Anisopter

The affordable solution for the rapid sizing of anisogrid structures.

Get a FREE TRIAL code at info@anisopter.com to quickly optimize your favorite cylindrical shell.

TRY DEMO v1.48

Credit: Unknown (from Tokkoro)

Why Anisogrid?

Anisogrid structures are the game-changing technology to save weight, reduce costs, and improve performance in modern spacecrafts and launchers.
Although transition to anisogrid is driven by the 14,000 €/kg of sending payloads to Space, Earth markets will also obtain important savings.




Anisopter

ANISOPTER on Earth

provides important benefits for companies developing high-performance structures where weight and cost efficiency is critical, like towers for electricity transport or wind power generation.


Credit: Stephane_Corvaja (Arianespace) - Vega-VV06 LISA-Pathfinder

Current state of development

ANISOPTER service is being implemented by ezeQ Apps and validated with our collaborator entities.



Credit: ESA-Stephane Corvaja, 2015 (source)

Quick Start

Contact us at info@anisopter.com to get a FREE TRIAL code.

Please, scroll down to test a predefined example or optimize your favorite cylindrical shell.

Basic workflow:

  • 1. Optimize the shell.
  • 2. Adjust optimal dimensions for manufacture. IN TESTS!
  • 3. Online FEA asessment of the model. IN TESTS!
  • 4. Visualize the 3D model and download it. AVAILABLE SOON!


Credit: NASA HQ PHOTO, 2016 (source)

Anisogrid cylindrical shell optimization
Please, select some example to display its technical info.


Anisogrid ribs type
  • Select at least one rib model to perform the optimization.
  • More than one model can be selected to compare with.
  • Including other non-anisogrid design concepts, like tubes or isogrids, is also possible!
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Material
  • Once you select the desired material on the drop-down list, all required material properties will be automaticaly loaded.
  • Alternatively, introduce your favorite properties, they will be stored in "Custom material" for further use.
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Strength
[MPa]
Stiffness
[GPa]
Density
[kg/m3]

Geometry
  • Length of the cylinder [m].
  • Diameters [m] of the cylinder or tapered tube. Leave this field empty to optimize diameter.
  • Thicknesses [m]. Wall thicknesses of the shell at bottom and top (tapered).
  • Tube wall [m]. Wall thickness for tubular ribs ONLY. NOT-AVAILABLE YET!
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LengthDiameters [m]Thicknesses [m]
[m]
Base
Top
Base
Top
Rib wall

Loads
  • Axial compressive force [N]. Applied on top. Compressive forces are positive.
  • Transverse force (top) [N]. Applied on top.
  • Bending moment [N·m] applied on top. E.g. the bending moment caused by a transverse force or the torque of a wind power generator (both applied on top).
  • Self weight. Check this box to consider the weight of the structure. Important in towers.
  • Lateral wind. ONLY for anisogrids with circular cross-section ribs! You can select Eurocode (EN 1991-1-4:2005) or Hoerner's aerodynamics book 1965 (it is based on pure aerodinamic considerations). Eurocode model is safer.
  • Wind category from Table 4.1 in Eurocode EN 1991-1-4:2005: 0= Sea or coastal area exposed to the open sea, 1= Lakes or flat and horizontal area with negligible vegetation and without obstacles, 2= Area with low vegetation such as grass and isolated obstacles (e.g. trees or buildings) with separations of at least 20 obstacle heights(default), 3= Area with regular cover of vegetation or buildings or with isolated obstacles with separations of maximum 20 obstacle heights (such as villages, suburban terrain, permanent forest), 4= Area in which at least 15 % of the surface is covered with buildings and their average height exceeds 15 m.
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Axial compressive force [N]
Transverse force [N]
Bending moment [N·m]
Self-weight

Wind
  • Lateral wind. ONLY for anisogrids with circular cross-section ribs! You can select Eurocode (EN 1991-1-4:2005) or Hoerner's aerodynamics book 1965 (it is based on pure aerodinamic considerations). Eurocode model is safer.
  • Wind category from Table 4.1 in Eurocode EN 1991-1-4:2005: 0= Sea or coastal area exposed to the open sea, 1= Lakes or flat and horizontal area with negligible vegetation and without obstacles, 2= Area with low vegetation such as grass and isolated obstacles (e.g. trees or buildings) with separations of at least 20 obstacle heights(default), 3= Area with regular cover of vegetation or buildings or with isolated obstacles with separations of maximum 20 obstacle heights (such as villages, suburban terrain, permanent forest), 4= Area in which at least 15 % of the surface is covered with buildings and their average height exceeds 15 m.
  • Roughness glass 0.0015, polished metal 0.002, fine paint 0.006, spray paint 0.02 bright steel 0.05, cast iron 0.2, galvanised steel 0.2, smooth concrete 0.2, planed wood 0.5, rough concrete 1.0, rough sawn wood 2.0, rust 2.0, brickwork 3.0.
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Lateral wind Solid
Base velocity [m/s]
Category
Roughness [mm]

Constraints
  • Shell boundary. Boundary conditions for Euler-buckling of the whole shell.
  • Ribs boundary. Boundary conditions for Euler-buckling of the ribs (local ribs buckling). In Variable boundary conditions, the ribs end-fixity constants depend on neighboring members thickness (ONLY available yet for Rectangular ribs).
  • Axial stiffness. Expresed as minimum axial stiffness [N/m] or as maximum axial displacement [m] allowed.
  • Axial min. frequency [Hz]. Minimum frequecy allowed in the axial direction.
  • Lateral min. frequency [Hz]. Minimum frequecy allowed in the lateral direction.
  • Mass on top [kg]. Mass attached to the free end of the shell. ONLY considered in the Clamped-Free shell boundary conditions (Cantilever beam). If empty, only self-mass will be considered in resonance frequency calculations.
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Shell boundary
Helical Ribs boundary
Hoop ribs boundary
Lateral max. shift [m]
Axial min. frequency [Hz]
Lateral min. frequency [Hz]
Mass on top [kg]

Advanced options
φ [º]  # Helical ribs  # Hoop ribs
Min
Max
  Min
Max
Step
  Min
Max
Step
Screen diameters [m]
Min
Max
Step


*Contact us at info@anisopter.com for a free trial code.

Adjust final geometry
  • Adjust final cylinder dimensions to fulfill manufacturing (or other) constraints.
  • Note that forces, boundary conditions, and other constraints will be taken from optimization form.
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Anisogrid ribs type
LengthDiameters [mm]Ribs/FEs [#]
[m]
Base
Top
Helical
Hoop
Diameters/Thicknesses [mm]
Helical,
Hoop, or
End ribs
Wall Thicknesses [mm]
Shell Ribs
Base
Top
Helical,
Hoop, or
End ribs

Finite Element Analysis
  • Perform a fast Finite Element Analysis to validate the optimized geometry.
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Nodes/beam Modes Element Boundary conditions
[#]
[#]
type
Bottom
Top
Straight beams
ANSYS   Element Type

FEA results will be shown here...