JPH01298928A - Layer short detector for field winding - Google Patents

Layer short detector for field winding

Info

Publication number
JPH01298928A
JPH01298928A JP63127054A JP12705488A JPH01298928A JP H01298928 A JPH01298928 A JP H01298928A JP 63127054 A JP63127054 A JP 63127054A JP 12705488 A JP12705488 A JP 12705488A JP H01298928 A JPH01298928 A JP H01298928A
Authority
JP
Japan
Prior art keywords
probe
rotor
field winding
air gap
groove
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
Application number
JP63127054A
Other languages
Japanese (ja)
Inventor
Masao Tachibana
立花 征夫
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.)
Toshiba Corp
Original Assignee
Toshiba Corp
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 Toshiba Corp filed Critical Toshiba Corp
Priority to JP63127054A priority Critical patent/JPH01298928A/en
Publication of JPH01298928A publication Critical patent/JPH01298928A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To eliminate the removal of a detecting probe at the time of removal and insertion of a rotor by rotatably mounting the probe. CONSTITUTION:A probe 3 is secured to a probe guide 16, and rotatably mounted in a probe wedge 14. It is pressed by a helical spring 22 fixedly in a probe position securing groove 18 at its measuring position, and directed toward the center of a rotor. The guide 16 is pressed at the time of removal and insertion of the rotor, the probe 3 is removed from the securing groove 18 against the spring 22, rotated at 90 deg., and secured toward the circumferential direction of the rotor. It does not disturb the removal and insertion of the rotor at this position.

Description

【発明の詳細な説明】 〔発明の目的〕 (産業上の利用分野) 本発明は回転電機のエアーギャップ中に設ける界磁巻線
の層間短絡を検出する装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Object of the Invention] (Industrial Application Field) The present invention relates to a device for detecting an interlayer short circuit in a field winding provided in an air gap of a rotating electric machine.

(従来の技術) 例えばタービン発電機においては、円筒状に形成された
回転子の外周面・軸方向に設けられた複数個の溝の中に
界磁巻線が埋込まれ回転子より発生する磁束により固定
子側鉄心に埋込まれた電機子巻線に商用周波数の電圧を
誘起する。
(Prior art) For example, in a turbine generator, a field winding is embedded in a plurality of grooves provided on the outer peripheral surface and axial direction of a cylindrical rotor, and the field is generated by the rotor. The magnetic flux induces a commercial frequency voltage in the armature winding embedded in the stator core.

万一、回転子溝に埋込まれた界磁巻線導体間に層間短絡
が発生すると、回転子中に磁気的、熱的不平衡を生じ、
振動アンバランスから発電機の事故に進展する虞れがあ
る。
In the unlikely event that an interlayer short circuit occurs between the field winding conductors embedded in the rotor grooves, magnetic and thermal imbalance will occur in the rotor.
There is a risk that the vibration imbalance will lead to a generator accident.

このような事故の原因となる界磁巻線導体間の層間短絡
を界磁巻線の抵抗変化によって検出する為には、例えば
界磁巻線の巻回数が114回として、このうち1回分の
導体の層間短絡による抵抗変化は0.9%位と僅かであ
り検出は極めて困難であった。
In order to detect an interlayer short circuit between the field winding conductors, which causes such an accident, by a change in resistance of the field winding, for example, assuming that the number of turns of the field winding is 114, it is necessary to The resistance change due to the interlayer short circuit of the conductor was as small as 0.9%, and it was extremely difficult to detect.

