ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT)
In order to solve the problems of dynamic response and structural vibration suppression of aircraft bevel gear thin-walled spoke plate, an optimal design scheme of damping pass structure was proposed. Taking a certain type of aeronautical spiral bevel gear as an example, the model of spiral bevel ge...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2022-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2022.06.031 |
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| author | SONG CongCong LI JiaQi WEI BingYang DAI Hua SHE DingJun |
| author_facet | SONG CongCong LI JiaQi WEI BingYang DAI Hua SHE DingJun |
| author_sort | SONG CongCong |
| collection | DOAJ |
| description | In order to solve the problems of dynamic response and structural vibration suppression of aircraft bevel gear thin-walled spoke plate, an optimal design scheme of damping pass structure was proposed. Taking a certain type of aeronautical spiral bevel gear as an example, the model of spiral bevel gear was established. The natural characteristics of the gear were calculated by Lanczos method, and the frequency margin between the first six natural frequencies and the excitation force was analyzed. The dynamic response characteristics of radial plates with different holes and their suppression effect on vibration transmission were studied by means of modal superposition method. The parameters of radial plate pass structure are optimized by orthogonal experiment design and simulation analysis. The results show that under the condition of the same area and the same number, the vibration responses of triangle, round, pillow and waist shapes decrease in turn. The optimized waist pass can effectively suppress vibration transmission and improve the smoothness of bevel gear transmission. |
| format | Article |
| id | doaj-art-6abe4acba31040aea9a442d6bb6514ab |
| institution | Kabale University |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2022-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-6abe4acba31040aea9a442d6bb6514ab2025-01-15T02:39:50ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692022-01-011498150336350472ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT)SONG CongCongLI JiaQiWEI BingYangDAI HuaSHE DingJunIn order to solve the problems of dynamic response and structural vibration suppression of aircraft bevel gear thin-walled spoke plate, an optimal design scheme of damping pass structure was proposed. Taking a certain type of aeronautical spiral bevel gear as an example, the model of spiral bevel gear was established. The natural characteristics of the gear were calculated by Lanczos method, and the frequency margin between the first six natural frequencies and the excitation force was analyzed. The dynamic response characteristics of radial plates with different holes and their suppression effect on vibration transmission were studied by means of modal superposition method. The parameters of radial plate pass structure are optimized by orthogonal experiment design and simulation analysis. The results show that under the condition of the same area and the same number, the vibration responses of triangle, round, pillow and waist shapes decrease in turn. The optimized waist pass can effectively suppress vibration transmission and improve the smoothness of bevel gear transmission.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2022.06.031Spiral bevel gearModal analysisOrthogonal testDynamic response |
| spellingShingle | SONG CongCong LI JiaQi WEI BingYang DAI Hua SHE DingJun ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT) Jixie qiangdu Spiral bevel gear Modal analysis Orthogonal test Dynamic response |
| title | ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT) |
| title_full | ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT) |
| title_fullStr | ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT) |
| title_full_unstemmed | ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT) |
| title_short | ANALYSIS OF DYNAMIC RESPONSE CHARACTERISTICS OF AERONAUTICAL SPIRAL BEVEL GEARS AND OPTINIZATION OF VIBRATION ABSORBING STRUCTURE OF SPOKE PLATE HOLE (MT) |
| title_sort | analysis of dynamic response characteristics of aeronautical spiral bevel gears and optinization of vibration absorbing structure of spoke plate hole mt |
| topic | Spiral bevel gear Modal analysis Orthogonal test Dynamic response |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2022.06.031 |
| work_keys_str_mv | AT songcongcong analysisofdynamicresponsecharacteristicsofaeronauticalspiralbevelgearsandoptinizationofvibrationabsorbingstructureofspokeplateholemt AT lijiaqi analysisofdynamicresponsecharacteristicsofaeronauticalspiralbevelgearsandoptinizationofvibrationabsorbingstructureofspokeplateholemt AT weibingyang analysisofdynamicresponsecharacteristicsofaeronauticalspiralbevelgearsandoptinizationofvibrationabsorbingstructureofspokeplateholemt AT daihua analysisofdynamicresponsecharacteristicsofaeronauticalspiralbevelgearsandoptinizationofvibrationabsorbingstructureofspokeplateholemt AT shedingjun analysisofdynamicresponsecharacteristicsofaeronauticalspiralbevelgearsandoptinizationofvibrationabsorbingstructureofspokeplateholemt |