The development of a lubrication system taking into account the scavenge pump, dry sump, etc. has started. Numerical studies were carried out to determine the overall dimensions and characteristics of the camshaft drive. This drive should have a rigid kinematic connection in accordance with aviation requirements. As a result of numerical studies, a kinematic diagram of the shaft drive was obtained. The development of 3D parts for this drive has started. The remaining engine outside-mounted components were developed. The engineering analysis is carried out in a three-dimensional model of the combustion chamber geometry and the fuel equipment of the engine under development. Experiments of similar fuel equipment go ahead, both on a non-motorized stand and experimental engine.