又、層間短絡は、回転子の高速回転による遠心力と運転
中の温度上昇に起因する力とが作用している時に起る為
、従来は層間短終の検出を抵抗変化によらず層間短絡を
起した界磁巻線導体が埋込まれた溝内巻線が起す回転子
外周面の局所的な減少磁束と層間短絡を起していない界
磁巻線が起す洩れ磁束との差異を検出する事により感度
よく層間短絡を起した界磁巻線導体が埋込まれ溝を特定
する方法が知られている。
In addition, interlayer short circuits occur when centrifugal force due to high-speed rotation of the rotor and force due to temperature rise during operation act, so conventionally, interlayer short circuits were detected without relying on resistance changes. Detects the difference between the locally decreased magnetic flux on the rotor outer circumferential surface caused by the grooved winding in which the field winding conductor is embedded, and the leakage magnetic flux caused by the field winding that has not caused the interlayer short circuit. A method is known in which the field winding conductor in which the interlayer short circuit has occurred is buried and the groove can be identified with high sensitivity.

この方法は第6図に示されるように回転子1と固定子鉄
心2との間に形成されたリング状のエアーギャップ中に
回転子1の外周面に近接して設けられた非磁性材1例え
ばステンレス鋼又は合成樹脂からなる筒状のプローブ3
中にピックアップコイル4を収容し回転子の溝5に埋込
まれた界磁巻線6によって生ずる洩れ磁束7をピックア
ップコイル4と交鎖させることにより回転子溝5の客数
と回転子の回転数との積から決まる磁束脈動周波数の電
圧をピックアップコイル4に誘起させ、この電圧波形の
不規則性から層間短絡を発生した界磁巻線導体の埋込ま
れた溝を特定するものである。
In this method, as shown in FIG. 6, a non-magnetic material 1 is provided close to the outer peripheral surface of the rotor 1 in a ring-shaped air gap formed between the rotor 1 and the stator core 2. For example, a cylindrical probe 3 made of stainless steel or synthetic resin
The number of customers in the rotor groove 5 and the rotation speed of the rotor can be changed by intersecting the leakage magnetic flux 7 generated by the field winding 6 embedded in the groove 5 of the rotor with the pickup coil 4. A voltage with a magnetic flux pulsation frequency determined by the product of the oscillation frequency and the oscillation frequency is induced in the pickup coil 4, and the groove in which the field winding conductor is buried, where the interlayer short circuit has occurred, is identified from the irregularity of this voltage waveform.

なお第7図に於て8は固定子鉄心2の溝に埋込まれた電
機子巻線、15は電機子巻線を固定する固定子極、第2
図に於て14はプローブ3を内蔵し固定子極15をエア
ーギャップ軸方向にスライドできるダブテール断面形状
を有したプローブ楔、12はピックアップコイル4に誘
起された電圧を発電機機外に設けられた表示装置13に
導くリード線である。
In Fig. 7, 8 is the armature winding embedded in the groove of the stator core 2, 15 is the stator pole for fixing the armature winding, and the second
In the figure, 14 is a probe wedge with a built-in probe 3 and a dovetail cross-sectional shape that allows the stator pole 15 to slide in the axial direction of the air gap, and 12 is a probe wedge provided outside the generator to transfer the voltage induced in the pickup coil 4. This is a lead wire leading to the display device 13.

(発明が解決しようとする課題) 以上のような検出装置に於てプローブ3は界磁巻線6の
鉄心端部を保持する保持環外径面より回転子中心側に突
起させ、回転子表面に近接させ固定する必要がある為、
回転子を固定子内部より引抜き、又は再挿入する時障害
になった。従って、回転子引抜き再挿入時はプローブ3
を内蔵するプローブ楔14と固定子極15のダブテール
断面形状部をエアーギヤツブ軸宝庫工にスライドさせて
該固定子極より取外す必要があった。
(Problem to be Solved by the Invention) In the detection device as described above, the probe 3 protrudes toward the center of the rotor from the outer diameter surface of the retaining ring that holds the end of the core of the field winding 6. It is necessary to fix it close to the
This caused an obstruction when removing or reinserting the rotor from inside the stator. Therefore, when the rotor is pulled out and reinserted, the probe 3
It was necessary to slide the dovetail cross section of the probe wedge 14 and the stator pole 15 into the air gear shaft to remove them from the stator pole.

