Dayanand_Patil_CV_Support

E-Mail:[email protected] DAYANAND PATIL Moble No:9739980307

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Overall 12+ experience of years of experience in CAE with technical support and engineering service background. As application engineer Worked in conjunction with the sales team as the key technical advisor and product advocate. As MSC Corporate Application Engineer identified and provide reliable solutions for all technical issues and assured complete customer satisfaction through all stages of the sales process. In engineering service field worked as project lead in different domains like aero, auto, new product

development in engineering services filed. Built and maintained positive relationships with consultants,

and key stakeholders to ensure projection and tap the future project those were in pipeline.

Companies Worked With:

Currently working as Assistant Manager in Larsen & Toubro InfoTech Limited, Bangalore from September 2011 to till date (5 years).

Worked as a Senior Consultant in Capgemini India Private Limited, Bangalore from October 2007 to September 2011 (4 years).

Worked as an Application Engineer in CSM Software India Private Limited, Bangalore from January 2005 to October 2007 (2 years).

Achievement Summary:

Platinum Team Award for year 2015 in outstanding contribution in Project Management from

Chief Executive – L&T Technology Services.

Project Star Award Q2 from Sogeti-htc_Development_AM form Country Head Sogeti India

Learning & Development Program:

Six Sigma Certification Training

Quality Control

First Time Manager

Certification on Project Management

Goal Setting for success

Certification in 5S Methodology

Spirit of Entrepreneurship

Reliability Engineering

Work Summary as Technical Support

Maintained expert level of product knowledge and application.

Presented MSC Products technology and product capability to both business and technical users.

Provided design and specification development support to consultants, integrators, and distributors.

Responded to functional and technical elements of RFIs/RFPs

Listened, understand and convey customer requirements.

Performed technical/ product training for sales people, estimators, and engineers at targeted accounts.

Assisted in the design and development of new macro and tools necessary to customer, there by exposing the technical team to optimize the GUI of MSC Product.

Maintained accurate records of target accounts, opportunities, quotes, projects, contacts and correspondence in company approved databases

Extensively traveled to project sites to perform start-up, integration, and training services


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Resolved customer issues or difficulties in a manner that is consistent with the company mission, values, and financial objectives.

Maintained professional business relationships within target accounts.

Provide status of ongoing projects and future projects.

Identify customer's needs and sales opportunities to help future growth

Work Summary as Technical Lead in Engineering Services

Having work experience at client place Germany (Bremen)

Worked several project right from project proposal creation, kickoff, PSMP creation to

successful execution of Project

Ensure projects are executed from the concept to certification phase

Participated in weekly drum beat to explain the Project progress of my team and improve the

process capabilities. Provides the necessary job / work instructions

Co-ordinate with the client in attaining the project target by giving the material input and design

feasibility.

Worked as onsite co-coordinator and then co-ordinate work from offshore Bangalore.

Exposure to DFEM & GFEM experience.

Proficient in proposal creation, domain expertise document preparation

Exposure to preparation of PSS, Justification and Certification Report preparation.

Conducted regular telephonic & video conference to understand client’s requirements.

Prepared PCL macro for the calculation of convergence of the elements and postprocessor

widget for the same.

Software Expertise

Altair Software Products

Hypermesh, Hyperview, OptiStruct Static and Dynamic Modules

MSC software Products

MSC Patran, MSC Nastran, MSC Fatigue,

Static, Dynamic, Thermal, Optimization, Non-Linear, Fatigue Module

Airbus Tools ISAMI, Samcef

ISAMI – Static, Samcef – ASEF (static), Mechno (Nonlinear), Reverse Mechno (Non-Linear), Dynam (Dynamic), PSN, Assist.

Other PCL (Patran Command language),

VPM, MS OFFICE MS-word, MS-excel, MS- Power Point

Education & Training

1. Bachelor of Engineering in Mechanical from visvesvaraya technological university

2. Master of Technology in Machine Design from visvesvaraya technological university

http://www.altairhyperworks.in/product/OptiStruct


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Achivement as Application Engineer

As a corporate application engineer provide various training program of MSC products to major OEM and engineering services companies.

