JPS58201030A - Device for supervising twisting oscillation of rotary shaft system - Google Patents
Device for supervising twisting oscillation of rotary shaft systemInfo
- Publication number
- JPS58201030A JPS58201030A JP8398882A JP8398882A JPS58201030A JP S58201030 A JPS58201030 A JP S58201030A JP 8398882 A JP8398882 A JP 8398882A JP 8398882 A JP8398882 A JP 8398882A JP S58201030 A JPS58201030 A JP S58201030A
- Authority
- JP
- Japan
- Prior art keywords
- shaft system
- torsional vibration
- monitoring point
- output
- operator
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000010355 oscillation Effects 0.000 title abstract description 6
- 238000012544 monitoring process Methods 0.000 claims abstract description 20
- 238000012806 monitoring device Methods 0.000 claims description 7
- 230000001052 transient effect Effects 0.000 abstract description 7
- 238000010586 diagram Methods 0.000 description 15
- 230000005540 biological transmission Effects 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 238000000354 decomposition reaction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
- G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
- G01H1/10—Measuring characteristics of vibrations in solids by using direct conduction to the detector of torsional vibrations
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
Abstract
Description
【発明の詳細な説明】 本発明は回転軸系捩り振動監視装置に関する。[Detailed description of the invention] The present invention relates to a rotating shaft system torsional vibration monitoring device.
例えば、第1図配置図に示すように、高圧タービン01
.中圧タービン02.低圧タービン03、発電機04.
励磁機05をタンデムに軸06で接続してなるタービン
発電機軸系においては、第2図体) 、 (B) 、
fcl 、 (DJ線図にそれぞれ示すように、各部の
質量及びバネ剛性にて決まる一次、二次、三次、四次モ
ード等の複数の捩り固有振動モードを有しているので、
送電系統故障等の急激々負荷変動があると、これを励振
力として捩り振動を起こし、軸糸各部には捩り振動応力
が発生する。For example, as shown in the layout diagram of FIG.
.. Medium pressure turbine 02. Low pressure turbine 03, generator 04.
In the turbine generator shaft system in which the exciter 05 is connected in tandem by the shaft 06, Fig. 2), (B),
fcl, (As shown in the DJ diagram, it has multiple torsional natural vibration modes such as primary, secondary, tertiary, and quartic modes determined by the mass and spring stiffness of each part,
When there is a sudden load change such as a power transmission system failure, this causes torsional vibration as an exciting force, and torsional vibration stress is generated in each part of the shaft thread.
MI図OA、B、C,D、Fl、F、Gはタービン軸、
カップリング等で捩り振動による疲労強度上チェックポ
イントとすべき複数の監視点であり、軸が一定回転で回
転している時は、電磁−ツクアッデo8により検出され
る歯車。70回転zfルスの周期は一定であるが、換り
振動が発生すると、捩り振動振幅に比例して回転)4ル
スは周波数変調されるので、従来この回j/fルスを検
波することにより各監視点の捩り振動振巾を計測してい
る
即ち振動挙上の知見によれば軸系の捩り振動は近似的に
その固有振動モードの合成として(1)式で表わされる
。MI diagram OA, B, C, D, Fl, F, G are turbine shafts,
These are multiple monitoring points that should be used as checkpoints for fatigue strength due to torsional vibration in couplings, etc., and when the shaft is rotating at a constant rotation, the gear is detected by electromagnetic gear. The period of the 70 rotation zf pulse is constant, but when rotational vibration occurs, it rotates in proportion to the torsional vibration amplitude.) Since the 4 pulse is frequency modulated, conventionally, by detecting this rotation j/f pulse, each According to the knowledge of vibration elevation, which measures the amplitude of torsional vibration at a monitoring point, the torsional vibration of a shaft system can be approximately expressed by equation (1) as a composition of its natural vibration modes.
F(x 、t )=a1(t)・g、fxl+a、(t
l・g 、 fx)+・・・+an(t)・gn(x)
・・・・・・・・・・・・・・・・・・・・・・・
・・・・fl)ここで、Y(X)は計測位置x点の計測
信号a 1 、a2’<・・anは各固有振動モード成
分の応答量
g 1 e g !・・・gnは例えば第2図に示すよ
うな固有振動モード
である。F(x, t)=a1(t)・g, fxl+a, (t
l・g, fx)+...+an(t)・gn(x)
・・・・・・・・・・・・・・・・・・・・・・・・
...fl) Here, Y(X) is the measurement signal a 1 at the measurement position x, a2'<...an is the response amount g 1 e g of each natural vibration mode component! ...gn is a natural vibration mode as shown in FIG. 2, for example.
