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公开(公告)号：KR1020170029260A
公开(公告)日：2017-03-15
申请号：KR1020150126371
申请日：2015-09-07
Applicant: 국방과학연구소
Abstract: 본발명은매트릭스스위치모듈을이용하여일일이단자를접속/해제하는과정없이자동으로점검할수 있는풍동시험용내장형밸런스점검장치에관한것이다. 본발명에따른풍동시험용내장형밸런스점검장치는, 풍동의내부에설치된비행체모형에장착되어상기비행체모형의공력계수를측정하는내장형밸런스를점검하기위해상기내장형밸런스에연결되는풍동시험용내장형밸런스점검장치에있어서, 정전압을공급하는전원부(21)와, 직류전압과저항을선택적으로측정하는멀티미터(22)와, 상기전원부(21), 상기멀티미터(22), 상기내장형밸런스(10)의각 단자와연결되고, 상기전원부(21)와상기멀티미터(22)와상기내장형밸런스(10)의단자와선택적으로접속되는매트릭스스위치모듈(23)과, 상기전원부(21)와상기멀티미터(22)의작동을제어하고상기전원부(21)와상기멀티미터(22)와상기내장형밸런스(10)의각 단자를선택적으로접속되도록상기매트릭스스위치모듈(23)의접속상태를제어하는계측부(31)를포함하는것을특징으로한다.
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公开(公告)号：KR101348724B1
公开(公告)日：2014-01-09
申请号：KR1020120039385
申请日：2012-04-16
Applicant: 국방과학연구소
Abstract: 본 발명은 풍동시험모형 내부에 배치되어 상기 풍동시험모형의 내부로 통과하는 유량을 조절하는 초음속영역의 풍동시험모형용 유량조절장치에 관한 발명이다. 서보모터를 이용하여 서로 상대 직선이동하는 제1 및 제2 바디를 포함하고, 모터제어부를 포함하여 상기 풍동시험장치의 풍동제어 시스템과 통신한다.
따라서, 초음속영역을 비행하는 실제 비행체 내부의 유량을 모사할 수 있으며, 통신에 의하여 상기 유량조절장치와 풍동시험모형의 자동화를 구현할 수 있어, 풍동시험자료의 신뢰성을 향상시킬 수 있다.-
公开(公告)号：KR101846118B1
公开(公告)日：2018-04-05
申请号：KR1020170014346
申请日：2017-02-01
Applicant: 국방과학연구소
CPC classification number: G01P3/36 , G01J1/44 , G01J2001/444 , G01P13/0073
Abstract: 본발명은광센서부와신호처리부를포함하는고속회전장치의회전속도및 진동편차를계측하는방법에있어서, 광신호가상기광센서부의반사판에서반사되는반사시간으로상기회전장치의회전속도를산출하는회전속도산출단계와상기반사시간의최대값과최소값, 패턴길이를이용하여상기진동편차를산출하는진동편차산출단계를포함하고상기회전속도산출단계와상기진동편차산출단계는단일광센서로진행되는것을특징으로하는 FPGA기반회전속도및 진동편차계측방법에관한것이다.
