SHOOTING MECHANISM
FIELD: weapons. ^ SUBSTANCE: invention concerns area of launching gears. The shooting mechanism contains a cylinder connected telescopically with a rod, gas producer with ignition cylinder, a gas cavity, a lock connecting the cylinder with the rod, and a stop block of the rod on the cylinder. The ro...
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| creator | MATRUSOV VLADIMIR DANILOVICH LEVCHENKO JURIJ NIKOLAEVICH SHCHEGLOV VALERIJ ANATOL'EVICH OBREZCHIKOV VLADIMIR VASIL'EVICH SYZDYKOV ELTUGAN KIMASHEVICH |
| description | FIELD: weapons. ^ SUBSTANCE: invention concerns area of launching gears. The shooting mechanism contains a cylinder connected telescopically with a rod, gas producer with ignition cylinder, a gas cavity, a lock connecting the cylinder with the rod, and a stop block of the rod on the cylinder. The rod is located outside the cylinder. The gas producer contains a nozzle supplied with the device for changing of traction vector. The ring space is created between the rod and the cylinder with the damper located on the cylinder, the said damper being executed in the form of elastic capacity with damping liquid and capable of moving against the rod and destructing of elastic capacity in the end of travel. There is a recoil-dampening cavity with throttle apertures from the side of ring space in the rod. The gas cavity is supplied with an operated valve of dump of gases. ^ EFFECT: decreased vibroimpulsive loads, increased power characteristics, ruling out influence of high-temperature gases on a design, reduced overall dimensions of the mechanism. ^ 1 dwg |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_RU2334933C1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>RU2334933C1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_RU2334933C13</originalsourceid><addsrcrecordid>eNrjZBAK9vD3D_H0c1fwdXX2cPTzDPblYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxQaFGxsYmlsbGzobGRCgBAA9hHd8</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SHOOTING MECHANISM</title><source>esp@cenet</source><creator>MATRUSOV VLADIMIR DANILOVICH ; LEVCHENKO JURIJ NIKOLAEVICH ; SHCHEGLOV VALERIJ ANATOL'EVICH ; OBREZCHIKOV VLADIMIR VASIL'EVICH ; SYZDYKOV ELTUGAN KIMASHEVICH</creator><creatorcontrib>MATRUSOV VLADIMIR DANILOVICH ; LEVCHENKO JURIJ NIKOLAEVICH ; SHCHEGLOV VALERIJ ANATOL'EVICH ; OBREZCHIKOV VLADIMIR VASIL'EVICH ; SYZDYKOV ELTUGAN KIMASHEVICH</creatorcontrib><description>FIELD: weapons. ^ SUBSTANCE: invention concerns area of launching gears. The shooting mechanism contains a cylinder connected telescopically with a rod, gas producer with ignition cylinder, a gas cavity, a lock connecting the cylinder with the rod, and a stop block of the rod on the cylinder. The rod is located outside the cylinder. The gas producer contains a nozzle supplied with the device for changing of traction vector. The ring space is created between the rod and the cylinder with the damper located on the cylinder, the said damper being executed in the form of elastic capacity with damping liquid and capable of moving against the rod and destructing of elastic capacity in the end of travel. There is a recoil-dampening cavity with throttle apertures from the side of ring space in the rod. The gas cavity is supplied with an operated valve of dump of gases. ^ EFFECT: decreased vibroimpulsive loads, increased power characteristics, ruling out influence of high-temperature gases on a design, reduced overall dimensions of the mechanism. ^ 1 dwg</description><language>eng ; rus</language><subject>AIRCRAFT ; APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINEERING ELEMENTS AND UNITS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HARPOON GUNS ; HEATING ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MEANS FOR DAMPING VIBRATION ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; SHOCK-ABSORBERS ; SPRINGS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2008</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=20080927&DB=EPODOC&CC=RU&NR=2334933C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25569,76552</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20080927&DB=EPODOC&CC=RU&NR=2334933C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MATRUSOV VLADIMIR DANILOVICH</creatorcontrib><creatorcontrib>LEVCHENKO JURIJ NIKOLAEVICH</creatorcontrib><creatorcontrib>SHCHEGLOV VALERIJ ANATOL'EVICH</creatorcontrib><creatorcontrib>OBREZCHIKOV