Stress – Static Engineer

Overview: Stress engineer Statics - 2- 3 Years **Responsibilities**: Knowledge of aircraft loads Experienced in spectrum generation, - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section) - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section, Flaps, Carriages) - Well versed...

Overview: Stress engineer Statics - 5- 6 Years **Responsibilities**: Knowledge of aircraft loads Experienced in spectrum generation, - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section) - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section, Flaps, Carriages) - Well versed...

Overview: - Extensive Knowledge of aircraft structure and aircraft loads - Experience on non-Airbus programs with a broad knowledge of hand calculations and not be FEM reliant - Expert in the static calculations for sizing and stress analysis of the aircraft structures, interfaces by means of hand calculations, valid methods, numerical simulations (FEM) -...

Overview: Stress - Static Composite, Fuselage - EFR **Responsibilities**: - Knowledge of aircraft Fuselage structure and aircraft loads - Experienced in the static calculations of Airbus aircrafts (fuselage section) - Knowledge and experience on composites and sandwich structures - Sizing and stress analysis of the fuselage Structure and interfaces by...

Responsibilities •Knowledge of aircraft Fuselage structure and aircraft loads • Experienced in the static calculations of Airbus aircrafts (fuselage section) • Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) • Well versed in ISAMI static modules and ISAMI template...

Responsibilities •Knowledge of aircraft Fuselage structure and aircraft loads • Experienced in the static calculations of Airbus aircrafts (fuselage section) • Knowledge and experience on composites and sandwich structures • Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations...

Overview: Knowledge of aircraft Fuselage structure and aircraft load Experienced in the static calculations of Airbus aircrafts (wing section) - Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) - Well versed in ISAMI static modules and ISAMI template preparation - Experience in...

Job Description : Static Analysis with Airbus Methods and Procedures. Minimum of 4 years execution experience on any of the two main Aircraft Primary structures (NCF, Center Fuselage, Empenage,Wing upper cover, VTP, HTP, Door Surrounds, Doors, Pylon) Minimum of 1 year execution experience on MSI, ESI, Hydraulic Brackets static stress analysis ...

Overview: Knowledge of aircraft Fuselage structure and aircraft load Experienced in the static calculations of Airbus aircrafts (wing section) Knowledge and experience on composites and sandwich structures Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) Well versed in ISAMI...

About UsAXISCADES is a technology solutions company focusing on engineering solutions and services. We bring expertise that caters to the engineering, technology, manufacturing and digital needs of fortune 100 clients in aerospace, defense, heavy engineering, automotive, energy & medical equipment sectors. With decades of experience in creating innovative,...

About UsAXISCADES is a technology solutions company focusing on engineering solutions and services. We bring expertise that caters to the engineering, technology, manufacturing and digital needs of fortune 100 clients in aerospace, defense, heavy engineering, automotive, energy & medical equipment sectors. With decades of experience in creating innovative,...

Overview: Static -Fuselage - 1 Opening **Responsibilities**: Knowledge of aircraft Fuselage structure and aircraft loads - Experienced in the static calculations of Airbus aircrafts (fuselage section) - Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) - Well versed in ISAMI static...

Job Description : Static Analysis with Airbus Methods and Procedures. Minimum of 4 years execution experience on any of the two main Aircraft Primary structures (NCF, Center Fuselage, Empenage,Wing upper cover, VTP, HTP, Door Surrounds, Doors, Pylon) Minimum of 1 year execution experience on MSI, ESI, Hydraulic Brackets static stress analysis ...

Técnicas Reunidas is a world leading international general contractor engaged in the engineering and construction of industrial facilities in the fields of Oil & Gas, Petrochemical, Power Generation, Energy Transition, Infrastructures and industries, etc. Tecnicas Reunidas has worked and built all over the world, in 60 countries of the 5...

Técnicas Reunidas is a world leading international general contractor engaged in the engineering and construction of industrial facilities in the fields of Oil & Gas, Petrochemical, Power Generation, Energy Transition, Infrastructures and industries, etc. Tecnicas Reunidas has worked and built all over the world, in 60 countries of the 5...

Job Description: Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMsExtraction of loads, stresses, generation of spectra and mission filesExtraction of material data, geometry details and fastener specifications from part & amp; assembly drawingsApplication of appropriate static, fatigue and damage...

Unspecified Overview: In this role, the Sr. Lead Engineer (Stress) will actively participate in structural analysis for NPI (New Product Introduction), redesign and technology programs of Actuation Systems business unit and will support various Actuation Systems product lines including Power Door Opening System (PDOS), Thrust Reverser Actuation...

RESPONSIBILITIES Ensure compliance with various ASME, API & IBR codes and standards.  Perform Pipe Stress analysis (Static & Dynamic) of Critical Piping Systems in accordance with ASME B31.3 Code Requirements, using CAESAR II software.  Knowledge of Stress Analysis for Compressor, Pumps, Air coolers piping system is preferred.  Perform flange...

Unspecified Overview: In this role, the Lead Engineer (Stress) will actively participate in structural analysis for NPI (New Product Introduction), redesign and technology programs of Collins Aerospace Actuation Systems business unit and will support various Actuation Systems product lines including Power Door Opening System (PDOS), Thrust...

Unspecified Overview: In this role the Principal Engineer-Cargo Systems will lead & support the structural validation thru detailed Stress Analysis activities for Cargo Systems components and check the detailed Stress report prepared by the Stress team. Position: Principal Engineer (P4) Primary Responsibilities: Responsible for stress...