この発明は以上に述べた従来方法の欠点を除き界磁巻線
の層間短終検出装置のプローブを回転子引抜き、再挿入
時に障害にならないように回転子保持環の外径より外周
側に移動、維持、固定を容易にする為の装置を提供する
ことを目的とする。
This invention eliminates the drawbacks of the conventional method described above and moves the probe of the field winding short interlayer detection device to the outer circumferential side of the rotor retaining ring so as not to become an obstacle when the rotor is pulled out and reinserted. The purpose is to provide a device that facilitates maintenance and fixation.

〔発明の構成〕[Structure of the invention]

(課題を解決するための手段) 上記の目的を達成するため本発明は、回転電機の回転子
溝に埋込まれた界磁巻線に発生した層間短絡を検出する
装置において、固定子と回転子との間に形成されたエア
ーギャップ中に回転子周面に近接して設けられ、ピック
アップコイルを内蔵したプローブとこのプローブを固定
する固定子鉄心内周溝に埋込まれた電機子巻線を保持す
る固定子極にエアーギャップ軸方向に容易にスライドで
きるプローブガイド丸穴と、プローブを回転子中心方向
に向けエアーギャップ軸方向および円周方向に位置固定
する半円形状のプローブ位置固定溝とを設け、プローブ
の固定を確実にしさらに、プローブガイドを軸方向に容
易にスライド可能とするスプリングを内蔵する事により
、プローブを固定子極より取外すことなく回転子を引抜
き再挿入できるように構成した事を特徴とするものであ
る。
(Means for Solving the Problems) In order to achieve the above object, the present invention provides a device for detecting an interlayer short circuit that occurs in a field winding embedded in a rotor groove of a rotating electrical machine. A probe with a built-in pickup coil is installed close to the circumferential surface of the rotor in the air gap formed between the probe and the armature winding embedded in the inner circumferential groove of the stator core that fixes this probe. A probe guide round hole that can easily slide in the air gap axial direction on the stator pole that holds the rotor, and a semicircular probe position fixing groove that fixes the probe in the air gap axial direction and circumferential direction toward the rotor center. The rotor can be pulled out and re-inserted without removing the probe from the stator pole by incorporating a built-in spring that securely fixes the probe and allows the probe guide to easily slide in the axial direction. It is characterized by the fact that

(作用) 本発明は上記のように構成されており、層間短絡検出時
においては、プローブの先端すなわち検出部は回転子中
心方向を向くように固定され1回転子の引抜きや挿入時
には1回転子の円周方向(接線方向)を向くように固定
されるので、回転子の引抜き、挿入等の作業が不用とな
り、プローブの破損やリード線の断線等も防止でき層間
短絡検出のイa頼性も向上する。
(Function) The present invention is configured as described above, and when detecting an interlayer short circuit, the tip of the probe, that is, the detection part is fixed so as to face the rotor center direction, and when one rotor is pulled out or inserted, one rotor is Since it is fixed so that it faces in the circumferential direction (tangential direction) of the rotor, there is no need to pull out and insert the rotor, and it also prevents damage to the probe and breakage of the lead wire, ensuring reliability in detecting interlayer short circuits. It also improves.

(実施例) 以下に本発明の一実施例について図を用いて説明する。(Example) An embodiment of the present invention will be described below with reference to the drawings.

第1図は本発明の一実施例を示すもので、固定子鉄心端
部の電機子巻線を保持する固定子楔にプローブを内蔵し
たプローブ楔14の全体図を示す。
FIG. 1 shows one embodiment of the present invention, and shows an overall view of a probe wedge 14 in which a probe is built into a stator wedge that holds an armature winding at the end of a stator core.

