Jose Ricardo Porro

Berufserfahrung von Jose Ricardo Porro

• Bis heute 5 Jahre und 2 Monate, seit Apr. 2019

  Stress Engineer

  Calidus LLC

  Collaborating in the stress analysis team for the certification process according to FAA PART-23 of the B250 Light Attack Aircraft and in the preliminary design of the B350 aircraft detailed design. Executed the linear and nonlinear stress analysis to evaluate the main body section structure, wings and other components. Verifying post-buckling of main composite parts to check the structural capacity load capacity before final failure occurs. Implemented and executed bird impact analysis.

• 1 Jahr und 1 Monat, Apr. 2018 - Apr. 2019

  Engineer Product Development

  AVIBRAS Indústria Aeroespacial S/A

  Responsible for impact/ballistic and explosion analysis, with Radioss solver. Carrying out the non-linear analysis to simulation the impact effects in the structure if a possible damage that Failure of turbine blade can raise. Definition of the specification and dimensions of the shield to mitigate possible damages. Perform Vibrations: modal frequency analysis considering the stress/strain response from PSD during operation and transportation missions, with OptiStruct solver.

• 1 Jahr und 10 Monate, Apr. 2016 - Jan. 2018

  Stress Engineer

  NOVAER CRAFT Aeronautical Ltda

  Collaborated in Stress analysis team of the B250 Bader all composite turboprop and checked conception, development and detail design of Main and Nose landing gears structures, Uplock box, Torque Arms, Sliding Members, beyond other components, with FE models and with hand methods (Bruhn, Niu, HSB). Researched, developed, and implemented bird impact analysis in WindShield and Leading Edge parts. Executed the linear and nonlinear stress analysis to evaluate metal and composite parts, flap, elevator systems.

• 3 Jahre und 6 Monate, Nov. 2012 - Apr. 2016

  Stress Engineer - FD&T

  AKAER Engenharia

  Responsible for F&DT analysis of ERJ 190 / 195 E2 center fuselage and KC-390 forward fuselage. Planned threshold and inspection interval according requirements (ANAC, FAA and EASA standards). Working in the Structural conception, stress analysis and optimization, preliminary and detail design of Machined Frames of Center Fuselage II (CFII). Team leader of 3 engineers, for stress analysis activities, for air conditioning test equipment another team of 2 engineers for stress analysis of KC-390 FWD.

• 1 Jahr und 11 Monate, Jan. 2011 - Nov. 2012

  Product Safety Engineer

  Ford Motor Company in Brazil

  Implemented and enforced procedure to roof impact analysis, to check the structure strength and integrity of occupants. Responsible for low speed crash analysis, Front and Rear, in order to check the vehicle integrity and damages generated by the impact between the car and the barrier.

• 6 Jahre und 10 Monate, Apr. 2004 - Jan. 2011

  System Stress Engineer

  FIBRAFORTE Engenharia, Indústria e Comércio Ltda

  Development of 5N-Thurster for Amazonia 1 Satellite and CBERS 3&4 Satellites performing the structural FE models. Perform modal analysis in order to verify natural frequencies and dynamic sinusoidal and random analysis, with the objective to calculate the safety margins in the welded regions, according to the launch environment specification. Perform static analysis to obtain the resultant loads to investigate the behaviour of central cylinder composite. Preparing VBA programs to check possible failures.