JPH0894432A - Mounting device of detector for measurement of rotor vibration - Google Patents

Mounting device of detector for measurement of rotor vibration

Info

Publication number
JPH0894432A
JPH0894432A JP22779794A JP22779794A JPH0894432A JP H0894432 A JPH0894432 A JP H0894432A JP 22779794 A JP22779794 A JP 22779794A JP 22779794 A JP22779794 A JP 22779794A JP H0894432 A JPH0894432 A JP H0894432A
Authority
JP
Japan
Prior art keywords
detector
rotor
mounting plate
rotary blade
detector mounting
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.)
Granted
Application number
JP22779794A
Other languages
Japanese (ja)
Other versions
JP3117370B2 (en
Inventor
Yoshiaki Mitsuyama
慶明 満山
Tadashi Yoshida
正 吉田
Masaaki Shibata
昌明 柴田
Ryoichi Sonoda
良一 薗田
Yoji Morita
洋二 森田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP06227797A priority Critical patent/JP3117370B2/en
Publication of JPH0894432A publication Critical patent/JPH0894432A/en
Application granted granted Critical
Publication of JP3117370B2 publication Critical patent/JP3117370B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

PURPOSE: To easily adjust the interval between a detector and a rotor regarding the mounting device of the detector used to measure the rotor vibration in a noncontact manner. CONSTITUTION: Rotational-signal-detector mounting plates 21a, 21b are attached to two split support rings 20a, 20b. A rotational-signal detector 10 and a noncontact displacement meter 11 are attached to the mounting plates 21a, 21b so as to keep a definite interval from a rotor. The support rings 20a, 20b are fixed to a foundation base board 23 via rail surface plates 35, sliding rails 32b and fitting parts. The mounting plates 21a, 21b are sandwiched between the support rings 20a, 20b from both sides by means of inclination adjusting bolts 22. The direction of a rotary shaft is adjusted on the sliding rails 32b, and its inclination is adjusted by beams of the inclination adjusting bolts 22 in such a way that an interval is adjusted. A change in the interval during a rotation can be measured by the displacement meter 11. As a result, a mounting device can be adjusted and measured easily.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明はタービン、ポンプ、ファ
ン、等の回転翼の振動を非接触で計測する検出器を取付
るための振動計測用検出器取付装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a vibration measuring detector mounting device for mounting a detector for measuring the vibration of rotors such as turbines, pumps and fans in a non-contact manner.

【0002】[0002]

【従来の技術】図4は従来の回転翼と回転信号検出器と
の関係を示す側面図である。図において、タービンなど
の回転翼1は回転軸3のディスク部2に円周方向に等間
隔で複数枚配設されている。本発明の対象となる回転翼
振動計測装置では、回転翼1の先端部と対向する静止側
に電磁式回転パルス検出器などの回転信号検出器10が
円周方向に多数個設置されている。
2. Description of the Related Art FIG. 4 is a side view showing the relationship between a conventional rotor and a rotation signal detector. In the figure, a plurality of rotary blades 1 such as a turbine are arranged on a disk portion 2 of a rotary shaft 3 at equal intervals in the circumferential direction. In the rotor blade vibration measuring device that is the subject of the present invention, a large number of rotation signal detectors 10 such as electromagnetic rotor pulse detectors are installed in the circumferential direction on the stationary side facing the tip of the rotor blade 1.

【0003】図5はこの回転翼振動計測装置の系統図で
ある。回転翼振動計測装置は隣接する回転信号検出器1
0の出力信号A1 ,A2 をゲート信号として、数10メ
ガヘルスから、数100メガヘルツの高周波基準信号発
信器4の発信回数を計数器5で計数する回路を回転信号
検出器10と同数備えている。
FIG. 5 is a system diagram of this rotary blade vibration measuring device. The rotor blade vibration measuring device has an adjacent rotation signal detector 1
Using the output signals A 1 and A 2 of 0 as gate signals, the same number of circuits as the rotation signal detector 10 are provided to count the number of transmissions of the high frequency reference signal transmitter 4 of several hundred megahertz from several tens of megahertz. There is.

