MECHANICAL PROJECTS


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2018-2019 LATEST AERONAUTICAL BASED PROJECTS

  • This category consists of Aeronautical 2018-2019 project list with abstract/synopsis.Here we provide latest collection of topics developed using latest designs and concepts. Using present Technology, an effort has been made to develop and provide latest features for human ease, features like automatic brakes, safety features, de-localised controls using Smart Phones and many more with latest automobile concepts for final year Diploma, Engineering students.

IEEE 2018-2019 Aeronautical project list for BE/Diploma/M.TECH in Bangalore.

TAE001
DEVELOPMENT OF BIRD DETECTION AND DEFLECTION SYSTEM IN AIRCRAFT

ABSTRACT Birds cause a lot of trouble in airports especially during take-off and landing of aircrafts. Incidence of the bird hitting the aircraft is called bird strike. A small bird, if gets struck inside the engine can cause serious consequences like losing the entire aircraft, passengers and its crew. It can sometimes damage the aircraft to major extent as shown in the figure below. Hence it is very important to detect any presence of birds within the range specified. If birds are detected, they have to be deflected so that they will not come into the path of the aircraft. One can use water jet as a deflector system since it is a harmless way to deflect the birds. The detection system will scan the range specified and will send a signal if any object is present within the region. Upon detection, the detector system will raise an alarm in the form of a signal. Once the signal is raised from the detector system, the location estimation system will estimate the position of the object relative to the aircraft. This is done so that the water jet can be turned on to reach the location of the object to deflect it away. Contact:
+91-9008169572
 +91-9008001602
 080-40969981

TAE002
DEVELOPMENT OF JET ENGINE

ABSTRACTThis project deals with researching, designing and building jet-engines. A simple turbojet engine was designed and construction was begun. The design was made by studying the work done by industry and researchers over the course of the history of jet engines. The methods were then discussed and chosen in a way that would simplify the design work as well as the construction of the engine. The goal was to create a self-sustaining combustion within the engine. The design settled upon consists of a radial compressor, an annular combustion chamber and an axial turbine. Since the compressor would have been the most difficult part to machine the decision was made early on to use the compressor from a turbocharger out of an automotive engine. Upon further study it was discovered that the characteristics of this compressor was not compatible with the rest of the design, as the compressor was made for an RPM range outside of what we could achieve and the compression ratio was too low. Most of the rest of the engine had already been built, and there was not enough time to design and build another compressor so work was aborted on the engine.Contact:
+91-9008169572
 +91-9008001602
 080-40969981

TAE003
RF BASED AIRCRAFT BLACK BOX

ABSTRACT Now a day’s black box is available in aircraft for storing the all activity of the air craft. Here we design the black box which will detect the fault and automatically inform to control room through RF TX. We use RF TX and RF RX for communication. It has the following feature: 1 Automatically senses the engine vibration; an announcement is displayed in the base station in case of any sort of vibration in engine. 2 To avoid the collision. 3 Automatically senses the engine temperature, an announcement is displayed in the base station in case of abandon rise in engine temperature. Contact:
+91-9008169572
 +91-9008001602
 080-40969981

TAE004
PNEUMATIC OVERWING EXIT SYSTEM

ABSTRACT We are fabricating a pneumatic operated emergency overwing exit system in aircrafts, which uses pneumatic cylinder to slide down the roller when the magnetic switch used in doors repels each other. The magnetic switches are connected to a microcontroller which in turn activated the relay. Once the relay is activated the solenoid valve connected to the relay will allow the air from compressor to pass through the pneumatic cylinder and the roller will slide down immediately for the passengers to exit the aircraft at emergency sit0uations.Contact:
+91-9008169572
 +91-9008001602
 080-40969981

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