沈阳航空航天大学学报2026，Vol.43Issue(3)：20-26,7.DOI:10.3969/j.issn.2095-1248.2026.03.003
某型四座电动飞机除雾系统设计与适航验证
Design and airworthiness verification of the defogging system for a certain type of four-seat electric aircraft
摘要
Abstract
To enable the cockpit defogging system of a certain type of four-seater electric aircraft to meet the airworthiness requirements.According to CCAR23.773(b),the initial design scheme of the cockpit defogging system was given.According to the idea of compliance verification of the provisions,method and steps of the ground test for defogging were designed.By carrying out the compliance verification of the defogging system,the initial scheme of the defogging system was improved based on the test results,and the test scheme of the defogging system was optimized.Finally,the verification results of meeting the airworthiness requirements were obtained,and the airworthiness verification work was completed.The cockpit defogging system and verification process studied can not only provide references for the subsequent design and airworthiness of other models,but also play a certain reference role for designers and airworthiness inspectors engaged in related work.关键词
四座电动飞机/除雾系统/驾驶舱/CCAR23.773(b)/适航验证Key words
four-seater electric aircraft/defogging system/cockpit/CCAR23.773(b)/airworthiness verification分类
航空航天引用本文复制引用
刘福佳,许炉军,徐海,李群芳,耿昊,包鸿飞..某型四座电动飞机除雾系统设计与适航验证[J].沈阳航空航天大学学报,2026,43(3):20-26,7.基金项目
国家科技重大专项(项目编号:MJG4-1N21、yf20180001). （项目编号:MJG4-1N21、yf20180001）
