There is a need to ensure a high level of safety of the aircraft's flight, in particular with regard to the redundancy of the hydraulic system. However, the introduction of additional hydraulic circuits entails, in addition to the advantages and many disadvantages, such as increasing the complexity and weight of the hydraulic system. One of the compromises in this situation was the installation of a power transfer unit. In this article, schematic solutions and peculiarities of operation of power transfer units, cases of their use are considered. An analysis of the current problems and possibilities of improving such aggregates is presented. Possible directions of further development of power transmission units have been identified. In particular, the directions for increasing pressure, reducing the gas content of the liquid, using pump power regulators, reducing gaps, reducing noise and temperatures, and introducing an intelligent component are highlighted. Possibilities for installation of power regulators, their various circuit solutions and operating principles are described. The characteristics of regulators , the operation of which is based on the principle of load sensitivity, the possibility of using these regulators to optimize the operation of the power transfer unit, and, therefore, increase the accuracy, stability, controllability of the entire hydraulic system of the aircraft are presented.