そこで、軸系上の歯車07と電磁ピックアップ08によ
り検出された回転パルス信号を第3図ブロック線図に示
す捩り振動検出器010に入力して第4図(A) 、
(B)に示すような捩り振動信号を検出する。こ\で同
図(B)は同図(A)の周波数スペクトルである。これ
を、′第4図(C1に示すように、中心周波数を捩り固
有振動数に調整したパントノ母スフイルタθ11(第3
図参照)に通すと、第4図(旬に示すようなその固有値
だけの振動成分
yi(xp、 t)=at(t)・gi(xp)CO5
(ω目+θi)・・・・・・・・・・・・・・・・・・
・・・(2)が得られる。Therefore, the rotational pulse signals detected by the gear 07 on the shaft system and the electromagnetic pickup 08 are input to the torsional vibration detector 010 shown in the block diagram of FIG.
A torsional vibration signal as shown in (B) is detected. Here, (B) in the same figure is the frequency spectrum of (A) in the same figure. As shown in Fig. 4 (C1), this is a pantone matrix filter θ11 (third
(see figure), the vibration component of only its eigenvalues yi (xp, t) = at (t) · gi (xp) CO5 as shown in Figure 4
(ωth+θi)・・・・・・・・・・・・・・・・・・
...(2) is obtained.
このバンドパスフィルタ011は、第3図に示すように
、固有振動の数だけ設置する。As shown in FIG. 3, the number of bandpass filters 011 is equal to the number of natural vibrations.
こうして、各固有振動毎の応答が判るので、第2図の固
有振動モードより得られる監視点の振動モード比を乗算
器012(第3図参照)により乗算することにより第4
図(E)に示すような各モード毎の監視点の振動応答
が得られる。In this way, the response for each natural vibration is known, so by multiplying the vibration mode ratio of the monitoring point obtained from the natural vibration mode in FIG.
The vibration response of the monitoring point for each mode is obtained as shown in Figure (E).
そこで、各監視点毎にすべてのモードを加算合成器o1
s(第3図参照)で合成することによりその監視点の振
動応答が得られ、各点での振動波形が分かるので、応力
は振動振幅に比例するから
δ(x人、t)=Σyl(x、t)−α(x)・・・・
・・・・・・・・(4)として応力波形を推定でき、各
監視点の応力波形が分かれば、ピークカウント法等の疲
労寿命推定法に基づいて寿命消費量を計算器014($
3図参照)で計算し、その結果を記録表示器015 (
@3図参照)にて表示するのである。Therefore, for each monitoring point, all modes are summed and synthesized by o1.
s (see Figure 3), the vibration response of the monitoring point is obtained, and the vibration waveform at each point is known. Since stress is proportional to the vibration amplitude, δ (x people, t) = Σyl ( x, t) - α(x)...
If the stress waveform can be estimated as (4) and the stress waveform at each monitoring point is known, then the life consumption can be calculated using Calculator 014 ($
(see Figure 3), and the results are displayed on the record display 015 (
@Refer to Figure 3).
以上述べたのが、従来のタービン発電機回転軸系におけ
る捩り振動監視装置のあらましである。What has been described above is an overview of the conventional torsional vibration monitoring device for the rotating shaft system of a turbine generator.
しかしながら、タービン発電機軸系・に疲労寿命を消費
するような巨大振動が発生する場合は、送電系統に落雷
等による送電故障があって急激な負荷変動が加わった時
であり、この時の捩り振動応答は過渡応答振動でその初
期に最大応力は発生するので、このため監視装置は過渡
応答特性が良く危ければならないにもかかわらず、各固
有モードに分解するためのノ々ンド/4’スフイルタは
、近接する固有値の影響を小さくする必要があり、その
ためにはパントノ4スフイルタの遮断特性は大きくとる
必要があるが、フィルタの特性として遮断特性を大きく
すると、過渡応答特性が著しく悪くなるという相反する
問題が生ずる。However, when huge vibrations that consume the fatigue life of the turbine generator shaft system occur, it is when there is a power transmission failure due to a lightning strike etc. in the power transmission system and sudden load changes are applied, and torsional vibration at this time occurs. The response is a transient response oscillation, and the maximum stress occurs at the beginning of the response, so the monitoring device must have a good transient response characteristic and a non-nodal/4' filter to decompose it into each eigenmode. It is necessary to reduce the influence of adjacent eigenvalues, and for this purpose, the cutoff characteristics of the pantone 4-sphere filter must be made large.However, increasing the cutoff characteristics of the filter has the trade-off that the transient response characteristics will deteriorate significantly. A problem arises.
