Computer Aided Aircraft Drawing detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AEL48), and for exam duration, Teaching Hr/week, Practical Hr/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below.
For all other aero 4th sem syllabus for be 2017 scheme vtu you can visit Aero 4th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for computer aided aircraft drawing is as follows.
Course Objectives:
This course will enable students to
- Understand and interpret drawings of machine and aircraft components
- Prepare assembly drawings either manually or by using standard CAD packages.
- Familiarize with standard components and their assembly of an aircraft.
Part – A:
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Part – B:
- Thread Forms: Thread terminology, sectional views of threads. ISO Metric (Internal & External) BSW (Internal & External) square and Acme. Sellers thread, American Standard thread.
- Fasteners: Hexagonal headed bolt and nut with washer (assembly), square headed bolt and nut with washer (assembly) simple assembly using stud bolts with nut and lock nut. Flanged nut, slotted nut, taper and split pin for locking, counter sunk head screw, grub screw, Allen screw.
- Keys & Joints: Parallel key, Taper key, Feather key, Gibhead key and Woodruff key
- Riveted Joints: Single and double riveted lap joints, butt joints with single/double cover straps (Chain and Zigzag, using snap head rivets). Cotter joint (socket and spigot), knuckle joint (pin joint) for two rods.
- Couplings: Split Muff coupling, protected type flanged coupling, pin (bush) type flexible coupling, Oldham’s coupling and universal coupling (Hooks’ Joint.
Part – C:
- Design of propeller and hub assembly
- Design of wing assembly
- Design of fuselage assembly
- Design of Engine Mounts
- Design of main rotor blade assembly of helicopter
- Design of UAV assembly
- Design of Landing Gear Assembly
Course Outcomes:
For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.
Conduct of Practical Examinations:
Internal Assessment: 20 Marks
Sketches shall be in sketch books and drawing shall be drawn through the use of software on A3/A4 sheets. Sketch book and all the drawing printouts shall be submitted.
Scheme of Evaluation for Internal Assessment (20 Marks)
(a. Class work (Sketching and Computer Aided Aircraft Drawing printouts in A4/A3 size sheets): 10Marks.
(b. Internal Assessment test in the same pattern as that of the main examination (Better of the two Tests): 10 marks.
Scheme of Examination:
Two questions are to be set from each Part.A, Part.B and Part.C.
Student has to answer one question each from Part.A and Part.B for 15 marks each and one question from Part.C for 50 marks.
i.e.
Part.A 1 x 15 = 15 Marks
Part.B 1 x 15 = 15 Marks
Part.C 1 x 50 = 50 Marks
Total = 80 Marks
INSTRUCTION FOR COMPUTER AIDED AIRCRAFT DRAWING EXAMINATION:
- There is no restriction of timing for sketching/ computerization of solutions. The total duration is 3 hours.
- It is desirable to do sketching of all the solutions before computerization.
- Drawing instruments may be used for sketching.
- For Part.A and Part.B 2D drafting environment should be used.
- For Part.C 3D part environment should be used for parts assembly drawing and extract 2D views.
Graduate Attributes (as per NBA):
- Engineering Knowledge.
- Problem Analysis.
- Design / development of solutions (partly)
- Interpretation of data.
For detail syllabus of all other subjects of BE Aero, 2017 scheme do visit Aero 4th Sem syllabus for 2017 scheme.
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