RAJA NATLA V V S N
Address:Flat No. C001, ISRSukrithiApartments, BehindVarthurPolicestation, Varthur,Bangalore-87, Karnataka
Phone: +91-9705195010
E-mail:raja.natla111@gmail.com
PRODUCT DESIGN & DEVELOPMENT | AERO ENGINES &AIRCRAFT STRUCTURES
Seeking a profile in the field of Mechanical Design & Development within a growth oriented
organization.
Professional Summary:
● Overall 6 years of experience in the field of Mechanical Design and Product Development
of Gas Turbines Engines (Aero Engines)-4 years and Aircraft Structures -3 years
● Experience drives into Feasibility Study, Conceptual design development, Modeling,
Drafting, Stack up Analysis, Cost and weight optimizations.
● Presently Working with QuEST-Global diving towards the product development of Aero
engines for more refined focus to components from various aspects – Design and
Manufacturing
● Worked with Rolls Royce in the segment of Combustor for RB3043 engine from initial
stage to manufacturing
● Worked with CYIENT in the segment of Aero structures for Design of Electrical Wire
Routing Installation,Structural components like ribs,mounting brackets,etc.,from scratch
or existing design modification for performance improvement of 737 MAX, 747 and 787-
10(Boeing)
● Worked on Product development and design of various airborne and industrial gas
turbine engines by Pratt & Whitney America (Segment of UTC) being part of NGPF (Next
Generation product Family). These are used on Mitsubishi Regional Jets, Bombardier C
Series, Airbus A-320 Neo and Irkut MC-21 aircrafts.
● Worked on Product Design and development of Longerons used on Sirkosky S92
(Chopper) by Sirkosky Aircraft (Segment of UTC).
● Have a proven ability to work with cross functional teams with analyzing the situation
practically and bringing out research oriented learnings towards product.
● Additionally performed analysis of components practically as well over the software and
validated to understating various contributing factors practically.
● Have a detailed exposure to various products worked on Aircraft Engines and Structures
Participated in disassembly adhering to the process for disassembly prescribe by the
document. For the display held in our organization for the products.
● Excellent interpersonal skills, drives towards fulfillment of personal goals with
completion of company goals landing into technical knowledge development and
disbursement to the team.
WORK EXPERIENCE
QuEST-Global
SeniorEngineer-Design| December2015–Present
 Understandingthecustomerdataandprocessingtofeedinvariousoperationsofmanufacturingdownthe
lanetillproductgettingrolledout.
 ProcessingincludesBOMstructurepatterncreationinteamcenter,reproducingtospecifiedmodellingand
definitionstandards,manufacturingstagewisecreationsandvendordatatransmits.
 Handlemanufacturingnonconformanceswithdesignandonlypersonidentifiedforthisworkprocessfrom
India.
PROJECT
Design & Manufacturing Support of Combustion chamber outer casing
forRB3043
Customers:RollsRoyce
SoftwareUsed:UnigraphicsNX 9.0,TeamCenter, SAP
Accomplishments
 Became one point of contactforDefinition Support for manufacturing from India.
 Identified as a team member for new technology developments.
CYIENT Ltd(FormerlyInfoTechEnterpriseslimited)
SeniorDesignEngineer|August2010 - November2015
 Design of ElectricalWire Routing Installation, Structural components like ribs, mounting brackets,
etc., from scratchor existing design modification forperformance improvement.
 Participating in design, assembly support activities and freezing the design concept.
 Planning detailed engineering activities and finalizing requirements and specifications in consultation
with Aero thermo group, Stress and Material group and Production Departments.
 Looking after technical activities like conceptualdesign, providing alternate design solutions in 3D
modelling & detailing of various aerospace components.
 Testing of Static Air Pressure at FIN TIP of 737Max Boeing aircraft.
 Migrate Catia V4 models to CatiaV5 whichincludes ElectricalWire Harness, Tubing and Structures
models. Validation is performed on this conversion using CatiaV5 DMU tools
 Studying and understanding multiple Boeing documents forevery process (selection of materials,
selection of fasteners, Installing processes, Cleaning processes, etc...)
 Maintained good quality and supported the team in various aspects.
