Aaron Del Rio Bellisco

Aaron Del Rio Bellisco

Machinery CAD Designer & F-18 Maintenance Intern

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location of Aaron Del Rio BelliscoCopenhagen, Capital Region of Denmark, Denmark

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  • Timeline

  • About me

    Aerodynamics Design Engineer at Siemens Gamesa | Wind Energy and Aerospace Engineer

  • Education

    • Universidad Politécnica de Madrid

      2008 - 2013
      Master of Engineering (MEng) Aerospace Engineering

      Activities and Societies: IAESTE, Asociación de Aeromodelismo, Delegación de Alumnos

    • DTU - Technical University of Denmark

      2021 - 2023
      MSc Eng in Wind Energy Wind Turbines Mechanics and Aerodynamics
  • Experience

    • Spanish Air Force

      Aug 2011 - Sept 2011
      Machinery CAD Designer & F-18 Maintenance Intern

      Internship in the Spanish Air Force related to the maintenance of the main Strike Fighter of this Army, the Boeing F-18 Hornet:• Design with CATIA V5 of the Air Ground Support Equipment-Dolly Tire Lifter of the F-18, which mechanizes the Process of change wheels in the aircraft and reduces the number of persons needed only to one.• Design with CATIA V5 of an Endoscope Guide Pipe for the maintenance of the afterburner jacket of the Turbofan General Electric GE F404.

    • Esdras Automatica

      Jul 2012 - Sept 2012
      Machinery CAD Designer & Electromagnetic CAE Simulation

      Internship in a Company dedicated to Engineering Technical Services, R & D, production and commercialization of energy from renewable sources. My labour was dedicated to the Project “Mar de Canarias”, consisting in build two experimental offshore wind turbines of 5MW Power each on the South of the Gran Canaria Island:• Design with CATIA V5 of the Polymeric Arrester class 2 INAEL INZSP 132/10/2 (132KV) for an electric substation of the offshore wind farm.• Design with CATIA V5 of different mechanical parts of the wind turbines.• Electrostatic analysis with ANSYS of the Polymeric Arrester class 2 INAEL INZSP 132/10/2 (132KV). Show less

    • Airbus

      Oct 2013 - Oct 2014
      Aerospace Engineering Intern: Mass Models and Payload Loading Algorithms

      One year Internship in the Mass Model Department (EGWOM: sub department of Flight Physics) with the responsibility of research how to make the weight estimation easier and implement this knowledge creating tools that can be managed by the personal of the Department:•Creator of the Advanced Loadability Tool for Optimization (ALTO), a Matlab Tool which automatizes the Payload Distribution Process along the different decks for all the aircrafts of the Airbus Family.•Design of the Density Model of the new Airbus Beluga XL Freighter Aircraft with Hypermesh for the calculation of its mass properties.•Creator of the Manual of the Density Model Creation Procedure for the standardization of the Process in futures aircraft designs. Show less

    • University of Strathclyde

      Nov 2014 - Sept 2015
      Postgraduate researcher - Mechanical & Aerospace Engineering Deparment

      EVIDENCE-BASED ROBUST OPTIMISATION BASED ON UPPER AND LOWER EXPECTATIONS. Devise and implement an efficient computational method to apply the theory of Upper and Lower Expectation to the uncertainty quantification of large scale engineering systems (with particular focus on aerospace and energy systems) with particular focus on controlled dynamical systems in the presence of model uncertainty (unmodelled components).. Devise and implement an efficient computational method for optimisation under uncertainty based on the theory of Upper and Lower Expectations and memetic multiobjective algorithms.. Apply the new methodology to the optimal design and control of a selected number of aerospace examples.. Integrate the new methodology in the commercial software modeFRONTIER Show less

