Course detail

Computer Aided Design and Manufacturing

FSI-OPPAcad. year: 2015/2016

The course is concerned with the following topics: Complex overview of means and methods of computer aided design, manufacturing and production control of aeroplanes. Methods for more efficient design process from first idea through production preparation to creation of drawing documentation or to direct production using NC machines. 3D modelling theory. Introduction to CAD/CAM systems Unigraphics and Catia.

Language of instruction

Czech

Number of ECTS credits

5

Mode of study

Not applicable.

Guarantor

Ing. Tomáš Urík, Ph.D.

Department

Institute of Aerospace Engineering (LÚ)

Learning outcomes of the course unit

Students acquire skills and knowledge of work at work-stations, they are made familiar with structure design systems using 3D modelling theory. They learn the basics of CATIA V5.

Prerequisites

Basic knowledge of computer geometry. Basic knowledge of any lower CAD system level (AutoCad, Inventory etc.).

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.

Assesment methods and criteria linked to learning outcomes

Graded course-unit requirements: a project must be submitted in a prescribed form and handed in by the deadline, The project assessment is done individually and in accordance with FME BUT rules.

Course curriculum

Not applicable.

Work placements

Not applicable.

Aims

The course objective is to make students familiar with design methods of aircraft structure using computer systems and with valid rules of the aircraft structure design.

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

Lectures and exercises are compulsory, and the attendance (80% at the minimum) is controlled and recorded. The absence (in justifiable cases) can be compensated by personal consultation with the lecturer.

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

D. Raymer: Aircraft Design: A Conceptual Approach.
J. Roskam: Airplane Design Part I - VIII.

Recommended reading

D. Raymer: Aircraft Design: A Conceptual Approach.
elektronický manuál: CATIA V5, (EN)
J. Roskam: Airplane Design Part I - VIII.

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

13 hod., optionally

Teacher / Lecturer

Ing. Jan Šplíchal, Ph.D.

Syllabus

1.Introduction to CAD/CAM methods in design and manufacturing of aeroplanes.
2.Introduction to CAD system CATIA V5.
3.Sketcher, setting of sketcher, main tools.
4.Design of part bodies derived from sketch.
5.Part bodies derived from surfaces. Transform operation (translate, rotation, symmetry, scaling).
6.Direct modelling in modelling area. Creating of basic geometry (point, line, circle, curve, plane, surface).
7.Modeling of surfaces, basic operation (fill, multi-section surface, extrude. etc.). Special surfaces (sphere,cylinder).
8.Operation over surfaces (split, trim, join).
9.Continuity of connected curves and surfaces. Levels of continuity.
10.Freestyle modelling curves and surfaces.
11.Analysis of curves and surfaces. Check of smoothness and continuity of surfaces.
12.Creating of assemblies. Inserting an existing component, relocation of component. Assembly constrains. Analysis of assembly.
13.Generative drafting. Defining of a drawing sheet, inserting of views, dimensioning.

Computer-assisted exercise

39 hod., compulsory

Teacher / Lecturer

Ing. Jan Šplíchal, Ph.D.

Syllabus

1.Introduction to CAD/CAM methods in design and manufacturing of aeroplanes.
2.Creation of a sketch-based part.
3.Creation of a rotary element by rotation of the sketch.
4.Definition of basic geometry of trapezoidal aerodynamically and geometrically twisted wing.
5.Definition of basic geometry of aileron and trailing-edge flap for given wing.
6.Definition of geometry of a wing tip cover.
7.Definition of basic geometry of round front part of a sailplane fuselage.
8.Creation of geometry of a wing-fuselage connection cover.
9.Creation of the assembly of the wing, the aileron and the trailing-edge flap from previously created models.
10.Utilization of previously created assembly to create schematic aileron rod control mechanism.
11.Solution of kinematics of differential ailerons.
12.Creation of front part of a sailplane fuselage with a hinged cabin cover.
13.Creation of glazing of cockpit of transport plane and examine all-round view graph.