【0004】このような構成の回転翼振動計測装置にお
いて、回転信号検出器10の前を回転翼1が通過するた
びに回転信号検出器10は回転信号を検出する。この回
転信号より、任意の回転翼1が隣接する2個の回転信号
検出器10間を通過する時間を基準信号発信器4の発信
回数として計数することによって回転翼1の瞬時速度を
得ることができる。
In the rotor blade vibration measuring device having such a configuration, the rotation signal detector 10 detects a rotation signal every time the rotor blade 1 passes in front of the rotation signal detector 10. From this rotation signal, it is possible to obtain the instantaneous speed of the rotor 1 by counting the time for the arbitrary rotor 1 to pass between the two adjacent rotation signal detectors 10 as the number of times of transmission of the reference signal transmitter 4. it can.

【0005】一円周等間隔に回転信号検出器10を取付
け、これと同数の計数器5を備えることによって、円周
上すべての位置で回転翼1の瞬時速度を得ることができ
る。この瞬時速度には回転軸の1回転と同じ回転速度分
と回転翼1が振動することによる振動速度分が含まれ平
均値として得られる回転速度分を差し引くと回転翼1の
振動成分を得ることができる。
By attaching the rotation signal detectors 10 at equal intervals on one circumference and equipping the same number of counters 5 with each other, it is possible to obtain the instantaneous speed of the rotor 1 at all positions on the circumference. This instantaneous speed includes the same rotation speed as one rotation of the rotary shaft and the vibration speed due to the vibration of the rotor 1, and subtracts the rotation speed obtained as an average value to obtain the vibration component of the rotor 1. You can

【0006】[0006]

【発明が解決しようとする課題】このような従来の回転
翼振動の検出において回転信号検出器として電磁式回転
パルス検出器を使用した場合回転翼との取付隙間は5mm
程度以下、各検出器間の取付隙間のばらつきを0.5mm
程度に押える必要がある。タービン翼1の場合、大きい
ものでは直径4m〜5mにもなり、リング状の回転信号
検出器取付治具にすることになるが、タービン及び取付
治具を設置した後1個ずつ検出器10を取付けるのは作
業性の悪い場所であり莫大な作業時間がかかる。
When an electromagnetic rotary pulse detector is used as a rotary signal detector in the conventional rotor blade vibration detection, the mounting gap with the rotary blade is 5 mm.
Less than about 0.5mm variation in mounting gap between each detector
It is necessary to hold down to a certain degree. In the case of the turbine blade 1, a large one has a diameter of 4 m to 5 m, which means that a ring-shaped rotation signal detector mounting jig is used. However, after installing the turbine and the mounting jig, the detectors 10 are mounted one by one. It is a place where workability is poor and it takes an enormous amount of work time.

【0007】回転軸3は運転中は温度上昇に伴ない熱膨
張する一方回転遠心力により縮む。これら伸び縮みの量
は数mmであり回転検出器10と回転翼1との間の隙間変
化となり、近づきすぎると接触し回転翼1や、回転検出
器10を傷つける危険があり、離れすぎると検出信号の
信頼性が低下する不具合がある。
During operation, the rotating shaft 3 thermally expands as the temperature rises, and contracts due to the rotating centrifugal force. The amount of expansion and contraction is a few mm, which causes a change in the gap between the rotation detector 10 and the rotary blade 1. If too close, there is a risk of contact and damage to the rotary blade 1 and rotation detector 10, and if too far away, detection There is a problem that signal reliability is reduced.

【0008】[0008]

【課題を解決するための手段】本発明はこのような課題
を解決するために、回転翼と対向する静止側の検出器取
付板の面を回転翼の軸方向に滑動させて間隔を調整する
手段と、この取付板の回転翼と対向する面の軸を傾斜さ
せる手段と、板付板の面と回転翼との間隔を計測する手
段とを設けた構成とする。
In order to solve the above problems, the present invention adjusts the interval by sliding the surface of the stationary detector mounting plate facing the rotor blade in the axial direction of the rotor blade. Means, means for inclining the axis of the surface of the mounting plate facing the rotary blade, and means for measuring the distance between the surface of the plate with plate and the rotary blade are provided.

