You are here

Improved Process Controls for the Laser Drilling of Small Holes(1000-989)

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-07-C-0176
Agency Tracking Number: N052-100-0048
Amount: $996,828.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N05-100
Solicitation Number: 2005.2
Timeline
Solicitation Year: 2005
Award Year: 2007
Award Start Date (Proposal Award Date): 2007-09-27
Award End Date (Contract End Date): 2010-03-18
Small Business Information
200 TURNPIKE ROAD
CHELMSFORD, MA 01824
United States
DUNS: 796010411
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Thomas McDonald
 Principal Investigator
 (978) 250-4200
 tmcdonald@tritonsystems.com
Business Contact
 Francis Veronesi
Title: Controller
Phone: (978) 250-4200
Email: contracts@tritonsystems.com
Research Institution
N/A
Abstract

Triton Systems, Inc., in partnership with the General Electric’s Laser Laboratory and the National Aerospace Leadership Initiative (NALI) funded Connecticut Center for Advanced Technology (CCAT), is developing the concurrent use of multiple sensor types and optical measurement methods to collect data. This data is then processed by an integrated control system to generate a real-time, corrective adjustment to the laser cooling hole drilling process for gas turbine components. The control system will collect data from acoustic, optical and spectral sensors related to the laser pulse and plasma plume, as well as from optical imaging devices relating to the cooling hole size, shape and positional coordinates. It will then process and compare the collected data to a data base previously characterized and correlated to targeted airflow values which have been specified for a particular gas turbine component. The real-time, in-process comparison will drive an appropriate compensating change in the laser process parameters to more closely control laser drilled hole geometry and thus cooling airflow. Tighter control of airflow will result in longer turbine component life, reduced overall production cycle times and costs and gas turbine efficiencies.

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

US Flag An Official Website of the United States Government