Successfully integrated the SMP and DMP for the large automotive OEM, so that they can run large model with minimum setup time.

Major Projects Executed at Onsite and offshore

1. Project Title Justification of Buffer Stop of Cargo Compartment of A400M Client Elan Ausys, Bremen, Germany Software used Hypermesh, MSC Nastran, MSC Patran, PCL MS word and MS Excel

Responsibility Team Lead

Objective is to pass the Buffer Stop and CRRS Compartments from MAT A to Certification phase.

The Base Structure of buffer stop is loaded under various conditions (G loading, Pallet loading, Crash loading) to check the stability.

The analysis involves 1D, 2D and 3D mesh, SUPORT elements

Static (Linear and Non-linear) and Buckling analysis of metallic components.

Hand calculation for Tensile, Shear, Combined, Bearing, Pull Through using HSB methods.

Failsafe analysis of critical parts.

Preparation of PSS (Preliminary Stress Sheet), Justification and Certification Stress Report

Achievement: Worked inside Airbus and worked in close coordination with platue head and attained the certification signature to base structure. The base structure was successfully tested and matched with simulated result.

2. Project Title Optimization of Open Blade Rotor (Ver2.1-2.13)

Client Sogeti High-Tech, melun, France

Software used Hypermesh, MSC Nastran, MSC Patran, PCL, Campbell, MS word and MS Excel


Meshing of open rotor blade was done with hexahedral mesh of first order using MSC. Patran 2005r2.

Reverse Mecano, Non-Linear static, dynamic analysis was performed using Samcef v12.

The report was generated for each version of blade with von misses, max principle, min principle TBC, Normalized Speed Campbell diagram values represented with counters at interested region.

Achievement: Made this project as the master thesis and had greater understanding of the concept and released the case study for the in-house company website. Received the Project Star Award Q2.

3. Project Title Composite Flap Track Fairings (FTF 2, 3, 4 fixed & moving) A340

Client Ferchau, Bremen, Germany

Software used Hypermesh, MSC Nastran, MSC Patran, MS word and MS Excel

Responsibility Team Member

Objective is to do validation of flap track faring for different (internal pressure, air loads, inertia loads and fail safe load case) load cases.

DFEM analysis involves 1D and 2mesh, rigid body elements

Application of composite properties for different ply layup

Perform AM2036 sanity check as per Airbus procedure

Static (Linear) analysis of components flap track fairing components

Analysis is accomplished in compliance with No 5750 M1B GR04 01 and all JAR-requirements

Preparation of Certification Stress Report


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Achievement: Worked in wing part of Airbus series and increase my knowledge on the wing component. Appreciated by the client on the speed of meshing and on time delivery

4. Project Title Static and non-linear analysis flap components of A350-XWB-1000

Client Ferchau, Bremen, Germany

Software used MSC/Nastran, Patran, MS Word, and Excel

Responsibility Team Member

Static and non-linear analysis of drive strut of maturity-B phase

DFEM analysis elements and application of material & properties

Perform AM2036 sanity check as per Airbus procedure

Static (linear-non-linear) analysis of components

Analysis is accomplished in compliance with No 5750 M1B GR04 01 and all JAR-requirements

Preparation of Certification Stress Report

Achievement: Worked in wing part of Airbus series and increase my knowledge on the wing component. Appreciated by the client on the speed of meshing and on time delivery

5. Project Title Static Strength Justification of center ceiling panel A380-800

Client Sogeti High-Tech, Germany (Hamburg)

Software used Hypermesh, MSC/Nastran, Patran, MS Word, and Excel

Responsibility Onsite coordinator

Brackets with DFEM were simulated with shell elements (CQUAD4 and less than 3% CTRIA3) and bar elements.

Fasteners are simulated with 1D element. Panel weight is simulated as mass at the cg (CONM2).

Panel area is simulated with rigid body elements (RBE2).

