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首页> 外文会议>International Seminar on Aerospace Science and Technology >Study on GL-1 Sailplane Internal Configuration and Control Mechanism Requirements using EASA CS-22
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Study on GL-1 Sailplane Internal Configuration and Control Mechanism Requirements using EASA CS-22

机译：使用EASA CS-22研究GL-1 Sailplane内部配置和控制机制要求

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GL-1 is single-seat mid-performance sailplane, designed to be Indonesian National Glider. GL-1 have been developed since 2014. The development produced a half scale prototype called BL-1, which had accomplished static test in 2016, then followed by first flight test in 2017. Full scale prototype is currently being fabricated, with flight test and type certification scheduled for 2020. Currently, there are no specific airworthiness design regulation for sailplane in Indonesia. Study of several regulation in America and Europe suggest that Certification Specification (CS)-22 from European Aviation Safety Agency (EASA) is the most suitable airworthiness regulation and specification for sailplane design. EASA CS-22 is divided into 9 subparts, with total of 260 Certification Specifications (CS) and 49 Applicable Means of Compliance (AMC). According to the study, only 162 CS and 45 AMC is applicable for GL-1 design. Furthermore, only 59 CS and 17 AMC is applicable and relevant for internal configuration and control mechanism. Those regulations are mapped and derived into 79 requirements for internal configuration and control mechanism. The result of this study will be used as design basis for GL-1 internal configuration and control mechanism.
机译：GL-1是单座中间性能帆船，旨在成为印尼国家滑翔机。自2014年以来已经开发了GL-1。该开发产生了一个半规模的原型，称为BL-1，在2016年完成了静态测试，然后在2017年进行首次飞行试验。目前正在制造出全规模的原型，使用飞行试验和飞行试验定于2020年的类型认证。目前，印度尼西亚的Sailplane没有具体的适航设计规范。在美国和欧洲的若干法规研究表明，欧洲航空安全局（EASA）的认证规范（CS）-22是Sailplane设计中最适合的适航规范和规范。 EASA CS-22分为9个子Part，总共260个认证规范（CS）和49个适用的合规手段（AMC）。根据该研究，仅适用于GL-1设计的162 CS和45 AMC。此外，仅适用于59 CS和17AMC，与内部配置和控制机制相关。这些法规映射并衍生成79个内部配置和控制机制要求。本研究的结果将用作GL-1内部配置和控制机制的设计基础。

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