1993-1998

Irkutsk Technical University

Main specialization – technical maintenance of aircrafts, helicopters and engines.

Degree – Mechanical Engineer
Key disciplines related to aircraft:
Design and stress analysis of aircrafts and helicopters
Design and stress analysis of jet and piston engines
Aerodynamics; flight dynamics; fluid dynamic of jet engines
Hydraulics; A/C hydraulics systems
Electrics; A/C electrical systems
A/C mechanical control systems
Flight safety
In total over 50 disciplines
Diploma – “Ultralight aircraft project”. Special part of the diploma – software for aerodynamic sizing of propeller

Aircraft mechanic

Airframe / power plant / hydraulic / mechanical systems maintenance and repair

2001-2008

Sukhoi civil aircrafts

Stress / design engineer

Stress calculations, FEMs and reports of composite and metal aircraft structures (fuselage, wing, empennage, movables – all structural ATAs)

Linear/nonlinear FE analysis of metals and composites

Estimating of structural loads based upon aerodynamic and gravity loads.

Metallic, composite and hybrid structures stress analysis,

Design of aircraft structure / Weight balance estimation / Sizing of AC structures

Development of 3D CAD models in UG NX/Teamcenter

Projects management.

Manufacturing support at industrialization, follow-on support/plant quality inspections

Repair design and stress analysis for concessions, technical signatory.

Daily and complex repairs design and stress review.

Composites test pyramid development

Interpreting full-scale tests results and stress reports validation

Supporting in-service occurrences topics

Development of stress methods in application to certain projects

Systems installation design and stress analysis

2008 -2011

Sukhoi civil aircrafts

Teamleader of the airframe design and stress analysis department

2011-2012

FACC AG

Stress engineer

Checking stress calculations, FEM, static and fatigue reports of composite and hybrid aircraft components (spoilers, airbrakes, flaps, aileron, rudder, elevator, pylon fairing for SSJ-100 project).

Definition of damage tolerance concepts for components.

Development of Composite analysis stress manual

Since 2012

Airbus GmbH

Design / stress engineer

Stress and fatigue analysis

Modifications development

Engineering support (design/stress/F&DT) of final assembly line and Flight Line

Engineering solutions for repairs

Service bulletins approval

Investigation into root causes of in-service problems

Fatigue test support

Service bulletins update

Certification activities

Analisys of in-service occurrences for continued airworthiness

Flight safety risk assessment

Stress tools development