PROPELLER ARRANGEMENT FOR AN AIRCRAFT

PROPELLER ARRANGEMENT FOR AN AIRCRAFT

A propeller arrangement (100) for an aircraft, and an aircraft having a propeller arrangement of said type, are specified. The propeller arrangement (100) has a first propeller blade (110) and a second propeller blade (120), and a propeller mount (130) on which both the first propeller blade (110) a...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Bichler, Bartholomaeus, Judas, Michael
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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 Bichler, Bartholomaeus
Judas, Michael
description A propeller arrangement (100) for an aircraft, and an aircraft having a propeller arrangement of said type, are specified. The propeller arrangement (100) has a first propeller blade (110) and a second propeller blade (120), and a propeller mount (130) on which both the first propeller blade (110) and the second propeller blade (120) are mounted. The propeller arrangement (100) furthermore has a drive shaft (140) with a holding unit (160), and a first connecting unit (150). The first propeller blade (110) is rotatable about a first axis of rotation (112) and the second propeller blade (120) is rotatable about a second axis of rotation (122). The propeller mount (130) is pivotable about a pivot axis (132). The first connecting unit (150) is coupled to the first propeller blade (110) and to the holding unit (160), such that, in the event of a pivoting of the propeller mount (130) about the pivot axis (132), the first propeller blade (110) is set in rotational motion about the first axis of rotation (112).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3434589B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3434589B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3434589B13</originalsourceid><addsrcrecordid>eNrjZFANCPIPcPXxcQ1ScAwKcvRzd_V19QtRcPMH8v0UHD2DnIMc3UJ4GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakm8a4CxibGJqYWlk6ExEUoAXSIi6Q</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>PROPELLER ARRANGEMENT FOR AN AIRCRAFT</title><source>esp@cenet</source><creator>Bichler, Bartholomaeus ; Judas, Michael</creator><creatorcontrib>Bichler, Bartholomaeus ; Judas, Michael</creatorcontrib><description>A propeller arrangement (100) for an aircraft, and an aircraft having a propeller arrangement of said type, are specified. The propeller arrangement (100) has a first propeller blade (110) and a second propeller blade (120), and a propeller mount (130) on which both the first propeller blade (110) and the second propeller blade (120) are mounted. The propeller arrangement (100) furthermore has a drive shaft (140) with a holding unit (160), and a first connecting unit (150). The first propeller blade (110) is rotatable about a first axis of rotation (112) and the second propeller blade (120) is rotatable about a second axis of rotation (122). The propeller mount (130) is pivotable about a pivot axis (132). The first connecting unit (150) is coupled to the first propeller blade (110) and to the holding unit (160), such that, in the event of a pivoting of the propeller mount (130) about the pivot axis (132), the first propeller blade (110) is set in rotational motion about the first axis of rotation (112).</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2020</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=20201104&amp;DB=EPODOC&amp;CC=EP&amp;NR=3434589B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20201104&amp;DB=EPODOC&amp;CC=EP&amp;NR=3434589B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Bichler, Bartholomaeus</creatorcontrib><creatorcontrib>Judas, Michael</creatorcontrib><title>PROPELLER ARRANGEMENT FOR AN AIRCRAFT</title><description>A propeller arrangement (100) for an aircraft, and an aircraft having a propeller arrangement of said type, are specified. The propeller arrangement (100) has a first propeller blade (110) and a second propeller blade (120), and a propeller mount (130) on which both the first propeller blade (110) and the second propeller blade (120) are mounted. The propeller arrangement (100) furthermore has a drive shaft (140) with a holding unit (160), and a first connecting unit (150). The first propeller blade (110) is rotatable about a first axis of rotation (112) and the second propeller blade (120) is rotatable about a second axis of rotation (122). The propeller mount (130) is pivotable about a pivot axis (132). The first connecting unit (150) is coupled to the first propeller blade (110) and to the holding unit (160), such that, in the event of a pivoting of the propeller mount (130) about the pivot axis (132), the first propeller blade (110) is set in rotational motion about the first axis of rotation (112).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFANCPIPcPXxcQ1ScAwKcvRzd_V19QtRcPMH8v0UHD2DnIMc3UJ4GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakm8a4CxibGJqYWlk6ExEUoAXSIi6Q</recordid><startdate>20201104</startdate><enddate>20201104</enddate><creator>Bichler, Bartholomaeus</creator><creator>Judas, Michael</creator><scope>EVB</scope></search><sort><creationdate>20201104</creationdate><title>PROPELLER ARRANGEMENT FOR AN AIRCRAFT</title><author>Bichler, Bartholomaeus ; Judas, Michael</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3434589B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2020</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Bichler, Bartholomaeus</creatorcontrib><creatorcontrib>Judas, Michael</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Bichler, Bartholomaeus</au><au>Judas, Michael</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROPELLER ARRANGEMENT FOR AN AIRCRAFT</title><date>2020-11-04</date><risdate>2020</risdate><abstract>A propeller arrangement (100) for an aircraft, and an aircraft having a propeller arrangement of said type, are specified. The propeller arrangement (100) has a first propeller blade (110) and a second propeller blade (120), and a propeller mount (130) on which both the first propeller blade (110) and the second propeller blade (120) are mounted. The propeller arrangement (100) furthermore has a drive shaft (140) with a holding unit (160), and a first connecting unit (150). The first propeller blade (110) is rotatable about a first axis of rotation (112) and the second propeller blade (120) is rotatable about a second axis of rotation (122). The propeller mount (130) is pivotable about a pivot axis (132). The first connecting unit (150) is coupled to the first propeller blade (110) and to the holding unit (160), such that, in the event of a pivoting of the propeller mount (130) about the pivot axis (132), the first propeller blade (110) is set in rotational motion about the first axis of rotation (112).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3434589B1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title PROPELLER ARRANGEMENT FOR AN AIRCRAFT
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T07%3A57%3A50IST&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=Bichler,%20Bartholomaeus&rft.date=2020-11-04&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3434589B1%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