Jayanth Shivakumar Email & Phone Number

Munich, By, De

Donauwörth, Bavaria, Germany

Working as an External Electrical systems engineer for Airbus Helicopters H145(EC145) and H135(EC135).

Donauwörth, Bavaria, Germany

Working as an External Electrical systems engineer at Airbus Helicopters for H145(EC145) MCA and H135(EC135) MCA. My areas of scope include:- Verification and validation of Communication (44-30 external communication systems, ATA 23 Cabin systems) and Navigation(ATA 34-00 nav general, ATA 34-10 flight environment data) electrical wiring diagrams (Schematics).- Preparation of Comm/ Nav wiring test requirements.- Preparation of programs for various wiring tests such as Continuity testing, Short circuit testing, HV & LV testing and Isolation testing.- Evaluation and correction of wiring design descriptions based on test simulation data obtained from wiring test bench.- Proficiency in SEE electrical (IGE+XAO) wiring diagram design software.- Conformity validation of the designed to installed wiring harnesses. Creation and management of NC’s.- Familiar with CS-29.1431 (subpart F) Electronic equipment, CS-29.1457 & AMC 29.1457 Cockpit voice recorders and CS-29.1459 flight data recorders.

Bruchsal, Baden-Württemberg, Germany

My areas of scope include:1. Creation of FTI/ EWIS harness, Formboard and installation drawings.2. Perform modification of harnesses (HV, LV, Co-axial and FO against proposed change requests).3. Review and verify the design modifications against segregation requirements with other EWIS and clearance against other systems (Structure, FCS and Avionics).4. Enabling the design discrepancies identified by the production/ Assembly (NCR, VCPR, DA).5. Creation of change request for the design modification.6. Creation of Harness accessories (brackets, mechanical attachment point, standard parts).7. Creation of design dataset (3D mock up, 2D manufacturing drawings and installation drawings, Creation of EBOM).8. Professional experience in engineering tools such as Siemens NX CAD tool and Teamcenter PLM.9. Knowledge of EWIS design guideline (AC43.13-1B, SAE AS50881H), Design verification/ compliance against CS25 and AC25.1701-1 part 25 subpart H).

Garching, Bavaria, Germany

As a part of my masters degree program in Aerospace Engineering at TUM, I have successfully completed my masters thesis at the institute for Rotorcraft and powered lift vehicles.Title: Investigation of Thermal load effects on flax and carbon/flax hybrid composite aircraft structures. Grade: 1.7The key features of this thesis were:1. Formulated and implemented a high-fidelity three-dimensional finite element model for thermal stress analysis in Flax Fiber Reinforced Epoxy Composites (FFREC).2. Conducted a systematic investigation into the enhanced thermal resilience of hybrid flax-carbon composite systems.3. Investigated the anisotropic thermal response mechanisms and quantified inter-laminar stress distributions in FFREC structures.4. Performed comprehensive quantitative analysis of tensile strength and stiffness degradation in FFREC under elevated thermal conditions.5. Developed and validated advanced numerical models for non-linear damping characteristics using both frequency-domain and time-domain methodologies.6. Employed the Half Power Bandwidth method to derive empirically-validated damping loss factors across a broad temperature spectrum.7. Validation of simulation models against extant literature, ensuring high fidelity in temperature-dependent material behavior predictions.8. Characterised the temperature-induced brittle-ductile transition phenomena in FFREC materials through multi-scale analysis.9. Conducted in-depth investigation into the thermal stress susceptibility of transversely oriented fiber composites, identifying critical failure modes.10. Established a comprehensive framework for temperature-dependent damping behavior in FFREC, with specific application to vibration and acoustic control scenarios.11. Rotor blade surface modelling and composite modelling in Catia V5 to analyse the feasibility of FFRP as aviation standard material.

Germany

As a structural design and simulation engineer at MPE, I worked on the development and optimization of the "magnetically coupled cryogenic gear mechanism" for the MICADO project which is a 40m class Extremely Large Telescope.my areas of work included the following:-usage of Siemens NX or solidworks 2022 for the design optimization process.-usage of COMSOL MULTIPHYSICS simulation software to simulate and study magnetic fields with no current in the mechanism.-magneto static analysis of the non contact gear mechanism-magneto mechanics analysis of non contact gear mechanism-finding optimum magnetic flux density between the driven and driving gear and finally to generate the required Torque to meet ESO's requirement for MICADO.

Oberplaffenhofen

Title: Redesigning and Commissioning of Rocket engine pump Test bench for the study of controlled Onset of instabilities.As a part of my master's degree in Aerospace engineering at TUM, I carried out my semester theses at the department of space propulsion and mobility.in my project, the test bench designated KONRAT was successfully Redesigned for management of varied NPSH of the Rocket engine Turbo pump and the Redesigned fields included the following:1. quantitative and qualitative analysis of the suction head of the turbo pump and its efficient management 2. structural changes to the test bench by varied CAD designs3. quantitative and qualitative analysis of heating equipment installation4. characteristic study of head and flow rate5. study of cavitation instability on the impeller blades of the turbo pump6. study of cavitation surge, auto oscillations, rotating stall and rotating cavitation.7. onset points of all the indicated instabilities were found and the pump curve was plotted.

Garching, Bavaria, Germany

India

I worked as graduate engineering trainee at OPPI where i was inculcated with the knowledge of industry manufacturing process chain where several automotive parts for TOYOTA cars were manufactured.some of them were:-manufacturing of gear box bearings and assembly of gear box.manufaturing of inner axle bearings.quality and repair of the inner cold weld and hot weld joints of the chassis with the help od laser metal deposition process (DMLS).

India

Master'S Degree, Aerospace, Aeronautical And Astronautical/Space Engineering, 2.3 (Passed With Merit)

Bachelor Of Engineering - Be, Mechanical Engineering, 1.5 (First Class With Distinction)

Pre University Diploma, Physics, Mathematics, Chemistry, Electronics, 94.8 %

Matriculation