PERSONAL DETAILS:
OBJECTIVE:
Looking for an Organization, which provides an atmosphere of freedom, flexibility
and a culture that encourages innovation in the field of Design and Production
Engineering
AREA OF INTERESTS
• Production, Assembly, Repair and Overhaul
• Design
EDUCATION QUALIFICATION:
2012- JULY B.Tech In AERONAUTICAL ENGINEERING from
C M ENGINEERING COLLEGE, (JNTUH). Secured 61.06%.
2008- APRIL SRI CHATINAYA JUNIOR COLLEGE, Vijayawada. Secured 62.4%.
2006- MARCH SECONDARY SCHOOL CERTIFICATE (SSC) from Montessori
English Medium High School, Yellandu. Secured 63.83 %.
ACADEMIC PROJECT:
1. FABRICATION AND TESTING OF SENCOND STAGE OF A MULTI STAGE SOLID
ROCKET WITH PAYLOAD RECOVERY
Description:
Building successful model rocket is a step by step process with several
different faces. Using design sample we can construct a model multi stage
rockets which consist of couple of stages that has to be fabricated by means
of using different materials. The building of a rocket continues to have a
major task of payload recovery. After the sustainer stage of solid rocket, has
fired. It requires high sophisticated techniques through which the rockets
sustainer stage would deploy the payload at a certain height and the
parachute will be deployed on to it to recover the payload.
VAJJA PAVAN KUMAR Page 1 of 3
VAJJA PAVAN KUMAR
Permanent Address:
5-7, VAJJONIGUDEM,
VIA-CHINTONICLAKA,
TEKULLAPALLY(MANDAL),
KHAMMAM(DISTRICT),
TELANGANA
Date of Birth: 13TH
AUGUST 1991
Phone No :+91-9502643088
e-mail : vpavankumar.28@gmail.com
Experience: 17-NOVEMBER- 2012 to 16-NOVEMBER 2013
2. DEESIGN OF LUNAR LANDING GEAR
Software: UG NX-5.0
Description:
We proposed a method of design of lunar landing gear which is only
suitable for preliminary design, particularly when the design have a clear
conception of the dimensions or the detailed layout of the landing gear
structure. The conceptual design of the landing gear is designed and
optimized theoretically with rigorous structural analysis. The design is
developed using a command language NX-5.0. The results are compared
with the early lunar landing gear module Apollo11 and the advantages are
pointed out.
JOB PROFILE:
RESPONSIBILITIES CARRIED OUT:
• Tip clearance for H.P and L.P Compressor Blades through DTI check.
• Concentricity (C.C) checks for both L.P and H.P Stator Vanes.
• W-Dimension and D-Dimension for L.P and H.P Turbine.
• Mass Moment and Segregation of all L.P and H.P Compressor and Turbine
blades.
• Concentricity check for L.P and H.P N.G.V’S (Nozzle Guide Vanes)
• All the Rotor bodies in the engine are carried into Balancing for Vibration
check i.e. Mo1, Mo4, Mo6, Mo8, Stub Shaft and L.P shaft.
• Flow check, Spacer selection and Back Clash checks are done during the
Assembly of Gear Box.
• Complete Assembly of Adour Mk811, 804E Engines.
• Boroscopic checks in Hot end and Cold end section of engine
• Spacer selection for L.P and H.P N.G.V’S, is to adjust the clearance between
the rotor and stator parts, before Assembly of complete engine.
• An Overall check is done before the Dispatch of every Engine.
VAJJA PAVAN KUMAR Page 2 of 3
EXPERIENCE:
Organization Designation Duration
ADOUR ASSEMBLY MK811, 804E,
ENGINE DIVISION H.A.L,
BANGALORE COMPLEX.
GRADUATE
APPRENTICE
17/11/2012 –
16/11/2013
• 1 Year of Experience in Hindustan Aeronautics Limited as Graduate Trainee.
• Proficiency in Assembly Adour Mk 811, 804E Engines.
• Sound Knowledge of Technical Documentation.
