Wear monitoring system with embedded conductors
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B32B-009/00
출원번호
US-0018816
(2004-12-20)
등록번호
US-7270890
(2007-09-18)
발명자
/ 주소
Sabol,Stephen M.
Subramanian,Ramesh
출원인 / 주소
Siemens Power Generation, Inc.
인용정보
피인용 횟수 :
25인용 특허 :
32
초록▼
Aspects of the invention relate to a system for monitoring the wear of a component. A conductor can be embedded in the component at a depth from a surface of the component. In one embodiment, the conductor can be operatively connected to a power source to form an electrical circuit. The resistance a
Aspects of the invention relate to a system for monitoring the wear of a component. A conductor can be embedded in the component at a depth from a surface of the component. In one embodiment, the conductor can be operatively connected to a power source to form an electrical circuit. The resistance across the conductor can be measured. As the component contacts a second component, the component can begin to wear. Once the wear progresses to the conductor, changes in the measured resistance can result. Thus, an operator can be alerted that the component has worn to a certain point and that service may be needed. Alternatively, impedance can be measured across the conductor. Because the dielectric permeability of the material surrounding the conductor can affect impedance, changes in impedance can occur as the surface material of the component is worn away.
대표청구항▼
What is claimed is: 1. A wear monitoring system comprising: a first component having a surface; a second component; a first conductor embedded in the first component at a predetermined depth beneath the surface and being electrically insulated from the first component; a power source operatively co
What is claimed is: 1. A wear monitoring system comprising: a first component having a surface; a second component; a first conductor embedded in the first component at a predetermined depth beneath the surface and being electrically insulated from the first component; a power source operatively connected to provide current to the first conductor, whereby an electrical circuit is formed; and a measurement device operatively positioned to measure an electrical value across at least a portion of the first conductor, wherein the second component contacts the surface of the first component such that at least the surface of the first component wears, whereby a user can monitor the measurement device for changes in the measured value indicating that the wear has progressed at least to the predetermined depth, wherein the current flows through the first conductor prior to the wear progressing to the predetermined depth. 2. The system of claim 1 wherein the first and second components are gas turbine engine components. 3. The system of claim 1 wherein the electrical value is one of resistance, current, voltage and impedance. 4. The system of claim 1 further including: a second conductor embedded in the first component at a predetermined depth beneath the surface, wherein the second conductor is operatively connected to receive current from the power source, and wherein the measurement device is operatively positioned to measure the value across at least a portion of the second conductor. 5. The system of claim 4 wherein the first and second conductors we electrically insulated from each other and are separately operatively connected to the power source, whereby two isolated circuits are formed. 6. The system of claim 4 wherein the first and second conductors are provided in the first component at substantially the same depth beneath the surface of the first component. 7. The system of claim 4 wherein the first and second conductors are electrically connected in parallel. 8. The system of claim 4 wherein the first and second conductors are provided in the first component at different depths beneath the surface of the first component. 9. The system of claim 8 wherein the first conductor and the second conductor provide at least partially overlapping areas of coverage about the first component. 10. The system of claim 1 wherein the first component includes a base material with at least one layer of a coating thereon, wherein the first conductor is embedded within the coating. 11. A wear monitoring system comprising: a first component having a fast surface; a second component having a second surface, wherein at least a portion of the second surface of the second component is conductive; a first conductor embedded in the first component at a predetermined depth beneath the first surface; a second conductor embedded in the first component at another predetermined depth beneath the first surface, and a power source operatively connected to the first conductor and to the conductive surface of the second component, wherein an initially open circuit is formed, the second surface and the first surface being in contact such that at least the fast surface wears, wherein, when the first surface is sufficiently worn such that the second surface contacts the first conductor, the circuit is completed, whereby the completion of the circuit can alert a user that the wear has progressed to at least the predetermined depth, wherein the second conductor is operatively connected to receive current from the power source such that an initially open circuit is formed, wherein when the first surface is sufficiently worn such that the second surface contacts the second conductor, the circuit is completed, whereby the completion of the circuit can alert a user that the wear has progressed to at least the another predetermined depth, wherein the first and second conductors are electrically insulated from each other and are separately operatively connected to the power source, whereby two isolated initially open circuits are formed, and wherein the first and second conductors are provided in the first component at different depths beneath the first surface of the first component. 12. The system of claim 11 further including a measurement device operatively positioned to measure at least one of resistance, current, voltage and impedance across at least a portion of the first conductor and the conductive surface of the second component, whereby changes in the measured resistance, current, voltage and impedance indicate that a predetermined amount of wear has occurred. 13. The system of claim 11 wherein the first component is a gas turbine engine component. 14. The system of claim 11 wherein the first conductor and the second conductor provide at least partially overlapping areas of coverage about the first component. 15. The system of claim 11 wherein the first and second conductors are electrically connected in parallel. 16. The system of claim 11 wherein the first component includes a base material with at least one layer of a coating thereon, wherein the first conductor is embedded within the coating.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (32)
Srivastava, Alok Mani; Setlur, Anant Achyut; Comanzo, Holly Ann; Devitt, John William; Ruud, James Anthony; Brewer, Luke Nathaniel, Apparatus for determining past-service conditions and remaining life of thermal barrier coatings and components having such coatings.
Patience Brian M. (Eastbourne GB3) West David A. (Bexhill on Sea MA GB3) Beam Palmer H. (Petersham MA), Apparatus for measuring changes in radial and/or axial position of a rotor in a drive system including an EMF producing.
Galasko Philip E. (3 The Boulders Khyber Rock ; Sandton ; Transvaal ZAX) Kruger Frans J. (Pretoria ZAX), Detection of a low pressure condition of a vehicle tire.
Masashi Takahashi JP; Kazuhide Matsumoto JP; Masayuki Itoh JP; Masahiro Saitou JP; Kunihiko Wada JP; Akinori Koga JP, High temperature component, gas turbine high temperature component and manufacturing method thereof.
Adiutori Eugene F. (Westchester OH), Method and apparatus for measuring the distribution of heat flux and heat transfer coefficients on the surface of a cool.
Zhao, Ji-Cheng; Ruud, James Anthony; Tkaczyk, John Eric; Ritter, Ann Melinda; Jackson, Melvin Robert; Tiemann, Jerome Johnson, Smart coating system with chemical taggants for coating condition assessment.
Morrison Jay Alan ; Merrill Gary Brian ; Ludeman Evan McNeil ; Lane Jay Edgar, Use of high temperature insulation for ceramic matrix composites in gas turbines.
Quinn, Thomas F.; Kulkarni, Anand A.; Landy, James F., Apparatus and method for monitoring and quantifying progression of a structural anomaly in a high temperature environment of a combustion turbine engine.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.