SELF-PROPELLED LAUNCHER
FIELD: rocketry, in particular, self-propelled launchers. ^ SUBSTANCE: the self-propelled launcher includes a self-propelled chassis, whose frame carries an intermediate body hinge-mounted by means of here bearing assemblies. A rotary platform, in which with the aid a circular support for rotation i...
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 | KOSNAREV LAJMOND KONSTANTINOVICH DANILOV NIKOLAJ MIKHAJLOVICH AULOV LEONID IL'ICH JAKOVLEV STANISLAV ANATOL'EVICH GOLUBEV LEONID BORISOVICH VISHCHUK VIKTOR ADAMOVICH PANTELEEV ALEKSEJ VASIL'EVICH VLADIMIROV UAR IVANOVICH GROMOV ANDREJ VIKTOROVICH KOLESNIKOV PETR PETROVICH ANDREEV VIKTOR MIKHAJLOVICH BEJUSOV RASHID ZHIGANOVICH PANKRATOV BORIS VALENTINOVICH BUTSKIKH EVGENIJ PETROVICH TROFIMOV NIKOLAJ ALEKSEEVICH |
| description | FIELD: rocketry, in particular, self-propelled launchers. ^ SUBSTANCE: the self-propelled launcher includes a self-propelled chassis, whose frame carries an intermediate body hinge-mounted by means of here bearing assemblies. A rotary platform, in which with the aid a circular support for rotation in the vertical plane mounted is a rocker with assemblies for fastening of the missiles. The circular support is joined on the intermediate body for detachment from it in assembly with the rotary platform and rocker for transportation of the self-propelled launcher by railway. The intermediate body is made for placement of the equipment and instrument of the self-propelled launcher. The external surfaces of the upper, rear and side walls of the intermediate body are made jet deflecting. The self-propelled launcher is provided with a device for fixing the mutual position of the rotary platform and the intermediate body in the traveling position. ^ EFFECT: enhanced transportability and expanded operating ability of the launcher. ^ 7 cl, 8 dwg |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_RU2312294C2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>RU2312294C2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_RU2312294C23</originalsourceid><addsrcrecordid>eNrjZBAPdvVx0w0I8g9w9fFxdVHwcQz1c_ZwDeJhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfFBoUbGhkZGlibORsZEKAEAnqAfLg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SELF-PROPELLED LAUNCHER</title><source>esp@cenet</source><creator>KOSNAREV LAJMOND KONSTANTINOVICH ; DANILOV NIKOLAJ MIKHAJLOVICH ; AULOV LEONID IL'ICH ; JAKOVLEV STANISLAV ANATOL'EVICH ; GOLUBEV LEONID BORISOVICH ; VISHCHUK VIKTOR ADAMOVICH ; PANTELEEV ALEKSEJ VASIL'EVICH ; VLADIMIROV UAR IVANOVICH ; GROMOV ANDREJ VIKTOROVICH ; KOLESNIKOV PETR PETROVICH ; ANDREEV VIKTOR MIKHAJLOVICH ; BEJUSOV RASHID ZHIGANOVICH ; PANKRATOV BORIS VALENTINOVICH ; BUTSKIKH EVGENIJ PETROVICH ; TROFIMOV NIKOLAJ ALEKSEEVICH</creator><creatorcontrib>KOSNAREV LAJMOND KONSTANTINOVICH ; DANILOV NIKOLAJ MIKHAJLOVICH ; AULOV LEONID IL'ICH ; JAKOVLEV STANISLAV ANATOL'EVICH ; GOLUBEV LEONID BORISOVICH ; VISHCHUK VIKTOR ADAMOVICH ; PANTELEEV ALEKSEJ VASIL'EVICH ; VLADIMIROV UAR IVANOVICH ; GROMOV ANDREJ VIKTOROVICH ; KOLESNIKOV PETR PETROVICH ; ANDREEV VIKTOR MIKHAJLOVICH ; BEJUSOV RASHID ZHIGANOVICH ; PANKRATOV BORIS VALENTINOVICH ; BUTSKIKH EVGENIJ PETROVICH ; TROFIMOV NIKOLAJ ALEKSEEVICH</creatorcontrib><description>FIELD: rocketry, in particular, self-propelled launchers. ^ SUBSTANCE: the self-propelled launcher includes a self-propelled chassis, whose frame carries an intermediate body hinge-mounted by means of here bearing assemblies. A rotary platform, in which with the aid a circular support for rotation in the vertical plane mounted is a rocker with assemblies for fastening of the missiles. The circular support is joined on the intermediate body for detachment from it in assembly with the rotary platform and rocker for transportation of the self-propelled launcher by railway. The intermediate body is made for placement of the equipment and instrument of the self-propelled launcher. The external surfaces of the