【0009】即ち、本発明は、回転翼に一定の間隔を保
ち、同回転翼と対向する静止側の検出器取付板に円周状
に複数個設置された回転信号検出器により回転翼振動を
計測する回転翼振動計測用検出器取付装置において、前
記検出器取付板の前記回転翼と対向する面を同回転翼の
回転軸方向に滑動させて前記間隔を調整する手段と、前
記検出器取付板の軸を前記回転翼の軸方向に対して傾斜
させて前記間隔の傾斜を調整する手段と、前記検出器取
付板と前記回転翼間の隙間を計測する手段とを具備して
なることを特徴とする回転翼振動計測用検出器取付装置
を提供するものである。
That is, according to the present invention, the rotor blade vibration is generated by a plurality of rotation signal detectors circumferentially arranged on a stationary-side detector mounting plate facing the rotor blade at a constant interval. A rotary blade vibration measuring detector mounting device for measuring, wherein a surface of the detector mounting plate facing the rotary blade is slid in a rotation axis direction of the rotary blade to adjust the interval, and the detector mounting A means for adjusting the inclination of the interval by inclining the axis of the plate with respect to the axial direction of the rotary blade; and means for measuring a gap between the detector mounting plate and the rotary blade. A detector mounting device for measuring the characteristic of a rotor blade vibration is provided.

【0010】[0010]

【作用】本発明はこのような手段により、検出器取付板
には、回転信号検出器を円周上に等間隔に配置し、すべ
ての検出器の検出端が検出器取付板の端面より等距離と
なるように取付ける。このような検出器取付板は計測が
実施される基礎台盤上に回転翼と一定の間隔を保ち設置
されるが、例えば、支持環、等に上半部と下半部とに2
分割して組込めば下半部、回転翼、上半部の順で基礎台
盤上に容易に設置することができる。次に、検出器取付
板を滑動手段により、例えば、基礎台盤にレールを設置
しておき、検出器取付板にはこのレールのはめ合い部を
設け、このレール上に検出器取付板を滑動させて、取付
板を回転翼の回転軸方向に滑動させて間隔が設定値とな
るように調整し、調整後はボルト、等で基礎台盤に固定
するようにすれば容易に調整することができる。
According to the present invention, the rotation signal detectors are arranged on the detector mounting plate at equal intervals on the circumference by such means, and the detection ends of all the detectors are equal to the end face of the detector mounting plate. Mount so that there is a distance. Such a detector mounting plate is installed on the foundation table on which the measurement is carried out with a certain distance from the rotor blades. For example, a support ring or the like may be installed in the upper half and the lower half.
If it is divided and incorporated, it can be easily installed on the base bed in the order of the lower half, the rotor, and the upper half. Next, slide the detector mounting plate by means of sliding means, for example, by installing a rail on the base table, and then provide a fitting part of this rail on the detector mounting plate, and slide the detector mounting plate on this rail. Then, slide the mounting plate in the direction of the rotation axis of the rotor blade to adjust the gap to the set value, and after adjustment, fix it to the foundation bed with bolts, etc. it can.

【0011】更に、傾斜調整手段により、検出器取付板
と回転翼との相対位置関係を調整する。これは、例え
ば、検出器取付板を円周各所に傾斜調整ボルトを設けて
おき、このボルトを廻すことによりすべての回転信号検
出器と回転翼との隙間が一定になるように検出器取付板
の傾斜を調整することで可能となる。
Further, the relative positional relationship between the detector mounting plate and the rotary blade is adjusted by the tilt adjusting means. This is because, for example, the detector mounting plate is provided with tilt adjusting bolts at various places on the circumference, and by rotating this bolt, the detector mounting plate is fixed so that the clearances between all the rotation signal detectors and the rotor blades become constant. It is possible by adjusting the inclination of.

