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| Influences of Service Environment on Weight of Carrier-based Aircraft |
| Received:March 15, 2017 Revised:July 15, 2017 |
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| DOI：10.7643/ issn.1672-9242.2017.07.011 |
| KeyWord:carrier-based aircraft land-based aircraft service environment weight function |
| Author | Institution |
| MA Jie-xiang |
AVIC The First Aircraft Institute, Xi'an , China |
| DUAN Qiong |
AVIC The First Aircraft Institute, Xi'an , China |
| WANG Chou-chou |
AVIC The First Aircraft Institute, Xi'an , China |
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| Abstract: |
| 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. |
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