Analyse et communication techniques
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1 Durée 4 heures SESSION : TA T Epreuve E2 TECHNOLOGIE (U2) Analyse et communication techniques DOSSIER TECHNIQUE Durée : 4 heures coefficient : 4 DT : Page 1 sur 16
2 SOMMAIRE 1- Présentation du système d étude 2- Identification du spoiler 3- Etude de la réparation composite 4- Etude de la réparation métallique 5- Etude des systèmes Aéronefs Présentation du système d étude Durée : 4 heures coefficient : 4 DT : Page 2 sur 16
3 Identification du spoiler Durée : 4 heures coefficient : 4 DT : Page 3 sur 16
4 Durée : 4 heures coefficient : 4 DT : Page 4 sur 16
5 Etude de la réparation composite Durée : 4 heures coefficient : 4 DT : Page 5 sur 16
6 Durée : 4 heures coefficient : 4 DT : Page 6 sur 16
7 Durée : 4 heures coefficient : 4 DT : Page 7 sur 16
8 Durée : 4 heures coefficient : 4 DT : Page 8 sur 16
9 Durée : 4 heures coefficient : 4 DT : Page 9 sur 16
10 Etude de la réparation métallique Durée : 4 heures coefficient : 4 DT : Page 10 sur 16
11 Durée : 4 heures coefficient : 4 DT : Page 11 sur 16
12 Etude des systèmes Aéronefs Durée : 4 heures coefficient : 4 DT : Page 12 sur 16
13 SPOILER - DESCRIPTION AND OPERATION 1. General Five spoilers numbered 1 thru 5 inboard to outboard are provided on the rear upper surface of each wing. The spoilers are used for: - Roll function - Load Alleviation function (LAF) - Speedbrake function - Ground spoilers function Each spoiler is electrically controled and Hydraulically actuated by an electrohydraulic servocontrol. 2. System Description A-. ROLL FUNCTION The spoilers 2 thru 5 assist the ailerons in roll control. The Roll axis is controlled and monitored by the three SEC s associated with ailerons. The SEC s elaborate the surface deflection orders in manual control mode, mainly from the side stick ; in autopilot mode from FMGES. B-. LOAD ALLEVIATION FUNCTION (LAF) The LAF relieves wing structure loads in turbulence by moving the spoilers 4 and 5 and ailerons symmetrical. The LAF order are added with Roll orders. C-. SPEEDBRAKE FUNCTION The speedbrake function is controlled and monitored by the three SEC s with spoilers 2, 3 and 4. The speedbrake lever controls the position of these spoilers and so is used for the preselection of ground spoilers function. D-. GROUND SPOILERS The ground spoilers function is ensured by all spoilers. The activation of this function is dependent upon : - The function preselection (give by speedbrake lever position) - The two engines at idle - Flight/Ground transition (With Ground and wheel speed information). Durée : 4 heures coefficient : 4 DT : Page 13 sur 16
14 AIRCRAFT MAINTENANCE MANUAL HYDRAULIC POWER Durée : 4 heures coefficient : 4 DT : Page 14 sur 16
15 Durée : 4 heures coefficient : 4 DT : Page 15 sur 16
16 Construction mécanique Symboles de liaison (extrait). Formulaire τmoy = T S Rpg = Reg k τmoy < ou = Rpg τmoy Rpg Rrg k T S contrainte de cisaillement Resistance pratique au cisaillement Résistance à la rupture au cisaillement coefficient de sécurité Effort tranchant Surface cisaillé Durée : 4 heures coefficient : 4 DT : Page 16 sur 16
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