第2図は第1図のプローブ楔14の断面を示し、プロー
ブ3が回転子中心方向を向き固定された状態を示す。第
3図は第1図のプローブ楔14の断面を示し、プローブ
3がエアーギャップ周方向に向き固定された状態を示す
。第4図は第1図ないし第3図に示すプローブガイド1
6に設けられたロック溝19に嵌合するロックスプリン
グ21を内蔵したロックナツトの断面を示す。第5図は
プローブ楔14に内蔵したヘリカルコイルスプリング2
2を示す。
FIG. 2 shows a cross section of the probe wedge 14 shown in FIG. 1, showing a state in which the probe 3 is fixed and facing toward the center of the rotor. FIG. 3 shows a cross section of the probe wedge 14 shown in FIG. 1, showing a state in which the probe 3 is oriented and fixed in the circumferential direction of the air gap. Figure 4 shows the probe guide 1 shown in Figures 1 to 3.
6 shows a cross section of a lock nut incorporating a lock spring 21 that fits into a lock groove 19 provided in the nut 6. Figure 5 shows the helical coil spring 2 built into the probe wedge 14.
2 is shown.

次に本実施例の作用について説明する。すなわち、上記
のように構成された界磁巻線の層間短終検出装置は次の
ように作用する。
Next, the operation of this embodiment will be explained. That is, the field winding interlayer short termination detection device configured as described above operates as follows.

(υ プローブ3の取付が固定子鉄心端に設けられる固
定子楔を兼用するプローブ楔14の為固定が確実で強固
にできる。
(υ Since the probe 3 is attached to the probe wedge 14 which also serves as a stator wedge provided at the end of the stator core, the probe 3 can be fixed securely and firmly.

■ プローブ3の取付位置が固定子鉄心端部の為固定子
1の表面からプローブ3までの間隙が実測できると共に
調整が容易にできる。
- Since the probe 3 is installed at the end of the stator core, the gap from the surface of the stator 1 to the probe 3 can be measured and adjusted easily.

■ プローブガイド16を軸方向にスライドさせる事に
よりプローブ3の向き方向を回転子中心方向、又はエア
ーギャップ周方向に変える事ができる。
(2) By sliding the probe guide 16 in the axial direction, the direction of the probe 3 can be changed to the rotor center direction or the air gap circumferential direction.

0) プローブガイド16を軸方向にスライドさせる時
、プローブ楔14に内蔵したスプリングのカにより容易
にスライドできる。
0) When the probe guide 16 is slid in the axial direction, it can be easily slid by the force of the spring built into the probe wedge 14.

■ スプリングの力による固定と共にプローブ楔14に
設けたプローブ位置固定溝18により確実に固定できる
(2) In addition to being fixed by the force of a spring, the probe position fixing groove 18 provided in the probe wedge 14 allows for reliable fixation.

■ プローブ楔14端部に設けたロックナツト位置をプ
ローブガイド16に添っ□て軸方向に移動するだけでプ
ローブガイド16に設けられたロック溝19にロックナ
ツト20に内蔵したスプリング21によりプローブ3の
方向1回転子中心方向又はエアーギャップ周方向に位置
固定する事が確実にできる。
■ By simply moving the lock nut provided at the end of the probe wedge 14 along the probe guide 16 in the axial direction, the spring 21 built into the lock nut 20 engages the lock groove 19 provided in the probe guide 16 to lock the probe 3 in the direction 1. The position can be reliably fixed in the rotor center direction or air gap circumferential direction.

■ プローブ楔14に内蔵したスプリング22にヘリカ
ルコイルを使用しスプリング端部の一方をプローブ楔に
固定又は他端をプローブガイド16に固定する事により
ヘリカルコイルの巻方向の反発力によりプローブ3の向
きを回転子中心方向又はエアーギャップ周方向に容易に
変える事ができる。
■ By using a helical coil in the spring 22 built into the probe wedge 14 and fixing one end of the spring to the probe wedge or the other end to the probe guide 16, the direction of the probe 3 is controlled by the repulsive force in the winding direction of the helical coil. can be easily changed toward the rotor center direction or the air gap circumferential direction.

