ELECTROHYDRAULIC SERVO UNIT
FIELD: actuating mechanisms for control of flying vehicles, for example shifting the flying vehicle controls at supply of control electrical signals. ^ SUBSTANCE: proposed electrohydraulic servo unit includes actuating mechanism, distributing unit communicating the cavities of actuating mechanism wi...
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | eng ; rus |
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 | RED'KO PAVEL GRIGOR'EVICH VERIN NIKOLAJ ALEKSEEVICH AMBARNIKOV ANATOLIJ VASIL'EVICH TROFIMOV SERGEJ EVGEN'EVICH |
description | FIELD: actuating mechanisms for control of flying vehicles, for example shifting the flying vehicle controls at supply of control electrical signals. ^ SUBSTANCE: proposed electrohydraulic servo unit includes actuating mechanism, distributing unit communicating the cavities of actuating mechanism with pressure or return hydraulic lines, electrohydraulic valve and two-position valve. Two-position valve is provided with two cavities which bring in communication the pressure hydraulic line and retraction cavity of actuating mechanism with distributing unit through hydraulic lines. ^ EFFECT: enhanced operational reliability due to avoidance of emergency operation of landing gear transmission. ^ 1 dwg |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_RU2268197C1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>RU2268197C1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_RU2268197C13</originalsourceid><addsrcrecordid>eNrjZJB29XF1Dgny94h0CXIM9fF0Vgh2DQrzVwj18wzhYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxQaFGRmYWhpbmzobGRCgBADRRIJo</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ELECTROHYDRAULIC SERVO UNIT</title><source>esp@cenet</source><creator>RED'KO PAVEL GRIGOR'EVICH ; VERIN NIKOLAJ ALEKSEEVICH ; AMBARNIKOV ANATOLIJ VASIL'EVICH ; TROFIMOV SERGEJ EVGEN'EVICH</creator><creatorcontrib>RED'KO PAVEL GRIGOR'EVICH ; VERIN NIKOLAJ ALEKSEEVICH ; AMBARNIKOV ANATOLIJ VASIL'EVICH ; TROFIMOV SERGEJ EVGEN'EVICH</creatorcontrib><description>FIELD: actuating mechanisms for control of flying vehicles, for example shifting the flying vehicle controls at supply of control electrical signals. ^ SUBSTANCE: proposed electrohydraulic servo unit includes actuating mechanism, distributing unit communicating the cavities of actuating mechanism with pressure or return hydraulic lines, electrohydraulic valve and two-position valve. Two-position valve is provided with two cavities which bring in communication the pressure hydraulic line and retraction cavity of actuating mechanism with distributing unit through hydraulic lines. ^ EFFECT: enhanced operational reliability due to avoidance of emergency operation of landing gear transmission. ^ 1 dwg</description><language>eng ; rus</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2006</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=20060120&DB=EPODOC&CC=RU&NR=2268197C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25569,76552</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20060120&DB=EPODOC&CC=RU&NR=2268197C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RED'KO PAVEL GRIGOR'EVICH</creatorcontrib><creatorcontrib>VERIN NIKOLAJ ALEKSEEVICH</creatorcontrib><creatorcontrib>AMBARNIKOV ANATOLIJ VASIL'EVICH</creatorcontrib><creatorcontrib>TROFIMOV SERGEJ EVGEN'EVICH</creatorcontrib><title>ELECTROHYDRAULIC SERVO UNIT</title><description>FIELD: actuating mechanisms for control of flying vehicles, for example shifting the flying vehicle controls at supply of control electrical signals. ^ SUBSTANCE: proposed electrohydraulic servo unit includes actuating mechanism, distributing unit communicating the cavities of actuating mechanism with pressure or return hydraulic lines, electrohydraulic valve and two-position valve. Two-position valve is provided with two cavities which bring in communication the pressure hydraulic line and retraction cavity of actuating mechanism with distributing unit through hydraulic lines. ^ EFFECT: enhanced operational reliability due to avoidance of emergency operation of landing gear transmission. ^ 1 dwg</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>2006</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB29XF1Dgny94h0CXIM9fF0Vgh2DQrzVwj18wzhYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxQaFGRmYWhpbmzobGRCgBADRRIJo</recordid><startdate>20060120</startdate><enddate>20060120</enddate><creator>RED'KO PAVEL GRIGOR'EVICH</creator><creator>VERIN NIKOLAJ ALEKSEEVICH</creator><creator>AMBARNIKOV ANATOLIJ VASIL'EVICH</creator><creator>TROFIMOV SERGEJ EVGEN'EVICH</creator><scope>EVB</scope></search><sort><creationdate>20060120</creationdate><title>ELECTROHYDRAULIC SERVO UNIT</title><author>RED'KO PAVEL GRIGOR'EVICH ; VERIN NIKOLAJ ALEKSEEVICH ; AMBARNIKOV ANATOLIJ VASIL'EVICH ; TROFIMOV SERGEJ EVGEN'EVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2268197C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2006</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>RED'KO PAVEL GRIGOR'EVICH</creatorcontrib><creatorcontrib>VERIN NIKOLAJ ALEKSEEVICH</creatorcontrib><creatorcontrib>AMBARNIKOV ANATOLIJ VASIL'EVICH</creatorcontrib><creatorcontrib>TROFIMOV SERGEJ EVGEN'EVICH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RED'KO PAVEL GRIGOR'EVICH</au><au>VERIN NIKOLAJ ALEKSEEVICH</au><au>AMBARNIKOV ANATOLIJ VASIL'EVICH</au><au>TROFIMOV SERGEJ EVGEN'EVICH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ELECTROHYDRAULIC SERVO UNIT</title><date>2006-01-20</date><risdate>2006</risdate><abstract>FIELD: actuating mechanisms for control of flying vehicles, for example shifting the flying vehicle controls at supply of control electrical signals. ^ SUBSTANCE: proposed electrohydraulic servo unit includes actuating mechanism, distributing unit communicating the cavities of actuating mechanism with pressure or return hydraulic lines, electrohydraulic valve and two-position valve. Two-position valve is provided with two cavities which bring in communication the pressure hydraulic line and retraction cavity of actuating mechanism with distributing unit through hydraulic lines. ^ EFFECT: enhanced operational reliability due to avoidance of emergency operation of landing gear transmission. ^ 1 dwg</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng ; rus |
recordid | cdi_epo_espacenet_RU2268197C1 |
source | esp@cenet |
subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | ELECTROHYDRAULIC SERVO UNIT |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-13T18%3A47%3A45IST&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=RED'KO%20PAVEL%20GRIGOR'EVICH&rft.date=2006-01-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ERU2268197C1%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 |