Technical Service engineer

CURRICULUM VITAE

J. GOPI SAI CHANDU

Mobile: +91-984*******

Mail ID: ac92va@r.postjobfree.com

CAREER OBJECTIVE:

To associate with a progressive organization that gives me the scope to apply my knowledge and involve myself as a part of the team that dynamically works towards the growth of the organization. PROFILE SUMMARY:

Good knowledge of having conducted training of 3D Models, 2D Drafting, Assemblies in the CAD packages like Solid Edge, Unigraphics NX, Auto cad, Solid Works.

Good knowledge in ANSYS (Structural and Thermal).

Basic knowledge in GD&T.

Expertise in Microsoft office (Word, Excel & Power point).

Always a keen learner in technical areas of capabilities dedicated and committed towards my work.

Willingness to take responsibilities to achieve the targets within the scheduled time.

Flexible and adapt quickly to the new working environment.

Self-motivated and hard working.

PROFESSIONAL SUMMARY:

Working as a Design/CBT Trainer in Talentedge for APSSDC-SIEMENS Project from Jan- 2019 to till date.

EDUCATION QUALIFICATION:

2018

B. Tech in Mechanical Engineering from V.R. Siddhartha Engineering college, Vijayawada, A.P, affiliated to JNTU Kakinada. Secured 8.3 CGPA. 2014 Intermediate Education from Narayana Junior College, Vijayawada, A.P., Secured 95.6%. 2012 S.S.C from Subhodaya E.M. High School, Vijayawada, A.P. Secured 9.5GPA. SKILL SET:

CAD Tools : Solid Edge, NX 10, Solid Works, Auto CAD CAE Tool : ANSYS (Structural and Thermal)

TRAININGS ATTENDED:

Underwent training on UNIGRAPHICS and Solid works in Aadim Cadd Technologies, Hyderabad for a period of 3 months.

A 2week Internship in “RASHTRIYA ISPAT NIGAM LIMITED” Vishakhapatnam Steel Plant Technical Training Institute in the department of “Coke Ovens & Coal Chemical Plant”.

A 4week Internship in “SOUTH CENTRAL RAILWAY WOMEN`S WELFARE ORGANISATION”, Vijayawada in the department of “Mechanical Engineering”. ACADEMIC PROJECT:

THERMO STRUCTURAL ANALYSIS OF ROCKET NOZZLE USING FEM. The objectives of project work:

The Rocket Nozzle is made with Steel, composite and Graphite across the wall of nozzle. The high thrust required for the rocket is obtained in expense of combustion of gases which results in severe Thermal Stresses in the materials of the wall due to rapidly varying high temperatures. The non-linearity in material properties and boundary conditions cannot yield theoretical solutions for temperature distribution and stresses inside the wall. So, a detailed Finite Element Analysis is done to predict temperature distribution and Thermal Stresses across the wall of nozzle using ANSYS. The analysis was carried out by numerical simulation.

Tool Used : ANSYS 17.2

PERSONAL DETAILS:

Mother’s name : J. Satya Veni

Date of Birth : 08th November, 1997.

Languages known : Telugu, English

Address : A Block 469, Vambay Colony, Ajith Singh nagar,Vijayawada. Place: Vijayawada Signature

Date: ( J. GOPI SAI CHANDU)

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