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    • 2. 发明授权
    • 포 발사식 탄약
    • KR101906373B1
    • 2018-10-10
    • KR1020160181330
    • 2016-12-28
    • 주식회사 풍산
    • 박창규박성우김기수임태규
    • F42B10/38F42B3/24F41F1/00
    • 본발명은노즐과로켓추진부가구비되어기존고폭탄에비해사거리를증대시킴과아울러, 간단한구조의봉인디스크를이용하여지연점화기의미부홈을밀폐시킴으로써기존로켓마개조립체와동일한밀폐효과를얻을수 있으면서도탄약의보관과사격을용이하게하는등 탄약운용의편리성을향상시킴은물론제조원가를낮출수 있도록한, 포발사식탄약에관한것으로서, 고폭화약또는자탄이탑재되는탄체와; 상기고폭화약을기폭시키거나자탄이방출되도록방출화약을기폭시키도록상기탄체의상부에결합되는신관조립체와; 내부에사거리연장을위한로켓추진제가탑재되고지연제(21)가구비되어상기탄체의하부에결합되는지연점화기(20);를포함하는포 발사식탄약에있어서, 상기지연점화기(20)의후단부에형성된미부홈(25)에압입결합되어상기지연제(21)를습기로부터보호하며, 포발사시발생하는화염에의해파손되어상기지연제(21)가점화되도록하는봉인디스크(10);를더 포함하는것을특징으로한다.
    • 5. 发明公开
    • 포 발사식 탄약
    • KR1020180076787A
    • 2018-07-06
    • KR1020160181330
    • 2016-12-28
    • 주식회사 풍산
    • 박창규박성우김기수임태규
    • F42B10/38F42B3/24F41F1/00
    • F42B10/38F41F1/00F42B3/24
    • 본발명은노즐과로켓추진부가구비되어기존고폭탄에비해사거리를증대시킴과아울러, 간단한구조의봉인디스크를이용하여지연점화기의미부홈을밀폐시킴으로써기존로켓마개조립체와동일한밀폐효과를얻을수 있으면서도탄약의보관과사격을용이하게하는등 탄약운용의편리성을향상시킴은물론제조원가를낮출수 있도록한, 포발사식탄약에관한것으로서, 고폭화약또는자탄이탑재되는탄체와; 상기고폭화약을기폭시키거나자탄이방출되도록방출화약을기폭시키도록상기탄체의상부에결합되는신관조립체와; 내부에사거리연장을위한로켓추진제가탑재되고지연제(21)가구비되어상기탄체의하부에결합되는지연점화기(20);를포함하는포 발사식탄약에있어서, 상기지연점화기(20)의후단부에형성된미부홈(25)에압입결합되어상기지연제(21)를습기로부터보호하며, 포발사시발생하는화염에의해파손되어상기지연제(21)가점화되도록하는봉인디스크(10);를더 포함하는것을특징으로한다.
    • 6. 发明授权
    • 이중결합구조를 구비한 포 발사식 탄약
    • 具有双重联结结构的MORTAR的弹药
    • KR101584488B1
    • 2016-01-19
    • KR1020150095731
    • 2015-07-06
    • 주식회사 풍산
    • 박창규이상준권용대김기수
    • F42B15/36F42B12/58F42B10/34F42B10/38
    • 본발명은대구경곡사포에장전되어발사되며로켓추진제를이용하여사거리를증대시키되, 탄체와로켓하우징이결합되는부분의구조를일부변경하여조립안정성을확보함으로써추진부조립체와탄체가분리되지않도록한 이중결합구조를구비한포 발사식탄약에관한것으로서, 내부에다수의자탄이조립되어이루어진자탄조립체(20)가채워진탄체(15)와, 자탄방출을위한방출장약(14) 및상기자탄조립체(20)를밀어내는방출판(40)과, 상기방출장약(14)을기폭시키도록상기탄체(15)의선단에나사체결되는신관(11)을포함하는탄두부(10)와; 내부에점화지연부(34)가구비된베이스(33)와, 내부에로켓추진제(32)가채워지고후단부가상기베이스(33)에나사결합되며상기탄체(15)의후단내측에수용되는로켓하우징(31)과, 상기베이스(33)의후단부에나사결합되어항력감소제(36)를고정시키는분사기몸체(35) 를구비하는추진부조립체(30);를포함하고, 목표위치에도달한후 신관(11)이작동하여방출장약(14)이기폭되면방출판(40)에의해로켓하우징(31)과탄체(15)가분리되어추진부조립체(30) 및자탄조립체(20)가방출되는포 발사식탄약에있어서, 상기로켓하우징(31) 내부의로켓추진제(32)가연소될때 발생한연소압력에의해로켓하우징(31)과탄체(15)의나사체결부(A)에변형이발생하지않도록베이스(33)와탄체(15)는쐐기결합또는요철결합을통해나사체결부(A)에수직한면에대하여서로엇갈리게맞붙어조립되는것을특징으로한다.