    • Airbus on behalf of Altran UK

      Sept 2015 - Sept 2017

      Mass Properties Engineer on behalf of AIRBUS ltd:. Aircraft Weight Estimation and Control: Estimation and monitoring of the weight and position of the centre of gravity of all the components of the wing and the landing gear for all aircrafts of the AIRBUS Family. . Advanced Mass Models generation based on Finite Elements Models and CAD information vital for Loads and Aeroelastical Analysis.. Construction and edition of the Weight Book for each aircraft. Document where is registered all the mass properties of every single component and system of the plane. Show less

      • Landing Gear and Fuel Systems Test Engineer

        Dec 2016 - Sept 2017
      • Materials and Processes Engineer

        Dec 2016 - Aug 2017
      • Weight and Mass Properties Engineer

        Sept 2015 - Dec 2016
    • Jaguar Land Rover

      Sept 2017 - Dec 2020

      As part of the TASE Team, my duty is to deliver aerodynamic performance, cooling performance, brake cooling, under body component thermal management and infotainment cooling for all the vehicle programmes of the Jaguar Land Rover SVO Family.Key Activities:. External Aerodynamics – analysis of full vehicle shape and specific aerodynamic features to optimise them for CD and CL performance. Extract of component loads to support durability and robustness analysis. Generation in CATIA V5 of external vehicle geometry proposals to improve aerodynamic efficiency and downforce. · Brake cooling – simulation of brake cooling characteristics and development of measures to optimise it. Toolset relies heavily on CFD· Heat management – analysis of all engine bay and under body components to ensure they remain within their temperature limits, particularly in the vicinity to the exhaust system or other heat sources, during extreme vehicle operating conditions.· EV battery cooling – simulation of battery thermal response to charge and discharge rates.· Cooling airflow – analysis of airflow through the apertures, cooling pack, engine bay, etc., to ensure vehicle cooling targets are met during extreme operating conditions.· General CFD – analysis of systems such as the engine air intake system and cooling ducts to ensure the affected systems meet their performance requirements in extreme operating conditions.I conduct this activities using Dasault Systemes Toolset: PowerDelta (meshing), PowerFLOW (CFD) and PowerTHERM (heat protection CAE, aka RadTherm) Show less • Preparation of Loading Charts and Mass Properties Parametric Models throughout the engineering process to estimate the weight, moments of inertia and centre of gravity of the car at system level using input information from CAD (Catia V5, TeamCenter and VisMockUp) to support CAE during the virtual phase and to enable correlation of physical prototypes during validation.• Lead the certification of the Car Masses with the Vehicle Certification Authority for all the SVO programmes.• Benchmarking and futuring of competitors, both at vehicle and system level and subsequent weight target setting for all our products.• Tracking status against targets. Helping to ensure correct system/commodity/architecture strategy is employed through the engineering phase. • Set and ensure target compatibility with programme content across multiple SVO vehicle programmes. Taking responsibility for seeing completion of all weight activities through from Kick-Off through to Job 1. Ownership of weights trackers and waterfalls including opportunities and gaps to target.• Support Programme Attribute Leadership Strategy (PALS), Benchmarking, Panel Chart creation and Statement of Intent (SOI) requirements delivery. • Ensure adherence to relevant standards, leading problem resolution and validating delivery throughout the vehicle design and development process.• Weighing of vehicles and car components though physical measuring and analysis of the CAD Mock Up in CATIA V5 and Teamcenter Digital VisMockup adding material properties to the design.• Generation of ballasting models using CAD Simulation to help generate real Production State mass properties in mule cars. • Assist with the Verification Prototype and Tooling Trial/Pilot Production.• Guide pre-programme start benchmarking plan and coordination as well as the attribute target setting.• Weights Attribute Representative for Programme Steering teams, the Vehicle Integration team, technical reviews, and Design PATs. Show less

      • Thermal and Aerodynamic Systems Engineer, Special Vehicle Operations

        Oct 2019 - Dec 2020
      • Lead Weights and Mass Properties Engineer

        Sept 2017 - Oct 2019
    • Mott MacDonald

      Jul 2021 - Aug 2021
      Wind Energy Engineer

      Summer position in between semesters at DTU to get a taste of the Industry of Owners Engineering and Lender's Technical Advisory typically conducted during the phases of design, development and operation of onshore and offshore wind farm projects: . Technical due diligence for lenders, buyers, sellers. Construction monitoring for lenders. Operation monitoring for lenders

