Structural Sizing Software optimizes design of composites.
May 31, 2012 -
Intended for spacecraft/aviation industries, HyperSizer® v6.2 targets weight while serving as independent and neutral data exchange hub for CAD, FEA, and composite software. Program iterates with FEA solvers, calculates margins of safety, validates failure predictions with test data, and sequences composite laminates for fabrication, avoiding weight growth as designs mature. Version 6.2 includes modeling capabilities for airframe wing box designs, as well as laminate zone and ply-count optimizations.
|Original Press release |
Collier Research Corporation
760 Pilot House Dr. Suite A
Newport News, VA, 23606
HyperSizer v6.2 from Collier Improves Design and Manufacturability of Composites and Metals
NASA-developed software cuts structural weight on average 20 percent
Hampton, VA, -Collier Research Corporation today announced the release of HyperSizer®v6.2 structural sizing and analysis software. The latest version of the product, which is used widely in the spacecraft and aviation industries, includes new modeling capabilities for airframe wing box designs, and laminate zone and ply-count optimization enhancements to improve manufacturing efficiency.
"Composites are booming due to stepped-up fuel consumption efficiency goals," says Craig Collier, president of Collier Research. "This is pushing the movement towards light-weighting. But creation of lighter, stronger designs is limited by many of today's standard industry practices. Weight is needlessly added because engineers have only a partial view of options. They often overdesign to play it safe."
To overcome such drawbacks, HyperSizer targets weight while serving as an independent and neutral data exchange hub for CAD, FEA, and composite software packages. It iterates with FEA solvers, calculates margins of safety, validates failure predictions with test data, and sequences composite laminates for fabrication-avoiding weight growth as designs mature.
"HyperSizer works from preliminary design through flight certification," says Collier. "This gives the engineering team a more wide-open conceptual design space for performing trade studies involving thousands of alternatives. They can find robust solutions that lead to significant weight and cost savings. On average our customers reduce weight by 20 percent."
"In the past, our designs were often overweight," says Ian Fernandez, former materials and analysis lead on NASA Ames Research Center's LADEE satellite project. "HyperSizer has enabled our Center to be more competitive in this regard. It's a robust analysis tool that allows us to complete our weight and strength studies in far less time, while finding optimal ply coverages."
HyperSizer has been used on a wide variety of NASA spacecraft projects including the current Space Launch System (SLS) rocket, previous Ares I and V launch vehicles, the Composite Crew Module, and the metal Orion Multi-Purpose Crew Vehicle. Commercial aviation customers include Boeing, Bombardier, Goodrich, Gulfstream, and Lockheed Martin. HyperSizer's capabilities are also appropriate for applications in wind turbine blades, ship hull and superstructures, high-speed railcars, and automobile body components.
New features and enhancements in HyperSizer v6.2 include:
o Discrete Stiffener Modeling - For airframe wing box and fuselage structures, the software automatically identifies in the FEM, skin shell and stiffener beam elements and optimizes their spacings, heights, and laminates. This provides the flexibility for designing panel bays with non-uniformly spaced stiffeners of varying directions, dimensions, and materials, while also assigning margins to each unique stiffener panel segment.
o Laminate Optimization for Manufacturability -An improved, six-step process optimizes laminates (transition zones, ply-count compatibility, ply drops/adds, global ply tracking) while balancing strength, stability, and manufacturability. This leads to fabrication efficiencies and factory-floor cost-savings.
o Other enhancements - New puck composite failure analysis for both 2D and 3D fiber fracture; new curved (skin) local buckling analysis; upgraded compression and shear postbuckling analyses; enhanced panel concepts (PRSEUS, reinforced core sandwich, and tapered tube beam); improved test data and other graphical displays and functions; and new methods documentation.
Collier Research will be demonstrating HyperSizer v6.2 at the upcoming SAMPE (Society for the Advancement of Material and Process Engineering) conference, Booth 1049, May 22-24 in Baltimore, MD.
For more information about HyperSizer v6.2, please visit www.hypersizer.com. For v6.2 PowerPoint: http://hypersizer.com/download.php?file=9103_HyperSizer-Whats_New-Version_6.2%20(ja)%202012-04-12.pdf
About Collier Research Corporation
Collier Research Corporation is a trusted industry leader, providing engineering software for aerospace and NASA, offering structural tools, methods research, and software solutions with its flagship product, HyperSizer. HyperSizer performs stress analysis and sizing optimization, reducing the weight of aircraft and space vehicles-whether designed with composites or traditional metallic materials. HyperSizer is developed by engineers, for engineers, and is currently being used by NASA on the Heavy Launch Vehicle and by industry leaders such as Boeing, Lockheed Martin, Goodrich, Bombardier, and Gulfstream for commercial transport planes and business jets. Collier is currently collaborating with Sandia National Laboratories Wind Energy Technology Department on the use of optimization in wind turbine blade prototype design. For more information, visit www.hypersizer.com