PROJECTS
DesignandDevelopmentofCompressorComponents
Client:Pratt&Whitney America,UnitedTechnologyCorporation
SoftwareUsed:Unigraphics,TeamCenter
Programsworkedon:
NGPF(NextGenerationproductFamily)
1. MitsubishiRegional Jets(AirborneEngines)
2. BombardierC Series(AirborneEngines)
3. AirbusA320Neo(AirborneEngines)
4. FT4000(IndustrialGasturbine)
TasksExecuted:
 ProductDefinition(Modelling,Detailing/Drafting)
 StackupAnalysis-Axial,Radial
 WorkingwithCross Functionalteams.
 Meetings conductand closure of iteration -Conclusions,Learnings
 Design Optimization-Cost Reduction,Weight Optimization,etc.
DesignandDevelopmentof WireRoutingInstallation(737MAX)
Client:Boeing
SoftwareUsed:CatiaV5,ENOVIA
TasksExecuted:
 ProductDefinition(Modelling,Detailing) CreationofNewdesignforinstallationof Wire
Routing
 DesigningSupportingbracketsasperStandards
 Decidingregardingwhatfastenerstackuptobeused
 MakesureRoutingshouldbeaspertheproductionwireroutingandinstallFlightTest
wiring
 ProvidingModificationInformationandRefurbishinformation
 PresentingtheConcept ReviewwithallStackholders
 MaintainingtheBoeingStandardsandcreatingthedrawingsasperdrawingstandards
 GeneratingdrawingsfornewdesignedbracketsandWireInstallation
 GettingtheApprovalsfromdifferentgroupslikeME,M&PT,Stress,Group,DE leadEtc.
DesignChanges in Structural components -Spars and Ribs (747-8& 787-9)
Client:Boeing
SoftwareUsed:CatiaV5,ENOVIA
TasksExecuted:
 Study of InputslikeBoeingDesignManuals(BDM),V4andBPNdrawings.
 EstimationofthepackageandprovidingtheExpectedCompletionDatesforeachpackage
(ECDs)tocustomer.
 Drawingstudy andcreatingtheclashreportsforthemechanicalparts.
 CreatingInstallations,assembliesanddetailingof mechanicalandelectricalpartsasper
BoeingStandardsanduploadingthemtoENOVIA.
 ResolvingthetechnicalIssuesintheteamandQualitycheckofdatabeforedeliveringto
customer.
 RunningEHT(ElectricalWireHarnessTool)&BSC(BackshellClocker)toolstoavoid
linkageerrors&electricalconnectionsandsticktothecustomerstandards.
 UploadingtoEnoviaandfillingattributesaccordingtoBoeingstandards.
 DeliveringthedatasetsontimethroughDCP aspertheclientrequirements.
 Maintainedgoodqualityandsupportedtheteaminvariousaspects.
 Supportingandhandlingtheteamwhenrequired.
Training& Certification
 Attended manufacturing training program conducted by IIT, Kanpur during July-2014.
 Obtained MSC Nastran/Patran Certification in 2013.
TECHNICAL SKILLS
Working Environments:
Aero Engine Systems
 Leadout - Combustor
 Electrical Systems
 Externals
Aircraft Structures
 Fuselage, Cockpit and Wing for Super First Class, Business
Class, Economy Class
 Electrical Wire harness, Tubing and Tooling
Technical Environments:
Cad Environments:
 Part, Assembly, Surfaces, Sheet metal, Wire Harness.
Drawing Environments:
 Adhere to ASME Y14.5 2009 standards.
 Well versed with Geometric Dimensioning and
Tolerancing
 Drawing Types Dealt :
1. Installation,Assembly Detail Part Drawings
2. Part Kinds (Material Based) – Machined, Sheet metal,
Plastics.
Cad Software's:
 Unigraphics
 Catia V5
PLM tools:
 Team Center
 ENOVIA
Analysis Software's:
 MSC Nastran/Patran
Office Tools:
 Microsoft Office -2003/-2007/-2010
ACADEMICS
 Diploma in Mechanical Engineering from Govt.Polytechnic, Kothagudem
 Graduated in Mechanical Engineering from J.N.T.University, Hyderabad in 2010
Nationality: Indian
Marital Status: Married
Date of Birth: 09th August 1988
Languages Known: English, Hindi, Telugu
Passport No:K4187798; Valid Upto: 5thAugust 2022
Linked-in Public Profile: http://www.linkedin.com/in/rajanatla
REFERENCES
Will be provided upon Request.