• Complete Sub-Assembly of High Pressure Compressor (Mo4). Low Pressure
Compressor (Mo1), High and Low Pressure Turbines (Mo6 and Mo8), Gear Box
(Mo10), Oil Tank (Mo11), High and Low Pressure N.G.V (Mo5 and Mo7),Jet Pipe.
• Complete Assembly of Adour Mk811, 804E Engines.
• Involved in Quality and Inspection by shop support during Sub-Assembly of
parts and also during assembly of the Engines. The snags were cleared in the
minimum possible time so as to facilitate faster release of the Engine.
• Preparation of Isometric views, Exploded views for Technical Manuals as per
ATA-100 standards.
TECHNICAL SKILLS:
Operating Systems MS-DOS, Windows 8,7,XP
Languages C
CAD PRO-E, UNIGRAPHICS NX 5.0,7.5
Authoring Tools MS Word, PowerPoint, Excel.
PERSONAL SKILLS
• Strong Analytical, Problem solving, Innovation, Adaptability and Learning
skills
• Good Presentation, Communication & Demonstration skills
• Preparation of lay out for various armaments, for all the seats, furnishing &
sound property
PERSONAL DETAILS
Fathers’ Name : VAJJA VENKATESWARLU.
Mother’s Name : VAJJA SAROJA.
Nationality : Indian.
Passport : K4773544.
Languages Known : English, Telugu, Hindi. Malayalam.
Hobbies : Listening music, cricket, Reading books.
REFERNCE:
1) R.ELLAN 2) M.H.K. BENAKATI
DY.GENERAL MANAGER MANAGER
Adour Assembly and Overhaul Shop Adour Assembly and overhaul shop
Engine Division, HAL (BC) Engine Division
Mob: +91 9731397929 Mob: +91-9945979321
Office: 080-22326347 Office: 080-22326347, 337
DECLARATION
I hereby declare that the above information given by me is true to the best of my
knowledge and belief.
DATE: SIGNATURE
PLACE: HYDERABAD (VAJJA PAVAN KUMAR)
VAJJA PAVAN KUMAR Page 3 of 3

PAVAN

  • 1.
    PERSONAL DETAILS: OBJECTIVE: Looking foran Organization, which provides an atmosphere of freedom, flexibility and a culture that encourages innovation in the field of Design and Production Engineering AREA OF INTERESTS • Production, Assembly, Repair and Overhaul • Design EDUCATION QUALIFICATION: 2012- JULY B.Tech In AERONAUTICAL ENGINEERING from C M ENGINEERING COLLEGE, (JNTUH). Secured 61.06%. 2008- APRIL SRI CHATINAYA JUNIOR COLLEGE, Vijayawada. Secured 62.4%. 2006- MARCH SECONDARY SCHOOL CERTIFICATE (SSC) from Montessori English Medium High School, Yellandu. Secured 63.83 %. ACADEMIC PROJECT: 1. FABRICATION AND TESTING OF SENCOND STAGE OF A MULTI STAGE SOLID ROCKET WITH PAYLOAD RECOVERY Description: Building successful model rocket is a step by step process with several different faces. Using design sample we can construct a model multi stage rockets which consist of couple of stages that has to be fabricated by means of using different materials. The building of a rocket continues to have a major task of payload recovery. After the sustainer stage of solid rocket, has fired. It requires high sophisticated techniques through which the rockets sustainer stage would deploy the payload at a certain height and the parachute will be deployed on to it to recover the payload. VAJJA PAVAN KUMAR Page 1 of 3 VAJJA PAVAN KUMAR Permanent Address: 5-7, VAJJONIGUDEM, VIA-CHINTONICLAKA, TEKULLAPALLY(MANDAL), KHAMMAM(DISTRICT), TELANGANA Date of Birth: 13TH AUGUST 1991 Phone No :+91-9502643088 e-mail : vpavankumar.28@gmail.com Experience: 17-NOVEMBER- 2012 to 16-NOVEMBER 2013
  • 2.
