旋转翼型件的旋转平面。</description><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>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAJyi9JLKpUKM_MS1dILC5OzU3KAfFKMhQSU7JKi0sSk3JSFQoyS5KBAnnpQHZafpFCYmZRclFiWolCal56Zl4qDwNrWmJOcSovlOZmUHRzDXH20E0tyI9PLS5ITE7NSy2Jd_YzNDQ3sjA3NjB1NCZGDQDHKDLo</recordid><startdate>20231226</startdate><enddate>20231226</enddate><creator>YADAV ABHIJIT</creator><creator>PAIYOR, NARAYANAN</creator><creator>GOVDAN, ABSHEK</creator><creator>BRYANT GARY W</creator><creator>SURESH BALARAJU</creator><creator>RICARDO HERNANDEZ PANDLI</creator><creator>ALKOS ILYA</creator><creator>CHAKRABARTI, SURYAGYA</creator><creator>DAGUETTE NICHOLAS M</creator><creator>RAJPUT, ASHISH</creator><creator>KAKARLA, AMANATH</creator><scope>EVB</scope></search><sort><creationdate>20231226</creationdate><title>Rotary wing assembly with adjustable pitch angle for aircraft engine</title><author>YADAV ABHIJIT ; PAIYOR, NARAYANAN ; GOVDAN, ABSHEK ; BRYANT GARY W ; SURESH BALARAJU ; RICARDO HERNANDEZ PANDLI ; ALKOS ILYA ; CHAKRABARTI, SURYAGYA ; DAGUETTE NICHOLAS M ; RAJPUT, ASHISH ; KAKARLA, AMANATH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117287305A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><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>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>YADAV ABHIJIT</creatorcontrib><creatorcontrib>PAIYOR, NARAYANAN</creatorcontrib><creatorcontrib>GOVDAN, ABSHEK</creatorcontrib><creatorcontrib>BRYANT GARY W</creatorcontrib><creatorcontrib>SURESH BALARAJU</creatorcontrib><creatorcontrib>RICARDO HERNANDEZ PANDLI</creatorcontrib><creatorcontrib>ALKOS ILYA</creatorcontrib><creatorcontrib>CHAKRABARTI, SURYAGYA</creatorcontrib><creatorcontrib>DAGUETTE NICHOLAS M</creatorcontrib><creatorcontrib>RAJPUT, ASHISH</creatorcontrib><creatorcontrib>KAKARLA, AMANATH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YADAV ABHIJIT</au><au>PAIYOR, NARAYANAN</au><au>GOVDAN, ABSHEK</au><au>BRYANT GARY W</au><au>SURESH BALARAJU</au><au>RICARDO HERNANDEZ PANDLI</au><au>ALKOS ILYA</au><au>CHAKRABARTI, SURYAGYA</au><au>DAGUETTE NICHOLAS M</au><au>RAJPUT, ASHISH</au><au>KAKARLA, AMANATH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Rotary wing assembly with adjustable pitch angle for aircraft engine</title><date>2023-12-26</date><risdate>2023</risdate><abstract>An engine for an aircraft. The engine includes a rotary wing assembly, at least one actuator, a torque generating system, and a controller. The rotary wing assembly includes an axis of rotation and a plurality of rotary wings configured to rotate about the axis of rotation in a plane of rotation. The at least one actuator is operable to vary a plane of rotation of the plurality of rotary wings. The torque generating system is coupled to the rotating wing assembly and is configured to rotate the rotating wing assembly about a rotational axis of the rotating wing assembly. The controller is configured to determine that the aircraft has an angle of attack and to operate the at least one actuator to vary a plane of rotation of the plurality of rotary airfoils based on the angle of attack.
一种用于飞行器的发动机。该发动机包括旋转翼型件组件、至少一个致动器、扭矩产生系统和控制器。旋转翼型件组件包括旋转轴线和多个旋转翼型件，多个旋转翼型件被构造成在旋转平面中围绕旋转轴线旋转。至少一个致动器能够操作，以改变多个旋转翼型件的旋转平面。扭矩产生系统联接到旋转翼型件组件，并且被构造成使旋转翼型件组件围绕旋转翼型件组件的旋转轴线旋转。控制器被构造成确定飞行器具有迎角，并且操作至少一个致动器，以基于迎角，改变多个旋转翼型件的旋转平面。</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN117287305A |
| source | esp@cenet |
| subjects | 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 HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS PARACHUTES PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS TRANSPORTING WEAPONS |
| title | Rotary wing assembly with adjustable pitch angle for aircraft engine |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T19%3A56%3A16IST&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=YADAV%20ABHIJIT&rft.date=2023-12-26&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN117287305A%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 |