LAUNCHERS
A launch pad according to an embodiment of the present invention comprises: a storage unit in which a launch body is stored; a first support member supporting the storage unit; a second support member arranged after being spaced from the first support member; a hinge member rotatably connecting the...
Gespeichert in:
| Hauptverfasser: | , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; kor |
| 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 | JUN DAE KEUN YANG BU YEOL HWANG JIN HA LEE HYE KWANG |
| description | A launch pad according to an embodiment of the present invention comprises: a storage unit in which a launch body is stored; a first support member supporting the storage unit; a second support member arranged after being spaced from the first support member; a hinge member rotatably connecting the interval between the first support member and the second support member; a first driving member supplying driving force such that the first support member may move about the hinge member; and an auxiliary driving unit supplying elastic force to the first support member when the first support member is operated, in order to be rotated in a direction in which the first support member retreats from the second support member.
본 발명의 실시예는 발사대에 관한 것으로, 발사대는 발사체가 수납되는 수납부와, 상기 수납부를 지지하는 제1 지지부재와, 상기 제1 지지부재와 이격 배치된 제2 지지부재와, 상기 제1 지지부재와 상기 제2 지지부재 사이를 회동 가능하게 연결하는 힌지부재와, 상기 힌지부재를 중심으로 상기 제1 지지부재가 이동되도록 구동력을 제공하는 제1 구동부재, 그리고 상기 제2 지지부재로부터 상기 제1 지지부재가 멀어지는 방향으로 회동되기 위해 상기 제1 구동부재의 동작 시 상기 제1 지지부재에 탄성력을 제공하는 보조 구동부를 포함한다. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_KR101977497BB1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>KR101977497BB1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_KR101977497BB13</originalsourceid><addsrcrecordid>eNrjZOD0cQz1c_ZwDQrmYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXx3kGGBoaW5uYmluZOTobGxKkCALNFHLM</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>LAUNCHERS</title><source>esp@cenet</source><creator>JUN DAE KEUN ; YANG BU YEOL ; HWANG JIN HA ; LEE HYE KWANG</creator><creatorcontrib>JUN DAE KEUN ; YANG BU YEOL ; HWANG JIN HA ; LEE HYE KWANG</creatorcontrib><description>A launch pad according to an embodiment of the present invention comprises: a storage unit in which a launch body is stored; a first support member supporting the storage unit; a second support member arranged after being spaced from the first support member; a hinge member rotatably connecting the interval between the first support member and the second support member; a first driving member supplying driving force such that the first support member may move about the hinge member; and an auxiliary driving unit supplying elastic force to the first support member when the first support member is operated, in order to be rotated in a direction in which the first support member retreats from the second support member.
본 발명의 실시예는 발사대에 관한 것으로, 발사대는 발사체가 수납되는 수납부와, 상기 수납부를 지지하는 제1 지지부재와, 상기 제1 지지부재와 이격 배치된 제2 지지부재와, 상기 제1 지지부재와 상기 제2 지지부재 사이를 회동 가능하게 연결하는 힌지부재와, 상기 힌지부재를 중심으로 상기 제1 지지부재가 이동되도록 구동력을 제공하는 제1 구동부재, 그리고 상기 제2 지지부재로부터 상기 제1 지지부재가 멀어지는 방향으로 회동되기 위해 상기 제1 구동부재의 동작 시 상기 제1 지지부재에 탄성력을 제공하는 보조 구동부를 포함한다.</description><language>eng ; kor</language><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; BLASTING ; HARPOON GUNS ; HEATING ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TOCARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS ; VEHICLES IN GENERAL ; WEAPONS</subject><creationdate>2019</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=20190510&DB=EPODOC&CC=KR&NR=101977497B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76418</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190510&DB=EPODOC&CC=KR&NR=101977497B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JUN DAE KEUN</creatorcontrib><creatorcontrib>YANG BU YEOL</creatorcontrib><creatorcontrib>HWANG JIN HA</creatorcontrib><creatorcontrib>LEE HYE KWANG</creatorcontrib><title>LAUNCHERS</title><description>A launch pad according to an embodiment of the present invention comprises: a storage unit in which a launch body is stored; a first support member supporting the storage unit; a second support member arranged after being spaced from the first support member; a hinge member rotatably connecting the interval between the first support member and the second support member; a first driving member supplying driving force such that the first support member may move about the hinge member; and an auxiliary driving unit supplying elastic force to the first support member when the first support member is operated, in order to be rotated in a direction in which the first support member retreats from the second support member.
