Sample Template Example of Beautiful Excellent Curriculum Vitae / CV Format with Career Objective, Job Profile & 5 Years Work Experience for Aeronautical Engineering Fresher Students & Experienced Professionals in Word / Doc / Pdf Free Download
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CURRICULUM
VITAE
A.VINEETA
309, 4th Main,
Jeevan
Bheema Nagar,
New Thippasandra
Post,
Bangalore-560075.
E-mail
ID : vineeta@gmail.com
Contact No : 09876543210
CAREER OBJECTIVE
To optimize
my personal skill, knowledge and experience to facilitate the growth and
development of self and the organization. Seeking Challenging Opportunities
that will utilize my background & experience & to grow in a
professionally managed organization where my talents, experience &
knowledge would be put in the best
EXPERIENCE
Ø Graduate Apprenticeship Trainee at HINDUSTAN AERONAUTICS LIMITED, BANGALORE
Project : LCH
(Light Combat Helicopter) - Flight Controls (RWRDC)
Period : Nov 2012 – Present
Environment : Component Design using UNIGRAPHICS
NX7.5
Description :
Ø 3D
Modelling of Control Rods, Bell Crank Levers, Link Rods, Cyclic Stick &
other Flight Controls Parts in LUH.
Ø
Surface
modelling of Covers, Bellow Covers.
Ø
Involved
in parametric modelling, assembling & drafting of various Flight Controls
Systems.
Project : GTSU
– Design Department (AERDC)
Period : July 2013 – Nov 2013
Environment : Component Design using UNIGRAPHICS
NX7.5, NX8, CATIA V5.
Description :
Ø
Modeling
of gas turbine engine part like impeller, starter unit parts & Components
such as Front-gear box assembly, Air intake casing, Back plate assembly under
the project of GTSU – 110.
Ø
Preparing
process sheets for various components in the projects of GTSU – 110 for the
manufacturing.
Ø
Creating
Journal Coding’s for the models
SOFTWARE
TOOLS
Ø CAD TOOLS : - UNIGRAPHICS
NX 7.5, NX 8, CATIA V5,
Auto Cad
2012
AERA OF INTEREST
Ø Power Plant
Ø Flight Mechanics
Ø Designing and Modeling
ACADAMIC PROJECT
DETAILS
TITLE : DESIGN AND ANALYSIS OF HOVERBIKE
DURATION : JULY 2011 – APRIL 2012
DESCRIPTION :
The Hover bike is the fusion
concept of hovercraft and normal 4-stroke engine , two ducted fans are used for
both forward and backward motion as well as for vertical take-off and landing,
the blade angle used for ducted fans are 140 to produce high thrust,
Carbon fiber with Kevlar reinforcement and foam core material used for
high structural strength, the
structural analysis with varying payloads as 60kg,70kg and 150kg by applying
these load we find a 75% ,50% reduction of the stress, strain and total
deformation is obtained in the modified design. This gives the high structural efficiency of the bike.
EDUCATIONAL
QUALIFICATION
Ø B.E AERONAUTICAL ENGINEERING 2012
(MECHANICAL DEPARTMENT)
Nehru Institute of Engineering and
Technology,
Coimbatore. Percentage: 83.7%
Ø HIGHER SECONDARY [XII MATRICULATION
BOARD] 2008
Don Bosco
Matriculation Higher Secondary School,
Thanjavur. Percentage: 79.67%
Ø S.S.L.C [X MATRICULATION BOARD] 2006
Don Bosco
Matriculation Higher Secondary School,
Thanjavur. Percentage: 72.55%
INDUSTRIAL VISIT
Ø Two days visit in ISRO (Indian Space Research Organization), Bangalore.
From 10th
– 12th April 2010
WORKSHOP
Ø Work shop
on “Advance in gas turbine engine”
by DRDO From 02 MAY to 06 MAY 2011.
Ø Two days’ workshop on “Aero
modeling workshop” on September 22&23, 2011. Organized by Barola
Aero Sports.
PERSONAL
DETAILS
Fathers Name :
Anand.R
Date of Birth :
19/08/1992
Gender :
Female
Nationality :
Indian
Marital Status : Single
Language :
English (R/W/S), Tamil (R/W/S)
Address : 12/Selliyamman Kovil Street,
Karandhai, Thanjavur,
Tamil Nadu-613002.
DECLARATION
I hereby declare that
the above mentioned information is correct to the best of my knowledge.
Yours faithfully,
(VINEETA.
A)
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