Abstract translation: 提供了一种测量包括光传感器单元和信号处理单元的高速旋转设备的旋转速度和振动偏差的方法，所述方法包括：测量旋转设备的旋转速度， 速度计算步骤，通过使用最大值和最小值，对反射时间图案长度，并且包括计算振动偏差步骤的振动偏差计算步骤计算的振动偏差和相位计算的旋转速度要与单个光传感器进行 本发明涉及基于FPGA的旋转速度和振动偏差测量方法。
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公开(公告)号：KR1020130116737A
公开(公告)日：2013-10-24
申请号：KR1020120039385
申请日：2012-04-16
Applicant: 국방과학연구소
Abstract: PURPOSE: A flow rate controlling device for a supersonic speed wind tunnel test and a wind tunnel testing device with the same are provided to enable the sliding movement of first and second bodies by driving a servo motor and to prevent damage caused by excessively driving the servo motor as the driving of the servo motor is controlled by a stopper. CONSTITUTION: A flow rate controlling device for a supersonic speed wind tunnel test includes first and second housing units, a servo motor (312), and a ball screw (304). The first and second housing units are received inside a wind tunnel testing model. The first and second housing units include spaces receiving fluid and relatively moved in one direction, thereby being joined to make the space enlarged or reduced. The servo motor is mounted on the first housing unit and controls the movement of the second housing unit. The ball screw is fixed inside the second housing unit. The ball screw is connected to the servo motor and makes the second housing reciprocate in one direction. [Reference numerals] (AA) Wind
Abstract translation: 目的：提供一种用于超音速风洞试验的流量控制装置和具有该超声速风洞试验用的风洞试验装置，以通过驱动伺服电动机来实现第一和第二主体的滑动运动，并且防止过度驱动伺服 驱动伺服电机的电机由止动器控制。 构成：用于超音速风洞试验的流量控制装置包括第一和第二壳体单元，伺服电动机（312）和滚珠丝杠（304）。 第一和第二壳体单元被接收在风洞测试模型内。 第一和第二壳体单元包括接收流体并在一个方向上相对移动的空间，从而被连接以使空间变大或减小。 伺服电动机安装在第一壳体单元上并控制第二壳体单元的运动。 滚珠丝杠固定在第二壳体单元内。 滚珠丝杠连接到伺服电机，使第二壳体沿一个方向往复运动。 （标号）（AA）风
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Patent Agency Ranking
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：KR101722394B1
公开(公告)日：2017-04-03
申请号：KR1020150126371
申请日：2015-09-07
Applicant: 국방과학연구소
Abstract: 본발명은매트릭스스위치모듈을이용하여일일이단자를접속/해제하는과정없이자동으로점검할수 있는풍동시험용내장형밸런스점검장치에관한것이다. 본발명에따른풍동시험용내장형밸런스점검장치는, 풍동의내부에설치된비행체모형에장착되어상기비행체모형의공력계수를측정하는내장형밸런스를점검하기위해상기내장형밸런스에연결되는풍동시험용내장형밸런스점검장치에있어서, 정전압을공급하는전원부(21)와, 직류전압과저항을선택적으로측정하는멀티미터(22)와, 상기전원부(21), 상기멀티미터(22), 상기내장형밸런스(10)의각 단자와연결되고, 상기전원부(21)와상기멀티미터(22)와상기내장형밸런스(10)의단자와선택적으로접속되는매트릭스스위치모듈(23)과, 상기전원부(21)와상기멀티미터(22)의작동을제어하고상기전원부(21)와상기멀티미터(22)와상기내장형밸런스(10)의각 단자를선택적으로접속되도록상기매트릭스스위치모듈(23)의접속상태를제어하는계측부(31)를포함하는것을특징으로한다.
Abstract translation: 本发明涉及一种自检查以风洞试验的集成的平衡检查装置，在不连接/手动释放所述终端使用矩阵开关模块的过程。 风洞试验的综合平衡了根据本发明检查装置，在安装在风洞风洞试验的内部的车辆模型耦合到所述集成平衡综合平衡，以检查内置的平衡用于测量车辆模型检查装置的空气动力系数 用于选择性地测量直流电压和电阻的万用表22以及用于向电源21，万用表22和万用表22提供恒定电压的电源21。 矩阵开关模块23连接到电源单元21和万用表22并选择性地连接到内置天平10的端子; 控制操作，并且包括用于控制动力源21和流量计22和集成平衡10 uigak终端到矩阵开关模块23的连接状态，以选择性地连接到一个测量单元31 和被表征。
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公开(公告)号：KR101572161B1
公开(公告)日：2015-11-26
申请号：KR1020140105947
申请日：2014-08-14
Applicant: 국방과학연구소
IPC: G01P3/486
CPC classification number: G01P3/486 , G01B11/272 , G01D5/305
Abstract: 본발명의엇각회전판을사용한회전계측시스템에는환형고리형상의테두리면으로빛을대부분정반사시키는정반사면(10-1)과빛을대부분엇각반사시키는엇각반사면(10-2)이교대로연속배열된엇각회전판(10), 정반사면(10-1)으로빛을발광하여정반사된빛을수광하는정반사면광센서(20), 엇각반사면(10-2)으로빛을발광하여엇각반사된빛을수광하는엇각반사면광센서(30)가포함됨으로써유도무기의꼬리날개회전특성파악을위한풍동실험시 해당회전특성들을오류없이정확히측정할수 있고, 특히정반사면(10-1)과엇각반사면(10-2)의각 면에상당한크기의스크래치(Scratch)가있더라도회전특성들을오류없이측정함으로써스크래치발생방지를위한과도한유지및 관리가요구되지않는특징이있다.
