07-10-2010, 04:00 PM
Turbojet Engines.ppt (Size: 2.85 MB / Downloads: 1,842)
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TURBOJET ENGINES
A seminar report is submitted
in partial fulfillment of the requirements
for the final year (8th semester) award of the Degree
of Bachelor of Engineering in
Mechanical Engineering
BY
GAJANAN C AVANTKAR
Under the Guidance of
Prof. M.S.PATIL
DEPARTMENT OF MECHANICAL ENGINEERING
K.L.S SOCIETY’S
GOGTE INSTITUTE OF TECHNOLOGY
BELGAUM-590008
ABSTRACT:
In today’s world it is possible to travel to any part of the world within short span of time
using air transport. Earlier aviation industry was not as well developed as today’; as they were
using Rotary Piston IC engines which limited the travel speed and distance; moreover the fuel
consumption of these engines was high leading to increased cost of transport.
A significant breakthrough in aviation industry took place with the advent of turbojet
engines which were Rotary -Reaction Turbine Engines which were much efficient than Rotary
piston engines and all other engines such as turbofan, turboprop, and turboshaft engines were
developed as improvement over turbojet engines.
This paper reviews the introduction to primary components of turbojet engines, principle
of operation, Newton’s third law of motion governing turbojet propulsion, Brayton cycle which
is governing thermodynamic cycle for open cycle gas turbines, vehicles currently employing
turbojet engines few advantages, disadvantages, applications & key differences.
Key