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Regime Recognition System

Award Information
Agency: Department of Defense
Branch: Office of the Secretary of Defense
Contract: DAAH01-03-C-R187
Agency Tracking Number: O012-0232
Amount: $0.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Solicitation Year: N/A
Award Year: 2003
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
13029 Danielson Street, Suite 200
Poway, CA 92064
United States
DUNS: 097858836
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Thomas Brotherton
 Principal Investigator
 (858) 679-4140
Business Contact
 Laura Goodrich
Title: Vice President, Contracts
Phone: (858) 679-4140
Research Institution

Accurate usage information collected by Health and Usage Monitoring Systems (HUMS) coupled with improved structural fatigue life calculation methodologies promise to reduce helicopter operational and support costs while maintaining current flight safetylevels. Current fatigue life calculations assume worst-case flight profiles in determining component life. This approach may be outdated or not reflective of actual aircraft usage.IAC proposes to develop and demonstrate a low cost regime recognition capability as an extension to the US Army's Vibration Management Enhancement program and related UH-60 engine diagnostic system. Our approach relies on multi-sensor data fusiontechnology and flight parameters collected by the VMEP to provide an accurate flight regime calculation. Recording time in particular flight regimes has the potential of extending aircraft component life without changing proven lifing models. IACdemonstrated that existing UH-60 aircraft parameters can be used to calculate aircraft gross weight and flight regime during the Phase 1 effort.Proposed technologies will: 1) Provide actual flight time, take off and landings, turns and climbs 2) Develop an inferred gross weight calculation 3) Create tools for modification of algorithms and parameters and comparison with established componentdamage tables The potential commercial applications for the technology, techniques, and systems to ultimately come out of this SBIR are significant. Sikorsky Aircraft, a partner on Phase I and II, is interested in applying the technology developed here to their ownhelicopters. If the Phase II is successful, Sikorsky will be a potential Phase III transition / commercialization partner. The technology to be developed here can be applied to significantly improve automated usage monitoring and condition-basedmaintenance of all military and commercial aircraft as well as all commercial / industrial gas turbine engines (such as those used in electrical generation plants).

* Information listed above is at the time of submission. *

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