{"title":"螺旋桨试验台传感器系统设计","authors":"N. Ihsan, Denny Dermawan, P. LazuardyRahendra","doi":"10.28989/vortex.v2i2.1006","DOIUrl":null,"url":null,"abstract":"The sensor system is a system that functions to detect signals that come from changes in energy such as electrical energy, physical energy, chemical energy, biological energy, mechanical energy, and so on. The propeller test bench is an propeller performance testing platform prior to propeller installation on an aircraft to ensure engine suitability. The purpose of this design is to test the performance capability of the engine with the right sensor system measurement tool so that it can generate the value of thrust, rpm speed, and the temperature of an engine which will be designed to be used in the learning process to support propulsion practicum activities. The method used in this research is an experimental method of sensor system design. The design of the sensor system consists of a tachometer as a rpm measurement sensor, a thermostat as a sensor to measure the temperature of the propeller spool and temperature of the engine fin, and also a load cell as a sensor to measure the thrust value.The sensor system test results were then validated using the measurement results by the sensor manufacturer. The test was carried out on a wood-type propeller measuring 22 x 8 chords 4,5 cm and 5 cm. Based on the test results, it is known that the chord wood type propeller is 4,5 cm, at the maximum rpm is 7021.7, the resulting thrust value is 6.75. In testing the 5cm chord wood type propeller shows the maximum speed of 6977.5 produces a thrust of 6.95. Validation was carried out on the measurement results of rpm and thrust, the average error factor obtained for 4,5 cm chord wood type propeller was 0.783%, while for 5 cm chord wood type propeller the average error factor obtained was 1.0582%. From the resulting average error, it can be concluded that the measuring instrument for this sensor system has good accuracy","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"12 1","pages":""},"PeriodicalIF":0.1000,"publicationDate":"2021-06-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"SENSOR SYSTEM DESIGN FOR PROPELLER TEST BENCH\",\"authors\":\"N. Ihsan, Denny Dermawan, P. LazuardyRahendra\",\"doi\":\"10.28989/vortex.v2i2.1006\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The sensor system is a system that functions to detect signals that come from changes in energy such as electrical energy, physical energy, chemical energy, biological energy, mechanical energy, and so on. The propeller test bench is an propeller performance testing platform prior to propeller installation on an aircraft to ensure engine suitability. The purpose of this design is to test the performance capability of the engine with the right sensor system measurement tool so that it can generate the value of thrust, rpm speed, and the temperature of an engine which will be designed to be used in the learning process to support propulsion practicum activities. The method used in this research is an experimental method of sensor system design. The design of the sensor system consists of a tachometer as a rpm measurement sensor, a thermostat as a sensor to measure the temperature of the propeller spool and temperature of the engine fin, and also a load cell as a sensor to measure the thrust value.The sensor system test results were then validated using the measurement results by the sensor manufacturer. The test was carried out on a wood-type propeller measuring 22 x 8 chords 4,5 cm and 5 cm. Based on the test results, it is known that the chord wood type propeller is 4,5 cm, at the maximum rpm is 7021.7, the resulting thrust value is 6.75. In testing the 5cm chord wood type propeller shows the maximum speed of 6977.5 produces a thrust of 6.95. Validation was carried out on the measurement results of rpm and thrust, the average error factor obtained for 4,5 cm chord wood type propeller was 0.783%, while for 5 cm chord wood type propeller the average error factor obtained was 1.0582%. 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引用次数: 0
摘要
传感器系统是对电能、物理能、化学能、生物能、机械能等能量变化所产生的信号进行检测的系统。螺旋桨试验台是螺旋桨安装在飞机上之前的一个性能测试平台,以确保发动机的适用性。本次设计的目的是使用合适的传感器系统测量工具来测试发动机的性能,从而产生发动机的推力、转速和温度的值,这些值将被设计用于学习过程中,以支持推进实践活动。本研究采用的方法是一种传感器系统设计的实验方法。传感器系统的设计由转速计作为转速测量传感器,温控器作为测量螺旋桨轴和发动机鳍温度的传感器,以及称重传感器作为测量推力值的传感器组成。然后使用传感器制造商的测量结果验证传感器系统测试结果。试验是在一个尺寸为22 x 8弦4、5厘米和5厘米的木制螺旋桨上进行的。根据试验结果可知,弦木型螺旋桨长4,5 cm,最大转速为7021.7,所得推力值为6.75。在测试中,5cm弦木型螺旋桨显示6977.5的最大速度产生6.95的推力。对转速和推力的测量结果进行了验证,4,5 cm弦型螺旋桨的平均误差系数为0.783%,而5 cm弦型螺旋桨的平均误差系数为1.0582%。从测量结果的平均误差可以看出,该传感器系统的测量仪器具有良好的精度
The sensor system is a system that functions to detect signals that come from changes in energy such as electrical energy, physical energy, chemical energy, biological energy, mechanical energy, and so on. The propeller test bench is an propeller performance testing platform prior to propeller installation on an aircraft to ensure engine suitability. The purpose of this design is to test the performance capability of the engine with the right sensor system measurement tool so that it can generate the value of thrust, rpm speed, and the temperature of an engine which will be designed to be used in the learning process to support propulsion practicum activities. The method used in this research is an experimental method of sensor system design. The design of the sensor system consists of a tachometer as a rpm measurement sensor, a thermostat as a sensor to measure the temperature of the propeller spool and temperature of the engine fin, and also a load cell as a sensor to measure the thrust value.The sensor system test results were then validated using the measurement results by the sensor manufacturer. The test was carried out on a wood-type propeller measuring 22 x 8 chords 4,5 cm and 5 cm. Based on the test results, it is known that the chord wood type propeller is 4,5 cm, at the maximum rpm is 7021.7, the resulting thrust value is 6.75. In testing the 5cm chord wood type propeller shows the maximum speed of 6977.5 produces a thrust of 6.95. Validation was carried out on the measurement results of rpm and thrust, the average error factor obtained for 4,5 cm chord wood type propeller was 0.783%, while for 5 cm chord wood type propeller the average error factor obtained was 1.0582%. From the resulting average error, it can be concluded that the measuring instrument for this sensor system has good accuracy