upper, rear and side walls of the intermediate body are made jet deflecting. The self-propelled launcher is provided with a device for fixing the mutual position of the rotary platform and the intermediate body in the traveling position. ^ EFFECT: enhanced transportability and expanded operating ability of the launcher. ^ 7 cl, 8 dwg</description><language>eng ; rus</language><subject>BLASTING ; FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; MOUNTINGS FOR SMALLARMS OR ORDNANCE ; WEAPONS</subject><creationdate>2007</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=20071210&DB=EPODOC&CC=RU&NR=2312294C2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20071210&DB=EPODOC&CC=RU&NR=2312294C2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KOSNAREV LAJMOND KONSTANTINOVICH</creatorcontrib><creatorcontrib>DANILOV NIKOLAJ MIKHAJLOVICH</creatorcontrib><creatorcontrib>AULOV LEONID IL'ICH</creatorcontrib><creatorcontrib>JAKOVLEV STANISLAV ANATOL'EVICH</creatorcontrib><creatorcontrib>GOLUBEV LEONID BORISOVICH</creatorcontrib><creatorcontrib>VISHCHUK VIKTOR ADAMOVICH</creatorcontrib><creatorcontrib>PANTELEEV ALEKSEJ VASIL'EVICH</creatorcontrib><creatorcontrib>VLADIMIROV UAR IVANOVICH</creatorcontrib><creatorcontrib>GROMOV ANDREJ VIKTOROVICH</creatorcontrib><creatorcontrib>KOLESNIKOV PETR PETROVICH</creatorcontrib><creatorcontrib>ANDREEV VIKTOR MIKHAJLOVICH</creatorcontrib><creatorcontrib>BEJUSOV RASHID ZHIGANOVICH</creatorcontrib><creatorcontrib>PANKRATOV BORIS VALENTINOVICH</creatorcontrib><creatorcontrib>BUTSKIKH EVGENIJ PETROVICH</creatorcontrib><creatorcontrib>TROFIMOV NIKOLAJ ALEKSEEVICH</creatorcontrib><title>SELF-PROPELLED LAUNCHER</title><description>FIELD: rocketry, in particular, self-propelled launchers. ^ SUBSTANCE: the self-propelled launcher includes a self-propelled chassis, whose frame carries an intermediate body hinge-mounted by means of here bearing assemblies. A rotary platform, in which with the aid a circular support for rotation in the vertical plane mounted is a rocker with assemblies for fastening of the missiles. The circular support is joined on the intermediate body for detachment from it in assembly with the rotary platform and rocker for transportation of the self-propelled launcher by railway. The intermediate body is made for placement of the equipment and instrument of the self-propelled launcher. The external surfaces of the upper, rear and side walls of the intermediate body are made jet deflecting. The self-propelled launcher is provided with a device for fixing the mutual position of the rotary platform and the intermediate body in the traveling position. ^ EFFECT: enhanced transportability and expanded operating ability of the launcher. ^ 7 cl, 8 dwg</description><subject>BLASTING</subject><subject>FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>MOUNTINGS FOR SMALLARMS OR ORDNANCE</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2007</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBAPdvVx0w0I8g9w9fFxdVHwcQz1c_ZwDeJhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfFBoUbGhkZGlibORsZEKAEAnqAfLg</recordid><startdate>20071210</startdate><enddate>20071210</enddate><creator>KOSNAREV LAJMOND KONSTANTINOVICH</creator><creator>DANILOV NIKOLAJ MIKHAJLOVICH</creator><creator>AULOV LEONID IL'ICH</creator><creator>JAKOVLEV STANISLAV ANATOL'EVICH</creator><creator>GOLUBEV LEONID BORISOVICH</creator><creator>VISHCHUK VIKTOR ADAMOVICH</creator><creator>PANTELEEV ALEKSEJ VASIL'EVICH</creator><creator>VLADIMIROV UAR IVANOVICH</creator><creator>GROMOV ANDREJ VIKTOROVICH</creator><creator>KOLESNIKOV PETR PETROVICH</creator><creator>ANDREEV VIKTOR MIKHAJLOVICH</creator><creator>BEJUSOV RASHID ZHIGANOVICH</creator><creator>PANKRATOV BORIS VALENTINOVICH</creator><creator>BUTSKIKH EVGENIJ PETROVICH</creator><creator>TROFIMOV NIKOLAJ ALEKSEEVICH</creator><scope>EVB</scope></search><sort><creationdate>20071210</creationdate><title>SELF-PROPELLED LAUNCHER</title><author>KOSNAREV LAJMOND