JP3362446B2 - Electrode for wing processing of integrated impeller - Google Patents
Electrode for wing processing of integrated impellerInfo
- Publication number
- JP3362446B2 JP3362446B2 JP11498393A JP11498393A JP3362446B2 JP 3362446 B2 JP3362446 B2 JP 3362446B2 JP 11498393 A JP11498393 A JP 11498393A JP 11498393 A JP11498393 A JP 11498393A JP 3362446 B2 JP3362446 B2 JP 3362446B2
- Authority
- JP
- Japan
- Prior art keywords
- wing
- electrode
- forming
- blade
- electrode portion
- 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.)
- Expired - Lifetime
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- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Description
【発明の詳細な説明】
【０００１】
【産業上の利用分野】本発明は一体型翼車の翼部加工用
電極に関するものである。
【０００２】
【従来の技術】近年、航空機用ガスタービンエンジンの
高性能化に伴い、ガスタービンエンジンのコンプレッサ
に用いられる翼車（ロータディスク）の軽量化を図り、
翼並びに車板の翼根部を応力集中から守るために、翼と
車板を一体的に構成した一体型翼車が用いられている。
【０００３】上記一体型翼車を切削加工を行うことなく
効率よく製作する一手段として、特開平１−２２２８２
０号公報に電解加工法による一体型翼車の加工法が開示
されている。
【０００４】以下、図５及び図６により、上記公報に開
示されている翼部加工用電極ついて説明する。
【０００５】１は形成すべき翼部の背面と略同形状の翼
背部形成曲面２を有する翼背部形成用電極部、３は形成
すべき翼部の腹面と略同形状の翼腹部形成曲面４を有す
る翼腹部形成用電極部であり、翼背部形成用電極部１、
翼腹部形成用電極部３の基端部は、該翼背部形成用電極
部１、翼腹部形成用電極部３を電解加工装置に装着する
ための電極支持体５，６に取り付けられている。
【０００６】一方の電極支持体６の反電極Ｂ側端部に
は、翼背部形成用曲面２と翼腹部形成用曲面４を対向さ
せた際に、他方の電極支持体５へ向って突出する突出部
８が設けられ、また、他方の電極支持体５の反電極側端
部には、前記突出部８が嵌合可能な切欠部７が形成され
ている。
【０００７】９，１０は翼背部形成用曲面２と翼腹部形
成用曲面４を対向させた際に、電極支持体５，６の互い
に対向する面に設けられた電極先端Ａ側へ向って延びる
導液溝、１１，１２は電極支持体５，６の反電極Ｂ側端
面から前記導液溝９，１０へ貫通するように穿設された
導液孔、１３，１４は前記導液孔１１，１２に接続され
た給液管である（図５参照）。
【０００８】更に、前記電極支持体５の一面には導液板
１５が、電極支持体６の一面及び各電極１，３の翼前縁
側端部に当接するように、また、電極支持体６の他面に
は導液板１６が、電極支持体５の他面及び各電極部１，
３の翼後縁側端部に当接するように取り付けられてい
て、導液板１５，１６、翼背部形成用電極部１、翼腹部
形成用電極部３により翼を形成するための電極先端Ａ側
が開口した電解液流路１８を、また、導液板１５，１
６、電極支持体５，６により前記電解液流路１８へ連通
する電解液流路１７を形成している（図６参照）。
【０００９】上述した構成を有する翼部加工用電極を用
いて一体型翼車の成形加工を行う際には、Ｙ軸上に対向
配置され且つ互いに近接離反可能な一対の側面ラムと、
Ｘ軸上に配置され且つＹ軸に対して近接離反可能でＸ軸
を中心に回動可能な正面ラムを有する電解加工装置を用
い、前記側面ラムの一方に翼背部形成用電極部１を、側
面ラムの他方に翼腹部形成用電極部３を、翼背部形成曲
面２と翼腹部形成曲面４が対向するように取り付け、更
に、一体型翼車の材料である金属部材１９を前記正面ラ
ムに取り付ける。
【００１０】次いで、翼背部形成用電極部１と翼腹部形
成用電極部３を所定の間隔に保ち、金属部材１９が＋極
に、各電極部１，３が−極になるように金属部材１９と
電極部１，３の間に電圧を印荷するとともに、給液管１
３，１４へ電解液を供給して導液孔１１，１２、導液溝
９，１０及び電解液流路１７を介して電解液流路１８の
電極先端Ａ側の開口より電解液を外部へ流出させ、金属
部材１９を各電極１，３部の先端部へ近接させると、金
属部材１９の表層部が電気分解され電解加工が行われ、
更に、電極部１，３を互いに近接させるとともに、電極
部１，３に対して金属部材１９を近接させながらＸ軸を
