You are here

Lubricant Condition and Wear Metal Analysis Sensor System (LUCAS)

Award Information
Agency: Department of Defense
Branch: Army
Contract: W911W6-09-C-0049
Agency Tracking Number: A082-025-0633
Amount: $729,136.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: A08-025
Solicitation Number: 2008.2
Timeline
Solicitation Year: 2008
Award Year: 2009
Award Start Date (Proposal Award Date): 2009-08-31
Award End Date (Contract End Date): 2011-08-30
Small Business Information
200 Canal View Blvd
Rochester, NY 14623
United States
DUNS: 073955507
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Carl S Byington
 Director, Systems Enginee
 (585) 424-1990
 carl.byington@impact-tek.com
Business Contact
 Mark Redding
Title: President
Phone: (585) 424-1990
Email: mark.redding@impact-tek.com
Research Institution
N/A
Abstract

Impact Technologies, in close collaboration with GasTOPS, Inc. and with the support of Boeing Rotorcraft Division and Sikorsky, proposes to develop a miniaturized, integrated, on-line sensing solution for detection of lubricant quality, metal wear debris and analysis of debris elemental composition for Army rotorcraft. The airworthy multi-sensor device created in this program will serve as a direct replacement for legacy chip detectors currently employed to detect metal particles in aircraft lubrication systems. The developed integrated LUCAS sensing technology will utilize mature technologies to: (1) detect and identify the source of wear debris, and (2) detect and classify numerous lubrication quality factors such as incorrect oil, water content, oil degradation, and fuel dilution that are life-limiting to oil-wetted components. The Phase II development will include merging and miniaturization of Impact’s electrochemical impedance spectroscopy (EIS) technology with GasTOPS’ proven metal debris sensing and analysis technologies that includes “at-line” energy-dispersive x-ray fluorescence (EDXRF) elemental analysis system. By the end of Phase II, the integrated, low-weight system will be evaluated and demonstrated in a realistic aircraft-style gearbox test rig.

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

US Flag An Official Website of the United States Government