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公开(公告)号：KR101250245B1
公开(公告)日：2013-04-04
申请号：KR1020110109572
申请日：2011-10-25
Applicant: 국방과학연구소
Abstract: PURPOSE: A pitot tube inspecting device and a pressure measuring system are provided to enable the movement of probe tubes along the height and in a circumferential direction as the probe tubes are laminated and arranged along the circumference of a body. CONSTITUTION: A pitot tube inspecting device(200) comprises a circular body(210), a probe tube module(220), and a joining unit. The probe tube module includes probe tubes of a pitot tube which are laminated along a diameter direction of the body. The joining unit is formed along the outer circumference of the body so that the probe tube module can be moved along the outer circumference of the body. The joining unit includes protrusions and a plurality of joining holes. The protrusions are protruded in the outer circumference of the body and formed along the outer circumference of the body. The joining holes are arranged separately from the protrusions.
Abstract translation: 目的：提供皮托管检查装置和压力测量系统，以便当探针管沿着身体的圆周层叠并布置时，使探针管沿着身高和周向移动。 构成：皮托管检查装置（200）包括圆形体（210），探针管模块（220）和接合单元。 探针管模块包括沿着身体的直径方向层叠的皮托管的探针管。 接合单元沿着主体的外周形成，使得探针管模块可以沿着身体的外周移动。 接合单元包括突起和多个接合孔。 突起在主体的外周突出，并沿主体的外周形成。 连接孔与突起分开设置。
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公开(公告)号：KR101364636B1
公开(公告)日：2014-02-20
申请号：KR1020110117106
申请日：2011-11-10
Applicant: 국방과학연구소
Abstract: 본 발명은 원통형 발사관에 사용될 수 있으며, 유도조종 성능이 우수하도록 롤링 모멘트를 줄이고 기동성을 향상시킨 유도탄을 위한 네 개의 접이식 곡면날개에 관한 것으로, 본 발명의 접이식 곡면날개의 일 실시예는, 곡면날개; 상기 곡면날개의 하부에 구비되어 상기 곡면형 날개를 회동가능하게 유도탄에 결합시키는 연결부;를 포함하고, 상기 곡면형 날개는 만곡된 내부를 형성하는 내부면과 외부면을 포함하고, 상기 곡면날개의 상단부는 곡면날개의 상단과 후단을 연결하는 중심선을 중심으로 외부면이 사각으로 절단되어 있는 것을 특징으로 한다.
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Patent Agency Ranking
公开(公告)号：KR101812602B1
公开(公告)日：2017-12-27
申请号：KR1020150134054
申请日：2015-09-22
Applicant: 국방과학연구소
Abstract: 본발명은배기유동의유동량과유동방향을동시에조절하는유동제어구동기를제안한다. 본발명에서제안하는유동제어구동기는, 유동을배기하도록이루어지는배기관; 및상기배기관으로부터배기되는유동의배기경로에설치되고, 서로이격되도록배치되어그 사이에상기유동을통과시키는노즐의목을형성하는복수의회전부재를포함하고, 상기목의단면적과상기유동의방향을동시에조절하도록, 상기각 회전부재의회전방향과회전각도가서로독립적으로제어된다.
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公开(公告)号：KR1020090117147A
公开(公告)日：2009-11-12
申请号：KR1020080043059
申请日：2008-05-08
Applicant: 국방과학연구소
Abstract: PURPOSE: A wind tunnel testing apparatus and method are provided to measure the power and the moment which act on a rotator, and the rotation number and speed of the rotator accurately and efficiently. CONSTITUTION: A wind tunnel testing apparatus includes a supporting member(100) which tilts a rotator(11) at a specific angle to the direction of compressed fluid and includes a flow channel for actuating fluid, a locking unit(200) which locks or releases the rotator, a rotating unit(300) which rotates the rotator by the actuating fluid when releasing the locked rotator, and a sensing unit(400) which measures the clamping force which acts on the rotator by the Magnus effect during the rotation of the rotator.
