School / Prep
ENSPIMA
Internal code
AP9SAPSA
Description
Objectives
The general objective of this module is to apply the skills acquired in aeronautical mechanics and structures to a concrete application involving the structure and mechanisms of an aircraft wing.
Integrate a research approach
Skills acquired
Be able to apply multidisciplinary skills to a physical model
Be able to present methodological and experimental results orally
Be able to work in a team.
Skills acquired at independent mastery level
Mobilize a wide range of fundamental and technical sciences related to aeronautical and space mechanical systems, and have the associated capacity for analysis and synthesis
Design and dimension mechanical systems
Choose and implement the relevant analysis and characterization methods for mechanical systems
Communicate and work as part of a team Manage and lead a work unit or project group
Integrate into a professional environment in France or abroad Communicate orally and in writing in English
Skills acquired at the supervised master's level
Design, dimension, implement and test a metallic or composite repair/modification
Have a global systemic approach to mechanical systems Reason in a context of international regulatory constraints
Anticipate, decide in a situation of uncertainty Be results-oriented (costs, deadlines, quality) and customer-oriented
Evaluate one's own skills and steer one's career path
Skills acquired - Level : In progress
Integrate financial, legal and contractual aspects into engineering practice
Teaching hours
- PRJProject40h
Mandatory prerequisites
All specialization courses
Syllabus
Contents
Based on an aeronautical system, students will:
Carry out bibliographical research
Produce a CAD model and FE simulations of an aeronautical part
Carry out experimental tests on material samples
Propose a manufacturing range for the part
Design or modify the aeronautical system studied
Optimize certain parts of the system
Students are coached to develop their commitment and co-construct performance.
Teaching method
Projects are organized in groups of three students. Each group is provided with physical models of structural elements, enabling them to validate their results experimentally. The project concludes with a presentation by each group, describing the methodology employed and the results obtained.
Further information
Aeronautical structures
Assessment of knowledge
Initial assessment / Main session - Tests
Type of assessment | Type of test | Duration (in minutes) | Number of tests | Test coefficient | Eliminatory mark in the test | Remarks |
---|---|---|---|---|---|---|
Project | Continuous control | 1 |