Stress - Static Composite

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...

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...

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: - 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) -...

Responsibilities Knowledge of aircraft structure and aircraft loads • Experience on non-Airbus programs with a broad knowledge of hand calculations and not be FEM reliant • Experienced in the static calculations for sizing and stress analysis of the aircraft structures, interfaces by means of hand calculations, valid methods, 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: 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...

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,...

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 ...

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...

Versatile experience on Analysis of Primary & Secondary (Fuselage, Wing and Empennage) structures - Good working experience in MRB / Concession on Metallic and Composite primary and Secondary structures - Airbus project exp is must - Very Strong knowledge on Strength of Materials and Engineering Mechanics - Expertise in Static and Fatigue and Damage...

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: 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...

Overview: Good Knowledge on Aerospace domain, structure, loads & Aircraft drawing Experience on the Stress Assessment for Aircraft wing components concessions. In depth knowledge of stress, fatigue and damage tolerance analysis of metallic structures (Fatigue analysis as per M2841) Effect of non-conformities of metallic and composite structures (good...

Job Description for **Aero-structure Design Engineers** - Experience with CATIA V5 on Aircraft structures and/or Airframe Design, Doors/Wings/HTP/VTP/Pylon and MSI. - Legacy conversion of Primary and secondary structural components Using Catia V5 (Machined, Sheet metal, Extruded, Metallic & Composite parts) - Strong experience in design, 3D modelling of...

**MSI JD** **1. Experience with CATIA V5 on Aircraft structures and Mechanical system installation (MSI)** **2. AIR CONDITIONING AND PRESSURIZATION (ATA 21)** **3. EQUIPMENT/FURNISHINGS (ATA25)** **4. HYDRAULIC POWER (ATA29)** **2. Airbus standards and process** **3. **PASS and VPM Certification Mandatory.

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...