    • Siemens Gamesa

      Nov 2021 - now
      Aerodynamics Design Engineer

      . Contribute to new product development projects with aerodynamic modelling, optimization and validation. Generation of aerodynamic performance simulations to investigate and optimize our wind turbine portfolio performance.. Conducting wind tunnel and field tests for flow visualization.. Interact with blade production on aerodynamic specifications and quality requirements.

  • Licenses & Certifications

    • PRINCE2 Foundation Certificate in Project Management

      AXELOS Global Best Practice
      Jun 2016
      View certificate certificate
    • Working at Heights Training

      Global Wind Organisation
      Jun 2024
    • Image Processing Onramp

      MathWorks
      Jun 2024
    • Fire Awareness

      Global Wind Organisation
      Nov 2024
    • CATIA V5: Surfacing

      Lynda.com
      Mar 2018
      View certificate certificate
    • Chartered Engineer MIMechE

      Engineering Council
      Dec 2019
  • Honors & Awards

    • Awarded to Aaron Del Rio Bellisco
      2020 JAGUAR LAND ROVER TECHNICAL EXCELLENCE AWARDS JAGUAR LAND ROVER Feb 2020
    • Awarded to Aaron Del Rio Bellisco
      Chartered Engineer (CEng MIMechE) Institution of Mechanical Engineers Nov 2019 Chartered engineers (CEng) are characterised by their ability to develop appropriate solutions to engineering problems using new or existing technologies, through innovation, creativity and change. They may develop and apply new technologies, promote advanced designs and design methods, introduce new and more efficient production techniques and marketing and construction concepts, and pioneer new engineering services and management methods. Chartered engineers are variously engaged in technical… Show more Chartered engineers (CEng) are characterised by their ability to develop appropriate solutions to engineering problems using new or existing technologies, through innovation, creativity and change. They may develop and apply new technologies, promote advanced designs and design methods, introduce new and more efficient production techniques and marketing and construction concepts, and pioneer new engineering services and management methods. Chartered engineers are variously engaged in technical and commercial leadership and possess interpersonal skills. Show less
    • Awarded to Aaron Del Rio Bellisco
      SAWE Technical Paper Award - 5th Central European Society of Allied Weight Engineers Regional Conference on Mass Properties Engineering February 11th & 12th, 2015 Finkenwerder, Hamburg, Germany Society of Allied Weight Engineers Feb 2015 Applications of an Aircraft Loading model based on Lagrange Multipliers FormulationAarón del Río-Bellisco / Sven Lanzán Ferran ABSTRACT: The loading of the aircraft can be done in several ways. To make use of computer techniques, we need to build models that can simulate the loading of the aircraft. In this paper we explain a formulation based on Lagrange Multiplier problem that is aimed to obtain unique mass distributions for several purposes controlled by objective… Show more Applications of an Aircraft Loading model based on Lagrange Multipliers FormulationAarón del Río-Bellisco / Sven Lanzán Ferran ABSTRACT: The loading of the aircraft can be done in several ways. To make use of computer techniques, we need to build models that can simulate the loading of the aircraft. In this paper we explain a formulation based on Lagrange Multiplier problem that is aimed to obtain unique mass distributions for several purposes controlled by objective functions.In this paper, a formulation of the problem based on Lagrange Multiplier formulation compatible with inequalities boundary constraints is explained: the Karus-Kunt-Tuker (KKT) Conditions. After proposing the mathematical model for the problem, different applications are shown. This methodology can be applied to get mass distributions targeted to: flight test targets [Mass, CG, Inertia]; maximization of shear and bending in specific sections for loads analysis; mass cases for static and fatigue design; and finally also mass distributions for loading limits definition / optimization [CG and S&B]. Show less