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http://dx.doi.org/10.9766/KIMST.2020.23.5.444

Development of an Aircraft Hydraulic Brake Assembly with a Self-gap-adjuster  

Yi, Miseon (Aerospace Technology Research Institute, Agency for Defense Development)
Song, Won-Jong (Aerospace Technology Research Institute, Agency for Defense Development)
Kwon, Jun-Yong (Aerospace Technology Research Institute, Agency for Defense Development)
Publication Information
Journal of the Korea Institute of Military Science and Technology / v.23, no.5, 2020 , pp. 444-451 More about this Journal
Abstract
This study was conducted to develop the hydraulic brake assembly for MUAV(Medium-altitude Unmanned Aerial Vehicle). The brake assembly has the self-gap adjuster which performs to maintain a constant gap between the piston and the disk, even if the friction pad wore down. The function of adjuster helps to keep the brake-reaction speed constant and prevent the unnecessary abrasion of the wear pad during the life of the brake assembly. The development of the aircraft hydraulic brake assembly with the self-gap-adjuster in this paper is the first ever in South Korea. The concept of the mechanism was defined and the formula which is necessary to calculate the friction force was set up in the paper. The tester was invented for the functional test and the proper operation of the self-gap-adjuster was confirmed through the test. Dynamo tests and flight tests were also carried out to verify the braking performance of the brake assembly.
Keywords
Aircraft Hydraulic Brake; Self-gap-adjuster; Dynamo Test; Flight Test;
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