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|Title:||Wear behavior in the tail plane or stabilizer in aircraft using mechanical analysis at extreme pressure in finite element modal||Authors:||Chamas, Mohannad Adel
Saba, Raymond Elias
Sadek, Maria Georges
The ball screw actuator of the airplane is subjected to wear which can greatly affect flight conditions. Different materials were used for testing, subjected to different efficient coatings, while the second technique was by means of lubrication. Finally, the techniques were contrasted to determine whether the first, second or both lead to the highest efficiency, with the aim being a longer lifespan and perhaps a better operational cost. A finite element analysis has been made on different balls of different materials while coated and uncoated. After inspecting the results of the relevant studies in the literature, several conclusions were arrived to that would help reduce wear, such as an optimized return path, better choice of material, better coating, and appropriate lubricant.
Includes bibliographical references (p.81-83).
Supervised by Dr. Gabi Nehme.
|URI:||https://scholarhub.balamand.edu.lb/handle/uob/3753||Rights:||This object is protected by copyright, and is made available here for research and educational purposes. Permission to reuse, publish, or reproduce the object beyond the personal and educational use exceptions must be obtained from the copyright holder||Ezproxy URL:||Link to full text||Type:||Project|
|Appears in Collections:||UOB Theses and Projects|
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