Library


 

The materials presented here are the intellectual property of the National Aerospace University "Kharkiv Aviation Institute".The manuals are in the RAR format archives. In order to protect the copyrights, the files are protected by the passwords. You can find out the password from your tutor or the department library (department 203).
Have questions? Please, contact us over the e-mail: k203@i.ua or konstr203@gmail.com.

 


01-E UDC 621.452.3 (075.8)
Y-44

Major units of aircraft gas turbine engines [Text] : Tutorial / S. Yepifanov, Y. Shoshin, Y. Gusev. — Kharkov.: National Aerospace University «Kharkov Aviation Institute», 2013. — 101 p.

This tutorial copes with main problems of designing gas turbine engines and their major units. They are compressors, turbines, combustion chambers and transmissions. Studying this tutorial, students will learn requirements, which are made for major units, their classification and information about constructive decisions to meet these requirements. The tutorial contains practical tasks which performing needs studying engine mockups, drawings and posters. There are questions for self-testing in the end of each part.


02-E UDC 629.7.036:621.438
Sh-88

Basic technical data of Soviet, Ukrainian and Russian cruise engines of aircrafts [Text]: tutorial / Yu. Shoshin, F. Sirenko. – Kharkiv.: National Aerospace University «Kharkiv Aviation Institute», 2015. – 66 p.

This tutorial comprises technical data and brief information about structural features of different aircraft gas turbine engines that belong to different generations. Tutorial also gives information about aircrafts and helicopters that are powered by these engines.


03-E UDC 621.438.03-226.01.24:539.4
Y-44

Strength analysis of rotor blade [Text]: Tutorial / S. Yepifanov, Y. Shoshin, R. Zelenskyi. — Kharkov: National Aerospace University «Kharkov Aviation Institute», 2013. — 32 p.

Analysis of compressor and turbine rotor blade static strength is considered which consists of stresses and safety factors calculation in the most loaded points on length of the blade body. Information about software, recommendations for calculation and examples are given. Variation of blade body geometric parameters on the blade length is determined by exponential functions which parameters are defined in three crosssections – root, meaning and peripheral. Turbine blade is analyzed taking into account its temperature.


04-E UDK 621.43.001.24:539.4(075.8)
B41

Pistons for internal combustion engines [Text]: Tutorial to laboratory work on the course "Aircraft piston engines"/ A.V. Bilogub. - Kharkov.: National Aerospace University “Kharkov Aviation Institute”, 2014. - 34 p.

Tutorial introduces the information of functions of piston assembly, features of their operation, features of pistons, piston pins and piston rings. There are examples of land and aircraft engines presented in the tutorial. The tutorial also involves information about materials used to manufacture parts of piston assembly. There are also given formulas for the strength analysis of parts of piston assembly.


05-E UDK 621.452.3(075.8)
G-20

General structure of aircraft engines and power plants [Text]: lect. summary / А. Garkusha, F. Sirenko. – Kharkov: National Aerospace University «Kharkov Aviation Institute», 2014. – 76 p.

This guide will be useful for students studying aircraft engine design in english. This guide addresses the base technical data, arrangement and construction of aircraft engines. Most diagrams let students get an overview of working process features and construction of main components. The information is presented in the order suitable for using at practical classes and during individual work. This guide will also be helpful for students studying aerospace engineering to get general overview of air-breathing and rocket engines.


06-E UDC 629.7.036:621.438-226 (075.8)
LBC 39.55:31.363я73
Y-44

Strength analysis of disc [Text]: Tutorial / S. Yepifanov, Y. Shoshin, R. Zelenskyi. – Kharkiv: National Aerospace University «Kharkiv Aviation Institute», 2014. – 28 p.

Tutorial addresses the static analysis of compressor and turbine discs. Analysis aims calculating stresses and safety factors distribution on disk radius. Student can find information about software, recommendations for calculation and examples. The analysis is carried out according to method of finite differences. Disc is considered symmetrical; its profile is set by values of width on given radiuses. The temperature of turbine disc is considered to vary with the radius.


07-E UDC 629.7.036:621.438-226
LBC 39.55:31.363я73
Y-44

Blade bending oscillations analysis [Text]: Tutorial / S. Yepifanov, Y. Shoshin, R. Zelenskyi. – Kharkiv: National Aerospace University «Kharkiv Aviation Institute», 2014. – 24 p.