因みに、通常バンドパスフィルタの遮断特性はQ−20
程度に選ぶのが好適であるといわれるが、これでも第5
図fc)に示すように、最初の15山は90%以下の応
答しか得られず、応力の大きい付近の振動を確実に監視
することはできない。By the way, the cutoff characteristic of a normal bandpass filter is Q-20.
It is said that it is best to choose according to the degree of
As shown in Figure fc), only a response of less than 90% was obtained for the first 15 peaks, making it impossible to reliably monitor vibrations near high stress areas.
本発明はこのような事情に鑑みて提案されたもので、過
渡応答特性に優れたモード分解法に基づく高性能の回転
軸系捩り振動監視装置を提供することを目的とし、捩り
振動検出器と、回転軸系の各固有振動数にそれぞれ等し
い中心周波数を有しそれぞれ上記捩り振動検出器の出力
を入力する複数のノクンドノ臂スフィルタと、それぞれ
上記各バンド・母スフイルタの出力を入力する複数の位
相計と、上記複数の位相針の出力を入力し上記回転軸系
の各監視点の捩り振動応答を演算する連立方程式演算器
と、上記連立方程式演算器の出力を入力し上記各監視点
の応力を演算する複数の監視点応力信号合成器とを具え
たことを特徴とする。The present invention was proposed in view of the above circumstances, and aims to provide a high-performance rotating shaft system torsional vibration monitoring device based on a mode decomposition method with excellent transient response characteristics. , a plurality of backbone filters each having a center frequency equal to each natural frequency of the rotating shaft system and inputting the output of the torsional vibration detector, and a plurality of backplane filters inputting the output of each band/mother filter, respectively. a phase meter, a simultaneous equation calculator that inputs the outputs of the plurality of phase hands and calculates the torsional vibration response of each monitoring point of the rotating shaft system; The present invention is characterized by comprising a plurality of monitoring point stress signal synthesizers for calculating stress.
本発明の一実施例を図面について説明すると。An embodiment of the present invention will be described with reference to the drawings.
第6図はその回路構成を示すブロック線図である。FIG. 6 is a block diagram showing the circuit configuration.
上図において、10は捩り振動検出器、11は検出器1
0の出力を入力するバンドパスフィルタ、12aはバン
ドパスフィルタ11の出力を入力する位相計、12aは
位相計12a及び検出器10の出力を入力する連立方程
式演算器、13は演算器12bの出力を入力する監視点
応力信号合成器、14は合成器13の出力を入力する疲
労寿命消費量計算器、15は疲労寿命消費量゛計算器1
4の出力を入力する記録表示装置である。In the above figure, 10 is the torsional vibration detector, 11 is the detector 1
12a is a phase meter that inputs the output of the bandpass filter 11, 12a is a simultaneous equation calculator that inputs the outputs of the phase meter 12a and the detector 10, and 13 is the output of the calculator 12b. 14 is a fatigue life consumption calculator that inputs the output of the synthesizer 13; 15 is a fatigue life consumption amount calculator 1
This is a recording/displaying device that inputs the output of 4.
このような装置において、捩り振動検出器10により検
出した捩り振動信号を各固有振動数に中心川波数に合わ
せたバンドパスフィルタ1ノに通し、各固有モード毎の
信号に分解し、この各モード毎の信号よりその信号の位
相情報を位相計12mで求める。In such a device, the torsional vibration signal detected by the torsional vibration detector 10 is passed through a bandpass filter 1 which is matched to the central river wave number at each natural frequency, and decomposed into signals for each natural mode. The phase information of each signal is obtained using a phase meter 12m.
この位相の求め方としては例えば次の方法による。すな
わち、パントノ母スフイルタ11の出力波形の最大値、
最小値、零クロスするタイミングを検出し、これらのタ
イミングは0度。This phase can be determined, for example, by the following method. That is, the maximum value of the output waveform of the pantone filter 11,
Detect the minimum value and zero crossing timing, and these timings are 0 degrees.
