V. Kaliyaram
Tel: 91-978*******
Email: *********@*****.***
Experience Summary:
A solution oriented individual with good exposure to the Aerospace and Automotive industry, experienced in successfully handling large projects. Developed long term customer relationships and handled large teams under very challenging conditions with Profit and Loss responsibility.
18 years of relevant experience (Total 26 years) experience in Aerospace, Automotive and general engineering with focus on managing large multi-skilled teams with extensive experience in aero-structural design, Product life cycle Management, Product Development and Design for Manufacturing, Application software development and Customization.
Core Skills:
Experience in Aerospace component design (Machined parts, Sheet metal panels & Concept design)
Fuselage Wing leading edge and Wing trailing edge Ribs, Stringers, Linkages, Frames, Shear Walls and Floors
Assy. Jig Components Skins & Canopy, Main under Carriage Nose under Carriage and Pallet design Plastic & Sheet metal parts
Functional Skills
Aerospace:
Extensive experience in Design of Aircraft Structures, Systems design & Integration.
Experience in creation of conceptual / detail design of Fuselage, empennage, wing to bottom fairing and wing structural components for long range passenger aircraft such as 747-8F,747-8IC and for military combat aircrafts such as LCA and its variants.
Experience in the detail design of interiors such as seating systems, galleys and lav's,emergency equipment installations, escape system installations of commercial airplanes such as 787
Ability to lead, guides, direct and manage complex project schedules.
Has Extensive experience in CATIA V5, CATIA V4, Enovia LCA, Enovia VPM, and Team centre.
Has OEM experience in Design and development of full life cycle of Passenger airplane structural and systems parts like frames, stringers, Stringer clips, Intercostals, Composite brackets, Aluminium brackets, Machined components etc.
Automotive:
Experience in Automotive Structure (BIW), Interiors, Chassis, Die-casting
Drafting and 3D Modeling and assemblies of Interiors and exteriors of the Car and truck
Design and concept development of Power Assisted Steering (PAS), Active Ride Control (ARC), Automotive A/C Fluid Line, different types of connectors, adaptors, flanges, brackets, sockets, tube end form, Transmission system, Engine Valves and valve train and engine supercharger etc
Experience in Geometric Dimensioning & Tolerance (GD&T) Carbon composites, Plastic & Sheet metal parts Value Engineering & Reverse Engineering
Extensive experience in body design & Integration.
Experience in Design Process and NRPD process
Experience in the detail design of interiors such as seating systems,
Knowledge of Automotive design criteria, load criteria, material properties and strength.
Ability to lead, guides, direct and manage complex project schedules.
Has OEM experience in Design and development of full life cycle of a Products..
Coordination with customer managers and the customer partners
Ability to design, develop, coordinate, integrate and document structural design requirements
Ability to provide product definition to concurrent engineering support groups such as systems, stress and production throughout the product development cycle
Skill set
CATIA V4, CATIA V5, Enovia LCA, Enovia VPM, and Team centre.
Qualifications
BE Mechanical, First class, 1994 Bangalore University.
Experience Summary
Working as a Senior Consultant from 2016 onwards independently.
Worked with Sri Mookambika info Solution Pvt Ltd (SMI) as a Program Manager in Chennai from May 2015 to 2016l
Entrepreneur Caprosys Engineering Services, Chennai. (JV with Brick and Byte Innovative Product Pvt. Ltd, Navy Mumbai) From July 2013 to Nov 2014,
Worked with i-Grandee Software Technologies, as a General Manager, New Delhi, during 2008- 2012
Worked as a Project Manager at I-Design Technologies, Chennai, during 2006-2008
Worked as a Project Manager at Enmas Process Technologies Pvt, Ltd. Chennai during 2003-2006.
Worked and involved in the Design and Development of LCA and LCA Navy Aircrafts at ADA (Aeronautical Development Agency) is an autonomous body under the ministry of defence, entrusted with the task of design & development of LCA (Light Combat Aircraft), during 1998-2003
Worked as a Lecture in Jerusalem College of Engineering during 1995-1998
Projects Handled at ADA, Bangalore
1.Digital Prototype Assembly Studies of LCA (Light Combat Aircraft)
Description:
Modelling of Frames, Ribs, Spars, Brackets, Bulkheads and other Aircraft Components at different stations. This has been modelled by using the NMG Surfaces and modelling involves solid &surface modelling. Also on completion of design, it has been sent for NC programming & for realization in Virtual Reality lab
2.Cockpit Design and Modelling of the LCA Trainer Aircraft
Description:
Drafting and modelling of different parts of Trainer Aircraft including shear Walls, Floors, and Windscreen and Canopy Bubbles etc. Drafting and modelling of various parts of Trainer Aircraft. Check for the Interference and Assembly. Models used for stress analysis.
