Design of flap/spoiler follower mechanism for civil aircraft
نویسندگان
چکیده
Abstract With the gradual development of lift device to a simple and efficient direction, drooped spoiler has become an emerging device. The can improve aerodynamic performance wing by reducing air flow separation increase coefficient, which requires deflect certain angle following downward deflection flap. Aiming at this requirement, paper proposes design method follower mechanism based on relative pole method. applicability correctness are verified kinematics simulation. Moreover, kinematic characteristics four-bar linkage complex compared, results show that is more stable in motion process.
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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/10.1088/1742-6596/2472/1/012016