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AerospaceAerospace

e-Xstream offers the aerospace industry the technology and expertise to considerably reduce the cost and time needed to develop innovative and higher quality composite materials and structures.
Process DescriptionProcess Description
DIGIMAT is a predictive software platform aimed at modeling the linear and nonlinear behaviors of multi-phase materials such as Carbon Fiber Reinforced Plastics (CFRP), honeycomb sandwich structures, short fiber reinforced thermoplastics or any other multi-phase material used in aerospace applications.

Airplane, space craft manufacturer and their suppliers start by using Digimat-MF  and Digimat-FE to study the thermo-mechanical behavior of material lab samples. Digimat to CAE is then used to predict the influence of the material microstructure on the structure end performance.

Material suppliers can also use DIGIMAT to develop advanced materials and support the needs of their customers in the optimal use of those materials.




Reference CustomersReference Customers
  • DIGIMAT is a powerful tool that is giving us a new insight into our composite polymers. Its ability to model thermal expansion as a function of temperature, for instance, has been instrumental in understanding some subtle mechanism of warpage of injection molded parts.Vito Leo, Principal Scientist, Solvay Advanced Polymers
  • Digimat-MF homogenisation approach allows accurate prediction of the composite material stiffness, Lucien Douven, Design Engineer, DSM Engineering Plastics


Targeted Materials & ApplicationsTargeted Materials & Applications

CFRP:

  •  Structural parts
  •  Interior parts
  •  Engine parts
  •  Satellite antennas
  •  Etc.

Honeycomb Sandwich Structures:

  • Structural parts
  • Interior parts
  • Engine covers
  • Etc.

Rubber:

  •  Aircraft tires
  •  Anti-vibration systems
  •  Fluid transfer hoses
  •  Seals
  •  Etc.

Graphite:

  • Brakes
  • Etc.

Hard Metals:

  • Landing gear
  • Etc.
Targeted PerformanceTargeted Performance
  • Structural stiffness
  • Vibration frequencies and modes
  • Damage under cyclic loading

  • Failure under quasi-static loading
  • Failure under crash loading
  • Shape stability (large temperature gradients)
  • Etc.

Related Materials and ProductsRelated Materials and Products
Thermo-mechanical analysis of a parabola. Courtesy of ESA/ESTEC
FE model of parabola. Courtesy of ESA/ESTEC

CASE STUDIESCASE STUDIES

DocumentationDocumentation

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