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1. 发明公开

KR20120068183A Apparatus for assembling and disassembling wind tunnel balance and wind tunnel testing system 有权
标题翻译：装配和拆除风洞平衡和风洞隧道测试系统的装置
公开(公告)号：KR20120068183A
公开(公告)日：2012-06-27
申请号：KR20100129684
申请日：2010-12-17
申请人： KOREA AEROSPACE RES INST
发明人： CHO TAE HWAN
IPC分类号： G01M9/04 , G01G19/07 , G01M9/02
摘要： PURPOSE: A wind tunnel balance assembling/disassembling device and a wind tunnel testing system are provided to securely assemble a wind tunnel balance and fixing supporter in pressing method and to easily disassemble the wind tunnel balance and fixing supporter using a wind tunnel balance disassembling unit. CONSTITUTION: A wind tunnel balance assembling/disassembling device comprises a wind tunnel balance assembling member and wind tunnel balance disassembling unit. The wind tunnel balance assembling member is comprised in a fixing supporter(130) and comprises an assembling hole. A taper unit formed in the wind tunnel balance is inserted and assembled to the assembling hole. The wind tunnel balance disassembling unit is inserted into a disassembling direction of the wind tunnel balance in the opposite side of the assembling hole where the taper unit is not assembled, thereby pushing the wind tunnel balance to the outside of the assembling hole when disassembling the wind tunnel balance.
摘要翻译：目的：提供风道平衡组装/拆卸装置和风洞试验系统，以便按照压力方式安全组装风洞平衡和固定支撑件，并使用风洞平衡拆卸装置轻松拆卸风洞平衡和固定支架。构成：风道平衡组装/拆卸装置包括风洞平衡组装构件和风洞平衡拆卸单元。风洞平衡组装构件包括在固定支撑件（130）中并且包括组装孔。形成在风洞平衡中的锥形单元插入并组装到组装孔。将风道平衡拆卸单元插入在未组装锥形单元的组装孔的相对侧的风洞平衡的拆卸方向上，从而在拆卸风时将风洞平衡推向组装孔的外侧隧道平衡。

2. 发明公开

KR1020080046719A 통합형 항공기 저울 및 수평 조절 장치와 그 사용 방법 无效
标题翻译：集成飞机规模和水平设备及其使用方法
公开(公告)号：KR1020080046719A
公开(公告)日：2008-05-27
申请号：KR1020087008804
申请日：2006-10-05
申请人： 벨 헬리콥터 텍스트론 인크.
发明人： 해밀턴에드워드씨 , 그린마이클에이
IPC分类号： G01G19/07 , G01G19/00
CPC分类号： G01G19/07 , G01M1/125
摘要： A combination apparatus for weighing an aircraft has a plurality of weight scales, each scale being adapted to be supported by a support surface in a position for receiving landing gear of an aircraft thereon. At least one riser supports at least one scale above the support surface, and the height of each riser is selected to position an aircraft on the scales in a level attitude while a weight of the aircraft is being supported by the landing gear on the scales. At least one scale may be recessed in the support surface, and the height of each riser may be adjustable.
摘要翻译：用于称重飞行器的组合装置具有多个称重秤，每个刻度尺适于由用于接收飞行器的起落架的位置的支撑表面支撑。至少一个提升管支撑在支撑表面上方的至少一个刻度，并且选择每个提升管的高度以使飞机在水平姿态下定位在秤上，同时飞行器的重量由秤上的起落架支撑。至少一个刻度可以凹入支撑表面，并且每个提升管的高度可以是可调节的。

