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航時(shí)可延展水稻輔助授粉無人飛機(jī)設(shè)計(jì)與作業(yè)參數(shù)優(yōu)選
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嶺南現(xiàn)代農(nóng)業(yè)實(shí)驗(yàn)室科研項(xiàng)目(NT2021009)和廣東省科技計(jì)劃項(xiàng)目(2023B10564002)


Design and Operational Parameter Optimization of Endurance-extended Drone for Supplementary Pollination in Hybrid Rice Breeding
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    摘要:

    無人飛機(jī)在雜交水稻制種輔助授粉領(lǐng)域得到廣泛應(yīng)用,但現(xiàn)有電動(dòng)農(nóng)用無人飛機(jī)續(xù)航時(shí)間短,換電頻次高,難以充分利用短暫的有效授粉時(shí)間窗口,影響授粉效率,。為解決無人飛機(jī)輔助授粉續(xù)航時(shí)間短的問題,同時(shí)優(yōu)選作業(yè)參數(shù)以提高輔助授粉作業(yè)效果,本文設(shè)計(jì)了一種采用多電池組分時(shí)并聯(lián)配電方案的航時(shí)可延展輔助授粉無人飛機(jī),最大續(xù)航時(shí)間達(dá)到50min,。采用基于LBM(Lattice Boltzmann method)的數(shù)值模擬方法對(duì)樣機(jī)旋翼產(chǎn)生的下洗風(fēng)場進(jìn)行了仿真,優(yōu)選出飛行速度4.5m/s和飛行高度2m(距離父本冠層)的作業(yè)參數(shù)。為驗(yàn)證樣機(jī)輔助授粉效果和優(yōu)選作業(yè)參數(shù)的有效性,設(shè)計(jì)了樣機(jī),、四旋翼,、六旋翼3種機(jī)型雜交水稻制種田間輔助授粉對(duì)比試驗(yàn),并通過采集單視野平均花粉粒數(shù)、結(jié)實(shí)率,、制種產(chǎn)量以及續(xù)航時(shí)間4個(gè)維度數(shù)據(jù)進(jìn)行離差標(biāo)準(zhǔn)化分析,。試驗(yàn)結(jié)果表明,樣機(jī)試驗(yàn)續(xù)航時(shí)間(42min)、輔助授粉作業(yè)效率(10.5hm2/架次),、單視野平均花粉粒數(shù)(6.98粒,農(nóng)藝上要求至少3粒)和制種產(chǎn)量(1996.5kg/hm2)以及綜合評(píng)分均優(yōu)于另外兩種對(duì)照機(jī)型,。研究結(jié)果可為提高雜交水稻制種無人飛機(jī)輔助授粉效率提供參考,。

    Abstract:

    In recent years, drones have been explored as a potential tool for pollination support in hybrid rice breeding. However, the limited flight endurance of existing electrical agricultural drones necessitates frequent battery replacements, hindering the efficient utilization of the limited effective pollination time window and reducing pollination efficiency. To address the limited endurance of drones in pollination tasks and optimize operational parameters to enhance pollination efficiency, a supplementary pollination drone was designed with extendable flight duration, utilizing a time-sharing parallel power distribution scheme with multiple battery packs, achieving a maximum flight endurance of 50 min. To improve the pollination effectiveness of the prototype, a numerical simulation of the downwash airflow generated by the rotors was conducted by using the Lattice Boltzmann method (LBM). The optimal flight parameters of the prototype were found to be a speed of 4.5 m / s and an altitude of 2 m above the male parental canopy. Field experiments were conducted to validate the prototype’s pollination effectiveness and the optimal flight parameters by comparing three drones: the prototype, a quadrotor, and a hexacopter. Data were collected in four dimensions: average pollen grain count per single field of view, fruiting rate, yield, and endurance time for standardized deviation analysis. Results showed that the flight endurance (42 min), the pollination efficiency (10.5 hm 2 per flight), the averaged pollen grain count (6.98 grains per view, meeting the agronomic requirement of at least 3 grains ), the yield ( 1 996.5 kg / hm 2 ) and the comprehensive score of designed drone were better than two comparison drones. The research result may serve as a reference for enhancing the efficiency of drone supplementary pollination in hybrid rice breeding.

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姜銳,林鍵沁,林宗輝,劉愛民,鄧孔洪,周志艷.航時(shí)可延展水稻輔助授粉無人飛機(jī)設(shè)計(jì)與作業(yè)參數(shù)優(yōu)選[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),2025,56(2):229-239. JIANG Rui, LIN Jianqin, LIN Zonghui, LIU Aimin, DENG Konghong, ZHOU Zhiyan. Design and Operational Parameter Optimization of Endurance-extended Drone for Supplementary Pollination in Hybrid Rice Breeding[J]. Transactions of the Chinese Society for Agricultural Machinery,2025,56(2):229-239.

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  • 收稿日期:2024-11-20
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  • 在線發(fā)布日期: 2025-02-10
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