Automated Health Management for Gas Turbine Engine Accessory Components

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,560.00
Award Year:
2006
Program:
SBIR
Phase:
Phase I
Contract:
FA8650-06-M-2641
Agency Tracking Number:
F061-171-0473
Solicitation Year:
2006
Solicitation Topic Code:
AF06-171
Solicitation Number:
2006.1
Small Business Information
IMPACT TECHNOLOGIES, LLC
200 Canal View Blvd, Rochester, NY, 14623
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
073955507
Principal Investigator:
Carl Byington, P.E.
Director of R&D
(814) 861-6273
carl.byington@impact-tek.com
Business Contact:
Mark Redding
President
(585) 424-1990
mark.redding@impact-tek.com
Research Institution:
n/a
Abstract
Impact Technologies, LLC proposes to develop embeddable software modules for autonomous health management of gas turbine engine accessory components, including actuators, valves, pumps, APUs, and other auxiliary components. As part of the proposed approach, customized physical models will be generated to determine changes in component health using only control command/response data. This proven model-based approach will be fused with innovate signal processing and classification techniques, again operating on control data, to provide a confident assessment of component health. Remaining useful life predictions will also be generated (if sufficient trending data is available) using a suite of trending algorithms and novel tracking methods. This effort will build upon ongoing development of similar technologies for flight control actuators/valves and aircraft generators, as well as previous development of health management for aircraft pumps. As part of this program, available historical data will be evaluated to 1) customize the existing suite of algorithms and models that have been developed for similar systems and 2) identify precursors to impending failures that can be used to increase detection horizon and prediction capability. The proposed algorithms/models will be developed with considerations to a number of implementations, including on-component (embedded within the component, possibly displayed through an LED indicator), on-engine (embedded with the engine controller or similar processing unit), and at-wing (as part of an at-wing automated test equipment package), in order to maximize commercialization and transition potential. False alarm mitigation techniques, such as sensor validation and feature separability analysis, will also be implemented to ensure system reliability. Although the effort will strive to utilize only existing engine sensors, a distributed system of low-overhead (low-cost, low-weight, low-power) sensors will be implemented if the existing suite does not provide sufficient fault coverage.

* information listed above is at the time of submission.

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