Abstract translation: 根据本发明，使用交替角旋转面板的旋转测量系统包括交替角度旋转面板（10），规则反射面（10-1）定期反射到环形边界表面，并且 相反地连续地布置反射大多数交替角的光的交替角度反射表面（10-2） 用于所述正反射表面的光学传感器（20），通过向所述正反射表面（10-1）发射光来接收规则的反射光; 和用于交替角度表面的光学传感器（30），通过向交替角度反射表面（10-2）发射光来接收反射光。 因此，当进行用于识别被引导武器的尾翼的旋转特性的风洞试验时，相应的旋转特性被准确地测量而没有错误。 特别是，即使在每个正反射面（10-1）和交替角度反射面（10-2）上都存在显着大的划痕，也不会产生旋转特性而没有错误，因此不需要 用于过度管理和维护以防止划伤。
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8.发明授权
公开(公告)号：KR101250258B1
公开(公告)日：2013-04-05
申请号：KR1020120027935
申请日：2012-03-19
Applicant: 국방과학연구소
CPC classification number: G01P3/495 , F16C32/0402 , G01M9/062 , G01P3/486 , G01P3/489
Abstract: PURPOSE: A wind tunnel testing apparatus including a rotation number measuring apparatus, a dual mode rotation number measuring method and a dual mode rotation number measuring apparatus is provided to measure the rotation number of a rotator which rotates more slowly than a first cycle speed, measure the distance between the rotator and the rotation number measuring apparatus in real time by a distance measuring sensor, and continuously record the dynamic balancing characteristic of the rotator, thereby improving the rotational stability of the rotator. CONSTITUTION: A rotation number measuring apparatus(500) includes first and second sensors(521,522) which are formed on the inner peripheral surface of a rotator(11), outputting signals by sensing rotation of the rotator and outputting first and second measurement data forming a 90 degree phase difference, a reflection bushing(510) forming a first and second patterns(511, 512) having different reflectivity on the inner peripheral surface, a holder(525) in which the first and second sensors are mounted by being separated from the reflection bushing, a sensing unit including a distance measuring sensor(526) for measuring the distance between the holder and the rotator, a circuit unit converting the first and second measurement data into digital signals and outputting the digital signals, and a processing unit calculating the rotational numbers of the rotator according to the digital signals. [Reference numerals] (AA) Circuit unit; (BB) Processing unit; (CC) Wind tunnel testing data storage system;
Abstract translation: 目的：提供一种包括转数测量装置，双模式转数测量方法和双模式转数测量装置的风洞测试装置，用于测量旋转速度比第一循环速度慢的旋转体的旋转数，测量 通过距离测量传感器实时地旋转旋转体与旋转数测量装置之间的距离，并连续地记录旋转体的动平衡特性，从而提高旋转体的旋转稳定性。 构成：旋转数测量装置（500）包括第一和第二传感器（521,522），其形成在旋转体（11）的内周面上，通过感测旋转体的旋转输出信号，并输出第一和第二测量数据，形成 形成90度相位差的反射衬套（510），形成在内周面上具有不同反射率的第一和第二图案（511,512）的反射套管（510），通过与第一和第二传感器 反射衬套，包括用于测量保持器和旋转体之间的距离的距离测量传感器（526）的感测单元，将第一和第二测量数据转换为数字信号并输出数字信号的电路单元，以及计算 根据数字信号的转子的转数。 （附图标记）（AA）电路单元; （BB）处理单元; （CC）风洞测试数据存储系统;
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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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