US4267733A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Torsional vibration monitoring method and an apparatus for performing the same
Assignee: Kansai Electric Power Co Inc
•
Filing: 1979-05-30
•
Granted: 1981-05-19
•
Expires: 1999-05-30
Abstract
Abstract The present invention is a torsional vibration monitoring method and an apparatus for performing the same, in which torsional vibrations produced in a rotating shaft system for use in such as a turbine generator are measured at a small number of certain positions therealong at which the measurements are possible, the torsional vibrations are linearly decomposed and torsional vibrations at arbitrary positions on the rotating shaft system are estimated from the linear decompositions.
Inventors
- 👤 Ichiji Shima
- 👤 Tatsuo Yamamoto
- 👤 Shigeru Yoshibayashi
- 👤 Hiroshi Teshima
- 👤 Akio Hizume
- 👤 Tetsuo Iki
- 👤 Takashi Yamamoto
- 👤 Kyozo Kanamori
- 👤 Kenzo Noguchi
- 👤 Shinobu Kishikawa
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 17:12
CPC Classifications
G; G01; G01H; G01H1/00; G01H1/10
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
176 words
In an apparatus for monitoring torsional vibration in which a torsional vibration at an arbitrary position on a rotating shaft system is measured from a torsional vibration detected at a certain position on the rotating shaft system on the basis of the facts that a torsional vibration occurred in the rotating shaft system is a sum of modal vibrations and the modal vibration can be represented by a product of a vibration mode type and a vibration mode component, the improvement comprising n sets of detectors for detecting torsional vibrations at each of n certain positions on the rotating shaft system, a matrix arithmetic unit for multiplying previously obtained n sets of n constants to the n sets of torsional vibrations obtained by said detectors, respectively, and for adding the results of the multiplications to obtain n vibration mode components and a modal arithmetic unit for multiplying the n vibration mode components to vibration mode types at arbitrary position on the rotating shaft system and for adding them to obtain torsional vibrations at the arbitrary positions.
Claim 2
Dependent Claim
176 words
In an apparatus for monitoring torsional vibration in which a torsional vibration at an arbitrary position on a rotating shaft system is measured from a torsional vibration detected at a certain position on the rotating shaft system on the basis of the facts that a torsional vibration occurred in the rotating shaft system is a sum of modal vibrations and the modal vibration can be represented by a product of a vibration mode type and a vibration mode component, the improvement comprising n sets of detectors for detecting torsional vibrations at each of n certain positions on the rotating shaft system, a matrix arithmetic unit for multiplying previously obtained n sets of n constants to the n sets of torsional vibrations obtained by said detectors, respectively, and for adding the results of the multiplications to obtain n vibration mode components and a modal arithmetic unit for multiplying the n vibration mode components to vibration mode types at arbitrary position on the rotating shaft system and for adding them to obtain torsional vibrations at the arbitrary positions.
Claim 3
Independent Claim
251 words
A method of monitoring torsional vibrations of a rotating shaft system comprising the steps of measuring the under-formulated torsional vibrations Y(x pk ,t) at a number n of certain positions x pk on the rotating shaft system to develop representative signals, said measurements being made with the assumptions that a torsional vibration occurring in the rotating shaft system is a sum of modal vibrations, that each of the modal vibrations is a product of a vibration mode type G i (x pk ) and a vibration mode component H i (t) and that the torsional vibration is an accumulation of the modal vibrations up to the n-th modal vibration, Y(x.sub.pk,t)=ΣG.sub.i (x.sub.pk)·H.sub.i (t) (k=1, 2, . . . , n); obtaining an unknown value as said vibration mode component, H i (t) by the use of intermediate signals representing the reverse matrix G ik of n row-n column matrix having the previously obtained and afore-formulated coefficient, G i (x pk ) as its element, namely, [G.sub.ik ]≡[G.sub.i (x.sub.pk)].sup.-1 , said reverse matrix G ik being responsive to said representative signals wherein i shows the row and k shows the column, and obtaining torsional vibration Y(x j ,t) from said intermediate signals at an arbitrary position x j on the rotating shaft system as an accumulation Y(x j ,t)=ΣG i (x j )·H i (t) of products of the vibration mode type G i (x j ) at said arbitrary position x j already known and the vibration mode component H i (t).
Claim 4
Independent Claim
251 words
A method of monitoring torsional vibrations of a rotating shaft system comprising the steps of measuring the under-formulated torsional vibrations Y(x pk ,t) at a number n of certain positions x pk on the rotating shaft system to develop representative signals, said measurements being made with the assumptions that a torsional vibration occurring in the rotating shaft system is a sum of modal vibrations, that each of the modal vibrations is a product of a vibration mode type G i (x pk ) and a vibration mode component H i (t) and that the torsional vibration is an accumulation of the modal vibrations up to the n-th modal vibration, Y(x.sub.pk,t)=ΣG.sub.i (x.sub.pk)·H.sub.i (t) (k=1, 2, . . . , n); obtaining an unknown value as said vibration mode component, H i (t) by the use of intermediate signals representing the reverse matrix G ik of n row-n column matrix having the previously obtained and afore-formulated coefficient, G i (x pk ) as its element, namely, [G.sub.ik ]≡[G.sub.i (x.sub.pk)].sup.-1 , said reverse matrix G ik being responsive to said representative signals wherein i shows the row and k shows the column, and obtaining torsional vibration Y(x j ,t) from said intermediate signals at an arbitrary position x j on the rotating shaft system as an accumulation Y(x j ,t)=ΣG i (x j )·H i (t) of products of the vibration mode type G i (x j ) at said arbitrary position x j already known and the vibration mode component H i (t).
References Cited (Backward Citations)
US3934459A
Cited
US4051427A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-05-18 | 1984-11-17 | 1985-05-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-05-18 | 1988-11-17 | 1989-05-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-05-18 | 1992-11-17 | 1993-05-19 | $7700.00 | Window Closed / Lapsed |