| 论飞机强度规范的发展 |
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| 引用本文： | 蒋祖国,王记,屈见忠,王根元,张永河. 论飞机强度规范的发展[J]. 航空学报, 1994, 1(1): 1-7 |
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| 作者姓名： | 蒋祖国 王记 屈见忠 王根元 张永河 |
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| 作者单位： | 西安市73分箱,西安,710089 |
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| 摘 要： | 简要叙述了美国军用飞机强度规范的历史演变；美国空军ＭＩＬＡ－８７２２１飞机结构通用规范的专业性质及ＭＩＬ－Ａ－８７２２１与ＭＩＬ－Ａ－００８８６０飞机强度和刚度规范的关系。通过对美国规范的理解和我国飞机研制及强度规范现状的分析,论证了我国新规范应是ＧＪＢ６７．１～１３－８５军用飞机强度和刚度规范的进一步发展,新规范发布实施后,ＧＪＢ６７．１～１３－８５将被取代。还叙述了我国新规范的适用范围和编制的技术途径。
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| 关 键 词： | 飞机设计 结构设计规范 飞机结构 |
| 收稿时间： | 1992-12-24; |
| 修稿时间： | 1993-09-05 |
ON THE DEVELOPMENT OF AIRCRAFT STRENGTH SPECIFICATION |
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| Jiang Zuguo, Wang Ji,QuJianzhong, WangGenyuan, ZhangYonghe. ON THE DEVELOPMENT OF AIRCRAFT STRENGTH SPECIFICATION[J]. Acta Aeronautica et Astronautica Sinica, 1994, 1(1): 1-7 |
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| Authors: | Jiang Zuguo Wang Ji QuJianzhong WangGenyuan ZhangYonghe |
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| Affiliation: | Box 73 of xi'an,Xi'an,710089 |
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| Abstract: | In this paper the historical evolution of american military aircraft strength specifica- tion,the speciality charactestics of the Aircraft Structure General Specification MIL-A-87221 of USAF and the relationship between MIL-A-87221 and MIL-A-8860 Serial Specifications of Aircraft Strength and Rigidity Specifications are Stated.By understanding american specifica- tions and analyzing the recent status of our aircraft development and strength specification,it is demonstrated that our future specification should be the further development of Military Aircraft Strength and Rigidity Specification GJB67.1～13-85 which should be substituted after the issue and application of the new specification. Finally,its adaptation scope and technical way of com- pilation are mentioned. |
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| Keywords: | aircraft design structural design criteria aircraft structure |
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