Fault localization for gear tooth failure in coupled mechanical systems

Jeffrey C. Banks; Mitchell Lebold; Karl Martin Reichard

doi:10.1109/AERO.2003.1234173

Fault localization for gear tooth failure in coupled mechanical systems

Jeffrey C. Banks, Mitchell Lebold, Karl Martin Reichard

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

The purpose of this paper is to discuss the results from a fault localization survey that was conducted using the Dual Gearbox Mechanical Diagnostic Test Bed. The test involved using two DC motors to drive and load two single reduction gear boxes coupled in series. An array of sensors including vibration, torque and temperature were used to.monitor each gearbox during a baseline and a seededhransitional gear fault test. The data was analyzed in order to evaluate the sensor types and locations and their ability to provide an indication and localization of a fault. The ultimate goal of this work is to find the least number of sensors that provide the greatest fault indication coverage for coupled mechanical systems.

Original language	English (US)
Title of host publication	2003 IEEE Aerospace Conference, Proceedings
Pages	3295-3304
Number of pages	10
DOIs	https://doi.org/10.1109/AERO.2003.1234173
State	Published - Dec 1 2003
Event	2003 IEEE Aerospace Conference - Big Sky, MT, United States Duration: Mar 8 2003 → Mar 15 2003

Publication series

Name	IEEE Aerospace Conference Proceedings
Volume	7
ISSN (Print)	1095-323X

Other

Other	2003 IEEE Aerospace Conference
Country/Territory	United States
City	Big Sky, MT
Period	3/8/03 → 3/15/03

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science

Access to Document

10.1109/AERO.2003.1234173

Cite this

@inproceedings{895cbbd3077748b083c19a1ca27d6c3f,

title = "Fault localization for gear tooth failure in coupled mechanical systems",

abstract = "The purpose of this paper is to discuss the results from a fault localization survey that was conducted using the Dual Gearbox Mechanical Diagnostic Test Bed. The test involved using two DC motors to drive and load two single reduction gear boxes coupled in series. An array of sensors including vibration, torque and temperature were used to.monitor each gearbox during a baseline and a seededhransitional gear fault test. The data was analyzed in order to evaluate the sensor types and locations and their ability to provide an indication and localization of a fault. The ultimate goal of this work is to find the least number of sensors that provide the greatest fault indication coverage for coupled mechanical systems.",

author = "Banks, {Jeffrey C.} and Mitchell Lebold and Reichard, {Karl Martin}",

year = "2003",

month = dec,

day = "1",

doi = "10.1109/AERO.2003.1234173",

language = "English (US)",

isbn = "078037651X",

series = "IEEE Aerospace Conference Proceedings",

pages = "3295--3304",

booktitle = "2003 IEEE Aerospace Conference, Proceedings",

note = "2003 IEEE Aerospace Conference ; Conference date: 08-03-2003 Through 15-03-2003",

}

TY - GEN

T1 - Fault localization for gear tooth failure in coupled mechanical systems

AU - Banks, Jeffrey C.

AU - Lebold, Mitchell

AU - Reichard, Karl Martin

PY - 2003/12/1

Y1 - 2003/12/1

N2 - The purpose of this paper is to discuss the results from a fault localization survey that was conducted using the Dual Gearbox Mechanical Diagnostic Test Bed. The test involved using two DC motors to drive and load two single reduction gear boxes coupled in series. An array of sensors including vibration, torque and temperature were used to.monitor each gearbox during a baseline and a seededhransitional gear fault test. The data was analyzed in order to evaluate the sensor types and locations and their ability to provide an indication and localization of a fault. The ultimate goal of this work is to find the least number of sensors that provide the greatest fault indication coverage for coupled mechanical systems.

AB - The purpose of this paper is to discuss the results from a fault localization survey that was conducted using the Dual Gearbox Mechanical Diagnostic Test Bed. The test involved using two DC motors to drive and load two single reduction gear boxes coupled in series. An array of sensors including vibration, torque and temperature were used to.monitor each gearbox during a baseline and a seededhransitional gear fault test. The data was analyzed in order to evaluate the sensor types and locations and their ability to provide an indication and localization of a fault. The ultimate goal of this work is to find the least number of sensors that provide the greatest fault indication coverage for coupled mechanical systems.

UR - http://www.scopus.com/inward/record.url?scp=84879351242&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84879351242&partnerID=8YFLogxK

U2 - 10.1109/AERO.2003.1234173

DO - 10.1109/AERO.2003.1234173

M3 - Conference contribution

AN - SCOPUS:84879351242

SN - 078037651X

SN - 9780780376519

T3 - IEEE Aerospace Conference Proceedings

SP - 3295

EP - 3304

BT - 2003 IEEE Aerospace Conference, Proceedings

T2 - 2003 IEEE Aerospace Conference

Y2 - 8 March 2003 through 15 March 2003

ER -

Fault localization for gear tooth failure in coupled mechanical systems

Abstract

Publication series

Other

All Science Journal Classification (ASJC) codes

Access to Document

Other files and links

Fingerprint

Cite this