The weight of the other attachment to the panel (PSU and oxygen box as well as interface points) is simulated with respective mass.

Strength justification is done for Ultimate load, Decompression, windmilling and Emma load in accordance with JAR-25.

Critical RF for part, critical load case & critical location of the bracket were summarized.

Justification report is prepared for same.

Achievement: Was able to coordinate with offshore and showcase the capability to sogeti high-tech (hamburg) that offshore is possible.

6. Project Title Life Evaluation of LPT turbine (Disque 1-4 and Flange 1-4) of CFM56-7

Client Sogeti High-Tech, melun, France

Software used Hypermesh, MSC Nastran, MSC Patran, PCL, Samcef, Toscan MS word and MS Excel


The Aerodynamic pressure, cavity pressure and temperature and inertia load are applied to the model.

In Samcef solver is used for calculation for transient loadings. The stresses induced in the transient loading are taken to the fatigue analysis to see that no crack is initiated at 25 000 cycles.

The next step would be to determine the crack propagation at 6500 cycles.

We used the in house tool called Toscane.

The detailed dossier is prepared which illustrated the zones of interest.

Achievement: Created the macro in PCL language for the convergence test of the hexahedral element thereby minimizing the time consumed for the life evaluation for each disque and flange.


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7. Project Title Gen Two End Caps to analyses

Client BA Aerospace, USA

Software used Hypermesh, MSC Nastran, MSC Patran, PCL, MS word and MS Excel


To perform a structural analysis for the maximum load carrying capacity (Axial load, when harness pulled outside).

Updating of material, property and loading.

Study the stress developed on the snap feature during incretions into housing and maximum deflection

Performed the analysis reports, with recommendation to improve the design.

Achievement: Client appreciate the optimized model and testing of same matched with the simulated result.

8. Project Title End Cap Analysis of Plastics

Client BA Aerospace, USA

Software used Hypermesh, MSC Nastran, MSC Patran, PCL, Campbell, MS word and MS Excel


To perform a structural analysis for the given G loading and suggest the optimized snap length and the size and topology of the snap.

Updating of material, property and loading.

Perform different iteration for different geometry

Prepare the presentation with the optimized shape.

Achievement: Client appreciate the optimized model and testing of same matched with the simulated result.

9. Project Title A350-900 XWB Door Frame Lining Panels

Client Sogeti High-Tech, Germany (Hamburg)

Software used Hypermesh, MSC/Nastran, Patran and MS Office

Responsibility Offshore coordinator & Team Lead

It consists of A-bracket, B-bracket, C-bracket, STD parts and the transition panel AFT, Upper transition panel AFT, attendant supply panel, Exit panel, guide arm cover, system strip FWD, system strip AFT, AS spacer.

DFEM consisted of CQUAD4 and some CTRIA3 are used for modeling the A-bracket, B-bracket, whereas the STD parts are not meshed but will be integrated into the FEM model by a RBE2 element.

As per the JAR-25 airworthiness requirements the ultimate loading and abuse loading is applied and critical RF for the part, critical load case & critical location of the bracket are summarized and Justification report is prepared.

Achievement: Was able to coordinate focal at Hamburg and bring in more projects and increase the head count of the team.

10. Project Title Random Response Analysis Mounting Tray

Client BEL, India (Bangalore)

Software used Hypermesh, MSC/Nastran, Patran and MS Office

Responsibility Corporate Account Sr Application Engineer

It is a Mounting tray assembly located in the fuselage of the aircraft consisting of shock mount, vertical and horizontal stiffeners.

This assembly was subjected to sever environmental loads such as static and random loads.

The finite element model and analysis was carried out using the MSC Patran 2005 and MSC Nastran 2005 respectively.


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Achievement: Showcase the MSC. Nastran/MSC. Patran capability and was able to convenience customer to buy the MSC Product for their in-house use.

Corporate training on MSC Products

Address D2-202, Shriram Shreyas Apartment, kodigehalli, Bangalore:560097

Languages Kannada English Hindi

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