【0012】このような調整が完了すると、回転翼を回
転し、運転を開始するが、運転中は検出器取付板に取付
けた計測手段、例えば変位計によって回転翼との隙間を
常時監視するので検出器と回転翼との間隔が熱応力、等
で変化した場合には、直ちに調整をすることができる。
When such adjustment is completed, the rotor is rotated to start the operation. During operation, the gap between the rotor and the rotor is constantly monitored by the measuring means attached to the detector mounting plate, for example, the displacement gauge. When the distance between the detector and the rotary blade changes due to thermal stress or the like, the adjustment can be performed immediately.

【0013】[0013]

【実施例】以下、本発明の実施例を図面に基づいて具体
的に説明する。図1は本発明の一実施例に係る回転翼振
動計測用検出器取付装置の正面図、図2は図1における
A−A断面図、図3は図1におけるB部の詳細な断面図
である。
Embodiments of the present invention will be described below in detail with reference to the drawings. FIG. 1 is a front view of a detector mounting device for rotor blade vibration measurement according to an embodiment of the present invention, FIG. 2 is a sectional view taken along the line AA in FIG. 1, and FIG. 3 is a detailed sectional view of a portion B in FIG. is there.

【0014】図1において、運転台盤24に設置された
基礎台盤23に二つ割りの支持環20a,20b及び回
転信号検出器取付板21a,21bが取付けられてい
る。支持環20a,20bにはこの支持環22によって
支持される回転信号検出器取付板21a,21bの傾斜
を調整する手段として傾斜調整ボルト22が数組取付け
られている。
In FIG. 1, a support ring 20a, 20b and a rotation signal detector mounting plate 21a, 21b which are divided into two are attached to a base platform 23 installed on a driver's platform 24. Several sets of tilt adjusting bolts 22 are attached to the support rings 20a, 20b as means for adjusting the tilt of the rotation signal detector mounting plates 21a, 21b supported by the support rings 22.

【0015】回転信号検出器取付板21a,21bには
円周等間隔に回転信号検出器10が取付けられ、又、非
接触変位計11が取付板の上半部21a,下半部21b
にそれぞれ取付けられている。
The rotation signal detectors 10 are attached to the rotation signal detector mounting plates 21a and 21b at equal intervals around the circumference, and the non-contact displacement gauge 11 is attached to the upper half 21a and the lower half 21b of the mounting plates.
Installed on each.

【0016】図2は図1のA−A断面図で、支持環20
aと回転信号検出器取付板21aとははめあい構造であ
り、回転信号検出器取付板21aの周辺位置を支持環2
0aに取付けた傾斜調整ボルト22a,22bで両側よ
り支持する。
FIG. 2 is a sectional view taken along the line AA of FIG.
a and the rotation signal detector mounting plate 21a have a fitting structure, and the peripheral position of the rotation signal detector mounting plate 21a is fixed to the support ring 2
It is supported from both sides by the tilt adjusting bolts 22a and 22b attached to 0a.

【0017】回転信号検出器取付板21aの周囲には、
回転翼1と対向するように回転信号検出器10が等間隔
に及びレーザ変位計、等の非接触変位計11が取付けら
れている。
Around the rotation signal detector mounting plate 21a,
Rotation signal detectors 10 are installed at equal intervals so as to face the rotary blades 1, and non-contact displacement gauges 11 such as laser displacement gauges are attached.

【0018】図3は図1のB部を拡大し、断面で示した
図である。
FIG. 3 is an enlarged sectional view of the portion B of FIG.

【0019】回転信号検出器取付板の上半部21a及び
下半部21bは、それぞれのフランジ部がボルト30で
結合される。支持環の上半部20aと下半部20bとも
それぞれのフランジ部においてボルト31で結合され
る。
The upper half portion 21a and the lower half portion 21b of the rotation signal detector mounting plate are connected at their flanges with bolts 30. The upper half portion 20a and the lower half portion 20b of the support ring are also connected by bolts 31 at their respective flange portions.

