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Engine life-limited parts are rotor and major static structural parts whose primary failure is likely to result in a hazardous engine effect. Typically, engine life-limited parts include, but are not limited to, disks, spacers, hubs, shafts, high-pressure casings, and non-redundant mount components. The safety goals for the airworthiness requirement of aircraft engine life-limited parts in European and American are analyzed. The airworthiness compliance requirement for the life evaluation of engine life-limited parts in AC33.70-1 and AMC515 are analyzed and interpreted. The key process and method of aircraft engine life-limited part airworthiness conformity test are given. The model of safe life prediction for life-limited parts is founded. 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科技导报
| 研究论文 2013, 31(13): 49-53
民用航空发动机限寿件适航符合性方法
全屏
王大伟, 王伟, 冯振宇
作者信息
中国民航大学天津市民用航空器适航与维修重点实验室,天津 300300
Airworthiness Compliance of Life-limited Part of Civil Aircraft Engine
Affiliations
出版时间: 2013-05-08
doi: 10.3981/j.issn.1000-7857.2013.13.007
文章导航
针对中国民用大涵道比涡扇发动机型号取证的需要,开展发动机限寿件适航符合性方法研究.分析欧美航空发动机限寿件适航要求的安全目标,对AC33.70-1和AMC515发动机限寿件定寿方面的适航符合性要求进行读解分析.以典型航空发动机为例,研究了限寿件的判定方法,分析发动机限寿件适航审定过程中的关键环节,从发动机载荷谱制定、材料性能数据、安全寿命制定3个方面给出航空发动机限寿件适航符合性验证的关键流程和方法.参考国外设计标准给出限寿件应力分析和试验方案设计流程,给出限寿件寿命散度系数的获取方法.本研究为编制航空发动机限寿件的适航指南提供参考依据.
航空发动机
/
限寿件
/
安全寿命
/
适航符合性
The airworthiness compliance method of civil aircraft engine life-limited parts is investigated, according to the needs of type forensics for civil high bypass ratio turbofan engine in China. Engine life-limited parts are rotor and major static structural parts whose primary failure is likely to result in a hazardous engine effect. Typically, engine life-limited parts include, but are not limited to, disks, spacers, hubs, shafts, high-pressure casings, and non-redundant mount components. The safety goals for the airworthiness requirement of aircraft engine life-limited parts in European and American are analyzed. The airworthiness compliance requirement for the life evaluation of engine life-limited parts in AC33.70-1 and AMC515 are analyzed and interpreted. The key process and method of aircraft engine life-limited part airworthiness conformity test are given. The model of safe life prediction for life-limited parts is founded. The proposed method provides an important reference for making airworthiness guide for aircraft engine life-limited parts.
aircraft engine
/
life-limited part
/
safe life
/
airworthiness compliance
王大伟;王伟;冯振宇.
民用航空发动机限寿件适航符合性方法.
科技导报,
2013
, 31
(13)
: 49
-53
.
DOI: 10.3981/j.issn.1000-7857.2013.13.007
WANG Dawei;WANG Wei;FENG Zhenyu.
Airworthiness Compliance of Life-limited Part of Civil Aircraft Engine[J].
Science & Technology Review ,
2013
, 31
(13)
: 49
-53
.
DOI: 10.3981/j.issn.1000-7857.2013.13.007
2013年第31卷第13期
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文章信息
doi: 10.3981/j.issn.1000-7857.2013.13.007
接收时间:2012-12-04
首发时间:2013-05-08
出版时间:2013-05-08
收稿日期:2012-12-04
修回日期:2013-02-25
https://castjournals.cast.org.cn/joweb/kjdb/CN/10.3981/j.issn.1000-7857.2013.13.007
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2种不同金属材料的力学参数
科 Family 属数 Number of genus 种数 Number of species 占总种数比例 Percentage of total species (%) 属 Genus 种数 Number of species 占总种数比例 Percentage of total species (%) 鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78 小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39 多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39 红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87 小菇属 Mycena 11 5.26 光柄菇属 Pluteus 5 2.39 红菇属 Russula 17 8.13 栓菌属 Trametes 5 2.39
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