3.Design and Modelling of the Modular structure for MMR (Multi Mode Radar)
Description:
Complete structural design of the MMR, which involves different Floors, Frames, and Brackets etc.
4.FIN Design of the Light Combat Aircraft
Description:
Complete structural design of the FIN, which involves different Torsional box, Nose box Frames, Brackets etc.
5.Digital Mock-up of the LCA Navy Aircraft
Description:
Drafting and modelling of different parts like Front fuselage, Center fuselage, and Rear fuselage of LCA Navy Aircraft including shear walls, Floors, Windscreen, Bulkheads and Canopy etc.
6.Electrical Harness routing of LCA Aircraft
Description
Electrical routing of the entire Aircraft of LCA Aircraft including Main landing gear, wing, Fin, Multimode Radar and Environment Control system.
Projects Handled at Enmas Process Technologies Pvt Ltd, Chennai
1. Digital Mock-Ups (DMU) - Fuselage Construction
Deliverables
Phase1: To create 3D DMU, clash detection and assembly resolution
Phase 2: To create manufacturing 2D drawings for individual parts, main and sub-assemblies
Create 3-D models & Assemblies from the wireframe model
Create complete 2-D manufacturing drawings and also implement the past ECNs into the drawings
Dual dimensioning followed for all drawings
2. 3D Modeling and detail design of Composite airframe structures
Scope: To model Equipment Bay, Air intake bay, Wing and Pressurized fuel tank
Input: Aircraft Numerical Master Geometry (NMG), Modeling standards and Drawing templates
3. Design and Optimization of Aircraft Assembly
Scope: To design of test rigs, Modeling the front fuselage assembly, Optimization of Nacelle Assembly and Optimization of Seat rail attachments
Input: Aircraft Numerical Master Geometry (NMG), Modeling standards and Drawing templates
Projects Handled at I-Design Technologies Pvt Ltd, Chennai
1.Simplifies Component Development of Wing Ribs for Airbus A320
Client: HSM Technologies
Role: 3D-Modelling & Detailing. Quality checking and delivery
Description:
The objective of the project is to extend a simplified approach to develop CATIA V5 parent wing ribs models from the client given CATIA V5 files. The activities stock design, surface extraction, stock split, fillet design, appending lug & pockets, wall thickness check & correction, feature recognition of holes,
2. Automotive Seat back Frame
Role: 3D-Modeling & Detailing, quality checking and delivery
Description:
Our customer required for a new seat back frame design for their Belt-in- Seat System type of Seat assembly which improves comfort and performance of seat belt restraint systems which is mounted on passenger seat instead of vehicle body.
3.Expandable Container Holder for Vehicles
Client: Hyundai Motor India
Role: 3D-Modelling & Detailing, quality checking and delivery
Description:
The objective of the project is to design a container holder which is flexible enough to hold different sized containers in a vehicle. The holder must be able to hold cans of different size and also tapered cups. To accomplish all these purposes a holder is designed that includes a resilient curvilinear wall with overlapping free ends movable toward and away from each other to vary the diameter of container holding opening defined by the wall.
4.Nacelle
Role: 3D-Modelling & Detailing, quality checking and delivery
Description:
Development of Nacelle to cover new combination switch, which is developed for car vehicle. Provision for
Ignition lock is provided in nacelle itself and gives more aesthetic.
Projects Handled at Caprosys Engineering Services, Chennai
1. Wing Box Rib - Surface Modeling
Scope: The scope of this project was to generate CATIA V5 parametric models using NMG
Input: Aircraft Numerical Master Geometry (NMG), Modeling standards and Drawing templates
2. Wing Box Spoiler rib - Surface Modeling
Scope: The scope of this project was to generate CATIA V5 parametric models using NMG
Input Aircraft NMG, Modeling standards and Drawing templates.