Pneumatically controlled hydraulic drive for aircraft or space vehicle - uses pneumatic charges for two piston-cylinder devices triggered alternately

The hydraulic drive is supplied via at least two piston/cylinder devices (1,4) operating in alternation. Each has a piston (2,5) acted on at one side by a pneumatic control press. and feeding the hydraulic fluid to at least one load (9). The pneumatic pressure is provided by individual charges (3a,3...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ECK,GERHARD, KOERNER,LOTHAR, GUENTERT,ALBERT
Format: Patent
Sprache:eng ; 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 ECK,GERHARD
KOERNER,LOTHAR
GUENTERT,ALBERT
description The hydraulic drive is supplied via at least two piston/cylinder devices (1,4) operating in alternation. Each has a piston (2,5) acted on at one side by a pneumatic control press. and feeding the hydraulic fluid to at least one load (9). The pneumatic pressure is provided by individual charges (3a,3b,3c..6a,6b,6c) lying in front of the piston (2,5) inside or outside of the cylinder. The charges are triggered one after the other in dependence on the minimum or required pressure of the hydraulic system in alternation for the two piston/cylinder devices (1,4). Pref. the two piston/cylinder devices (1,4) are connected in series relative to the hydraulic flow.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_DE2828775A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>DE2828775A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_DE2828775A13</originalsourceid><addsrcrecordid>eNqNTTuOwkAMTUOBgDv4AikIQtCiXVZbUtBHlsdJLHlnIo-TVQ7CfQkIeqr39L7L4naJPPyhC6HqBJSiW1LlAN0UDAcVgmAyMjTJAMXIsHGYee6RGEbuhJShhCFzhv69BtShtbPyqPl_gl6yp1jSpBIDGwQehWbfTdqWbT5EdbaIzjqti0WDmnnzwlUBP-fr12_Jfar5-RzZ6-9zdayOh8P-tN19ELkDQmVRwQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Pneumatically controlled hydraulic drive for aircraft or space vehicle - uses pneumatic charges for two piston-cylinder devices triggered alternately</title><source>esp@cenet</source><creator>ECK,GERHARD ; KOERNER,LOTHAR ; GUENTERT,ALBERT</creator><creatorcontrib>ECK,GERHARD ; KOERNER,LOTHAR ; GUENTERT,ALBERT</creatorcontrib><description>The hydraulic drive is supplied via at least two piston/cylinder devices (1,4) operating in alternation. Each has a piston (2,5) acted on at one side by a pneumatic control press. and feeding the hydraulic fluid to at least one load (9). The pneumatic pressure is provided by individual charges (3a,3b,3c..6a,6b,6c) lying in front of the piston (2,5) inside or outside of the cylinder. The charges are triggered one after the other in dependence on the minimum or required pressure of the hydraulic system in alternation for the two piston/cylinder devices (1,4). Pref. the two piston/cylinder devices (1,4) are connected in series relative to the hydraulic flow.</description><language>eng ; ger</language><subject>BLASTING ; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR ; FLUID-PRESSURE ACTUATORS ; FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS ; HEATING ; HYDRAULICS OR PNEUMATICS IN GENERAL ; LIGHTING ; MECHANICAL ENGINEERING ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL ; WEAPONS</subject><creationdate>1982</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=19820819&amp;DB=EPODOC&amp;CC=DE&amp;NR=2828775A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=19820819&amp;DB=EPODOC&amp;CC=DE&amp;NR=2828775A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ECK,GERHARD</creatorcontrib><creatorcontrib>KOERNER,LOTHAR</creatorcontrib><creatorcontrib>GUENTERT,ALBERT</creatorcontrib><title>Pneumatically controlled hydraulic drive for aircraft or space vehicle - uses pneumatic charges for two piston-cylinder devices triggered alternately</title><description>The hydraulic drive is supplied via at least two piston/cylinder devices (1,4) operating in alternation. Each has a piston (2,5) acted on at one side by a pneumatic control press. and feeding the hydraulic fluid to at least one load (9). The pneumatic pressure is provided by individual charges (3a,3b,3c..6a,6b,6c) lying in front of the piston (2,5) inside or outside of the cylinder. The charges are triggered one after the other in dependence on the minimum or required pressure of the hydraulic system in alternation for the two piston/cylinder devices (1,4). Pref. the two piston/cylinder devices (1,4) are connected in series relative to the hydraulic flow.</description><subject>BLASTING</subject><subject>DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR</subject><subject>FLUID-PRESSURE ACTUATORS</subject><subject>FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS</subject><subject>HEATING</subject><subject>HYDRAULICS OR PNEUMATICS IN GENERAL</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1982</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNTTuOwkAMTUOBgDv4AikIQtCiXVZbUtBHlsdJLHlnIo-TVQ7CfQkIeqr39L7L4naJPPyhC6HqBJSiW1LlAN0UDAcVgmAyMjTJAMXIsHGYee6RGEbuhJShhCFzhv69BtShtbPyqPl_gl6yp1jSpBIDGwQehWbfTdqWbT5EdbaIzjqti0WDmnnzwlUBP-fr12_Jfar5-RzZ6-9zdayOh8P-tN19ELkDQmVRwQ</recordid><startdate>19820819</startdate><enddate>19820819</enddate><creator>ECK,GERHARD</creator><creator>KOERNER,LOTHAR</creator><creator>GUENTERT,ALBERT</creator><scope>EVB</scope></search><sort><creationdate>19820819</creationdate><title>Pneumatically controlled hydraulic drive for aircraft or space vehicle - uses pneumatic charges for two piston-cylinder devices triggered alternately</title><author>ECK,GERHARD ; KOERNER,LOTHAR ; GUENTERT,ALBERT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE2828775A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; ger</language><creationdate>1982</creationdate><topic>BLASTING</topic><topic>DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR</topic><topic>FLUID-PRESSURE ACTUATORS</topic><topic>FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS</topic><topic>HEATING</topic><topic>HYDRAULICS OR PNEUMATICS IN GENERAL</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ECK,GERHARD</creatorcontrib><creatorcontrib>KOERNER,LOTHAR</creatorcontrib><creatorcontrib>GUENTERT,ALBERT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ECK,GERHARD</au><au>KOERNER,LOTHAR</au><au>GUENTERT,ALBERT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Pneumatically controlled hydraulic drive for aircraft or space vehicle - uses pneumatic charges for two piston-cylinder devices triggered alternately</title><date>1982-08-19</date><risdate>1982</risdate><abstract>The hydraulic drive is supplied via at least two piston/cylinder devices (1,4) operating in alternation. Each has a piston (2,5) acted on at one side by a pneumatic control press. and feeding the hydraulic fluid to at least one load (9). The pneumatic pressure is provided by individual charges (3a,3b,3c..6a,6b,6c) lying in front of the piston (2,5) inside or outside of the cylinder. The charges are triggered one after the other in dependence on the minimum or required pressure of the hydraulic system in alternation for the two piston/cylinder devices (1,4). Pref. the two piston/cylinder devices (1,4) are connected in series relative to the hydraulic flow.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; ger
recordid cdi_epo_espacenet_DE2828775A1
source esp@cenet
subjects BLASTING
DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
FLUID-PRESSURE ACTUATORS
FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS
HEATING
HYDRAULICS OR PNEUMATICS IN GENERAL
LIGHTING
MECHANICAL ENGINEERING
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL
WEAPONS
title Pneumatically controlled hydraulic drive for aircraft or space vehicle - uses pneumatic charges for two piston-cylinder devices triggered alternately
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-22T23%3A07%3A51IST&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=ECK,GERHARD&rft.date=1982-08-19&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EDE2828775A1%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