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Igor Viktorovish Borisov 

Associate Professor

Institute of Radioengineering Systems and Control

E-mail:
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Degree: Candidate of Sciences

Personal page in Russian:
https://sfedu.ru/person/ivborisov
Personal page in English:
https://sfedu.ru/en/person/ivborisov

Teaching:

  • Management of research and development of STS
    Introduction to the subject. Basic concepts and definitions Management input to the design and development of at. Planning design and development at Managing development of technical proposals (avant-project) Managing development of a sketch (preliminary) project Development management technical project The management of work design A critical review of the project Analysis of design and development at Verification of design and development at Validation of the project at Control the output of design and development at Configuration management sample of at Change management project Supervision of products in production at Supervision of products in use at Features of process control design and development at
  • Quality management in aviation industry
    Introduction. The goals and objectives of the course. The principles of product quality assurance Family of international standards series ISO 9000 for quality management products The rationale of the QMS. Terms and definitions QMS The quality manual Document management protocols and quality The company's policy in the field of quality. Customer orientation Planning of the QMS. Goals in the field of quality Responsibility, authority and exchange of information The management of resources. Staff Planning of enterprise activity The processes associated with the consumer Manage the design and development Planning, input, output, project analysis and development Procurement management Software design and research activities Change, analysis and improvement in the QMS. Audits. Correcting and warning actions System quality management methods
  • Certification of aviation equipment
    The goals and objectives of the course. Basic information about certification. Safety. Basic information about certification of aviation technology (at). System of certification of aviation equipment in the U.S., Europe and the CIS. The system of certification of aviation equipment in Russian Federation. Basic information about the aviation rules (AP) and airworthiness (NLG). Aviation rules part 21, 23, 25 and APOLS. Aviation rules part 27, 29, 33, 34, 35, 36, 39, 145, 183. Communication design and certification at. Classification of aircrafts (AC). Certification Developer at. The stages of aircraft certification. The certification basis (SB). The stages of aircraft certification. The table of correspondence (TC). Application for a certificate type (ST). The stage layout of the aircraft. Certification testing of the aircraft. Bench tests of the aircraft. Organizing and conducting the first flight of the aircraft. The certification factory test. Certification control tests (MIS) and operational tests. The issuance of the type certificate. Certification of production and products at.
  • The construction of the chassis and control systems
    Features of design of control systems for AIRCRAFT. The role of the person in control system LA. The contents of the Technical specifications and baseline data for the development of the control system Basic requirements for the design of control systems LA The main stages of the design of control systems Constructive elements of mechanical transaction management system LA Laying of tracks of the control plane (trace). Vibration control wiring. Frequency-phase characteristics (CFH) Efforts on arms control The calculation of the control strength. Features of design of elements mechanical controls Design of boot devices. Calculation of springs Constructive measures to ensure the reliability of the control systems and increase safety. Further development of control systems General provisions. The composition of technical specifications and requirements for the design of the chassis The definition of the type, size and number of wheels mounted on the support chassis The definition of the power circuit chassis Build the kinematic scheme of the gear The distribution of the normalized maximum work between wheels and shock absorber Identify the current chassis loads The design of the liquid-gas absorber. The diagram of work and the definition of the parameters of the shock absorber Calculation of basic load rating and design loads lifts chassis
  • Design of aircraft
    Purpose and structure of the course. Introduction to the course design. The design object is a complex technical system. The plane in the structure of complex aircraft complex. The overall design of the aircraft. The outer design. The preliminary design. Limitations in the design. Main parameters and characteristics of the aircraft. The analysis and selection of scheme LA and the type of the power plant. The selection scheme of the aircraft on separate grounds. Select the type of the power plant. The algorithm for determining the main parameters of the aircraft. The weight of the design aircraft. The layout of the aircraft. Aerodynamic configuration. Body-weight layout. The alignment of the aircraft.
  • The efficiency of aviation complexes
    The goals and objectives of the course. Introduction Classification of performance criteria Functional efficiency Weight of the perfection of the aircraft The energy excellence of the aircraft The performance of the aircraft Weight returns payload, transportation to the specified range Given the performance of the aircraft Quality criteria of the aircraft The production efficiency of the plane The economic efficiency of the aircraft operation The competitiveness of the aircraft, indicators of competitiveness A comprehensive analysis of the efficiency of aviation complexes
  • Features the design of passenger and cargo aircraft
    Basic requirements and limitations applicable to modern passenger and cargo planes, their influence on the design process Analysis and comparison of constructive-power circuits of modern passenger and cargo aircraft. Modification of passenger aircraft into freighters The main types of structural assemblies glider passenger and cargo aircraft, made of metal and composite materials Features the design of passenger and cargo aircraft Methods optimization of design parameters of passenger and cargo aircraft The choice of material of construction. Factors influencing the choice of material The design of the parts produced by different technological ways The principles of rational design of passenger and cargo aircraft Classification of compounds according to structural and technological characteristics Design butt nodes Design panels The design of the ribs Design frames Principles of design of units of a glider passenger and cargo aircraft. Safely damaged airframe of the aircraft with a long service life. The restrictions imposed on the wing of KSS. Principles of design of units of a glider passenger and cargo aircraft. Monolithic construction. The task of construction. Principles of design of units of a glider passenger and cargo aircraft. Design design of the positive elements of the longitudinal set of a wing. Features of design design of interface panels, cut the edges of the panels and stringers. Principles of design of units of a glider passenger and cargo aircraft. Brief technical requirements for the design of the fuselage. The development of KCC fuselage. Design shell of the pressurized cabin.
  • Design features of aircraft maneuvering
    Introduction. The goals and objectives of the discipline The stages of development and classification of aircraft maneuvering The relationship of maneuvering characteristics with the design parameters The influence of the main parameters of the power plant for the maneuverability of the aircraft The choice of parameters of wing shape in the plan Directions of improving of handling of polars by improving aerodynamic layout Types of control system and stability requirements of the maneuverable plane The basic layout solutions that ensure the stability of the aircraft in the longitudinal channel The basic layout solutions, providing lateral stability of the aircraft The main elements of the system SUPR maneuverable plane Constructive and layout decision in a maneuvering aircraft Promising fighters. Requirements to the tactics of air combat Requirements speed cruising flight New modes of maneuvering The main directions of development of new constructive and technological solutions
  • Features of design of seaplanes and amphibians.
    Classification of seaplanes The buoyancy of a seaplane The stability of a seaplane The buoyancy of a seaplane The concept of gliding of a seaplane Fundamentals of the theory of similarity Modeling of movement of a seaplane The wave motion of water Fundamentals of the theory of planing The steady-state gliding plate The hypothesis of flat sections The immersion of the wedge Steady gliding the flat-keeled bottoms Stability and planing. Characteristics of resistance of planing Loading of a seaplane when operating on the water Rationing loads on the bottom of the boat seaplane Features of design of seaplanes and aircraft amphibians