VLADIMIR VASIL'EVICH</creatorcontrib><creatorcontrib>SYZDYKOV ELTUGAN KIMASHEVICH</creatorcontrib><title>SHOOTING MECHANISM</title><description>FIELD: weapons. ^ SUBSTANCE: invention concerns area of launching gears. The shooting mechanism contains a cylinder connected telescopically with a rod, gas producer with ignition cylinder, a gas cavity, a lock connecting the cylinder with the rod, and a stop block of the rod on the cylinder. The rod is located outside the cylinder. The gas producer contains a nozzle supplied with the device for changing of traction vector. The ring space is created between the rod and the cylinder with the damper located on the cylinder, the said damper being executed in the form of elastic capacity with damping liquid and capable of moving against the rod and destructing of elastic capacity in the end of travel. There is a recoil-dampening cavity with throttle apertures from the side of ring space in the rod. The gas cavity is supplied with an operated valve of dump of gases. ^ EFFECT: decreased vibroimpulsive loads, increased power characteristics, ruling out influence of high-temperature gases on a design, reduced overall dimensions of the mechanism. ^ 1 dwg</description><subject>AIRCRAFT</subject><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MEANS FOR DAMPING VIBRATION</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>SHOCK-ABSORBERS</subject><subject>SPRINGS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2008</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBAK9vD3D_H0c1fwdXX2cPTzDPblYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxQaFGxsYmlsbGzobGRCgBAA9hHd8</recordid><startdate>20080927</startdate><enddate>20080927</enddate><creator>MATRUSOV VLADIMIR DANILOVICH</creator><creator>LEVCHENKO JURIJ NIKOLAEVICH</creator><creator>SHCHEGLOV VALERIJ ANATOL'EVICH</creator><creator>OBREZCHIKOV VLADIMIR VASIL'EVICH</creator><creator>SYZDYKOV ELTUGAN KIMASHEVICH</creator><scope>EVB</scope></search><sort><creationdate>20080927</creationdate><title>SHOOTING MECHANISM</title><author>MATRUSOV VLADIMIR DANILOVICH ; LEVCHENKO JURIJ NIKOLAEVICH ; SHCHEGLOV VALERIJ ANATOL'EVICH ; OBREZCHIKOV VLADIMIR VASIL'EVICH ; SYZDYKOV ELTUGAN KIMASHEVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2334933C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2008</creationdate><topic>AIRCRAFT</topic><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MEANS FOR DAMPING VIBRATION</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>SHOCK-ABSORBERS</topic><topic>SPRINGS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>MATRUSOV VLADIMIR DANILOVICH</creatorcontrib><creatorcontrib>LEVCHENKO JURIJ NIKOLAEVICH</creatorcontrib><creatorcontrib>SHCHEGLOV VALERIJ ANATOL'EVICH</creatorcontrib><creatorcontrib>OBREZCHIKOV VLADIMIR VASIL'EVICH</creatorcontrib><creatorcontrib>SYZDYKOV ELTUGAN KIMASHEVICH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MATRUSOV VLADIMIR DANILOVICH</au><au>LEVCHENKO JURIJ NIKOLAEVICH</au><au>SHCHEGLOV VALERIJ ANATOL'EVICH</au><au>OBREZCHIKOV VLADIMIR VASIL'EVICH</au><au>SYZDYKOV ELTUGAN KIMASHEVICH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SHOOTING MECHANISM</title><date>2008-09-27</date><risdate>2008</risdate><abstract>FIELD: weapons. ^ SUBSTANCE: invention concerns area of launching gears. The shooting mechanism contains a cylinder connected telescopically with a rod, gas producer with ignition cylinder, a gas cavity, a lock connecting the cylinder with the rod, and a stop block of the rod on the cylinder. The rod is located outside the cylinder. The gas producer contains a nozzle supplied with the device for changing of traction vector. The ring space is created between the rod and the cylinder with the damper located on the cylinder, the said damper being executed in the form of elastic capacity with damping liquid and capable of moving against the rod and destructing of elastic capacity in the end of travel. There is a recoil-dampening cavity with throttle apertures from the side of ring space in the rod. The gas cavity is supplied with an operated valve of dump of gases. ^ EFFECT: decreased vibroimpulsive loads, increased power characteristics, ruling out influence of high-temperature gases on a design, reduced overall dimensions of the mechanism. ^ 1 dwg</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | SHOOTING MECHANISM |
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