Vibration Reduction Design and Test of UAV Load Radar
It is challenging to design complex structures and calculate their dimensions only on the basis of theory. This issue was resolved efficiently by the FEM. Using the applicable test, the mechanical properties of the materials used in the damper are estimated, effectively guiding the design of the dev...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2022-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2022/4186303 |
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| _version_ | 1832567722898096128 |
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| author | Jia Fu Chaohui Fan Changshuai Yu Guangming Liu Haitao Luo |
| author_facet | Jia Fu Chaohui Fan Changshuai Yu Guangming Liu Haitao Luo |
| author_sort | Jia Fu |
| collection | DOAJ |
| description | It is challenging to design complex structures and calculate their dimensions only on the basis of theory. This issue was resolved efficiently by the FEM. Using the applicable test, the mechanical properties of the materials used in the damper are estimated, effectively guiding the design of the device and boosting its vibration-reducing performance. A large-load unmanned aerial vehicle (UAV) airborne radar is the subject of this research article. According to particular use case, vibration dampers for the radar-mounting platform are designed using passive vibration isolation technology to reduce aircraft vibration transmission to the radar. A conference paper has already presented prior research on the same topic. Earlier research confirmed the vibration-isolating efficacy of the T-type rubber isolator, which can greatly improve the operational conditions of the airborne radar. In contrast, earlier studies relied more on experimental validation and did not use numerical simulations. This research’s primary objective is the development of a T-type rubber isolator, whose vibration reduction performance is proven using FEM and experiments. Utilizing a suitable simulation analysis method to investigate the vibration reduction of an unmanned aerial vehicle’s (UAV) airborne component is a crucial technical task. By comparing multiple material models, a more precise model for characterizing rubber was developed. |
| format | Article |
| id | doaj-art-4cd464b890864cf5a3f45c8f21f44dec |
| institution | Kabale University |
| issn | 1687-5974 |
| language | English |
| publishDate | 2022-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-4cd464b890864cf5a3f45c8f21f44dec2025-02-03T01:00:44ZengWileyInternational Journal of Aerospace Engineering1687-59742022-01-01202210.1155/2022/4186303Vibration Reduction Design and Test of UAV Load RadarJia Fu0Chaohui Fan1Changshuai Yu2Guangming Liu3Haitao Luo4State Key Laboratory of RoboticsState Key Laboratory of RoboticsState Key Laboratory of RoboticsState Key Laboratory of RoboticsState Key Laboratory of RoboticsIt is challenging to design complex structures and calculate their dimensions only on the basis of theory. This issue was resolved efficiently by the FEM. Using the applicable test, the mechanical properties of the materials used in the damper are estimated, effectively guiding the design of the device and boosting its vibration-reducing performance. A large-load unmanned aerial vehicle (UAV) airborne radar is the subject of this research article. According to particular use case, vibration dampers for the radar-mounting platform are designed using passive vibration isolation technology to reduce aircraft vibration transmission to the radar. A conference paper has already presented prior research on the same topic. Earlier research confirmed the vibration-isolating efficacy of the T-type rubber isolator, which can greatly improve the operational conditions of the airborne radar. In contrast, earlier studies relied more on experimental validation and did not use numerical simulations. This research’s primary objective is the development of a T-type rubber isolator, whose vibration reduction performance is proven using FEM and experiments. Utilizing a suitable simulation analysis method to investigate the vibration reduction of an unmanned aerial vehicle’s (UAV) airborne component is a crucial technical task. By comparing multiple material models, a more precise model for characterizing rubber was developed.http://dx.doi.org/10.1155/2022/4186303 |
| spellingShingle | Jia Fu Chaohui Fan Changshuai Yu Guangming Liu Haitao Luo Vibration Reduction Design and Test of UAV Load Radar International Journal of Aerospace Engineering |
| title | Vibration Reduction Design and Test of UAV Load Radar |
| title_full | Vibration Reduction Design and Test of UAV Load Radar |
| title_fullStr | Vibration Reduction Design and Test of UAV Load Radar |
| title_full_unstemmed | Vibration Reduction Design and Test of UAV Load Radar |
| title_short | Vibration Reduction Design and Test of UAV Load Radar |
| title_sort | vibration reduction design and test of uav load radar |
| url | http://dx.doi.org/10.1155/2022/4186303 |
| work_keys_str_mv | AT jiafu vibrationreductiondesignandtestofuavloadradar AT chaohuifan vibrationreductiondesignandtestofuavloadradar AT changshuaiyu vibrationreductiondesignandtestofuavloadradar AT guangmingliu vibrationreductiondesignandtestofuavloadradar AT haitaoluo vibrationreductiondesignandtestofuavloadradar |