Design and Research of Missile launcher Drive System for Anti-aircraft Gun and Missile Weapon System
نویسندگان
چکیده
Abstract Aiming at the problems of large size and weight electric cylinder, low efficiency pressure fluctuation centralized hydraulic drive system, a system anti-aircraft gun missile weapon based on electro-hydrostatic actuator is designed. The working principle discussed, its components are selected designed, micro cartridge control check valve designed analyzed integrated structure designed;The simulation model established by AMEsim software. results show that can move driving device to highest position within 2s, meet requirements, have certain guiding significance for research development launcher driving.
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ژورنال
عنوان ژورنال: Journal of physics
سال: 2023
ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']
DOI: https://doi.org/10.1088/1742-6596/2478/9/092005