180度、90度、270度の位相に相当するので、こ
れより近似することで各タイミングの位相角θ1が分る
。Since this corresponds to phases of 180 degrees, 90 degrees, and 270 degrees, the phase angle θ1 at each timing can be found by approximating this.
このようにして各モード毎の位相角が分かると、計測信
号は、(1)式に基づいて(5)式y(x、t)=Σa
1(t)、 g 1(x) ・cosθ巾)・・・・
・・・・・(5)東
で表わされ、わずかに時間の異なる点では(6)式(6
)式において、未知数はalだけであり、モード数(1
)より多い数の方程式を作ることも容易であり、この連
立方程式を解くことにより各モードの応答量が演算器1
2bで得られる。以後は従来の装置におけると同様の回
路により疲労寿命消費量を監視する。Once the phase angle for each mode is known in this way, the measurement signal can be calculated using equation (5) based on equation (1): y(x,t)=Σa
1(t), g 1(x) ・cosθ width)...
...(5) Expressed in the east, and at a point with a slightly different time, Equation (6) (6
), the only unknown quantity is al, and the number of modes (1
) It is also easy to create a larger number of equations, and by solving these simultaneous equations, the response amount of each mode can be calculated using the calculator 1.
Obtained in 2b. Thereafter, fatigue life consumption is monitored using the same circuit as in conventional equipment.
このような装置によれば下記の効果が奏せられる。Such a device provides the following effects.
(1) バンドパスフィルタの出力は、位相情報とし
てのみ使用するので、遮断特性を大きくし、過渡特性を
下げても、装置性能に影響せず、全体性能として装置の
過渡特性は良くなる。(1) Since the output of the bandpass filter is used only as phase information, increasing the cut-off characteristics and lowering the transient characteristics does not affect the device performance, and the overall performance of the device improves the transient characteristics.
(2)回転ノ母ルスより捩り振動を求めた場合、必ず軸
回転数成分のノイズが混入するが、これもモード分解と
同一要領で除去することができる。(2) When torsional vibration is determined from the rotation base, noise of the shaft rotational speed component is always mixed in, but this can also be removed in the same manner as mode decomposition.
要するに本発明によれば、捩り振動検出器と、回転軸系
の各固有振動数にそれぞれ等しい中心川波数を有しそれ
ぞれ上記捩り振動検出器の出力を入力する複数のパント
ノ量スフイルタと、それぞれ上記各バンドパスフィルタ
の出力を入力する複数の位相計と、上記複数の位相計の
出力を入力し上記回転軸系の各監視点の捩り振動応答を
演算する連立方程式演算器と、上記連立方程式演算器の
出力を入力し上記各監視点の応力を演算する複数の監視
点応力信号合成器とを具えたことにより、高性能の回転
軸系捩り振動監視装置を得るから本発明は産業上極めて
有益なものである。In short, according to the present invention, a torsional vibration detector, a plurality of pantone filters each having a center wave number equal to each natural frequency of the rotating shaft system and inputting the output of the torsional vibration detector, and each of the above-mentioned a plurality of phase meters that input the output of each bandpass filter; a simultaneous equation calculator that inputs the output of the plurality of phase meters and calculates the torsional vibration response of each monitoring point of the rotating shaft system; and a simultaneous equation calculator that inputs the output of each of the bandpass filters; The present invention is industrially extremely useful because it provides a high-performance rotating shaft system torsional vibration monitoring device by including a plurality of monitoring point stress signal synthesizers that input the output of the device and calculate the stress at each of the monitoring points. It is something.
第1図は公知のタービン発[機軸系の配置図、第2区内
、 (B) 、 fc) 、 (D)はそれぞれ′第1
図の軸系の捩り振動モード図、第3図は公知の回転軸系
援り振動監視装置のブロック線図、第4図(Nは第1図
の電磁ピックアップの出力線図、第4図(B)は第4図
(Nの問波数スペクトル線図、@4図(C)は第3図の
パントノ量スフィルタの特性図、第4図山は第3図のバ
ンドパスフィルタの出力線図、第4図(均は第1図の監
視点の振動応答線図、第5図(A)はバンドパスフィル
タへの標準入力波形図、第5図(Bl 、 (C1、(
Dlはそれぞれ第5図(〜の入力波形に対する各出力波
形図でそれぞれQ=10.20.40の各場合を示す、
第6図は本発明の一実施例のブロック線図である。
10・・・捩り振動検出器、11・・・パンドパスフィ
ルタ、12a・・・位相計、12b・・・連立方程式演
算器、13・・・監視点応力信号合成器、14・・・疲
労寿命消費量計算器、15・・・記録表示装置。
出頗人復代理人 弁理士 鈴 江 武 彦第2図
第4図
□J
CJJI va
!−8
3Figure 1 shows a well-known turbine generator [arrangement diagram of the machine shaft system, in the 2nd section, (B), fc), and (D) are in the '1st section, respectively.
