Course detail

Aircraft Materials

FSI-OLRAcad. year: 2013/2014

Relationships between compositions,processing effects, microstructures,properties and typical applications of selected aircraft materials. Special material requirements. Aluminium alloys, magnesium alloys, titanium alloys, high strength steels, nickel-base and cobalt-base superalloys, fibre and particle composites, structural polymers,structural ceramics, wood and plywood for aircraft structures. New research and development, international material standards and equivalents.

Language of instruction

Czech

Number of ECTS credits

Mode of study

Not applicable.

Guarantor

doc. Ing. Josef Klement, CSc.

Department

Institute of Aerospace Engineering (LÚ)

Learning outcomes of the course unit

The course Aircraft Materials makes students familiar with representative aircraft structural materials as well as with their optimal use. Students will be able to evaluate different material variants of aircraft structures according their strength, lifetime and damage tolerance.

Prerequisites

Basic knowledge of relations between composition, processing, structure and properties of structural materials. Basic terminology of physical metallurgy and material limit states.

Co-requisites

Not applicable.

Planned learning activities and teaching methods

The course is taught through lectures explaining the basic principles and theory of the discipline. Exercises are focused on practical topics presented in lectures. Teaching is suplemented by practical laboratory work.

Assesment methods and criteria linked to learning outcomes

For the course-unit credit it is necessary to attend seminars and to meet requirements of three written tests. A final evaluation consists of tests results (40 %) and oral examination (60 %).

Course curriculum

Not applicable.

Work placements

Not applicable.

Aims

The aim of the course Aircraft Materials is to inform students of present state in the area of structural materials for aircraft structures and to provide them with methodical and objective knowledge.

Specification of controlled education, way of implementation and compensation for absences

Attendance at seminars is compulsory. In case of justified absence, the missed seminar may be compensated with an individual assignment. Continuous checking is made by means of written tests. In case of a failure, it is required to repeat the test.

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

ASM Handbook, Vol. 02 Properties nad Selection of Nonferrous Alloys (EN)
ASM Handbook, Volume 21, Composites, ASM International, 2002 (EN)
Cenek,M.-Jeníček,L.: Nauka o materiálu I,3. svazek, Neželezné kovy,Academia,Praha 1973 (CS)
Hussey B., Wilson J.: Light Alloys. Directory and databook. Chapman&Hall, 1998 (EN)
Middleton,D.H.: Composite materials in aircraft structures,Longman Group, 1990 (EN)
Michna a kol.: Encyklopedie hliníku (CS)
Vlot A., Gunnink J. W.: Fibre Metal Laminates, ISBN 1-4020-0038-3 (EN)

Recommended reading

Baker, A.: Composite materials for aircraft structures, AIAA 2004
Michna, Š. a kol.: Encyklopedie hliníku, Prešov 2005, ISBN 80-89041-88-4
Ustohal,V.: Letecké materiály,VUT Brno,1988

Classification of course in study plans

  • Programme N2301-2 Master's

    branch M-STL , 1 year of study, winter semester, compulsory

Type of course unit

 

Lecture

39 hod., optionally

Teacher / Lecturer

doc. Ing. Josef Klement, CSc.

Syllabus

1.Aircraft materials and strength conceptions
2.Characteristics of aluminium alloys for aircraft structures. Standards
3.Wrought aluminium alloys. Properties, application, heat treatment
4.Casting aluminium alloys for aircraft structures. Properties, application, heat treatment 5.Magnesium alloys for aircraft structures
6.Titanium alloys for aircraft structures
7.Typical aircraft steels
8.High temperature materials. Nickel alloys, cobalt alloys
9.Fibre reinforced composite materials.
10.Discoutinously reinforced composite materials
11.Structural plastics for aircraft structures
12.Ceramic materials and composites
13.Wood and plywood for light aeroplanes

Exercise

11 hod., compulsory

Teacher / Lecturer

doc. Ing. Josef Klement, CSc.

Syllabus

1.Standardization of aircraft materials
2.Standards of aluminium alloys
3.Choice of material for given airframe component
4.Relationship between microstructure and properties - DAS.
5.Test No 1
6.Design of airframe structure from Mg alloy
7.Schaeffler diagram of high alloy steels
8.Test No 2
9.Properties of high temperature alloys
10.Properties of wood for light aeroplanes
11.Test No 3