3. 发明公开

KR1020030079335A 레벨러 有权
标题翻译： LEVELER
公开(公告)号：KR1020030079335A
公开(公告)日：2003-10-10
申请号：KR1020020018297
申请日：2002-04-03
申请人： 한국항공우주산업 주식회사
发明人： 신동학
IPC分类号： G01G19/07
摘要： PURPOSE: A leveler is provided to measure the weight and the center of gravity accurately, and to reduce measuring process by preventing measuring errors from side load with adjusting the load cell to the vertical shaft of an aircraft and correcting the weight by measuring the inclination angle. CONSTITUTION: A leveler is composed of an upper plate(420) supporting a load cell in the lower part of the load cell measuring the weight of an aircraft; a lower plate(410) placed in the lower part of the upper plate and supported by a shaft of a hydraulic cylinder; plural through holes vertically penetrating the upper plate and the lower plate; and plural assembling units connecting the upper plate and the lower plate with penetrating the through holes, and adjusting the inclination angle between the upper plate and the lower plate according to the combination degree.
摘要翻译：目的：提供一个调平器，用于精确测量重量和重心，并通过将负载传感器调整到飞机的垂直轴并通过测量倾斜角来校正重量来防止侧向载荷的测量误差来减少测量过程。构成：矫直机由支撑负载传感器下部测量飞机重量的测力传感器的上板（420）组成; 下板（410），放置在上板的下部并由液压缸的轴支撑; 垂直贯穿上板和下板的多个通孔; 以及多个组装单元，其连接上板和下板，穿透通孔，并根据组合度来调节上板和下板之间的倾斜角度。

4. 发明授权

KR100283316B1 항공기 중량 예측장치 有权
标题翻译：飞机重量预测装置
公开(公告)号：KR100283316B1
公开(公告)日：2001-03-02
申请号：KR1019980054876
申请日：1998-12-14
申请人： 한국항공우주산업 주식회사
发明人： 이윤호
IPC分类号： G01G19/07
摘要： 본 발명은 전투기 또는 훈련기급의 항공기의 기본 설계 단계에서 세부 중량을 예측하여 데이터베이스화하는 항공기 중량 예측 장치로서, 항공기의 중량을 예측하는 과정에서 중량 예측식의 매개변수로서 사용되는 설계변수의 값을 사용자 또는 소정의 기억장소로부터 입력받는 데이터 입력부; 예측하려는 상기 항공기의 설계형상명과 작성하려는 상기 데이터베이스의 파일명을 구비한 헤더부; 항공기의 각 세부 항목별 예측중량을 산출하는 중량 예측부; 중량 예측부에서 산출된 세부 항목별 예측중량 데이터로 데이터베이스를 설정하고, 보고서 출력을 위해 소정의 서식을 작성하여 주는 데이터베이스 작성부; 및 소정의 저장매체에 저장된 예측중량 데이터 베이스를 포함함을 특징으로 한다.
본 발명에 의하면, 항공기 중량 예측 과정에서 보다 정확한 중량 예측 결과를 얻을 수 있으므로 항공기의 기본 설계에 필요한 시간을 감축시킬 수 있으며, 보다 정밀한 중량 분포를 가진 항공기를 설계할 수 있다.

5. 发明授权

KR102394047B1 항공기의 에어포일용 중량 측정장치 有权
公开(公告)号：KR102394047B1
公开(公告)日：2022-05-06
申请号：KR1020200145894
申请日：2020-11-04
IPC分类号： G01G19/07 , G01G17/00 , G01G21/16
摘要： 본발명에따른항공기의에어포일용중량측정장치는베이스, 베이스의길이방향을따라양측에배치되어항공기의에어포일(airfoil)의양측리딩에지(leading edge)를지지하는지지부, 한쌍의지지부의하부에각각배치되어지지부에지지된에어포일의중량을감지하는하중감지부및 하중감지부로부터감지된에어포일의중량을디스플레이하는디스플레이부를포함하는것을특징으로한다.

