OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET

Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is ass...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: KIM, Geun Il, ROHR, Timothy C, FREGNANI, Jose A
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 KIM, Geun Il
ROHR, Timothy C
FREGNANI, Jose A
description Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is associated with an optimum ratio of the takeoff safety speed to the stall speed that satisfies a specific set of climb/obstacle constraints. Targeting this optimum initial pitch angle allows the maximum takeoff gross weight that corresponds to the optimum takeoff safety speed/stall speed ratio to be selected.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3528080B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3528080B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3528080B13</originalsourceid><addsrcrecordid>eNrjZAj1Dwjx9PWM8vRzV3D28fR1UghwDXLzD_J19HN2VXAJDQJJhDh6u_q7uSmEBoN4YY5Bno5OPq4Knn6eIZ6OPgoBniHOHgqOfu5AsRDHIHfXEB4G1rTEnOJUXijNzaDg5gpUpJtakB-fWlyQmJyal1oS7xpgbGpkYWBh4GRoTIQSAAwnMAI</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET</title><source>esp@cenet</source><creator>KIM, Geun Il ; ROHR, Timothy C ; FREGNANI, Jose A</creator><creatorcontrib>KIM, Geun Il ; ROHR, Timothy C ; FREGNANI, Jose A</creatorcontrib><description>Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is associated with an optimum ratio of the takeoff safety speed to the stall speed that satisfies a specific set of climb/obstacle constraints. Targeting this optimum initial pitch angle allows the maximum takeoff gross weight that corresponds to the optimum takeoff safety speed/stall speed ratio to be selected.</description><language>eng ; fre ; ger</language><subject>CONTROLLING ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</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&amp;date=20220406&amp;DB=EPODOC&amp;CC=EP&amp;NR=3528080B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220406&amp;DB=EPODOC&amp;CC=EP&amp;NR=3528080B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KIM, Geun Il</creatorcontrib><creatorcontrib>ROHR, Timothy C</creatorcontrib><creatorcontrib>FREGNANI, Jose A</creatorcontrib><title>OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET</title><description>Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is associated with an optimum ratio of the takeoff safety speed to the stall speed that satisfies a specific set of climb/obstacle constraints. Targeting this optimum initial pitch angle allows the maximum takeoff gross weight that corresponds to the optimum takeoff safety speed/stall speed ratio to be selected.</description><subject>CONTROLLING</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAj1Dwjx9PWM8vRzV3D28fR1UghwDXLzD_J19HN2VXAJDQJJhDh6u_q7uSmEBoN4YY5Bno5OPq4Knn6eIZ6OPgoBniHOHgqOfu5AsRDHIHfXEB4G1rTEnOJUXijNzaDg5gpUpJtakB-fWlyQmJyal1oS7xpgbGpkYWBh4GRoTIQSAAwnMAI</recordid><startdate>20220406</startdate><enddate>20220406</enddate><creator>KIM, Geun Il</creator><creator>ROHR, Timothy C</creator><creator>FREGNANI, Jose A</creator><scope>EVB</scope></search><sort><creationdate>20220406</creationdate><title>OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET</title><author>KIM, Geun Il ; ROHR, Timothy C ; FREGNANI, Jose A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3528080B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>CONTROLLING</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><toplevel>online_resources</toplevel><creatorcontrib>KIM, Geun Il</creatorcontrib><creatorcontrib>ROHR, Timothy C</creatorcontrib><creatorcontrib>FREGNANI, Jose A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KIM, Geun Il</au><au>ROHR, Timothy C</au><au>FREGNANI, Jose A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET</title><date>2022-04-06</date><risdate>2022</risdate><abstract>Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is associated with an optimum ratio of the takeoff safety speed to the stall speed that satisfies a specific set of climb/obstacle constraints. Targeting this optimum initial pitch angle allows the maximum takeoff gross weight that corresponds to the optimum takeoff safety speed/stall speed ratio to be selected.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3528080B1
source esp@cenet
subjects CONTROLLING
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
title OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T02%3A57%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=KIM,%20Geun%20Il&rft.date=2022-04-06&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3528080B1%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