Abstract translation: 目的：提供一种风洞试验装置和方法，用于测量转子的功率和力矩，准确而有效地测量转子的转速和转速。 构成：风洞测试装置包括支撑构件（100），该支撑构件以与压缩流体的方向成特定角度倾斜旋转体（11）并且包括用于致动流体的流动通道，锁定或释放的锁定单元（200） 旋转器，当释放锁定的旋转器时由致动流体旋转旋转器的旋转单元（300）以及感测单元（400），其在旋转体旋转期间测量作用在旋转体上的马克努斯效应的夹紧力 。
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公开(公告)号：KR1020130051770A
公开(公告)日：2013-05-21
申请号：KR1020110117106
申请日：2011-11-10
Applicant: 국방과학연구소
Abstract: PURPOSE: A four folding curved wing for a guided missile launched from a cylindrical torpedo tube is provided to secure high mobility by reducing static stability of the guided missile. CONSTITUTION: A four folding curved wing comprises a curved wing and a connection unit. The connection unit is equipped on a lower part of the curved wing and connects the curved wing to a guided missile to be rotated. The curved wing includes inner surface and outer surface forming a curved inner space. An upper part of the curved wing includes outer surface which is cut in a square shape around a central line connecting the upper end and the lower end of the curved wing.
Abstract translation: 目的：提供一个从圆柱形鱼雷管发射的导弹的四折弯曲翼，以通过降低导弹的静态稳定性来确保高度的移动性。 构成：四个弯曲的弯曲翼包括弯曲的翼和连接单元。 连接单元配备在弯曲翼的下部，并将弯曲的翼连接到导弹以旋转。 弯曲的机翼包括形成弯曲的内部空间的内表面和外表面。 弯曲翼的上部包括围绕连接弯曲翼的上端和下端的中心线切成正方形的外表面。
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公开(公告)号：KR100929002B1
公开(公告)日：2009-11-27
申请号：KR1020080043059
申请日：2008-05-08
Applicant: 국방과학연구소
Abstract: PURPOSE: A wind tunnel testing apparatus and method are provided to measure the power and the moment which act on a rotator, and the rotation number and speed of the rotator accurately and efficiently. CONSTITUTION: A wind tunnel testing apparatus includes a supporting member(100) which tilts a rotator(11) at a specific angle to the direction of compressed fluid and includes a flow channel for actuating fluid, a locking unit(200) which locks or releases the rotator, a rotating unit(300) which rotates the rotator by the actuating fluid when releasing the locked rotator, and a sensing unit(400) which measures the clamping force which acts on the rotator by the Magnus effect during the rotation of the rotator.
Abstract translation: 目的：提供一种风洞试验装置和方法，以准确和高效地测量作用在旋转器上的功率和力矩以及旋转器的旋转次数和速度。 本发明公开了一种风洞试验装置，该风洞试验装置包括：使旋转体（11）相对于压缩流体的方向成特定角度倾斜的支承部件（100），该支承部件包括用于驱动流体的流道;锁定单元（200） 旋转体，在释放锁定的旋转体时通过致动流体旋转旋转体的旋转单元（300）以及在旋转体旋转过程中测量通过马格努斯效应作用在旋转体上的夹持力的感测单元（400） 。
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公开(公告)号：KR1020170035223A
公开(公告)日：2017-03-30
申请号：KR1020150134054
申请日：2015-09-22
Applicant: 국방과학연구소
Abstract: 본발명은배기유동의유동량과유동방향을동시에조절하는유동제어구동기를제안한다. 본발명에서제안하는유동제어구동기는, 유동을배기하도록이루어지는배기관; 및상기배기관으로부터배기되는유동의배기경로에설치되고, 서로이격되도록배치되어그 사이에상기유동을통과시키는노즐의목을형성하는복수의회전부재를포함하고, 상기목의단면적과상기유동의방향을동시에조절하도록, 상기각 회전부재의회전방향과회전각도가서로독립적으로제어된다.
Abstract translation: 本发明提出了一种用于同时控制排气流量和流动方向的流量控制致动器。 在本发明中提出的流量控制致动器包括：排气管，其构造成排出流体; 并且在从排气管中排出的流动的排气路径中，它被设置成彼此间隔开的多个构成所述喷嘴的喉部穿过其间的流动旋转构件，并且所述横截面面积的方向和所述颈部的所述流 每个旋转构件的旋转方向和旋转角度被彼此独立地控制。
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