Integrated Vehicle Health Management "Intelligent Engine" Turbopump Concept

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,823.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
FA9300-05-M-3011
Agency Tracking Number:
F051-201-1698
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
TURBO SOLUTIONS ENGINEERING LLC
PO Box 722, 16 Beaver Meadow Road, Norwich, VT, 05055
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
169816837
Principal Investigator:
Nicholas D'Orsi
Chief Engineer, Managing Partner
(802) 649-8710
ndorsi@turbosoleng.com
Business Contact:
Ralph Hobson
Project Engineer, Managing Partner
(802) 649-8710
chobson@turbosoleng.com
Research Institution:
n/a
Abstract
Turbo Solutions Engineering LLC is providing this proposal for a Phase I Small Business Innovation Research Program. The technical objectives are to demonstrate the feasibility of the integration of real-time performance monitoring and diagnostics within a turbopump system, to provide operational status data, and to predict the remaining life of critical components. This Integrated Vehicle Health Management (IVHM) System would provide information regarding the behavior and condition of the turbopump equipment, which would lead to technological improvements, reduce the design cycle time and development costs, and enable the turbopumps to operate for greater durations between expensive inspections and overhaul teardowns. Turbo Solutions Engineering LLC intends to leverage existing technologies and experience from other sectors of the aerospace and industrial marketplace to develop an IVHM system specifically adapted for use within turbopump systems. The IVHM system provides direct measurement of the condition and performance of critical components including bearings, shafts, impellers, seals and casings in the turbopumps. This Phase I proposal can be leveraged in cooperation with Applied Astronautics Corporation's current AFRL Hydrocarbon-Fueled Innovative Rocket Engine (HyFIRE) program, which involves a liquid oxygen/methane turbopump development effort. The HyFIRE turbopump can serve as a future test-bed for the IVHM turbopump system.

* information listed above is at the time of submission.

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