We specialize in the design of composite and metallic structures of the aircraft and technological instrumentation for their production. We conduct performance analysis, load analysis, and modernization projects for currently used aircraft. The experience of our design team allows us to perform work beyond the aviation industry and propose optimal solutions that take into account the Client’s specific requirements.
Our offer in the field of aircraft design includes:
• metal structures;
• composite structures;
• aeronautical structures from glass and carbon composite;
technological instrumentation:
• molds for making composite structures,
• assembly jigs;
• additional equipment in currently used airplanes and helicopters;
• organization and management of the aircraft design process and its optimization;
• aircraft performance calculations;
• strength calculations;
• development of flight test programs;
• aircraft certification
The design process we perform with the use of CATIA software, strength analyzes are performed using ANSYS software.
We perform the work based on the Design Organization Approval (ADOA), approval No. AP 270, issued by the European Aviation Authority (EASA), and the quality management systems ISO 9001: 2015, AQAP 2110: 2016.
In the field of design and optimization of airframe elements, we offer the following services:
• construction of parametric models of objects for tests and optimization (e.g. a wing);
• aerofoil profiles design;
• multi-criteria and multidisciplinary design of aircraft and its components.
Aircraft landing gears
Our offer in the field of design includes:
• wheeled and skid types aircraft landing gear;
• shimmy and anti-resonance dampers;
• one- and two-stage shock absorbers for aircraft landing gear;
• landing gear integration elements;
• test beds;
• ABS anti-skid systems for aircraft landing gear applications;
actuators and locks;
• wheels and high-energy brakes;
• landing gears for unmanned aerial vehicles;
• technology demonstrators;
• electric brakes for manned and unmanned aerial vehicles;
• assessment of the design process and its compliance with aviation standards;
• assessment of the state of knowledge in the field of technological solutions of aerial landing gears;
• other solutions depending on the Customer’s needs.
In the field of drives design, we offer the following services:
• construction of parametric models of objects for tests and optimization (engine intake duct, engine exhaust nozzle, etc.);
• construction of parametric models of objects for research and optimization (engine intake duct, engine exhaust nozzle, etc.);
• aerodynamic design of flow channels;
• aerodynamic design of the main rotor of the helicopter;
• propellers design;
• design of aircraft engine components;
• software development.