(8)  プローブ3の向きをエアーギャップ周方向に
変える事ができる為、回転子挿入、分解時に回転子鉄心
部外径より大きい回転子コイル保持環がプローブ3に当
る事がない。従ってエアーギャップ円周方向任意にプロ
ーブ取付場所が選定できる。
(8) Since the direction of the probe 3 can be changed in the circumferential direction of the air gap, the rotor coil retaining ring, which is larger than the outer diameter of the rotor core, does not come into contact with the probe 3 when the rotor is inserted or disassembled. Therefore, the probe mounting location can be selected arbitrarily in the circumferential direction of the air gap.

次に本実施例の効果を以下に述べる6 (1)  プローブ3の取付位置が固定子鉄心端部にあ
る為、取付状態の確認が目視てき又、回転子表面とプロ
ーブ間の間隙が実測でき、調整容易になる為信頼性の高
い波形が得られる。
Next, the effects of this embodiment will be described below.6 (1) Since the probe 3 is installed at the end of the stator core, the installation status can be visually confirmed, and the gap between the rotor surface and the probe can be actually measured. Since the adjustment is easy, a highly reliable waveform can be obtained.

■ 回転子+ff16が非磁性材料の横位置にプローブ
3を取付ける為プローブ楔14を含め内蔵するプローブ
ガイド16、ロックナツト20、スプリング22等を非
磁性1例えばステンレス鋼、合成樹脂材にする事により
洩れ磁束波形が鮮明になりより精度の高い層間短絡検出
装置が提供できる。
■ Since the rotor + ff16 mounts the probe 3 horizontally on a non-magnetic material, the built-in probe guide 16 including the probe wedge 14, lock nut 20, spring 22, etc. are made of non-magnetic materials such as stainless steel or synthetic resin to prevent leakage. The magnetic flux waveform becomes clearer, and a more accurate interlayer short circuit detection device can be provided.

■ プローブ3はプローブガイド16をプローブ楔14
の内部にて軸方向にスライドさせる事により方向が変え
られる為、回転子挿入、又は引抜き時にプローブ楔14
を分解する必要がなくなりプローブ取付の信頼性が向上
する。
■ Probe 3 connects probe guide 16 to probe wedge 14
The direction of the probe wedge 14 can be changed by sliding it in the axial direction inside the probe wedge 14 when inserting or removing the rotor.
There is no need to disassemble the probe, which improves the reliability of probe installation.

に) エアーギャップ周方向任意の位置にプローブ取付
が可能になる為、プローブ取付の作業における信頼性・
が向上する。
) Since the probe can be installed at any position in the circumferential direction of the air gap, reliability and
will improve.

■ 界磁巻線の層間短絡検出が第1図に示すようにプロ
ーブ梗14の内部でプローブ3の方向を変える事ができ
る為、プローブを取付だ後、回転子挿入、引抜き時プロ
ーブ楔を分解する必要がなくなり復旧が容易になり発電
機連続運転はもとより、界磁巻線の層間短絡検出試験が
容易にできるようになった。
■ Since the direction of the probe 3 can be changed inside the probe stem 14 to detect interlayer short circuits in the field winding as shown in Figure 1, the probe wedge can be disassembled when the rotor is inserted or removed after the probe is installed. There is no longer a need to do this, making recovery easier, and not only can the generator be operated continuously, but it has also become easier to test the field winding for interlayer short circuit detection.

〔発明の効果〕〔Effect of the invention〕

以上に説明したように本発明の界磁巻線の層間短絡検出
装置はプローブ取付固定位置を固定子鉄心内周の軸方向
端部に位置する固定子楔とし固定子楔自体にプローブを
取付る事によりシンプルな構造となり、プローブ取付部
の固定が確実になり目視確認と共に手触確認もできるよ
うになった。
As explained above, in the field winding interlayer short circuit detection device of the present invention, the probe is fixed at the stator wedge located at the axial end of the inner circumference of the stator core, and the probe is attached to the stator wedge itself. As a result, the structure is simple, the probe mounting part is securely fixed, and it is now possible to check both visually and by touch.

