Electrochemical machining (ECM) is widely used in modern aircraft engine technology. This method was
developed on a step-by-step basis in accordance with development of gas turbine equipment. Introduction of new difficult
to machine materials into engines designs and improvement of accuracy of detail geometric parameters required new
technological solutions. ECM method has a number of advantages: zero tool wear, the process does not depend on
physical-mechanical properties of work piece material, no heat and force action on a work piece; these facts provide high
quality of the surface layer and increase engine life. However, electrochemical machining has also disadvantages which
essentially limit its applicability. This is primarily a low localization of ECM process. In order to eliminate this
disadvantage new ECM schemes were developed, inter-electrode gap was reduced, switched mode power supply units,
vibration of electrochemical machining electrode, etc. were used. Electrochemical machines design became more
complicated and ECM operations design techniques required new solutions, therefore the scientific inquiry in this area
continued intensively. Rapid development of computer technology contributed to the creation of digital models that
adequately describe processes in the inter-electrode spacing at ECM. It is necessary to create electronic databases for
various electrochemical metal-electrolyte systems, to develop techniques to simulate electric fields in the inter-electrode
spacing, and to profile tool electrode automatically. The authors carried out active researches in this area at all stages of
ECM development; they have a large number of publications in the field, including 4 monographs.