Course detail

Reliability and Maintainability of Aircraft

FSI-OSD-AAcad. year: 2022/2023

The course offers a general overview on modern methods of safety and reliability assessment with special attention on an aircraft and aircraft systems. This includes reliability analyses, calculations, estimates and test methods. Emphasis is put on the main properties of dependability: reliability, availability and safety.

Language of instruction

English

Number of ECTS credits

4

Mode of study

Not applicable.

Offered to foreign students

The home faculty only

Learning outcomes of the course unit

The course provides students with basic knowledge of the area of dependability (reliability and maintainability) of aircraft. This includes information about modern methods and procedures for safety assessment (reliability analyses, etc) and information about international standards and airworthiness requirements.

Prerequisites

Students are expected to have mastered the basics in statistics and probability calculations and they have at least basic knowledge of aerospace engineering (structure and systems of an aircraft).

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

To meet requirements for the course-unit credit award it is necessary to attend 80% of compulsory seminars, to hand in student works and meet requirements of 2 written tests.

Course curriculum

Not applicable.

Work placements

Not applicable.

Aims

The main course objective is to give students an introduction to procedures and methods used to ensure safety and dependability of an aircraft (and other industrial products).

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

The attendance at seminars is compulsory. In case of justified absence, the seminar may be compensated by an individual assignment.

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

Patrick D.T..CONNOR.:: Practical Reliability Engineering, , , 0
Villemeur,A.:: Reliability,Availability,Maintainlability and Safety Assessment, , 0

Recommended reading

Holub,R.:: Základy spolehlivosti technických systémů, skripta S-1586, , 0
Holub,R.:: Zkoušky spolehlivosti, skripta S-1590, , 0
Holub,R.;Vintr,Z.: Spolehlivost letadlové techniky (elektronická učebnice), skripta, VUT-FSI, Brno, 2001, 233 str.

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Classification of course in study plans

  • Programme N-AST-A Master's 2 year of study, winter semester, compulsory
  • Programme N-ENG-Z Master's 1 year of study, winter semester, elective
  • Programme MPA-SAP Master's 2 year of study, winter semester, compulsory

  • Programme LLE Lifelong learning

    branch CZV , 1 year of study, winter semester, compulsory

Type of course unit

 

Lecture

26 hod., optionally

Teacher / Lecturer

Syllabus

1.Concept of dependability (reliability and maintainability) assurance in aerospace engineering.
2.Terms and definitions in dependability.
3.Mathematics used in dependability. Basics of systems dependability.
4.Inherent dependability of products. Dependability (with focus on reliability) of non-repaired systems.
5.FMEA/FMECA.
6.Reliability Block Diagrams (RBD).
7.Fault Tree Analysis (FTA).
8.Dependability of repaired systems. State Space Method (SSM).
9.Reliability analyses and airworthiness certification.
10.Software reliability. Introduction to the reliability of space devices.
11.Evaluation of reliability tests and operational data.
12.Evaluation of reliability tests and operational data.
13. Software tools in dependability.

Exercise

13 hod., compulsory

Teacher / Lecturer

Syllabus

1-2.Application of probability principles for the purpose of component reliability calculation.
3-5.Inherent reliability calculations for complex systems.
6.Application of FMEA/FMECA.
7-8.Application of reliability block diagrams (RBD) and fault trees (FTA).
9-11.Certification analysis of a representative aircraft system.
12-13.Evaluation of reliability tests and operational data.

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