| 马界祥,段琼,王丑丑.使用环境对舰载飞机重量的影响研究[J].装备环境工程,2017,14(7):56-60. MA Jie-xiang,DUAN Qiong,WANG Chou-chou.Influences of Service Environment on Weight of Carrier-based Aircraft[J].Equipment Environmental Engineering,2017,14(7):56-60. |
| 使用环境对舰载飞机重量的影响研究 |
| Influences of Service Environment on Weight of Carrier-based Aircraft |
| 投稿时间：2017-03-15 修订日期：2017-07-15 |
| DOI：10.7643/ issn.1672-9242.2017.07.011 |
| 中文关键词: 舰载飞机 陆基飞机 使用环境 重量函数 |
| 英文关键词:carrier-based aircraft land-based aircraft service environment weight function |
| 基金项目: |
|
|
|
|
| 摘要点击次数: |
| 全文下载次数: |
| 中文摘要: |
| 目的 寻求舰载飞机与陆基飞机的重量关系，评估在舰面使用环境条件下舰载飞机的增重代价。方法 根据重量设计分析方法，确定研究对象，建立舰载机、陆基飞机的主要特征重量分析函数，求解函数中的相关参量，进而计算舰载机相对陆基飞机的重量增量。结果 相同空机重量时，舰载机比陆基飞机的最大起飞重量要减小11.3%～12%；相同最大起飞重量时，舰载机比陆基飞机的空机重量要增大12.1%～12.9%。结论 基于重量函数的综合分析方法，可以全面考虑使用环境条件对舰载机重量影响的诸要素，其分析结果能够满足舰载机重量设计分析的需要。 |
| 英文摘要: |
| Objective To find out the weight relation between carrier-based aircraft and land-based aircraft and evaluate its weight penalty of using carried-based aircraft in shipboard environment. Methods According to weight analysis method, the object of study was determined, the main characteristic weight functions of carrier-based aircraft and land-based aircraft were constructed respectively, relevant parameters in the functions were solved, and then characteristic weight increment between carrier-based aircraft and land-based aircraft was calculated. Results The maximum take-off weight of carrier-based aircraft was 11.3 to 12 percent less than that of land-based aircraft at the same empty weight. The empty weight of carrier-based aircraft was 12.1 to 12.9 percent more than that of land-based aircraft at the same maximum take-off weight. Conclusion All service environment influence elements on carrier-based aircraft weight was considered by the integrated analysis method based on weight function, the result can satisfy the need of the carrier-based aircraft weight design and analysis. |
| 查看全文 查看/发表评论 下载PDF阅读器 |
| 关闭 |