【0020】基礎台盤23には滑動調整手段として滑動
レール32bとレール定盤35及びこの定盤35に設け
た滑動レールはめ合い部32aとがあり、支持環の下半
部20b取付面に設けられた滑動レールはめあい部32
aと滑動レール32bとをあわせた後、レール定盤取付
ボルト33とレール定盤プラグ34とにより基礎台盤2
3に固定される。
The base table 23 has a slide rail 32b as a slide adjusting means, a rail surface plate 35, and a slide rail fitting portion 32a provided on the surface plate 35, and is provided on the mounting surface of the lower half portion 20b of the support ring. Sliding rail fitting part 32
After aligning a and the sliding rail 32b, the foundation table 2 is fixed by the rail surface plate mounting bolt 33 and the rail surface plate plug 34.
Fixed to 3.

【0021】次に、このような構成の実施例において、
回転信号検出器取付板21の端面から回転信号検出器1
0の先端が等距離になるように回転信号検出器10を円
周上に取付けた後、運転台盤24上に取付治具全体を設
置し、滑動レール32とレール定盤35とで回転翼1の
軸方向の位置を決め、傾斜調整ボルト22a,22bを
両側から回転し、回転信号検出器10と回転翼1との隙
間を設定値に調整する。
Next, in an embodiment having such a configuration,
From the end surface of the rotation signal detector mounting plate 21, the rotation signal detector 1
After the rotation signal detector 10 is mounted on the circumference such that the tips of 0 are equidistant, the entire mounting jig is installed on the cab base 24, and the sliding rail 32 and the rail surface plate 35 are used to rotate the rotor blades. 1 is determined in the axial direction, the tilt adjusting bolts 22a and 22b are rotated from both sides, and the gap between the rotation signal detector 10 and the rotary blade 1 is adjusted to a set value.

【0022】更に、このように調整した後、回転翼を回
転させ、非接触変位計11で回転中の回転翼1との隙間
を図示省略の表示装置、等で常時監視できるので、回転
信号検出器と回転翼との隙間に異常がある場合には直ち
に修正することができる。
Further, after such adjustment, the rotary blade is rotated, and the gap between the rotary blade 1 and the rotating blade 1 can be constantly monitored by the non-contact displacement meter 11 by means of a display device (not shown) or the like. If the gap between the vessel and the rotor is abnormal, it can be corrected immediately.

【0023】以上、詳述した実施例の構成を要約する
と、回転翼振動計測装置の回転信号検出器取付治具にお
いて、回転信号検出器10を取付る取付板21と取付板
21を支持する支持環20とから構成され、支持環20
は基礎台盤23に取付けられる。
To summarize the configuration of the embodiment described in detail above, in the rotation signal detector attachment jig of the rotor blade vibration measuring apparatus, the attachment plate 21 for attaching the rotation signal detector 10 and the support for supporting the attachment plate 21. And a support ring 20.
Is attached to the base table 23.

【0024】支持環20と基礎台盤23との取付け面
は、基礎台盤23上の滑動レール32bにそって支持環
20を回転翼1の軸方向に滑動させる機構と、基礎台盤
23上のレール定盤35により支持環20と基礎台盤2
3を固定する機構を備えている。
The mounting surfaces of the support ring 20 and the base table 23 are mounted on the base table 23 by a mechanism for sliding the support ring 20 in the axial direction of the rotary blade 1 along the sliding rails 32b on the base table 23. Support ring 20 and foundation base 2 by rail surface plate 35 of
It has a mechanism for fixing 3.

【0025】回転信号検出器取付板21はその外周を支
持環20の中にはめ込む形状であり支持環20から一対
のボルト31によって固定されている。
The rotation signal detector mounting plate 21 has a shape in which its outer periphery is fitted into the support ring 20 and is fixed from the support ring 20 by a pair of bolts 31.