Resume_Raja_3

  • 1.
    RAJA NATLA VV S N Address:Flat No. C001, ISRSukrithiApartments, BehindVarthurPolicestation, Varthur,Bangalore-87, Karnataka Phone: +91-9705195010 E-mail:raja.natla111@gmail.com PRODUCT DESIGN & DEVELOPMENT | AERO ENGINES &AIRCRAFT STRUCTURES Seeking a profile in the field of Mechanical Design & Development within a growth oriented organization. Professional Summary: ● Overall 6 years of experience in the field of Mechanical Design and Product Development of Gas Turbines Engines (Aero Engines)-4 years and Aircraft Structures -3 years ● Experience drives into Feasibility Study, Conceptual design development, Modeling, Drafting, Stack up Analysis, Cost and weight optimizations. ● Presently Working with QuEST-Global diving towards the product development of Aero engines for more refined focus to components from various aspects – Design and Manufacturing ● Worked with Rolls Royce in the segment of Combustor for RB3043 engine from initial stage to manufacturing ● Worked with CYIENT in the segment of Aero structures for Design of Electrical Wire Routing Installation,Structural components like ribs,mounting brackets,etc.,from scratch or existing design modification for performance improvement of 737 MAX, 747 and 787- 10(Boeing) ● Worked on Product development and design of various airborne and industrial gas turbine engines by Pratt & Whitney America (Segment of UTC) being part of NGPF (Next Generation product Family). These are used on Mitsubishi Regional Jets, Bombardier C Series, Airbus A-320 Neo and Irkut MC-21 aircrafts. ● Worked on Product Design and development of Longerons used on Sirkosky S92 (Chopper) by Sirkosky Aircraft (Segment of UTC). ● Have a proven ability to work with cross functional teams with analyzing the situation practically and bringing out research oriented learnings towards product. ● Additionally performed analysis of components practically as well over the software and validated to understating various contributing factors practically. ● Have a detailed exposure to various products worked on Aircraft Engines and Structures Participated in disassembly adhering to the process for disassembly prescribe by the document. For the display held in our organization for the products. ● Excellent interpersonal skills, drives towards fulfillment of personal goals with completion of company goals landing into technical knowledge development and disbursement to the team.
  • 2.
    WORK EXPERIENCE QuEST-Global SeniorEngineer-Design| December2015–Present Understandingthecustomerdataandprocessingtofeedinvariousoperationsofmanufacturingdownthe lanetillproductgettingrolledout.  ProcessingincludesBOMstructurepatterncreationinteamcenter,reproducingtospecifiedmodellingand definitionstandards,manufacturingstagewisecreationsandvendordatatransmits.  Handlemanufacturingnonconformanceswithdesignandonlypersonidentifiedforthisworkprocessfrom India. PROJECT Design & Manufacturing Support of Combustion chamber outer casing forRB3043 Customers:RollsRoyce SoftwareUsed:UnigraphicsNX 9.0,TeamCenter, SAP Accomplishments  Became one point of contactforDefinition Support for manufacturing from India.  Identified as a team member for new technology developments. CYIENT Ltd(FormerlyInfoTechEnterpriseslimited) SeniorDesignEngineer|August2010 - November2015  Design of ElectricalWire Routing Installation, Structural components like ribs, mounting brackets, etc., from scratchor existing design modification forperformance improvement.  Participating in design, assembly support activities and freezing the design concept.  Planning detailed engineering activities and finalizing requirements and specifications in consultation with Aero thermo group, Stress and Material group and Production Departments.  Looking after technical activities like conceptualdesign, providing alternate design solutions in 3D modelling & detailing of various aerospace components.  Testing of Static Air Pressure at FIN TIP of 737Max Boeing aircraft.  Migrate Catia V4 models to CatiaV5 whichincludes ElectricalWire Harness, Tubing and Structures models. Validation is performed on this conversion using CatiaV5 DMU tools  Studying and understanding multiple Boeing documents forevery process (selection of materials, selection of fasteners, Installing processes, Cleaning processes, etc...)  Maintained good quality and supported the team in various aspects. PROJECTS DesignandDevelopmentofCompressorComponents Client:Pratt&Whitney America,UnitedTechnologyCorporation SoftwareUsed:Unigraphics,TeamCenter Programsworkedon: NGPF(NextGenerationproductFamily) 1. MitsubishiRegional Jets(AirborneEngines) 2. BombardierC Series(AirborneEngines) 3. AirbusA320Neo(AirborneEngines) 4. FT4000(IndustrialGasturbine)
  • 3.