    • 本发明涉及一种用于具有双重接合结构的砂浆的弹药,其通过在增加使用火箭推进剂的范围的同时确保组装稳定性来防止推进部件组件和机身彼此分离。 用于具有双重结构结构的砂浆的弹药包括:弹头部分(10),其包括填充有炸弹组件(20)的机身(15),点火装置(14),排放板(40)和 保险丝(11)拧入机体(15)的前端; 和具有点火延迟部分(34)的基座(33)和填充有火箭推进剂(32)并被容纳在机体(15)的后端中的火箭壳体(31)的推进部件组件(30) ,以及与主体(33)的后端螺纹连接的枪体(35)。
    • 7. 发明公开
    • 풀림성이 좋은 필라멘트 권선방법 및 권선체
    • 用于轻松解决小型BOBBIN的FILAMENT卷绕方法
    • KR1020140147219A
    • 2014-12-30
    • KR1020130070060
    • 2013-06-19
    • 주식회사 와이제이씨주식회사 풍산
    • 배지수김재근김승일박성우박창규김기수
    • B65H54/10B65H55/04
    • B65H55/04B65H54/06B65H75/10B65H2701/31
    • The present invention relates to a winding method for smoothly unwinding long and thin fibers (filaments) wound on a small bobbin, and the manufacturing of a winding body wound with the fibers (filaments) on the small bobbin thereof by this winding method, wherein the fibers (filaments) wound on a light and small cylindrical bobbin can be freely released. The present invention as above provides a filament winding method for winding filaments on a bobbin, wherein a filament is wound on a bobbin while forming a polar winding azimuth of a predetermined angle with respect to the bobbin rotation axis of the bobbin by the polar winding method and, after winding the filament once at the polar winding azimuth, next winding is carried out after the bobbin rotates at the predetermined angle with respect to the bobbin rotation axis.
    • 卷绕方法技术领域本发明涉及一种卷绕方法,用于平滑地卷绕缠绕在小线轴上的长而细的纤维(长丝),并且通过该卷绕方法制造卷绕在其小线轴上的纤维(长丝)的卷绕体,其中, 卷绕在轻小圆柱形筒管上的纤维(细丝)可以自由释放。 如上所述,本发明提供了一种用于将线圈缠绕在线轴上的长丝缠绕方法,其中通过极性卷绕法将丝线缠绕在线轴上,同时以相对于线轴的线轴旋转轴线形成预定角度的极坐标方位角 并且,在以极圈方位卷绕灯丝一次之后,在筒管相对于筒管旋转轴以预定角度旋转之后进行下一次卷绕。
    • 8. 发明公开
    • 비상체 관측 어셈블리 및 이를 구비하는 비상체
    • 观察飞行对象和具有相同对象的飞行对象的组装
    • KR1020130087155A
    • 2013-08-06
    • KR1020120008217
    • 2012-01-27
    • (주)화이트스톤주식회사 풍산
    • 노동수박찬현이용수홍찬호김기수진희식양성진박동준김정립
    • F42B12/34G01S7/04
    • F42B12/382F42B12/38
    • PURPOSE: Assembly for observing a flying body and a flying body including the same are provided to facilitate replacing a set-back battery in a power supply unit, thereby helping people to actively cope with the situation when the set-back battery is discharged. CONSTITUTION: Assembly for observing a flying body comprises a light emitting unit (41) and a protecting body (31). The light emitting unit shines a beam when being supplied with power so that a flying object is observed. The protection body is arranged at the end of the flying body. The protection body has the light emitting unit at the end in order to protect the light emitting unit from any force applied to the flying object for the purpose of making the flying object fly. The light emitting unit is fixed to the protection body with a screw.
    • 目的:提供用于观察飞行体和包括其的飞行体的组装件,以便于更换电源单元中的安装式电池,从而帮助人们积极应对安全电池放电时的情况。 构成:用于观察飞行体的组件包括发光单元(41)和保护体(31)。 发光单元在被供电时照射光束,从而观察飞行物体。 保护体设置在飞行体的末端。 保护体在末端具有发光单元,以便保护发光单元不受施加到飞行物体的任何作用力以使飞行物体飞行。 发光单元用螺钉固定在保护体上。