SBIR-STTR Award

Global/Local Methodology for Optimum Design of AAAV Structures
Award last edited on: 4/2/2002

Sponsored Program
STTR
Awarding Agency
DOD : Navy
Total Award Amount
$697,092
Award Phase
2
Solicitation Topic Code
N99T002
Principal Investigator
Scott Ragon

Company Information

Adoptech Inc

2000 Kraft Drive Suite 1204
Blacksburg, VA 24060
   (540) 961-9190
   N/A
   www.adoptech.com

Research Institution

Virginia Polytechnic Institute and State University

Phase I

Contract Number: N00014-99-M-0253
Start Date: 1/1/2006    Completed: 12/1/1999
Phase I year
1999
Phase I Amount
$98,292
TThe designers of the Advanced Amphibious Assault Vehicle (AAAV) face a number of technical challenges which include developing methodologies for estimating the actual structural loads, predicting critical structural responses, and estimating the vehicle's reliability. In addition, the development of a design methodology for minimizing the cost and weight of the vehicle is critical to the success of the program. We propose to develop a global/local software environment for integrating design and analysis tools. Included will be tools for modeling rough terrain and blast loads, performing nonlinear finite element analysis, and estimating the reliability of the structure. ADOPTECH's university partner has considerable experience in each of these critical technological areas and will be responsible for adapting existing design and analysis methodologies as well as developing innovative new methods for use in the software environment.

Benefits:
The proposed project will provide the Navy, the Marine Corps, and their contractors with a capability to optimize components or subsystems of an AAAV for reduced cost and weight while maintaining high performance and reliability. The optimization approach will allow designers to determine those components that can be downsized and those that need to be reinforced to achieve minimum cost and weight of the entire structure. The proposed global/local design methodology will allow existing and future design and analysis codes to work together in a common vehicle design environment and will provide a platform for integrating future analysis packages.

Keywords:
Global/local design methodolog Non-Linear Finite Element Anal Global/Local Design Optimum Design Reliability Global/local design methodolog Non-Linear Finite Element Anal Global/Local Design Optimum Design Reliability

Phase II

Contract Number: M67854-00-C-3050
Start Date: 8/24/2000    Completed: 8/24/2002
Phase II year
2000
Phase II Amount
$598,800
The major objective of Phase-II is to develop a set of software tools for implementation of the global/local design methodology demonstrated in Phase-I. The proposed software will provide design engineers with a web-based graphical user interface and a set of tools that will allow them to use their existing design codes to implement the global/local design methodology for a variety of design problems. During the first year, the methodology will be extended to include improved local design models relevant to AAAV design, and the software tools will be developed with the immediate goal of assisting GDAS engineers in reducing the AAAV structural weight. Information and experience gained during this AAAV design process will be used to refine and validate the software. A beta version of the software will be delivered to GDAS at the end of the first year of work. The second year of the proposed work will concentrate on refining the software tools generated in the first year and commercializing the software. During this time, ADOPTECH will provide technical support to the GDAS engineers using the beta software. In parallel with the software development effort in the first year, the university research team will pursue a research plan aimed at including reliability and load updating methodologies in the design process. If the Phase-II option is exercised, the university research team will demonstrate the reliability and load updating tools and methodologies using the AAAV structure. Knowledge and tools generated by the university team will be used after the completion of Phase-II to enhance the baseline software product.

Benefits:
The software tools developed during the Phase-II effort will provide the immediate benefit of assisting GDAS engineers in reducing the weight of the AAAV vehicle. Although the initial focus of the Phase-II project will be the AAAV structure, the global/local design methodology presented is a general design procedure, and is not limited to any particular application. The original motivation for the development of the present global/local methodology arose out of industry's need for an affordable approach for applying optimization techniques to the design of complete structural systems. Presently, industry uses optimization techniques to design the overall structure, but local details are often neglected until late in the design process. This practice is often not satisfactory, as unexpected local failures require costly redesign efforts. The software proposed for Phase-II would give customers in the aerospace, automotive, and related industries a new and unique capability for designing complex structures in a computationally efficient manner while taking into account these important local details.

Keywords:
Design Optimization Reliability Structural Optimization Global/Local Design Optimal Design