Tutorial addresses the dynamic analysis of compressor and turbine blades. Analysis aims calculating dynamic frequency on first shape mode. The analysis is carried out according to method of Raleigh-Ritz. The frequency diagram is built to determine the engine resonant operational modes. Student can find information about software, recommendations for calculation and examples.


08-E UDK 629.7.036:621.438-226 (075.8)
LBC 39.55:31.363я73
Y-44

Afterburners and exhaust systems of turbine engines [Text]: Tutorial / S. Yepifanov, Y. Shoshin, V. Chygryn. – Kharkiv: National Aerospace University «Kharkiv Aviation Institute», 2014. – 32 p.

Tutorial addresses operation and construction of afterburners and exhaust systems of turbine engines. First part of the tutorial contains information about purpose, operational process and construction of afterburners. Second part concerns exhaust systems. Difference between exhaust systems of direct-reaction engines and indirect-reaction engines is shown. Requirements to these components of engines and methods to meet these equirements are given. Materials used to manufacture parts of these components are named. The tutorial contains practical tasks which performing needs studying engine mockups, drawings and posters. There are questions for self-testing in the end of each part.


09-E UDC 629.7.036 (075.8)
BBL 31.76я73
Y-44

Systems and units of aircraft power plants [Text]: lect. summary / S. Bezuglyi, S. Yepifanov, R. Tsukanov. - Kharkov: National Aerospace University «Kharkov Aviation Institute», 2015. - 100 p.

This guide will be useful for students studying systems of aircraft power plants in English. This guide addresses the base technical data, arrangement and design of aircraft power plants systems and their units. Most diagrams let students get familiar with working process features and design of main components. The information is presented in the order suitable for using at practical classes and during individual work. This guide is also helpful for students studying aerospace engineering to get general overview of the air-breathing engines power plant systems and their units.


10-E UDC 621.452.3-226.001.24 (075.8)
ББК 39.15я73
M25

The strength analysis of blade roots [Text]: Manual / E. Martsenyuk. – Kharkiv: National aerospace university «Kharkiv aviation institute», 2016. – 52 p.

The tutorial addresses different constructive methods to secure impeller blades in the disks of GTE, advantages and disadvantages of the most used joints, methods of the root strength analysis. Manual also comprises examples of strength analyses.


11-E UDC [621.452.3.03-585+629.735.45+621.452.33.03-585](075.8)
BBL 39.55+39.54Я43
G-18

Gearboxes of helicopter power plants and turboprops [Text]: tutorial / A. Garkusha, F. Sirenko. - Kharkiv.: National Aerospace University «Kharkiv Aviation Institute», 2016. - 52 p.

The tutorial focuses on aircraft gearboxes, their classification, generic schemes and configurations. The authors describe the design and functions of gearboxes and their components, as well as structural features of serial turboprop engine gearboxes and helicopter gas turbine engines.


12-E UDC 629.7.036 (075.8)
BBL 31.76я73
B-44

Components of Aircraft Power Plant Systems [Text]: lect. summary / S. Bezuglyi, F. Sirenko, M. Shevchenko. - Kharkov: National Aerospace University «Kharkov Aviation Institute», 2016. - 104 p.

The synopsis deals with the general information about the construction of aircraft power plant accessories. The synopsis also contains the technical specifications, application range and operation principle of these accessories. The synopsis addresses the general information about the construction and analysis of the accessories used in the fuel and oil feeding systems. The specific features of construction and operation of centrifugal pumps, displacement pumps and fuel nozzles are considered.


13-E UDC 621.432:621.824.32.001.24 (075.8)
BBL 31365я73
B 58

Connecting rods, crankshafts, cylinders and cylinder blocks of aircraft piston engines [Text]: manual / O. Bilohub, Yu. Gusev, F. Sirenko. - Kharkiv.: National Aerospace University «Kharkiv Aviation Institute», 2017. - 76 p.

The manual considers the construction of connecting rods, crankshafts, cylinders and cylinder blocks of the aircraft piston engines. The manual also contains the information about the materials, of which piston engines are made, and the strength analysis of the elements.


14-E UDC 621.432.3.001.24 (075.8)
BBL 31.365я73
B 58

Thermal analysis of aircraft piston engine [Text] : manual / O. Bilohub, F. Sirenko. - Kharkiv.: National Aerospace University «Kharkiv Aviation Institute», 2017. - 28 p.

The manual considers the method of the thermal analysis of the aircraft four-stroke spark ignition piston engine and its particular sample including the method to get the main geometrical parameters of the engine (diameter of the cylinder and piston stroke).