Store/Aircraft Interface Force Measurement System

Award Information
Agency:
Department of Defense
Amount:
$69,931.00
Program:
STTR
Contract:
N68335-09-C-0339
Solitcitation Year:
2009
Solicitation Number:
2009.A
Branch:
Navy
Award Year:
2009
Phase:
Phase I
Agency Tracking Number:
N09A-003-0335
Solicitation Topic Code:
N09-T003
Small Business Information
Progeny Systems Corporation
9500 Innovation Drive, Manassas, VA, 20110
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
945837219
Principal Investigator
 Ed Michna
 Principal Investigator
 (401) 846-0111
 emichna@progeny.net
Business Contact
 Christine Sigety
Title: Manager of Business Support
Phone: (703) 368-6107
Email: csigety@progeny.net
Research Institution
 University of Massachusetts Dartmou
 Julie Smith
 151 Martine Street
Fall River, MA, 2723
 (508) 910-9829
 Nonprofit college or university
Abstract
Naval air platform stores include various payloads including ordinance. Fatigue induced failures can occur without warning at the interface between the payload and the airframe hardpoints. There is currently no systematic means of monitoring, recording, and tracking the forces which lead to fatigue and eventual catastrophic failure of the store hangers or their attachment points. A system of sensors is required to accurately measure transmitted forces and moments that will be fed into a predictive fatigue model for these components. Acceleration measurements cannot be used to explicitly measure forces and moments that are required for use in predicting cumulative fatigue damage. Additionally, direct strain measurements are difficult to correlate to transmitted forces and moments due to placement and orientation sensitivity, as well as averaging errors that occur due to measurement of strain gradients. Direct measurement of the transmitted forces and moments is required. Our solution is focused on innovative sensor placement across all load axes combined with using the deformations that occur across the store interface structure in response to applied loads, in order to measure force and moment time histories. Macro Fiber Composite (MFC) piezoelectric smart materials will be assessed for the primary sensor element.

* information listed above is at the time of submission.

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