    2. DEESIGN OFLUNAR LANDING GEAR Software: UG NX-5.0 Description: We proposed a method of design of lunar landing gear which is only suitable for preliminary design, particularly when the design have a clear conception of the dimensions or the detailed layout of the landing gear structure. The conceptual design of the landing gear is designed and optimized theoretically with rigorous structural analysis. The design is developed using a command language NX-5.0. The results are compared with the early lunar landing gear module Apollo11 and the advantages are pointed out. JOB PROFILE: RESPONSIBILITIES CARRIED OUT: • Tip clearance for H.P and L.P Compressor Blades through DTI check. • Concentricity (C.C) checks for both L.P and H.P Stator Vanes. • W-Dimension and D-Dimension for L.P and H.P Turbine. • Mass Moment and Segregation of all L.P and H.P Compressor and Turbine blades. • Concentricity check for L.P and H.P N.G.V’S (Nozzle Guide Vanes) • All the Rotor bodies in the engine are carried into Balancing for Vibration check i.e. Mo1, Mo4, Mo6, Mo8, Stub Shaft and L.P shaft. • Flow check, Spacer selection and Back Clash checks are done during the Assembly of Gear Box. • Complete Assembly of Adour Mk811, 804E Engines. • Boroscopic checks in Hot end and Cold end section of engine • Spacer selection for L.P and H.P N.G.V’S, is to adjust the clearance between the rotor and stator parts, before Assembly of complete engine. • An Overall check is done before the Dispatch of every Engine. VAJJA PAVAN KUMAR Page 2 of 3 EXPERIENCE: Organization Designation Duration ADOUR ASSEMBLY MK811, 804E, ENGINE DIVISION H.A.L, BANGALORE COMPLEX. GRADUATE APPRENTICE 17/11/2012 – 16/11/2013 • 1 Year of Experience in Hindustan Aeronautics Limited as Graduate Trainee. • Proficiency in Assembly Adour Mk 811, 804E Engines. • Sound Knowledge of Technical Documentation. • Complete Sub-Assembly of High Pressure Compressor (Mo4). Low Pressure Compressor (Mo1), High and Low Pressure Turbines (Mo6 and Mo8), Gear Box (Mo10), Oil Tank (Mo11), High and Low Pressure N.G.V (Mo5 and Mo7),Jet Pipe. • Complete Assembly of Adour Mk811, 804E Engines. • Involved in Quality and Inspection by shop support during Sub-Assembly of parts and also during assembly of the Engines. The snags were cleared in the minimum possible time so as to facilitate faster release of the Engine. • Preparation of Isometric views, Exploded views for Technical Manuals as per ATA-100 standards.
  • 3.
    TECHNICAL SKILLS: Operating SystemsMS-DOS, Windows 8,7,XP Languages C CAD PRO-E, UNIGRAPHICS NX 5.0,7.5 Authoring Tools MS Word, PowerPoint, Excel. PERSONAL SKILLS • Strong Analytical, Problem solving, Innovation, Adaptability and Learning skills • Good Presentation, Communication & Demonstration skills • Preparation of lay out for various armaments, for all the seats, furnishing & sound property PERSONAL DETAILS Fathers’ Name : VAJJA VENKATESWARLU. Mother’s Name : VAJJA SAROJA. Nationality : Indian. Passport : K4773544. Languages Known : English, Telugu, Hindi. Malayalam. Hobbies : Listening music, cricket, Reading books. REFERNCE: 1) R.ELLAN 2) M.H.K. BENAKATI DY.GENERAL MANAGER MANAGER Adour Assembly and Overhaul Shop Adour Assembly and overhaul shop Engine Division, HAL (BC) Engine Division Mob: +91 9731397929 Mob: +91-9945979321 Office: 080-22326347 Office: 080-22326347, 337 DECLARATION I hereby declare that the above information given by me is true to the best of my knowledge and belief. DATE: SIGNATURE PLACE: HYDERABAD (VAJJA PAVAN KUMAR) VAJJA PAVAN KUMAR Page 3 of 3