又従来の鉄心端部の固定子楔にプローブを内蔵したダブ
テール形状断面のプローブ楔を挿入固定する方法では回
転子を固定子に挿入又は引抜時にプローブが回転子中心
方向に突起している為、回転子鉄心外径より径の大きい
界磁巻線エンドを保持する保持環が障害になりプローブ
楔をその都度分解する必要があったが、本発明提案では
プローブ撲を分解する事なく回転子の挿入、引抜きが可
能となった為、プローブ楔の分解、再組立に要する作業
におけるプローブ固定の信頼性が一段と向上し、発電機
の連続運転中に於ける界磁巻線層間短絡検出試験がプロ
ーブ取付部不具合により試験できなくなる事を解消でき
る。従って例えば内部水素ガス冷却の発電機に於ては、
機内の水素ガスを放出、再挿入等水素ガス濃度によって
は爆発の危険性を有する放出、再封入のプロセスを省略
する事ができると共に、プローブ楔の分解、再組立の工
程が省略できる大きな効果を有するものである。
Furthermore, in the conventional method of inserting and fixing a dovetail-shaped probe wedge with a built-in probe into the stator wedge at the end of the iron core, the probe protrudes toward the center of the rotor when the rotor is inserted or removed from the stator. The retaining ring that holds the field winding end, which has a diameter larger than the outer diameter of the rotor core, became an obstacle and the probe wedge had to be disassembled each time.However, with the present invention, the rotor can be removed without disassembling the probe wedge. Since it is now possible to insert and pull out the probe, the reliability of fixing the probe during disassembly and reassembly of the probe wedge is further improved, and the probe can be used to detect short circuits between the field winding layers during continuous operation of the generator. This eliminates the possibility of being unable to test due to a problem with the mounting part. Therefore, for example, in a generator with internal hydrogen gas cooling,
It is possible to omit the process of releasing and re-inserting the hydrogen gas inside the machine, which has a risk of explosion depending on the hydrogen gas concentration, and has the great effect of omitting the process of disassembling and reassembling the probe wedge. It is something that you have.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明によるプローブ取付部詳細の一実施例図
、第2図はプローブが回転子中心方向を向いている時の
実施例断面図、第3図はプローブがエアーギャップ周方
向を向いている時の実施例断面図、第4図はプローブガ
イドをロックするロックナツト断面の一実施例、第5図
はプローブ楔に内蔵するスプリングの一実施例図、第6
図は界磁巻線層間短絡検出用プローブを回転電機エアー
ギャップ中に取付けた全体樋成図、第7図は従来のプロ
ーブ取付部詳細図である。 1・・・回転子、     2・・・固定子鉄心、3・
・・プローブ、   4・・・ピックアップコイル5・
・・回転子の溝、   6・・・界磁巻線、7・・・洩
れ磁束、    8・・・電機子巻線。 10・・・固定子フレーム外周板、 12・・・リード線、    13・・・電圧表示装置
。 14・・・プローブ楔、  15・・・固定子楔、16
・・・回転子楔、   17・・・プローブガイド穴、
18・・・プローブ位置固定溝、 19・・・ロック溝、    20・・・ロックナツト
、21・・・ロックナツトスプリング、 22・・・ヘリカルコイルスプリング。 代理人 弁理士 則 近 憲 佑 同  第子丸 健 第4図
Fig. 1 is a detailed view of an embodiment of the probe mounting part according to the present invention, Fig. 2 is a sectional view of the embodiment when the probe is oriented toward the rotor center, and Fig. 3 is a sectional view of the embodiment when the probe is oriented toward the circumferential direction of the air gap. FIG. 4 is a cross-sectional view of a lock nut that locks the probe guide, FIG. 5 is a cross-sectional view of a spring built into the probe wedge, and FIG.
The figure shows the overall structure of a probe for detecting a short circuit between the field winding layers installed in the air gap of a rotating electrical machine, and FIG. 7 is a detailed view of a conventional probe mounting part. 1... Rotor, 2... Stator core, 3...
...Probe, 4...Pickup coil 5.
... Rotor groove, 6... Field winding, 7... Leakage flux, 8... Armature winding. 10... Stator frame outer peripheral plate, 12... Lead wire, 13... Voltage display device. 14... Probe wedge, 15... Stator wedge, 16
...Rotor wedge, 17...Probe guide hole,
18... Probe position fixing groove, 19... Lock groove, 20... Lock nut, 21... Lock nut spring, 22... Helical coil spring. Agent Patent Attorney Noriyuki Chika Ken Yudo Daishimaru Ken Figure 4

