Udhasu L Nayak

• Worked on Passenger Door, Service Door and Cargo Door.
• Working on Centre, AFT Fuselage Structure Design.
• Performing 3D and 2D check activity of DMU and Drawings.
• Design reviews, drawing releases, quality requirements, assembly analyses, amongst other activities.
• Communicate risks within the designs to appropriate stakeholders to help drive to collective decisions.
• Checking the Dornier Legacy drawing to understand and resolve the technical issues.
• Coordinating with diverse teams from multiple disciplinary functions such as aero design, and systems design on the design changes done.
• Preparing Technical document like Interface alignment document, MTS by communicating with stress and Materials teams.
• Have knowledge on repairs topic.
• Project: D-328 ECO Aircraft

Project: DMU ART (Agile Release train) Real Kheops team

• Monitoring team delivery and timeline adherence to achieve teamwork, train and develop, measure work in progress projects.
• Attending PI planning to get to know about the deployments on design tools Preparing Roadmaps according to the information collected from developers.
• Preparing Release notes after the deployment.
• Communicating to all internal Airbus users about the features added or changed in tools through PLM alerting centre.
• Updating the user guide documents of design tools according to deployments.
• Publishing the Documents in ECM.
• Preparing the Awareness material and providing awareness session on the design tools according to the supplier’s requirements.

Tools Used: - Catia V5, ADScontextbuilder, Trend V5, Novo Desk

• Coordinating with the client about technical design requirements and delivery during stand-up meetings and presentation reviews.

Project: Cargo Door Surroundings (CDS), Secondary Structure Installation

• DMU analysis to check for clash and clearance.
• Single part Designed, PPS parts according to DMU and Design Guideline.
• Worked on Bonded Bracket Installation and riveted brackets installation drawings.

Project: IFOT (Fuselage of Tomorrow)

• Working on Conceptual Design for Seat Attachment.
• Concept design for Cargo floor and Seat floor.

Project: DEMONSTRATOR ACTIVITY (A320)

• Check gaps and penetrations between frames and door fittings with panel bonded doubler assembly.
• Creation of Repair Angle and Shims on the area where there is penetration between Skin and Door surrounding.
• Checklist preparation and Estimation creation.

Tools Used: - Catia V5, 3DExperience, Pass, VPM

Project: PAX Floor

• Worked on Seat Rail and Cross Beam installation for A350-900, 1000 on SEC 13/14 & SEC 16/18.

Project: Interior Cabin Validation and Galley Check Activity

• Validating dimensions of different kinds of seats from different Airlines.
• Validation includes Seat Movable Components like Backrests, Movable headrests, In-arm tables.
• Video arm, the monitor shall be shown as volumes composed of geometrical surfaces in the stowed and in use position.
• CRP, SRP, EP, SEAT FURNITURE MOVABLE COMPONENTS, Compartment doors, Cupboard doors, Drawers, Privacy dividers/screens, PAX compartment doors, Sliding partition elements.
• Checking galley G2A, G2F installation instruction like Lower attachment, Upper attachment, Catering equipment Electrical and cooling installment.

Project: Landing gear - Airbus A350 XWB- 1000

• Creation of design for manufacturing drawings for A350-Landing Gear.
• Creation of picture drawing for certain design solutions to provide clear pictures which are difficult to show in orthographic.
• Providing instruction procedures to the design solution, how it is installed & providing torque tightening values.
• Referring interface drawings for material used and checking whether parts are supplied by the vendor or Airbus.
• Providing clearance between up lock hook and roller, when the roller is in both open and closed position using kinematic simulation.
• Measuring the distance between tire and bay when the gear is in a retraction position.

Project: Landing gear - Airbus A380 Hoses Task.

• Due to Kevlar material around the hoses, during retraction hoses will bend and Kevlar material will damage the hoses.
• Changing the material around hoses from KEVLAR to CRES and providing the SWIVEL hoses point. SWIVEL will rotate and help the hoses to hogg during unlocking of side stay.
• Changing the drawing and bill of material where it is affected

Project: Fixed Bracket Design - Airbus A350 XWB -1000 Section 15.

• Volumetric Search carried out before designing parts for clearance & clash checks. Stress Zone Checking was done before designing any part.
• Designing of Fixed Bracket for as per Standard for section 15. Cross verifying the fixed bracket in detail and in installation level for the position.
• Generation of Design for Manufacturing (DFM) drawings, BOM, and ECN as per Airbus Standard.

Project: SARAS 14-seater multi-role twin-propeller aircraft.

• Interaction and coordination with design (fuselage, wing, nacelle, HT, and VT groups), manufacturing (NC and Sheet Metal) group, assembly shop, etc... Regarding the models, loft/NMG and flat pattern generation and its respective assemblies.
• Intimating required design change (requesting for DCR) and incorporating design change notice for models and assemblies from different design groups.
• Surface, Solid modelling, Drafting, and Assembly using CATIA V5.
• Bend and bevel angles are calculated at certain locations. Using bevel angle, developmental length is calculated.
• Create NC programs using Catia V5 R20 based on provided part geometry and models.
• Create set-up sheets based on programming.
• The tool path is generated for both roughing and finishing operations. In the case of complex negative face machining, sine reference tables are used to machine using 3 axis machines.