Course detail

Aircraft Manufacture I

FSI-OT1-AAcad. year: 2015/2016

Basic technological methods and processes in aircraft production. Heat treatment technology of light alloys and steels. Forming techniques in aircraft manufacture. Fundamentals of composites and sandwich structures manufacturing. Rivets and riveting.

Language of instruction

English

Number of ECTS credits

4

Mode of study

Not applicable.

Offered to foreign students

Of all faculties

Learning outcomes of the course unit

Students acquire the knowledge necessary for evaluation of technological methods, design from technology point of view and for technology planning of heat treatment, forming, composite manufacture and joining.

Prerequisites

Basic knowledge of the structure, phase transformations and properties of metal structural materials. Basic technological principles and methods of materials processing - heat treatment, forming.

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

Satisfying the course-unit credit conditions it is necessary to attend compulsory seminars and to pass three written tests. The final evaluation consists of the tests results (40%) and oral examination (60%).

Course curriculum

Not applicable.

Work placements

Not applicable.

Aims

The objective of the course Aircraft Manufacture I is to inform of aircraft manufacture specific attributes and methods and procedures, which are necessary for design specialists.

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

Attendance at seminars is compulsory. In the case of legitimate absence, students are required to work out an alternative individual assignment. Continuous checking is done during seminars.

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

ASM Handbook, Vol. 21 Composites (EN)
ASM Handbook Vol. 5 Surface Engineering (EN)
ASM Handbook Vol.02, Properties and Selection Nonferrous Alloys (EN)
DIN-DVS-Taschenbuch 215: Schweisstechnik in Luft- und Raumfahrt, Beuth.DVS-Verlag, 1998
Lee L.-H.:Adhesive Bonding, Plenum Press, 1991
Metals Handbook, Volume 14: Forming and forging,ASM International,1988
Peterka, J.: Lepení konstrukčních materiálů ve strojírenství,SNTL,Praha 1980

Recommended reading

Flaška,M.-Růžička,A.-Štekner,B.: Speciální letecké technologie, , 0
Žák,J.-Samek,R.-Bumbálek,B.: Speciální letecké technologie I,VUT Brno,1990

Classification of course in study plans

  • Programme N2301-2 Master's

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

  • Programme M2E-P Master's

    branch M-IND , 1 year of study, summer semester, compulsory

Type of course unit

 

Lecture

26 hod., optionally

Teacher / Lecturer

Syllabus

1. Specific features of aircraft production
2. Heat treatment of light alloys
3. Hardening of aircraft steels
4. Formability of aircraft materials, prepare operations for forming
5. Bending and drawing with solid and rubber tools, fluid forming
6. Stretch forming, spinning and non conventional forming
7. Manufacture of structural parts from tubes, bars and shapes
8. Extrusion and forging
9. Manufacture of composite structures
10.Manufacture of composite structure
11.Manufacture of sandwich structures
12.Riveting, rivets - types and materials
13.Riveting methods, joint damages

Exercise

11 hod., compulsory

Teacher / Lecturer

Syllabus

1. Heat treatment of aircraft component
2. Heat treatment of aircraft component
3. Optimisation of steel heat treatment
4. Formability of aircraft metal materials
5. Manufacture of component by bending
6. Elastoforming - technological technique
7. Elastoforming - technological technique
8. Forming limits of bars and tubes
9. Aluminium die forging
10.Machining and forming of sandwich panel
11.Design of rivet joint