    TasksExecuted:  ProductDefinition(Modelling,Detailing/Drafting)  StackupAnalysis-Axial,Radial WorkingwithCross Functionalteams.  Meetings conductand closure of iteration -Conclusions,Learnings  Design Optimization-Cost Reduction,Weight Optimization,etc. DesignandDevelopmentof WireRoutingInstallation(737MAX) Client:Boeing SoftwareUsed:CatiaV5,ENOVIA TasksExecuted:  ProductDefinition(Modelling,Detailing) CreationofNewdesignforinstallationof Wire Routing  DesigningSupportingbracketsasperStandards  Decidingregardingwhatfastenerstackuptobeused  MakesureRoutingshouldbeaspertheproductionwireroutingandinstallFlightTest wiring  ProvidingModificationInformationandRefurbishinformation  PresentingtheConcept ReviewwithallStackholders  MaintainingtheBoeingStandardsandcreatingthedrawingsasperdrawingstandards  GeneratingdrawingsfornewdesignedbracketsandWireInstallation  GettingtheApprovalsfromdifferentgroupslikeME,M&PT,Stress,Group,DE leadEtc. DesignChanges in Structural components -Spars and Ribs (747-8& 787-9) Client:Boeing SoftwareUsed:CatiaV5,ENOVIA TasksExecuted:  Study of InputslikeBoeingDesignManuals(BDM),V4andBPNdrawings.  EstimationofthepackageandprovidingtheExpectedCompletionDatesforeachpackage (ECDs)tocustomer.  Drawingstudy andcreatingtheclashreportsforthemechanicalparts.  CreatingInstallations,assembliesanddetailingof mechanicalandelectricalpartsasper BoeingStandardsanduploadingthemtoENOVIA.  ResolvingthetechnicalIssuesintheteamandQualitycheckofdatabeforedeliveringto customer.  RunningEHT(ElectricalWireHarnessTool)&BSC(BackshellClocker)toolstoavoid linkageerrors&electricalconnectionsandsticktothecustomerstandards.  UploadingtoEnoviaandfillingattributesaccordingtoBoeingstandards.  DeliveringthedatasetsontimethroughDCP aspertheclientrequirements.  Maintainedgoodqualityandsupportedtheteaminvariousaspects.  Supportingandhandlingtheteamwhenrequired. Training& Certification  Attended manufacturing training program conducted by IIT, Kanpur during July-2014.  Obtained MSC Nastran/Patran Certification in 2013.
  • 4.
    TECHNICAL SKILLS Working Environments: AeroEngine Systems  Leadout - Combustor  Electrical Systems  Externals Aircraft Structures  Fuselage, Cockpit and Wing for Super First Class, Business Class, Economy Class  Electrical Wire harness, Tubing and Tooling Technical Environments: Cad Environments:  Part, Assembly, Surfaces, Sheet metal, Wire Harness. Drawing Environments:  Adhere to ASME Y14.5 2009 standards.  Well versed with Geometric Dimensioning and Tolerancing  Drawing Types Dealt : 1. Installation,Assembly Detail Part Drawings 2. Part Kinds (Material Based) – Machined, Sheet metal, Plastics. Cad Software's:  Unigraphics  Catia V5 PLM tools:  Team Center  ENOVIA Analysis Software's:  MSC Nastran/Patran Office Tools:  Microsoft Office -2003/-2007/-2010 ACADEMICS  Diploma in Mechanical Engineering from Govt.Polytechnic, Kothagudem  Graduated in Mechanical Engineering from J.N.T.University, Hyderabad in 2010 Nationality: Indian Marital Status: Married Date of Birth: 09th August 1988 Languages Known: English, Hindi, Telugu Passport No:K4187798; Valid Upto: 5thAugust 2022 Linked-in Public Profile: http://www.linkedin.com/in/rajanatla REFERENCES Will be provided upon Request.