公开(公告)号：KR1020020080944A

公开(公告)日：2002-10-26

申请号：KR1020010020819

申请日：2001-04-18

Applicant: 국방과학연구소

Inventor： 김인학

IPC: F42B10/32

CPC classification number: F41A31/00 ,  F41F1/00

Abstract: PURPOSE: A shot testing apparatus is provided to carry out a shot test without varying a structure of testing equipment by performing the shot test using hydraulic and pneumatic pressure. CONSTITUTION: A shot testing apparatus includes a housing(10) forming a chamber(11) therein. A coupling pipe(13) and a guiding pipe(15) communicated with the chamber(11) are protruded to inner and outer portions of the housing(10). A pressure inlet(17) is formed at the other side of the housing(10). A shooting barrel(20) is coupled to the coupling pipe(13). An object(80) to be shot is accommodated in the shooting barrel(20). An outer peripheral portion of the coupling pipe(13) makes contact with an inner peripheral portion of the shooting barrel(20). In addition, an inner peripheral portion of the shooting barrel(20) makes contact with an outer peripheral portion of the object(80).

Abstract translation: 目的：提供射击测试设备，通过使用液压和气动压力进行射击测试，不改变测试设备的结构进行射击测试。 构成：射出试验装置包括在其中形成腔室（11）的壳体（10）。 与室（11）连通的联接管（13）和引导管（15）突出到壳体（10）的内部和外部。 压力入口（17）形成在壳体（10）的另一侧。 射击枪管（20）联接到联接管（13）。 待拍摄的物体（80）容纳在射击枪管（20）中。 连接管（13）的外周部与射出筒（20）的内周部接触。 另外，拍摄筒（20）的内周部与物体（80）的外周部接触。

公开(公告)号：KR1020020065996A

公开(公告)日：2002-08-14

申请号：KR1020010006150

申请日：2001-02-08

Applicant: 국방과학연구소

Inventor： 전완수 ,  독고욱 ,  김인학 ,  신용재 ,  김찬기 ,  박정기

IPC: B64D17/00

Abstract: PURPOSE: A parachute assembly for a light torpedo of an aircraft is provided to stabilize the torpedo by controlling the posture of the torpedo continuously after firing with deploying the parachute promptly and accurately. CONSTITUTION: A parachute assembly for a light torpedo is composed of a parachute having a canopy(1a) and a rope(1b); a parachute container(2) assembled with the lower part of the rope to contain the parachute, and opened in the upper part; a cover(4) closing the upper part of the parachute container; a pulling rope(5) fixed in an aircraft, and connected to the canopy to pull the parachute in falling the torpedo; an opening unit opening the cover; a pulling rope cutting unit cutting the parachute from the pulling rope; a rotation preventive assembling unit installed in the lower part of the parachute container to restrict rotation of the container, and to assemble with the light torpedo for separating by moving back and forth; and a sleeve(9) fixed in the lower part of the parachute container. The torpedo is controlled stably after firing with deploying the parachute promptly.

Abstract translation: 目的：提供用于飞机轻型鱼雷的降落伞组件，通过快速准确地部署降落伞，在射击后不间断地控制鱼雷的姿势来稳定鱼雷。 构成：用于轻型鱼雷的降落伞组件由具有顶篷（1a）和绳索（1b）的降落伞组成。 与绳索的下部组装以包含降落伞并在上部开口的降落伞容器（2）; 关闭降落伞容器的上部的盖（4）; 固定在飞机上的拉绳（5），并连接到伞架以在落下的鱼雷上拉降伞; 打开盖子的打开单元; 牵引绳切割单元从牵引绳切割降落伞; 旋转防止组装单元，其安装在降落伞容器的下部，以限制容器的旋转，并与轻型鱼雷组装以通过前后移动进行分离; 以及固定在降落伞容器的下部的套筒（9）。 射击后，鱼雷迅速地部署在降落伞上。