Eskisehir Technical University Info Package Eskisehir Technical University Info Package
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About the Program Educational Objectives Key Learning Outcomes Course Structure Diagram with Credits Field Qualifications Matrix of Course& Program Qualifications Matrix of Program Outcomes&Field Qualifications
  • Faculty of Aeronautics and Astronautics
  • Department of Avionics
  • Course Structure Diagram with Credits
  • Aircraft Instrument Systems I
  • Description
  • Description
  • Learning Outcomes
  • Course's Contribution to Prog.
  • Learning Outcomes & Program Qualifications
  • ECTS Credit Load

Course Introduction Information

Code - Course Title HEE453 - Aircraft Instrument Systems I
Course Type Required Courses
Language of Instruction Türkçe
Laboratory + Practice 2+0
ECTS 3.0
Course Instructor(s) ÖĞRETİM GÖREVLİSİ DOKTOR NEVZET KAYA, ÖĞRETİM GÖREVLİSİ DOKTOR NEVZET KAYA, ÖĞRETİM GÖREVLİSİ DOKTOR NEVZET KAYA
Mode of Delivery The mode of delivery of this course is face-to-face.
Prerequisites There is no prerequisite or co-requisite for this course.
Courses Recomended It is suggested for students to take HEE318 Basic Electronics III course/courses.
Required or Recommended Resources
Recommended Reading List TTS, FAA Books
Assessment methods and criteria 1 Midterm, 1 Final Exam
Work Placement None
Sustainability Development Goals

Content

Weeks Topics
Week - 1 EN: EN: Aircraft Indicating Systems – General: Variable resistance systems, DC selsyn, Magnesyn
Week - 2 EN: Syncrhos: Torque syncrho, Control transformer, Differential sysncrho; LVDT, RVDT.
Week - 3 Pressure Measurement Methods: Pressure definitions; Mechanical pressure sensors: diaphragm, capsule, aneroid capsule, bourdon tube, bellow; Electrical sensors and systems: straingauge, piezo-electrical sensor, pressure measurement by varying vibration frequency.
Week - 4 Temperature Measurement Principles and Instruments: Mechanical principles: liquid expansion, gas pressure, bimetal strip; Electrical principles: PTC and NTC temperature dependent resistors, temperature sensing bulb, ratiometer circuits, Wheatstone Bridge circuits, thermocouples, CHT and EGT measurement.
Week - 5 Fuel Quantity Indication Systems: Mechanical indicators: direct reading tubes, float and magnet; DC electrical indicators: float and ratiometer, magnetic float and reed switches; Capacitive indicators: capacitors, parameters determining electrical capacitance, measuring circuits, calibration for temperature and dielectricity changes; Analogue and digital cockpit indications; Fuel Flow Indication Systems: Transmitters types: vane, turbine, impeller, differential pressure.
Week - 6 Angle of Attack and Stall Warning Systems: Stall definition, measurement, display, aileron type sensor, pressure probe, cockpit displays; Effect of angle of attack on stall, stall warning systems: whistle, aileron and microswitch, stall strip; Engine Vibration Measurement and Display: operating principle, cockpit display.
Week - 7 Gyroscopic Principles: Rigidity, precession, degrees of freedom; Basic gyro elements: rotor and gimbals; Electrical and air driven rotors; Gyro types: vertical gyro, directional gyro, rate gyro, rate integrating gyro; Apparent drift and topple.
Week - 8 Attitude Indicator (Artificial Horizon): Description, use and operating principles of the instrument; Rotor, gimbals, horizon bar, indicator, pitch and roll indication; Gyro erection: with balls, pendulous vanes, levelling switches and torque motors; Remote Artificial Horizon; Acceleration and turning errors.
Week - 9 Directional Gyro: Description, use and operating principles of the instrument; Rotor, gimbals, horizon bar, indicator, old style (compass type) and vertical card heading indication; Slaving of directional gyro (automatic and manual) ; Gyro Wander: Real wander, apparent wander, correction with latitude nut, transport drift.
Week - 10 Rate Gyro: Description, use and principles of operation; Rotor and gimbal; Turn and slip indication. Turn Coordinator Indicator: Description, use and principles of operation; Turn coordination indication, Gyro Powering Systems: Electric motors, pneumatic systems, comparison of electrical and air driven gyros.
Week - 11 General Magnetism Concepts: source of magnetism, magnetic forces and moments; Earth’s Magnetic Field: poles, inclination, variation.
Week - 12 Magnetic Compass: Elements, indication principle, requirements; Compass errors: acceleration and turning errors, reading errors.
Week - 13 Gyro Compass (Slaved Gyro): Elements, principle of operation, light aircraft gro-compass systems, MD-80 compass system, manual synchronization, remote compensator, new technology.
Week - 14 Aircraft Magnetism: Sources of magnetism in aircraft, hard and soft iron magnetism, components of aircraft magnetism; Compass calibration procedure: Finding the A, B, and C coefficients, preparing the compass correction table, EASA limits.

Learning Activities and Teaching Methods

  • Teaching Methods
  • Lecture
  • Discussion
  • Question & Answer
  • Competences
  • Rational
  • Effective use of Turkish
  • Problem solving
  • Concern for quality
  • Information Management

Assessment Methods

Assessment Method and Passing Requirements
Quamtity Percentage (%)
1.Midterm Exam 1 40
Final Exam 1 60
Toplam (%) 100
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