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"외부장착물"

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"외부장착물"

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Validation of Structural Safety for Flight Compatibility of Pod Mounted Aircraft External under Flight Load Conditions
Woo Je Cho, Dong Seol Choi, Jin Bo Park, Sun Kyu Ann
J. Korean Soc. Precis. Eng. 2024;41(4):251-260.
Published online April 1, 2024
DOI: https://doi.org/10.7736/JKSPE.023.113
A pod mounted on an aircraft external must be installed on an aircraft after its structural safety is verified under flight conditions. This paper presents methods of flight load and test load generation. Evaluation of test result data and standards for failure mode are also presented. First of all, to verify the static structural stability, flight loads for the aircraft maneuvering conditions were calculated. Finite element analysis was then performed with flight loads. As a result of the analysis, structures were verified to have a margin of safety for a given design requirement. In addition, it was confirmed that the launcher tube had enough rigidity to support the missile. Thus, the role of stinger such as longeron and hardback was insignificant. Finally, based on results of tests and analysis, the static structural stability of pod was substantiated and the reliability and effectiveness of the analysis model were obtained. These results and dynamic stability verification results suggest that an optimal design is necessary.

Citations

Citations to this article as recorded by  Crossref logo
  • Calculation of Flight Loads and Structural Robustness Analysis of Aircraft External Stores Considering Low Speed Rotorcraft Installation
    Ji Hwan Park, Chang Bong Ban, Jong Hwan Kim, Sun Kyu Ahn
    Journal of the Korean Society for Precision Engineering.2025; 42(8): 613.     CrossRef
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Analysis of Operating Mechanism and Experimental Verification of Store Automatic Fixing Equipment
Jung Pil Kim, Dong Hun Song, Duk Hyun Nam, Jong Yoon Choi, Jin Hyun Cha
J. Korean Soc. Precis. Eng. 2018;35(10):951-956.
Published online October 1, 2018
DOI: https://doi.org/10.7736/KSPE.2018.35.10.951
The Store Automatic Fixing Equipment operates as an external force acting on fixing the Store during the flight and as a device designed to prevent the Store from being shaken when the aircraft is flying with the Store. In this paper, we derived the mathematical modeling of the Store Automatic Fixing Equipment through the analysis of the operating principles of the Equipment. The gap occurred by the external vibration forces was calculated through the mathematical model and structure analysis. And then the shape and stiffness design of the wedge, i.e., the Store Automatic Fixing Equipment was derived by the mathematical modeling and structural analysis. We made the Store Automatic Fixing Equipment and took the vibration testing under the aircraft flight conditions. We used the load cell to measure the reaction forces acting on the gap between the Store Automatic Fixing Equipment and the Store. The results of the reaction force measurements were compared with the analysis results of the design and the suitability of the Store Automatic Fixing Equipment’s design was verified based on the analysis.
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