| 航空发动机起动过程的微机控制研究 |
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| 引用本文： | 樊丁,吴琪华.航空发动机起动过程的微机控制研究[J].航空学报,1990,11(2):93-97. |
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| 作者姓名： | 樊丁 吴琪华 |
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| 作者单位： | 西北工业大学
(樊丁)，西北工业大学(吴琪华) |
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| 摘 要： | <正> 1.概述 通常对航空发起动过程的要求是:起动迅速,不发生熄火、超温、喘振等现象。在航空发动机使用液压机械式控制器时,为了保证起动过程的顺利完成,一般都设置了自动起动器,但由于不同地区和不同大气条件对起动过程的影响,这种自动起动器常因不能对起动供油量及的进行自动修正,而导致发动机起动失败。
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| 关 键 词： | 航空发动机 起动 微机 |
STUDY ON PROCESS CONTROL OF AEROENGINE USING MICROCOMPUTER |
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| Northweastern Polytechnical University Fan Ding and Wu Chihua.STUDY ON PROCESS CONTROL OF AEROENGINE USING MICROCOMPUTER[J].Acta Aeronautica et Astronautica Sinica,1990,11(2):93-97. |
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| Authors: | Northweastern Polytechnical University Fan Ding and Wu Chihua |
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| Institution: | Northweastern Polytechnical University Fan Ding and Wu Chihua |
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| Abstract: | In this paper the start process of the aeroengine controlled by the microcomputer was studied.The start fuel supply was controlled according to the relation between corrective start fuel supply and corrective speed for automatic regulation of the start fuel supply under different climatic conditions. In order to guarantee the safety and reliablity of the aeroengine, several parameters of the engine were monitored. The hybird simulation test for the whole start process was carried out and satifactory results were obtained. |
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| Keywords: | aeroengine start microcomputer |
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