Forming the Technical Concept of Aircraft Power Systems of the Perspective Aircraft Taking Into Account the Outside Mechanical Impacts

Problems related to the layout of aircraft hydraulically and electrically actuated systems, as well as innovative approaches to their designing are discussed in this article in terms of the concept of the fully electrical equipment airplane, and their impact on the performance of the aircraft being developed, with outside mechanical impacts taken into account. Complex aggregate factors must be taken into account when conducting research into battle tolerance of combat airplanes and helicopters. The applicability of a method to previously analyzed aggregate uncertainties intrinsic to the process of development of an innovative military aircraft is the criterion for the choice of methods. A fully electrical airplane will radically change the design principles and functionality parameters of major aircraft systems and units. This design of aircraft hydraulic and electrical system allows functional localization of each actuation loop to provide its independent operation, thus minimizing its vulnerability to enemy weapons and reducing the weight of aircraft hydraulic and electrical systems.