Aircraft propeller and aircraft

An aircraft propeller, including a propeller shaft and propeller blades or propeller airfoils secured on the propeller shaft, wherein an inlet-side flow channel and an outlet-side flow channel are introduced into each of the propeller blades or each of the propeller airfoils, wherein each inlet-side...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT
Format: Patent
Sprache:eng
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 DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT
description An aircraft propeller, including a propeller shaft and propeller blades or propeller airfoils secured on the propeller shaft, wherein an inlet-side flow channel and an outlet-side flow channel are introduced into each of the propeller blades or each of the propeller airfoils, wherein each inlet-side flow channel has an inlet opening and each outlet-side flow channel has an outlet opening on each of the propeller blades or propeller airfoils, wherein each inlet-side flow channel has a connection to the outlet-side flow channel of a respective other propeller blade or propeller airfoil such that air flowing in via the inlet-side flow channel flows out via the outlet-side flow channel of the respective other propeller blade or propeller airfoil, and wherein the inlet opening and the outlet opening of each propeller blade or propeller airfoil are arranged on different sides of the propeller blade or propeller airfoil.
format Patent
fullrecord <record><control><sourceid>uspatents_EFH</sourceid><recordid>TN_cdi_uspatents_grants_11679863</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>11679863</sourcerecordid><originalsourceid>FETCH-uspatents_grants_116798633</originalsourceid><addsrcrecordid>eNrjZJB3zCxKLkpMK1EoKMovSM3JSS1SSMxLUUiECvMwsKYl5hSn8kJpbgYFN9cQZw_d0uKCxJLUvJLi-PSiRBBlaGhmbmlhZmxMhBIADu4l5g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft propeller and aircraft</title><source>USPTO Issued Patents</source><creator>DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT</creator><creatorcontrib>DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT</creatorcontrib><description>An aircraft propeller, including a propeller shaft and propeller blades or propeller airfoils secured on the propeller shaft, wherein an inlet-side flow channel and an outlet-side flow channel are introduced into each of the propeller blades or each of the propeller airfoils, wherein each inlet-side flow channel has an inlet opening and each outlet-side flow channel has an outlet opening on each of the propeller blades or propeller airfoils, wherein each inlet-side flow channel has a connection to the outlet-side flow channel of a respective other propeller blade or propeller airfoil such that air flowing in via the inlet-side flow channel flows out via the outlet-side flow channel of the respective other propeller blade or propeller airfoil, and wherein the inlet opening and the outlet opening of each propeller blade or propeller airfoil are arranged on different sides of the propeller blade or propeller airfoil.</description><language>eng</language><creationdate>2023</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/11679863$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,780,802,885,64037</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/11679863$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT</creatorcontrib><title>Aircraft propeller and aircraft</title><description>An aircraft propeller, including a propeller shaft and propeller blades or propeller airfoils secured on the propeller shaft, wherein an inlet-side flow channel and an outlet-side flow channel are introduced into each of the propeller blades or each of the propeller airfoils, wherein each inlet-side flow channel has an inlet opening and each outlet-side flow channel has an outlet opening on each of the propeller blades or propeller airfoils, wherein each inlet-side flow channel has a connection to the outlet-side flow channel of a respective other propeller blade or propeller airfoil such that air flowing in via the inlet-side flow channel flows out via the outlet-side flow channel of the respective other propeller blade or propeller airfoil, and wherein the inlet opening and the outlet opening of each propeller blade or propeller airfoil are arranged on different sides of the propeller blade or propeller airfoil.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EFH</sourceid><recordid>eNrjZJB3zCxKLkpMK1EoKMovSM3JSS1SSMxLUUiECvMwsKYl5hSn8kJpbgYFN9cQZw_d0uKCxJLUvJLi-PSiRBBlaGhmbmlhZmxMhBIADu4l5g</recordid><startdate>20230620</startdate><enddate>20230620</enddate><creator>DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT</creator><scope>EFH</scope></search><sort><creationdate>20230620</creationdate><title>Aircraft propeller and aircraft</title></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_116798633</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2023</creationdate><toplevel>online_resources</toplevel><creatorcontrib>DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><aucorp>DR. ING. H.C. F. PORSCHE AKTIENGESELLSCHAFT</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft propeller and aircraft</title><date>2023-06-20</date><risdate>2023</risdate><abstract>An aircraft propeller, including a propeller shaft and propeller blades or propeller airfoils secured on the propeller shaft, wherein an inlet-side flow channel and an outlet-side flow channel are introduced into each of the propeller blades or each of the propeller airfoils, wherein each inlet-side flow channel has an inlet opening and each outlet-side flow channel has an outlet opening on each of the propeller blades or propeller airfoils, wherein each inlet-side flow channel has a connection to the outlet-side flow channel of a respective other propeller blade or propeller airfoil such that air flowing in via the inlet-side flow channel flows out via the outlet-side flow channel of the respective other propeller blade or propeller airfoil, and wherein the inlet opening and the outlet opening of each propeller blade or propeller airfoil are arranged on different sides of the propeller blade or propeller airfoil.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_uspatents_grants_11679863
source USPTO Issued Patents
title Aircraft propeller and aircraft
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T08%3A50%3A01IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-uspatents_EFH&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.aucorp=DR.%20ING.%20H.C.%20F.%20PORSCHE%20AKTIENGESELLSCHAFT&rft.date=2023-06-20&rft_id=info:doi/&rft_dat=%3Cuspatents_EFH%3E11679863%3C/uspatents_EFH%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