KS W 4020-2007(2012)-装备的飞机推进系统-国家数字标准馆

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항공기용 추진 계통 장착 装备的飞机推进系统

发布日期： 2007-11-22

废止日期： 2013-12-12

该规格规定了飞机推进装备系统（发动机装备）机身部分的性能、设计及试验，也规定了下列推进装备部分系统及适用于特殊领域的技术要求。发动机启动（3.4.1）推进系统控制装置（3.4.2）防火（3.4.3）拖板（3.4.4）冷却和通风（3.4.5）发动机排气系统（3.4.6）进气系统（3.4.7）配管和配线设备（3.4.8）发动机（快速可更换发动机组装）（3.4.9）接近性（3.4.10）脆弱性（3.4.11）非高规格中{}加上表示的单位及数值历来是根据单位的，是参考值。注:该规格的内容相当于MIL-I-83294（安装要求、Aircraft Propulsion Systems、General Specification for）。

이 규격은 항공기의 추진 장비 계통(엔진 장비)의 기체 부분의 성능, 설계 및 시험에 대하여 규정하 고, 다음의 추진 장비 부분 계통 및 특수 분야에 적용하는 기술 요구사항에 대하여도 규정한다. 엔진의 시동(3.4.1) 추진 계통 제어 장치(3.4.2) 방화(3.4.3) 드레인(3.4.4) 냉각 및 환기(3.4.5) 엔진 배기 계통(3.4.6) 흡기 계통(3.4.7) 배관 및 배선 장비(3.4.8) 의장 엔진(급속 교환 가능 엔진 조립)(3.4.9) 접근성(3.4.10) 취약성(3.4.11) 비고 이 규격 중 { }를 붙여 표시한 단위 및 수치는 종래 단위에 따른 것으로서 참고값이다. 참고 이 규격의 내용은, MIL－I－83294(Installation Requirements, Aircraft Propulsion Systems, General Specification for)에 해당한다.

分类信息

发布单位或类别：韩国-韩国标准

ICS分类： 49.050航空器和航天器工程 - 航空航天发动机和推进系统

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