6. 发明授权

KR100415010B1 레벨러 有权
公开(公告)号：KR100415010B1
公开(公告)日：2004-01-13
申请号：KR1020020018297
申请日：2002-04-03
申请人： 한국항공우주산업 주식회사
发明人： 신동학
IPC分类号： G01G19/07
摘要： PURPOSE: A leveler is provided to measure the weight and the center of gravity accurately, and to reduce measuring process by preventing measuring errors from side load with adjusting the load cell to the vertical shaft of an aircraft and correcting the weight by measuring the inclination angle. CONSTITUTION: A leveler is composed of an upper plate(420) supporting a load cell in the lower part of the load cell measuring the weight of an aircraft; a lower plate(410) placed in the lower part of the upper plate and supported by a shaft of a hydraulic cylinder; plural through holes vertically penetrating the upper plate and the lower plate; and plural assembling units connecting the upper plate and the lower plate with penetrating the through holes, and adjusting the inclination angle between the upper plate and the lower plate according to the combination degree.
摘要翻译：目的：提供一台矫直机来精确测量重量和重心，并通过防止侧向载荷的测量误差来减少测量过程，同时将称重传感器调整到飞机的垂直轴上，并通过测量倾斜角来校正重量。构成：整平器由测量飞机重量的称重传感器下部支撑称重传感器的上板（420）组成; 放置在上板的下部并由液压缸的轴支撑的下板（410）垂直穿过上板和下板的多个通孔; 以及多个组装单元，所述多个组装单元穿过所述通孔连接所述上板和所述下板，并且根据所述组合程度调节所述上板和所述下板之间的倾斜角度。

7. 发明公开

KR1020000039523A 항공기 중량 예측장치 有权
标题翻译：预测飞机重量的系统
公开(公告)号：KR1020000039523A
公开(公告)日：2000-07-05
申请号：KR1019980054876
申请日：1998-12-14
申请人： 한국항공우주산업 주식회사
发明人： 이윤호
IPC分类号： G01G19/07
摘要： PURPOSE: A system for preestimating a weight of an airplane is provided to design the airplane having a precise weight distribution by accurately preestimating the weight of the airplane. CONSTITUTION: A system for preestimating a weight of an airplane includes a data input part(100) for receiving a design parameter from a user or a memory element and a header(110) having a file name of the database and a design specification of the airplane. A weight preestimating part(120) has a weight preestimating equation for each part of the airplane to calculate the preestimated weight of the parts using the design parameter input from the data input part. A database generator generates a database on the calculated preestimated weight.
摘要翻译：目的：提供一种用于预先估计飞机重量的系统，通过精确预先确定飞机的重量来设计具有精确重量分布的飞机。构成：用于预先估计飞机重量的系统包括用于从用户或存储元件接收设计参数的数据输入部分（100）和具有数据库的文件名的标题（110）和飞机。重量预先估计部件（120）具有用于飞机的每个部分的重量预定公式，以使用从数据输入部分输入的设计参数来计算部件的预先估计的重量。数据库生成器根据计算的预估权重生成数据库。

