Course detail

Aircraft On-Board Systems I

FSI-OPZAcad. year: 2021/2022

Course is focused on building of knowledge in the area of aircraft on-board systems. Attention is given to hydraulic system, pneumatic systems, electric systems, flight control systems, fuel systems, pressurization, heating and air-condition systems, de-icing systems, and fire protection systems.

Language of instruction

Czech

Number of ECTS credits

4

Mode of study

Not applicable.

Learning outcomes of the course unit

Students will gain the basic knowledge and experience of function and construction of aircraft onboard systems. The knowledge is necessary for aircraft designing, service and maintenance.

Prerequisites

Basic knowledge of mathematics and physics. Fundamentals of Electrical engineering.

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 supplemented by practical individual and team work.

Assesment methods and criteria linked to learning outcomes

The course-unit credit requirements: The attendance at exercises is compulsory (80% at the minimum). The exam is written or oral.

Course curriculum

Not applicable.

Work placements

Not applicable.

Aims

Students will learn principles and technologies of the aircraft onboard systems.

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

The attendance at seminars is compulsory (80% at the minimum). The absence (in justifiable cases) can be compensated by personal consultation with the lecturer and working out individually assignments. Individual assignments must be finished and handed in during the course-unit credit week at the latest.

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

Letecké předpisy FAR 23/CS 23, FAR 25/CS 25
I. Moir, A.Seabridge: Design and development of aircraft systems, AIAA, 2004.
E.Langton, C.Clark, M.Hewitt, L.Richards: Aircraft Fuel Systems, John Wiley & Sons, 2009
Moir, I., Seabringe, A.: Aircraft systems, John Wiley & Sons, Ltd, 2008
Akers, A., Gasman, M.: Hydraulic power system analysis,Taylor & Francis Group, LLC, 2006

Recommended reading

Předpisy EASA CS-23, CS-25 (CS)
I. Moir, A. Seabridge: Aircraft Systems, John Wiley & Sons, 2008. (EN)
I. Moir, A.Seabridge: Design and development of aircraft systems, AIAA, 2004. (EN)
E.Langton, C.Clark, M.Hewitt, L.Richards: Aircraft Fuel Systems, John Wiley & Sons, 2009 (EN)

eLearning

Classification of course in study plans

  • Programme N-LKT-P Master's

    specialization STL , 1. year of study, summer semester, compulsory
    specialization TLT , 1. year of study, summer semester, compulsory

Type of course unit

 

Lecture

52 hours, optionally

Teacher / Lecturer

Syllabus

1. Aircraft onboard systems, distribution, purpose, requirements.
2-3. Hydraulic systems.
4-5. Electric systems.
6-7. Flight control systems.
8. Power elements of control systems.
9. Fuel systems.
10. Pneumatic systems.
11. Air conditioning and pressurization.
12. Ice and rain protection.
13. Fire protection.

12. Zdroje elektrické energie a jejich charakteristiky.
13. Conception of power lines, force actuators.

Laboratory exercise

2 hours, compulsory

Teacher / Lecturer

Syllabus

1-2. Modelling and calculations for example aircraft system.

Exercise

11 hours, compulsory

Teacher / Lecturer

Syllabus

1. Aircraft onboard systems, distribution, purpose, requirements.
2-3. Hydraulic systems.
4-5. Electric systems.
6-7. Flight control systems.
8. Power elements of control systems.
9. Fuel systems.
10. Pneumatic systems.
11. Air conditioning and pressurization.
12. Ice and rain protection.
13. Fire protection.

eLearning