【0026】回転信号検出器取付板21及び支持環20
とも上半部20a,21a及び下半部20b,21bの
二つ割り構造であり回転信号検出器取付板21には上半
部20a、下半部20bにそれぞれレーザ変位計などの
非接触方式変位計11が回転翼シュラウド部と対向する
位置に取付けられている。
Rotation signal detector mounting plate 21 and support ring 20
Both have a two-part structure of upper half portions 20a, 21a and lower half portions 20b, 21b. The rotation signal detector mounting plate 21 has a non-contact type displacement gauge 11 such as a laser displacement gauge on the upper half portion 20a and the lower half portion 20b, respectively. Is mounted at a position facing the rotor blade shroud portion.

【0027】このような構成の実施例により、回転翼1
の振動計測装置の取付工数を大幅に低減することができ
る。これにより、全体の組立工程の大幅短縮ができる。
According to the embodiment having such a configuration, the rotary blade 1
It is possible to significantly reduce the number of installation steps of the vibration measuring device. As a result, the overall assembly process can be significantly shortened.

【0028】更に、非接触変位計11で回転中の回転翼
1と回転信号検出器取付板21との隙間を常時監視する
ことによって熱や回転遠心力によって、回転翼1との隙
間が変化するのを把握でき、安全に精度良く回転信号検
出ができる。
Further, by constantly monitoring the gap between the rotating blade 1 and the rotation signal detector mounting plate 21 by the non-contact displacement gauge 11, the gap between the rotating blade 1 and the rotor blade 1 is changed by heat or rotary centrifugal force. Therefore, the rotation signal can be detected safely and accurately.

【0029】[0029]

【発明の効果】以上、具体的に説明したように、本発明
においては、回転翼と対向する静止側の検出器取付板の
面を回転翼の回転軸方向に滑動させて間隔を調整する手
段と、この取付板の回転翼と対向する軸を傾斜させる手
段と、検出器取付板の面と回転翼との間隔を測定する手
段とを設けた構成としたので、次のような効果を奏する
ものである。
As described above in detail, in the present invention, means for sliding the surface of the stationary detector mounting plate facing the rotary blade in the direction of the rotary axis of the rotary blade to adjust the interval. And a means for inclining the shaft of the mounting plate facing the rotary blade, and a means for measuring the distance between the surface of the detector mounting plate and the rotary blade, the following effects can be obtained. It is a thing.

【0030】(1)回転翼振動計測装置の取付工数を大
幅に低減することができる。これにより、全体の組立工
程の大幅短縮ができる。
(1) The number of man-hours for mounting the rotor blade vibration measuring device can be greatly reduced. As a result, the overall assembly process can be significantly shortened.

【0031】(2)回転中の回転翼との隙間を隙間測定
手段で常時監視することによって熱や回転遠心力によっ
て、回転翼との隙間が変化するのを把握でき、安全に精
度良く回転信号検出ができる。
(2) By constantly monitoring the clearance between the rotating blade and the rotating blade with the clearance measuring means, it is possible to understand that the clearance between the rotating blade and the rotor changes due to heat or rotational centrifugal force. Can be detected.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の一実施例に係る回転翼振動計測用検出
器取付装置の正面図である。
FIG. 1 is a front view of a rotor blade vibration measuring detector mounting device according to an embodiment of the present invention.

【図2】図1におけるA−A断面図である。FIG. 2 is a sectional view taken along line AA in FIG.

【図3】図1におけるB部の拡大断面図である。FIG. 3 is an enlarged cross-sectional view of a B part in FIG.

【図4】従来の回転翼と回転信号検出器との位置関係を
示す側面図である。
FIG. 4 is a side view showing a positional relationship between a conventional rotary blade and a rotation signal detector.

【図5】回転翼振動計測装置の一般的な系統図である。FIG. 5 is a general system diagram of a rotor blade vibration measuring device.