KONSTANTINOVICH ; DANILOV NIKOLAJ MIKHAJLOVICH ; AULOV LEONID IL'ICH ; JAKOVLEV STANISLAV ANATOL'EVICH ; GOLUBEV LEONID BORISOVICH ; VISHCHUK VIKTOR ADAMOVICH ; PANTELEEV ALEKSEJ VASIL'EVICH ; VLADIMIROV UAR IVANOVICH ; GROMOV ANDREJ VIKTOROVICH ; KOLESNIKOV PETR PETROVICH ; ANDREEV VIKTOR MIKHAJLOVICH ; BEJUSOV RASHID ZHIGANOVICH ; PANKRATOV BORIS VALENTINOVICH ; BUTSKIKH EVGENIJ PETROVICH ; TROFIMOV NIKOLAJ ALEKSEEVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2312294C23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2007</creationdate><topic>BLASTING</topic><topic>FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>MOUNTINGS FOR SMALLARMS OR ORDNANCE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KOSNAREV LAJMOND KONSTANTINOVICH</creatorcontrib><creatorcontrib>DANILOV NIKOLAJ MIKHAJLOVICH</creatorcontrib><creatorcontrib>AULOV LEONID IL'ICH</creatorcontrib><creatorcontrib>JAKOVLEV STANISLAV ANATOL'EVICH</creatorcontrib><creatorcontrib>GOLUBEV LEONID BORISOVICH</creatorcontrib><creatorcontrib>VISHCHUK VIKTOR ADAMOVICH</creatorcontrib><creatorcontrib>PANTELEEV ALEKSEJ VASIL'EVICH</creatorcontrib><creatorcontrib>VLADIMIROV UAR IVANOVICH</creatorcontrib><creatorcontrib>GROMOV ANDREJ VIKTOROVICH</creatorcontrib><creatorcontrib>KOLESNIKOV PETR PETROVICH</creatorcontrib><creatorcontrib>ANDREEV VIKTOR MIKHAJLOVICH</creatorcontrib><creatorcontrib>BEJUSOV RASHID ZHIGANOVICH</creatorcontrib><creatorcontrib>PANKRATOV BORIS VALENTINOVICH</creatorcontrib><creatorcontrib>BUTSKIKH EVGENIJ PETROVICH</creatorcontrib><creatorcontrib>TROFIMOV NIKOLAJ ALEKSEEVICH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KOSNAREV LAJMOND KONSTANTINOVICH</au><au>DANILOV NIKOLAJ MIKHAJLOVICH</au><au>AULOV LEONID IL'ICH</au><au>JAKOVLEV STANISLAV ANATOL'EVICH</au><au>GOLUBEV LEONID BORISOVICH</au><au>VISHCHUK VIKTOR ADAMOVICH</au><au>PANTELEEV ALEKSEJ VASIL'EVICH</au><au>VLADIMIROV UAR IVANOVICH</au><au>GROMOV ANDREJ VIKTOROVICH</au><au>KOLESNIKOV PETR PETROVICH</au><au>ANDREEV VIKTOR MIKHAJLOVICH</au><au>BEJUSOV RASHID ZHIGANOVICH</au><au>PANKRATOV BORIS VALENTINOVICH</au><au>BUTSKIKH EVGENIJ PETROVICH</au><au>TROFIMOV NIKOLAJ ALEKSEEVICH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SELF-PROPELLED LAUNCHER</title><date>2007-12-10</date><risdate>2007</risdate><abstract>FIELD: rocketry, in particular, self-propelled launchers. ^ SUBSTANCE: the self-propelled launcher includes a self-propelled chassis, whose frame carries an intermediate body hinge-mounted by means of here bearing assemblies. A rotary platform, in which with the aid a circular support for rotation in the vertical plane mounted is a rocker with assemblies for fastening of the missiles. The circular support is joined on the intermediate body for detachment from it in assembly with the rotary platform and rocker for transportation of the self-propelled launcher by railway. The intermediate body is made for placement of the equipment and instrument of the self-propelled launcher. The external surfaces of the upper, rear and side walls of the intermediate body are made jet deflecting. The self-propelled launcher is provided with a device for fixing the mutual position of the rotary platform and the intermediate body in the traveling position. ^ EFFECT: enhanced transportability and expanded operating ability of the launcher. ^ 7 cl, 8 dwg</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; rus |
| recordid | cdi_epo_espacenet_RU2312294C2 |
| source | esp@cenet |
| subjects | BLASTING FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS HEATING LIGHTING MECHANICAL ENGINEERING MOUNTINGS FOR SMALLARMS OR ORDNANCE WEAPONS |
| title | SELF-PROPELLED LAUNCHER |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-03T19%3A03%3A48IST&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=KOSNAREV%20LAJMOND%20KONSTANTINOVICH&rft.date=2007-12-10&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ERU2312294C2%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 |