8. 发明授权

KR101299343B1 실시간 항공기 화물 중량 측정시스템 有权
标题翻译：飞机和货物重量系统
公开(公告)号：KR101299343B1
公开(公告)日：2013-08-26
申请号：KR1020120020297
申请日：2012-02-28
申请人： 주식회사 에스아이엠티 , 김홍균 , 김기태
发明人： 김홍균 , 김기태
IPC分类号： G01G19/07 , G01G23/18 , B64D45/00
CPC分类号： G01G19/07 , G01G3/13 , G01G23/3742 , G06K9/183
摘要： PURPOSE: A real-time aircraft cargo weight measurement system is provided to lighten a weight measurement pad, to significantly reduce the number of require weight measurement pad, and to more conveniently calculate the cargo weight and the total aircraft weight by using a smart terminal. CONSTITUTION: A real-time aircraft cargo weight measurement system includes a weight measurement pad (100), a smart terminal (200), and a smart server. The weight measurement pad is installed on the route of the wheel of aircraft required to measure load. The weight measurement pad converts the weight that is applied by the wheel of aircraft passing over the weight measurement pad into a weight signal and outputs the signal. The smart terminal directly transfers the result of aircraft weight measurement to an aircraft airline, an airport, and an executing organization. The smart server systematically manages the measurement data that is generated, hour by hour, in various places in which the weight measurement pad is installed. [Reference numerals] (110) Weight sensor unit; (120) Signal conversion unit; (121) Amplification unit; (122) Filter unit; (123) A/D conversion unit; (130) First communication unit; (140) First control unit; (150) Power source unit; (201) Second communication unit; (202) Third communication unit; (203) Measurement requiring unit; (204) Memory unit; (205) Input unit; (206) Position measuring unit; (207) Camera unit; (208) Total weight calculation unit; (209) Freight weight calculation unit; (210) Measured data calculation unit; (211) Bar code generation unit; (212) Display unit; (220) Second control unit; (221) Measured data transmission unit
摘要翻译：目的：提供实时飞机货物重量测量系统，以减轻重量测量垫，显着减少需要重量测量垫的数量，并通过使用智能终端更方便地计算货物重量和总飞机重量。规定：实时飞机货物重量测量系统包括重量测量垫（100），智能终端（200）和智能服务器。重量测量垫安装在测量负载所需的飞机车轮的路线上。重量测量垫将通过重量测量垫的飞机的车轮施加的重量转换成重量信号并输出该信号。智能终端将飞机重量测量的结果直接传输到飞机航空公司，机场和执行机构。智能服务器在安装了重量测量垫的各个地方系统地管理每小时产生的测量数据。（附图标记）（110）重量传感器单元; （120）信号转换单元; （121）放大单元; （122）过滤单元; （123）A / D转换单元; （130）第一通信单元; （140）第一控制单元; （150）电源单元; （201）第二通信单元; （202）第三通信单元; （203）测量要求单位; （204）存储单元; （205）输入单元; （206）位置测量单元; （207）相机单元; （208）总重量计算单位; （209）货运重量计算单位; （210）测量数据计算单元; （211）条形码生成单元; （212）显示单元; （220）第二控制单元; （221）测量数据传输单元

9. 发明授权

KR101169173B1 Apparatus for assembling and disassembling wind tunnel balance and wind tunnel testing system 有权
标题翻译：装配和拆除风洞平衡和风洞隧道测试系统的装置
公开(公告)号：KR101169173B1
公开(公告)日：2012-07-30
申请号：KR20100129684
申请日：2010-12-17
IPC分类号： G01M9/04 , G01G19/07 , G01M9/02
摘要： 본 발명의 일실시예는 풍동 저울 장탈착 기구 및 풍동 시험 시스템에 관한 것으로써, 풍동 저울을 고정지지대에 견고하게 결합할 수 있고, 풍동 저울을 고정지지대로부터 간편하게 분해할 수 있다.

10. 发明公开

KR1020090100882A 항공기의 무게 및 무게중심 측정 장치 有权
标题翻译：飞机重量测量装置重量和重心
公开(公告)号：KR1020090100882A
公开(公告)日：2009-09-24
申请号：KR1020080026387
申请日：2008-03-21
申请人： 한국항공우주연구원
发明人： 장성호 , 이정진 , 김종건 , 최희주
IPC分类号： G01G19/07 , G01G19/00
CPC分类号： G01G19/07 , G01G3/12 , G01G21/28 , G01G23/02 , G01M1/125
摘要： PURPOSE: An apparatus for measuring the weight and center of gravity of an aircraft is provided to prevent a landing device or wheel from being separated from the measuring apparatus. CONSTITUTION: An apparatus for measuring the weight and center of gravity of an aircraft(10) comprises a measurement unit(100), a control unit(200) and a calculating unit(300). The measurement unit measures the weight of the aircraft by being arranged at lower parts of each wheel of the aircraft. The control unit adjusts the interval between measurement units. The calculating unit produces the center of gravity by collecting weight information.
摘要翻译：目的：提供一种用于测量飞机重量和重心的装置，以防止着陆装置或车轮与测量装置分离。构成：用于测量飞行器（10）的重量和重心的装置包括测量单元（100），控制单元（200）和计算单元（300）。测量单元通过布置在飞行器的每个车轮的下部来测量飞行器的重量。控制单元调整测量单位之间的间隔。计算单元通过收集重量信息产生重心。

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