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Grid Structures

WHAT THE ADVANCED LATTICE/GRID STRUCTURES (A.G.S.) ARE

Grid stiffened structures are shells supported by a grid lattice of stiffeners used as a possible replacement to monocoque, skin-stringer, and honeycomb sandwich structures

BENEFITS OF GRID STRUCTURES

ENVIRONMENTAL ROBUSTNESS

  • Significantly higher damage tolerance than honeycomb sandwich
  • Tendency to contain delamination to within one cell (open cell feature)
  • Do not absorb and retain water over their lifetime, unlike honeycomb sandwich structures.

LOW-COST MANUFACTURING
Automated and single cure process (not hand operations are involved)

STRUCTURAL EFFICIENCY

  • Stiffer in plane and less stiff out-of-plane: a grid structure design tends to be preferable when deflection or fundamental frequency requirements govern the design space. Sandwich structure designs are preferable when global buckling is the driving factor
  • From 20% up to 61% lighter, 300% stronger, and 1000% stiffer than the aluminum structure it replaces
  • Thermal stability

DRAWBACKS OF GRID STRUCTURES

  • The complexity of a grid pattern can lead to excessive manufacturing times
  • Temperature swings due to very nature asymmetric through the thickness
  • Tooling is significantly more complex than tooling for sandwich structures

How we make Advanced Grid Structure: engineering & manufacturing capabilities

1 • ENGINEERING PHASE: Design (CATIA V5) & Stress analysis (Nastran/Patran)

Lattice Design Structure (IJERT source)

Stress Distribution with Skin and Stringers (IJERT source)

 2 • MANUFACTURING ENGINEERING PHASE: Tooling & Manufacturing process

3 • MANUFACTURING: 3D Stitching/Tufting automated process

3D Stitching machine head

Zoom on multi cross node

Cured multi-cross node

CFRP ANISOGRID cylinder elementary module

Kevlar-reinforced dry preform flat CFRP grid

We are working for European Space Agency

OUR PROPOSALS

Russian experience heritage.
Central Research Institute of Special Machinery.

 

 

FURTHER APPLICATIONS:

  • Wing structures
  • Fuselage and Rudder panels
  • Payload and cargo Floor
  • AircTail Cone
  • Rocket’s interstages
  • Payload adapters
  • Spacecraft central cylinders
  • Antenna booms

GRID PATTERNS

The possibility to vary the number and change the positioning of the ribs, rings and vertical hoops allows the creation of n. 5 different regular and symmetric grid pattern

  • the orthogrid made by the intersection of horizontal rings and vertical hoops (Fig. 1);
  • the diamond grid made by the intersection of helicoidal ribs (Fig. 1);
  • the isogrid made by the intersection of helicoidal ribs and horizontal rings (Fig. 3);
  • the triangle & rectangle grid made by the intersection of helicoidal ribs, horizontal rings and vertical hoops (Fig. 4);
  • the kagome grid, similar to the isogrid, having the horizontal rings do not intersect the helicoidal ribs in their point of intersection, in this way the pattern is a hexagon with 6 triangles build on his sides (Fig. 5).

Fig. 1- Orthogrid

Fig. 2 – Diamond grid

Fig. 3 - Isogrid

Fig. 4 – Triangle rectangle grid

Fig. 5- Kagome grid

The shape and the number of the grid patterns will be defined according to materials Systems Geometry and Shape

SATOR capabilities in design and configuration evaluation

The possibility to vary the number and change the positioning of the ribs, rings and vertical hoops allows the creation of n. 5 different regular and symmetric grid pattern

CATIA V5 Model

CATIA V5 Model: intersection detail

SATOR capabilities in design and stress analysis

3D isogrid structure view - BUCKLING ANALYSIS made with Nastran Patran

Grid intersection detail: mesh

3D isogrid structure view

SATOR capabilities in manufacturing and technical feasibility

Grid structure specimen lamination