An aircraft cabin door opening device

The invention provides an aircraft cabin door opening device, which comprises an electric push rod and a cabin body; one side of the cabin is an mounting opening, and the other three sides are provided with bulkheads; an upper mounting seat is arranged on the inn walls of the bulkheads, and a hatch...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: HUANG ZHENG, WANG LI, RUAN GUOMIN
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 HUANG ZHENG
WANG LI
RUAN GUOMIN
description The invention provides an aircraft cabin door opening device, which comprises an electric push rod and a cabin body; one side of the cabin is an mounting opening, and the other three sides are provided with bulkheads; an upper mounting seat is arranged on the inn walls of the bulkheads, and a hatch door is connected with the mounting opening; low mounting seats are arrange on the upper and lower ends of the hatch door; one sides of the lower mounting seats are sequentially provided with rotating seats and fixing seats, and the fixing seats are connected with the rotating seats through rotatingshafts; one end of the electric push rod is connected with the upper mounting seat, and the other end is connected with the lower mounting seats. The invention adopts a simple structure and a lightweight structure, so that the opening time of the hatch door is shorter than 4-5s, and the maximum angle at which the hatch door can be opened is 90-110 degrees, and the quick opening, closing and larger opening angle of the ha
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN108945387A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN108945387A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN108945387A3</originalsourceid><addsrcrecordid>eNrjZFB1zFNIzCxKLkpMK1FITkzKzFNIyc8vUsgvSM3LzEtXSEkty0xO5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgYWliamxhbmjsbEqAEADpcm0g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>An aircraft cabin door opening device</title><source>esp@cenet</source><creator>HUANG ZHENG ; WANG LI ; RUAN GUOMIN</creator><creatorcontrib>HUANG ZHENG ; WANG LI ; RUAN GUOMIN</creatorcontrib><description>The invention provides an aircraft cabin door opening device, which comprises an electric push rod and a cabin body; one side of the cabin is an mounting opening, and the other three sides are provided with bulkheads; an upper mounting seat is arranged on the inn walls of the bulkheads, and a hatch door is connected with the mounting opening; low mounting seats are arrange on the upper and lower ends of the hatch door; one sides of the lower mounting seats are sequentially provided with rotating seats and fixing seats, and the fixing seats are connected with the rotating seats through rotatingshafts; one end of the electric push rod is connected with the upper mounting seat, and the other end is connected with the lower mounting seats. The invention adopts a simple structure and a lightweight structure, so that the opening time of the hatch door is shorter than 4-5s, and the maximum angle at which the hatch door can be opened is 90-110 degrees, and the quick opening, closing and larger opening angle of the ha</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; CHECKS FOR WINGS ; COSMONAUTICS ; DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION ; FIXED CONSTRUCTIONS ; HELICOPTERS ; KEYS ; LOCKS ; PERFORMING OPERATIONS ; SAFES ; TRANSPORTING ; WINDOW OR DOOR FITTINGS ; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THEFUNCTIONING OF THE WING</subject><creationdate>2018</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=20181207&amp;DB=EPODOC&amp;CC=CN&amp;NR=108945387A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20181207&amp;DB=EPODOC&amp;CC=CN&amp;NR=108945387A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUANG ZHENG</creatorcontrib><creatorcontrib>WANG LI</creatorcontrib><creatorcontrib>RUAN GUOMIN</creatorcontrib><title>An aircraft cabin door opening device</title><description>The invention provides an aircraft cabin door opening device, which comprises an electric push rod and a cabin body; one side of the cabin is an mounting opening, and the other three sides are provided with bulkheads; an upper mounting seat is arranged on the inn walls of the bulkheads, and a hatch door is connected with the mounting opening; low mounting seats are arrange on the upper and lower ends of the hatch door; one sides of the lower mounting seats are sequentially provided with rotating seats and fixing seats, and the fixing seats are connected with the rotating seats through rotatingshafts; one end of the electric push rod is connected with the upper mounting seat, and the other end is connected with the lower mounting seats. The invention adopts a simple structure and a lightweight structure, so that the opening time of the hatch door is shorter than 4-5s, and the maximum angle at which the hatch door can be opened is 90-110 degrees, and the quick opening, closing and larger opening angle of the ha</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>CHECKS FOR WINGS</subject><subject>COSMONAUTICS</subject><subject>DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION</subject><subject>FIXED CONSTRUCTIONS</subject><subject>HELICOPTERS</subject><subject>KEYS</subject><subject>LOCKS</subject><subject>PERFORMING OPERATIONS</subject><subject>SAFES</subject><subject>TRANSPORTING</subject><subject>WINDOW OR DOOR FITTINGS</subject><subject>WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THEFUNCTIONING OF THE WING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB1zFNIzCxKLkpMK1FITkzKzFNIyc8vUsgvSM3LzEtXSEkty0xO5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgYWliamxhbmjsbEqAEADpcm0g</recordid><startdate>20181207</startdate><enddate>20181207</enddate><creator>HUANG ZHENG</creator><creator>WANG LI</creator><creator>RUAN GUOMIN</creator><scope>EVB</scope></search><sort><creationdate>20181207</creationdate><title>An aircraft cabin door opening device</title><author>HUANG ZHENG ; WANG LI ; RUAN GUOMIN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN108945387A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2018</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>CHECKS FOR WINGS</topic><topic>COSMONAUTICS</topic><topic>DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION</topic><topic>FIXED CONSTRUCTIONS</topic><topic>HELICOPTERS</topic><topic>KEYS</topic><topic>LOCKS</topic><topic>PERFORMING OPERATIONS</topic><topic>SAFES</topic><topic>TRANSPORTING</topic><topic>WINDOW OR DOOR FITTINGS</topic><topic>WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THEFUNCTIONING OF THE WING</topic><toplevel>online_resources</toplevel><creatorcontrib>HUANG ZHENG</creatorcontrib><creatorcontrib>WANG LI</creatorcontrib><creatorcontrib>RUAN GUOMIN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUANG ZHENG</au><au>WANG LI</au><au>RUAN GUOMIN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>An aircraft cabin door opening device</title><date>2018-12-07</date><risdate>2018</risdate><abstract>The invention provides an aircraft cabin door opening device, which comprises an electric push rod and a cabin body; one side of the cabin is an mounting opening, and the other three sides are provided with bulkheads; an upper mounting seat is arranged on the inn walls of the bulkheads, and a hatch door is connected with the mounting opening; low mounting seats are arrange on the upper and lower ends of the hatch door; one sides of the lower mounting seats are sequentially provided with rotating seats and fixing seats, and the fixing seats are connected with the rotating seats through rotatingshafts; one end of the electric push rod is connected with the upper mounting seat, and the other end is connected with the lower mounting seats. The invention adopts a simple structure and a lightweight structure, so that the opening time of the hatch door is shorter than 4-5s, and the maximum angle at which the hatch door can be opened is 90-110 degrees, and the quick opening, closing and larger opening angle of the ha</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN108945387A
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
CHECKS FOR WINGS
COSMONAUTICS
DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION
FIXED CONSTRUCTIONS
HELICOPTERS
KEYS
LOCKS
PERFORMING OPERATIONS
SAFES
TRANSPORTING
WINDOW OR DOOR FITTINGS
WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THEFUNCTIONING OF THE WING
title An aircraft cabin door opening device
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-03T13%3A36%3A14IST&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=HUANG%20ZHENG&rft.date=2018-12-07&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN108945387A%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