SBIR/STTR Research Award

A Data-Driven Digital Twin Approach for the Aging Prediction of Airworthiness of Aircraft Composite Components Accounting for Flight and Environmental

Award identifier 30b8f2ea1039d93b8cb8584a335c6b8097b997dd8aaccf65d85b8f12016400d5Awarding agency Department of Defense · Navy

Award amount

$1,999,720

Program and phase

SBIR · Phase II

Award year

2022

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
CMSOFT, INC.
Proposal award date
2022-06-30
Contract end date
2025-12-31
UEI
CMZ6LMJZAMS3
Solicitation number
21.1
Topic code
N211-019

Research abstract

The main objective of this SBIR effort is two-fold. First, to develop a digital twin of an aircraft structure and its composite components capable of accurate aging predictions for any mission-specific loading and environmental variability, in a manner that enables the assessment of the structural airworthiness of the aircraft and its composite components from a damage tolerance perspective. Second, to identify potential multiphysics trade-offs to enable accelerated testing. To this end, the detailed technical objectives for Phase II are to: Extend the multiphysics MDD (multiphysics data-driven modeling approach) developed during Phase I to enable the increased fidelity associated with capturing aging-induced damage. Generalize the MDD -NPM (nonparametric probabilistic method for model-form uncertainty (MFU)) computational framework developed in Phase I to an arbitrary number of levels (coupon, element, subcomponent, component, aircraft), to minimize MFU and test uncertainty introduced at each level, thereby leading to the construction of a robust digital twin instance of a structural system that can replace the current role of the building block approach (BBA) for qualification and sustainment operations. Validate this multiphysics framework using laboratory tests that simulate the in-service loading environment for different blocks of the BBA. Demonstrate that the MDD-NPM framework is functional with actual data from multiaxial testing at the coupon, subcomponent, and component levels. Equip the MDD-NPM computational framework with a fast approach for identifying potential multiphysics trade-offs to enable accelerated testing. Develop ASLM (aircraft structural life management), a set of minimally intrusive software modules for this computational framework and a universal interface between this software end product and third-party CFD, FEA, and coupled CFD-FEA solvers to ease the commercialization of ASLM.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

26 SBIR/STTR records share this UEI (2005–2025). Reported award amounts total $12,259,379. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

Department of Defense

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