Novel Non-Intrusive Vibration Monitoring System for Turbopumps

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$69,994.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
NNM05AA53C
Agency Tracking Number:
040175
Solicitation Year:
2004
Solicitation Topic Code:
X6.01
Solicitation Number:
n/a
Small Business Information
AI Signal Research, Inc.
3411 Triana Blvd. SW, Huntsville, AL, 35805-4641
Hubzone Owned:
N
Socially and Economically Disadvantaged:
Y
Woman Owned:
N
Duns:
799109194
Principal Investigator:
Jen-Yi Jong
Principal Investigator
(256) 551-0008
jjong@aisignal.com
Business Contact:
Kevin Barr
Business Official
(256) 551-0008
kbarr@aisignal.com
Research Institution:
n/a
Abstract
AI Signal Research, Inc. proposes to develop a Non-Intrusive Vibration Measurement System (NI-VMS) for turbopumps which will provide effective on-board/off-board fault detection diagnostic capabilities without relying on any intrusive installation of once per revolution (1/Rev) tachometer key phasor measurement. Many vibration signature analysis techniques use a key phasor signal to identify and detect critical vibration characteristics and fault signatures. However, in many operational environments (e.g., SSME HPOTP), the tachometer measurement is not available usually due to its intrusive installation requirement or safety consideration. For this situation, many powerful diagnostic analyses cannot be performed. With our system, we over come this problem by utilizing a novel signal analysis technique called Pseudo Key Phasor (PKP) to reconstruct an equivalent 1/Rev PKP signal directly from a non-intrusive vibration measurement. The resulting PKP signal enables the use of effective signature analysis to enhance diagnostic capabilities. The applicable innovation is attributed to to effectively achieve non-intrusive health monitoring and diagnosis without intrusive tachometer installation. This technology will enhance incipient fault detection capability, reducing catastrophic engine failure risks and improve reliability of NASA's advanced propulsion systems. Phase I objectives are to demonstrate the feasibility and relative benefits of NI-VMS non-intrusive monitoring capabilities.

* information listed above is at the time of submission.

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