Abstract
Ramp and its units as one of the most important aggregates in the tail cargo door is reviewed. Such geometric parameters and units of the ramp as its maximum length Lp, the cutout in the ramp area, the theoretical line of the cargo door beam, the theoretical line of the ramp flooring, the ramp hinge units, its longitudinal and transverse beams, the ramp power locks, the ramp control cylinders and ramp rods, as well as the ramp sealing are presented. The main algorithms for determination are described using theoretical and practical data of most popular and used transport aircrafts such as An-124, An-26, Il-76, C-141, C-5 M. Most of presented information is collected considering time-tested best technical solutions as well as modern requirements of regulatory documents for transport category aircrafts (AP-25, CS-25, ICAO SRP A6, AC-25, OST).
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Konyshev, D., Humennyi, A., Grebenikov, O., Chumak, A., Buival, L. (2021). Transport Aircrafts Rear Cargo Door Ramp with Sealed Floor Main Parameters and Components Description and Determination. In: Nechyporuk, M., Pavlikov, V., Kritskiy, D. (eds) Integrated Computer Technologies in Mechanical Engineering - 2020. ICTM 2020. Lecture Notes in Networks and Systems, vol 188. Springer, Cham. https://doi.org/10.1007/978-3-030-66717-7_50
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