Claims (3)

【特許請求の範囲】[Claims] (1)回転電機の回転子溝に埋込まれた界磁巻線の層間
短絡を検出する装置において、固定子と回転子との間に
形成されたリング状の空隙(以下エアーギャップと称す
)中に回転子外周面に近接して設けられ、ピックアップ
コイルを内蔵したプローブと、該プローブを固定するプ
ローブガイドと、このプローブガイドをエアーギャップ
軸方向に移動させるプローブガイド丸穴とこのプローブ
ガイド丸穴に挿入されたスプリングと、前記プローブを
回転子中心方向ならびにエアーギャップ軸方向および円
周方向に位置固定する半円形状のプローブ位置固定溝と
が固定子鉄心内周溝に埋込まれた固定子巻線を保持する
固定子楔に設けられている事を特徴とする界磁巻線の層
間短絡検出装置。
(1) In a device that detects an interlayer short circuit in a field winding embedded in a rotor groove of a rotating electric machine, a ring-shaped air gap (hereinafter referred to as an air gap) formed between a stator and a rotor is used. A probe that is provided close to the outer peripheral surface of the rotor and has a built-in pickup coil, a probe guide that fixes the probe, a probe guide round hole that moves this probe guide in the air gap axial direction, and this probe guide round A fixing device in which a spring inserted into a hole and a semicircular probe position fixing groove that fixes the probe in position in the rotor center direction, air gap axial direction, and circumferential direction are embedded in a stator core inner circumferential groove. An interlayer short circuit detection device for a field winding, characterized in that it is provided on a stator wedge that holds a child winding.
(2)プローブガイドにプローブを回転子中心方向およ
び回転子周方向に向け位置固定する為のロック溝を設け
た事を特徴とする界磁巻線の層間短絡検出装置。
(2) An interlayer short-circuit detection device for a field winding, characterized in that the probe guide is provided with a locking groove for positioning and fixing the probe in the rotor center direction and rotor circumferential direction.
(3)プローブガイドのロック溝に嵌合するロックスプ
リングを内蔵したロックナットを設けた事を特徴とする
特許請求の範囲第2項記載の界磁巻線の層間短絡検出装
置。
(3) The interlayer short-circuit detection device for a field winding according to claim 2, further comprising a lock nut having a built-in lock spring that fits into a lock groove of the probe guide.
JP63127054A 1988-05-26 1988-05-26 Layer short detector for field winding Pending JPH01298928A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63127054A JPH01298928A (en) 1988-05-26 1988-05-26 Layer short detector for field winding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63127054A JPH01298928A (en) 1988-05-26 1988-05-26 Layer short detector for field winding

Publications (1)

Publication Number Publication Date
JPH01298928A true JPH01298928A (en) 1989-12-01

Family

ID=14950461

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63127054A Pending JPH01298928A (en) 1988-05-26 1988-05-26 Layer short detector for field winding

Country Status (1)

Country Link
JP (1) JPH01298928A (en)

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