【符号の説明】[Explanation of symbols]

1 回転翼 10 回転信号検出器 11 非接触変位計 20 支持環 21 回転信号検出器取付板 22 傾斜調整ボルト 23 基礎台盤 24 運転台盤 30 ボルト 31 ボルト 32 滑動レール 33 レール定盤取付ボルト 35 レール定盤 DESCRIPTION OF SYMBOLS 1 Rotor 10 Rotation signal detector 11 Non-contact displacement meter 20 Support ring 21 Rotation signal detector mounting plate 22 Tilt adjustment bolt 23 Foundation bed 24 Driving bed 30 Bolt 31 Bolt 32 Sliding rail 33 Rail surface plate mounting bolt 35 Rail Surface plate

───────────────────────────────────────────────────── フロントページの続き (72)発明者 薗田 良一 長崎市飽の浦町1番1号 三菱重工業株式 会社長崎造船所内 (72)発明者 森田 洋二 長崎市飽の浦町1番1号 三菱重工業株式 会社長崎造船所内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Ryoichi Sonoda 1-1, Atsunouramachi, Nagasaki City Mitsubishi Heavy Industries Ltd. Nagasaki Shipyard (72) Inventor Yoji Morita 1-1, Atsunouracho Nagasaki City Mitsubishi Heavy Industries Ltd. Nagasaki Shipbuilding Co., Ltd. In-house

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 回転翼に一定の間隔を保ち、同回転翼と
対向する静止側の検出器取付板に円周状に複数個設置さ
れた回転信号検出器により回転翼振動を計測する回転翼
振動計測用検出器取付装置において、前記検出器取付板
の前記回転翼と対向する面を同回転翼の回転軸方向に滑
動させて前記間隔を調整する手段と、前記検出器取付板
の軸を前記回転翼の軸方向に対して傾斜させて前記間隔
の傾斜を調整する手段と、前記検出器取付板と前記回転
翼間の隙間を計測する手段とを具備してなることを特徴
とする回転翼振動計測用検出器取付装置。
1. A rotary blade which measures a rotary blade vibration by a plurality of rotation signal detectors circumferentially arranged on a stationary-side detector mounting plate facing the rotary blade with a constant interval. In the vibration measuring detector mounting device, a means for sliding the surface of the detector mounting plate facing the rotary blade in the rotational axis direction of the rotary blade to adjust the interval, and a shaft of the detector mounting plate. Rotation, comprising means for adjusting the inclination of the interval by inclining with respect to the axial direction of the rotary blade, and means for measuring a gap between the detector mounting plate and the rotary blade. Detector mounting device for blade vibration measurement.
JP06227797A 1994-09-22 1994-09-22 Detector mounting device for rotor blade vibration measurement Expired - Lifetime JP3117370B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP06227797A JP3117370B2 (en) 1994-09-22 1994-09-22 Detector mounting device for rotor blade vibration measurement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP06227797A JP3117370B2 (en) 1994-09-22 1994-09-22 Detector mounting device for rotor blade vibration measurement

Publications (2)

Publication Number Publication Date
JPH0894432A true JPH0894432A (en) 1996-04-12
JP3117370B2 JP3117370B2 (en) 2000-12-11

Family

ID=16866546

Family Applications (1)

Application Number Title Priority Date Filing Date
JP06227797A Expired - Lifetime JP3117370B2 (en) 1994-09-22 1994-09-22 Detector mounting device for rotor blade vibration measurement

Country Status (1)

Country Link
JP (1) JP3117370B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011252875A (en) * 2010-06-04 2011-12-15 Mitsubishi Electric Corp Turbine monitoring device
JP2013061224A (en) * 2011-09-13 2013-04-04 Toshiba Corp Blade vibration measuring apparatus
JP2013195101A (en) * 2012-03-16 2013-09-30 Mitsubishi Electric Corp Turbine monitoring device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011252875A (en) * 2010-06-04 2011-12-15 Mitsubishi Electric Corp Turbine monitoring device
JP2013061224A (en) * 2011-09-13 2013-04-04 Toshiba Corp Blade vibration measuring apparatus
JP2013195101A (en) * 2012-03-16 2013-09-30 Mitsubishi Electric Corp Turbine monitoring device

Also Published As

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