본 발명의 실시예는 발사대에 관한 것으로, 발사대는 발사체가 수납되는 수납부와, 상기 수납부를 지지하는 제1 지지부재와, 상기 제1 지지부재와 이격 배치된 제2 지지부재와, 상기 제1 지지부재와 상기 제2 지지부재 사이를 회동 가능하게 연결하는 힌지부재와, 상기 힌지부재를 중심으로 상기 제1 지지부재가 이동되도록 구동력을 제공하는 제1 구동부재, 그리고 상기 제2 지지부재로부터 상기 제1 지지부재가 멀어지는 방향으로 회동되기 위해 상기 제1 구동부재의 동작 시 상기 제1 지지부재에 탄성력을 제공하는 보조 구동부를 포함한다.</description><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>BLASTING</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TOCARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS</subject><subject>VEHICLES IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOD0cQz1c_ZwDQrmYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXx3kGGBoaW5uYmluZOTobGxKkCALNFHLM</recordid><startdate>20190510</startdate><enddate>20190510</enddate><creator>JUN DAE KEUN</creator><creator>YANG BU YEOL</creator><creator>HWANG JIN HA</creator><creator>LEE HYE KWANG</creator><scope>EVB</scope></search><sort><creationdate>20190510</creationdate><title>LAUNCHERS</title><author>JUN DAE KEUN ; YANG BU YEOL ; HWANG JIN HA ; LEE HYE KWANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR101977497BB13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2019</creationdate><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>BLASTING</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TOCARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS</topic><topic>VEHICLES IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>JUN DAE KEUN</creatorcontrib><creatorcontrib>YANG BU YEOL</creatorcontrib><creatorcontrib>HWANG JIN HA</creatorcontrib><creatorcontrib>LEE HYE KWANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JUN DAE KEUN</au><au>YANG BU YEOL</au><au>HWANG JIN HA</au><au>LEE HYE KWANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LAUNCHERS</title><date>2019-05-10</date><risdate>2019</risdate><abstract>A launch pad according to an embodiment of the present invention comprises: a storage unit in which a launch body is stored; a first support member supporting the storage unit; a second support member arranged after being spaced from the first support member; a hinge member rotatably connecting the interval between the first support member and the second support member; a first driving member supplying driving force such that the first support member may move about the hinge member; and an auxiliary driving unit supplying elastic force to the first support member when the first support member is operated, in order to be rotated in a direction in which the first support member retreats from the second support member.
본 발명의 실시예는 발사대에 관한 것으로, 발사대는 발사체가 수납되는 수납부와, 상기 수납부를 지지하는 제1 지지부재와, 상기 제1 지지부재와 이격 배치된 제2 지지부재와, 상기 제1 지지부재와 상기 제2 지지부재 사이를 회동 가능하게 연결하는 힌지부재와, 상기 힌지부재를 중심으로 상기 제1 지지부재가 이동되도록 구동력을 제공하는 제1 구동부재, 그리고 상기 제2 지지부재로부터 상기 제1 지지부재가 멀어지는 방향으로 회동되기 위해 상기 제1 구동부재의 동작 시 상기 제1 지지부재에 탄성력을 제공하는 보조 구동부를 포함한다.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; kor |
| recordid | cdi_epo_espacenet_KR101977497BB1 |
| source | esp@cenet |
| subjects | APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS BLASTING HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TOCARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS VEHICLES IN GENERAL WEAPONS |
| title | LAUNCHERS |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-08T19%3A36%3A11IST&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=JUN%20DAE%20KEUN&rft.date=2019-05-10&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EKR101977497BB1%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 |