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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
WANG Dawei, WANG Wei, FENG Zhenyu
Affiliations
Tianjin Key Lab oratory for Airworthiness and Maintenance of Civil Aircraft, Civil Aviation University of China, Tianjin 300300, China
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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