Figure 3 is a block diagram of a known rotary shaft system assisted vibration monitoring device, Figure 4 (N is an output diagram of the electromagnetic pickup in Figure 1, Figure 4 is B) is the wavenumber spectrum diagram of Figure 4 (N), Figure 4 (C) is the characteristic diagram of the pantone quantity filter of Figure 3, and the peak of Figure 4 is the output diagram of the bandpass filter of Figure 3. , Figure 4 (Unit is the vibration response diagram of the monitoring point in Figure 1, Figure 5 (A) is the standard input waveform diagram to the bandpass filter, Figure 5 (Bl, (C1, ()
Dl is shown in Figure 5 (each output waveform diagram for the input waveform of ~ shows each case of Q = 10, 20, 40, respectively,
FIG. 6 is a block diagram of one embodiment of the present invention. DESCRIPTION OF SYMBOLS 10... Torsional vibration detector, 11... Band pass filter, 12a... Phase meter, 12b... Simultaneous equation calculator, 13... Monitoring point stress signal synthesizer, 14... Fatigue life Consumption calculator, 15...recording display device. Representative Patent Attorney Suzue Takehiko Figure 2 Figure 4 □J CJJI va! -8 3
Claims (1)
等しい中心周波数を有しそれぞれ上記捩り振動検出器の
出力を入力する複数のパントノ4スフイルタと、それぞ
れ上記各パントノぐスフイルタの出力を入力する複数の
位相計と、上記複数の位相計の出力を入力し上記回転軸
系の各監視点の捩り振動応答を演算する連立方程式演算
器と、上記連立方程式演算器の出力を入力し上記各監視
点の応力を演算する複数の監視点応力信号合成器とを具
えたことを特徴とする回転軸系捩り振動監視装置。a torsional vibration detector, a plurality of pantone 4-sphere filters each having a center frequency equal to each natural frequency of the rotating shaft system and each inputting the output of the torsional vibration detector, and each inputting the output of each of the pantone gusset filters; a simultaneous equation calculator that inputs the outputs of the plurality of phase meters and calculates the torsional vibration response of each monitoring point of the rotating shaft system; A rotating shaft system torsional vibration monitoring device comprising a plurality of monitoring point stress signal synthesizers for calculating stress at monitoring points.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8398882A JPS58201030A (en) | 1982-05-20 | 1982-05-20 | Device for supervising twisting oscillation of rotary shaft system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8398882A JPS58201030A (en) | 1982-05-20 | 1982-05-20 | Device for supervising twisting oscillation of rotary shaft system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS58201030A true JPS58201030A (en) | 1983-11-22 |
Family
ID=13817915
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8398882A Pending JPS58201030A (en) | 1982-05-20 | 1982-05-20 | Device for supervising twisting oscillation of rotary shaft system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58201030A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6284309A (en) * | 1985-10-08 | 1987-04-17 | Yaskawa Electric Mfg Co Ltd | Mechanical stiffness compensation servo control system |
| JPS6375625A (en) * | 1986-09-19 | 1988-04-06 | Kansai Electric Power Co Inc:The | Apparatus for monitoring torsional vibration of rotary shaft system |
| JPS6375626A (en) * | 1986-09-19 | 1988-04-06 | Kansai Electric Power Co Inc:The | Apparatus for monitoring torsional vibration of rotary shaft system |
-
1982
- 1982-05-20 JP JP8398882A patent/JPS58201030A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6284309A (en) * | 1985-10-08 | 1987-04-17 | Yaskawa Electric Mfg Co Ltd | Mechanical stiffness compensation servo control system |
| JPS6375625A (en) * | 1986-09-19 | 1988-04-06 | Kansai Electric Power Co Inc:The | Apparatus for monitoring torsional vibration of rotary shaft system |
| JPS6375626A (en) * | 1986-09-19 | 1988-04-06 | Kansai Electric Power Co Inc:The | Apparatus for monitoring torsional vibration of rotary shaft system |
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