ata chapter 22 & chapter 27
DESCRIPTION
This slides is a preview on the introduction of Air Transport Association specifically on Chapter 22 - Auto Flight and Chapter 27 - Flight ControlsTRANSCRIPT
![Page 1: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/1.jpg)
EAS3713:AEROSPACE VEHICLE
DESIGN
Presented by: ODYSSEY
Muhammad Izzuddin Bin Abd Aziz 167349
Ahmad Mustafa Bin Rayney Azmi 168443
Nurnabilah Binti Sha’ari 168593
Saifudin Bin Sajadi 169994
Ng Wi Tet 170208
Nurul Hamizah Binti Zainal Abidin 170656
Mohd Azizi Bin Ab Malek 170837
Omid Shahabadi 171612
ATA CHAPTERS 22 & 27
![Page 2: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/2.jpg)
PRESENTATION CONTENTS Working Principle General Schematic
Main Components Functions of Every Component Interrelationships
![Page 3: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/3.jpg)
CHAPTER 22: AUTO FLIGHT Autopilot Speed-Attitude Correction Auto Throttle System Monitor Aerodynamic Load Alleviating
![Page 4: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/4.jpg)
WORKING PRINCIPLE Based on a closed-loop feedback
mechanism
![Page 5: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/5.jpg)
GENERAL SCHEMATIC
![Page 6: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/6.jpg)
FUNCTIONS OF COMPONENTS Autopilot
Enable flying with minimal ‘hands on’ Speed-Attitude Correction
Rectify attitude and speed Auto Throttle
Maintain thrust System Monitor
Provide display of system Aerodynamic Load Alleviating
Nullify gusts, reduce wing bending moments
![Page 7: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/7.jpg)
CHAPTER 27: FLIGHT CONTROLS Aileron & Tab Rudder & Tab Elevator & Tab Horizontal Stabilizer Flaps Spoiler, Drag Devices, Fairings Gust Lock & Damper Lift Augmenting
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WORKING PRINCIPLE Similar as lift on a wing Create difference in pressure
Increase streamlining to reduce drag
Lock control surfaces when parked Damp disturbances
![Page 9: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/9.jpg)
GENERAL SCHEMATIC
A319/ A320/ A321
![Page 10: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/10.jpg)
FUNCTIONS OF COMPONENTS Aileron & Tab
Roll control Rudder & Tab
Yaw control Elevator & Tab
Pitch control Horizontal Stabilizer
Provide horizontal stability, prevent pitching up and down
![Page 11: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/11.jpg)
FUNCTIONS OF COMPONENTS Flaps
Extension of wing, can reduce speed and shorten takeoff and landing distance Spoiler, Drag Devices, Fairings
Reduce lift & Increase drag, Increase streamline to reduce drag Gust Lock & Damper
Lock control surfaces, damp disturbances Lift Augmenting
Increase lift generated
![Page 12: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/12.jpg)
INTERRELATIONSHIPS 27 can be viewed as the mechanism 22 integrates them and allow
automation
![Page 13: ATA Chapter 22 & Chapter 27](https://reader034.vdocuments.site/reader034/viewer/2022050702/563db80c550346aa9a900ab6/html5/thumbnails/13.jpg)
Spoilers Fairings