中心に所定の角度まで回動させると、金属部材１９に略
翼背部形成曲面２と翼腹部形成曲面４に合致した背面と
腹面を有する翼部２０が形成される。
【００１１】
【発明が解決しようとする課題】ところが、電解液流路
１８を流通する電解液により、翼背部形成用電極部１と
翼腹部形成用電極部３が振動して形成すべき翼部２０を
所定の形状に形成することができなかったり、また、導
液板１５，１６が振動することにより該導液板１５，１
６と電極部１，３の間に間隙が形成され、電解液の一部
が前記間隙から外部へ漏洩し、一体型翼車を電解加工に
より効率よく形成することができない場合があった。
【００１２】一方、各電極部１，３及び導液板１５，１
６の振動を防止するために、電極部１，３の厚さ及び導
液板１５，１６の厚さを厚くして強度向上を図ることが
考えられるが、電極部１，３の厚さは形成すべき一体型
翼車の隣接する翼部２０間の寸法により決定されてしま
うので、一体型翼の翼部２０間の寸法が小さい場合に
は、電極部１，３の厚さを増大することができなかっ
た。
【００１３】本発明は上述した実情に鑑みなしたもの
で、各電極部の振動を防止することが可能な一体型翼車
の翼部加工用電極を提供することを目的としている。
【００１４】
【課題を解決するための手段】本発明の一体型翼車の翼
部加工用電極は、形成すべき翼の背面と略同形状の翼背
部形成曲面を一面に有する電極部の巾方向の両縁に、当
該電極部の先端から基端までの全長にわたって、形成す
べき翼の先端側から基端側へ延びる突設部を設けた翼背
部形成用電極部と、形成すべき翼の腹面と略同形状の翼
腹部形成曲面を一面に有する電極部の巾方向の両縁に、
当該電極部の先端から基端までの全長にわたって、形成
すべき翼の先端側から基端側へ延びる突設部を設けた翼
腹部形成用電極部とを備え、前記翼背部形成用電極部と
翼腹部形成用電極部を対峙させた際に、両電極部の突設
部がその全長にわたり相互に接して翼背部形成曲面と翼
腹部形成曲面の間に前記翼の先端側から基端側へ延びる
流路が形成され且つ両電極部の対峙間隔を変化せしめ得
るように構成したものである。
【００１５】
【作用】本発明の一体型翼車の翼部加工用電極では、翼
背部形成用電極部、翼腹部形成用電極部は、突設部を設
けることにより強度が高くなっているので、翼背部形成
曲面と翼腹部形成曲面、並びに突設部により囲まれる流
路に電解液を流通させても、前記両電極部が振動するこ
とがない。
【００１６】
【実施例】以下本発明の実施例を図面を参照しつつ説明
する。
【００１７】図１から図４は本発明の一体型翼車の翼部
加工用電極の一実施例を示すもので、２１は形成すべき
翼の背面と略同形状の翼背部形成曲面２２を一面に有す
る電極部２５の両端に、突設部２６，２７を設けた翼背
部形成用電極部、２３は形成すべき翼の腹面と略同形状
の翼腹部形成曲面２４を一面に有する電極部２８の両端
他端に、突設部２９，３０を設けた翼腹部形成用電極部
である。
【００１８】前記翼背部形成用電極部２１と翼腹部形成
用電極部２３を対峙させると、両電極部２１，２３の翼
背部形成曲面２２と翼腹部形成曲面２４、並びに突設部
２６，２７，２９，３０により囲まれた電解液流路３１
が形成されるようになっており、また、両電極部２１，
２３の翼背部形成曲面２２と翼腹部形成曲面２４を互い
に近接離反させることができるようになっている。
【００１９】更に、３２，３３は翼背部形成用電極部２
１、翼腹部形成用電極部２３の基端部に形成された電極
基部である。
【００２０】上述した構成を有する翼部加工用電極を用
いて一体型翼車の成形加工を行う際には、前述した電解
加工装置の一方の側面ラムに翼背部形成用電極部２１の
電極基部３２を、他方の側面ラムに翼腹部形成用電極部
２３の電極基部３３を、翼背部形成曲面２２と翼腹部形
成曲面２４が対向するように取り付ける。
【００２１】この状態で、翼背部形成曲面２２と翼腹部
形成曲面２４、並びに突設部２６，２７，２９，３０に
より囲まれた流路３１に、電解液を電極基部３２，３３
側から電極部２１，２３の先端へ向って流通させたとす
ると、前記翼背部形成用電極部２１、翼腹部形成用電極
部２３は突設部２６，２７，２９，３０を設けることに
より強度が高くなっているので、前記両電極部２１，２
３が電解液の流通によって振動することがない。
【００２２】よって、上述した翼背部形成用電極部２
１、翼腹部形成用電極部２３を有する翼部加工用電極に
より一体型翼車の電解加工を行えば、形成すべき翼部を
所定の形状に形成することができ、また、両電極部２
１，２３の振動による間隙が形成されないので、電解液
の漏洩が発生せず、一体型翼車を電解加工により効率よ
く形成することができる。
【００２３】更に、前記両電極部２１，２３の厚さを厚
くして強度向上を図らなくてもよいので、形成すべき一
体型翼の翼部間の寸法が小さい場合でも、上述した構成
を有する翼部加工用電極を用いることができる。
【００２４】なお、本発明の一体型翼車の翼部架構用電
極は、上述の実施例にのみ限定されるものではなく、本
発明の要旨を逸脱しない範囲内において種々変更を加え
得ることは勿論である。
【００２５】
【発明の効果】上記した本発明の一体型翼車の翼部加工
用電極によれば、下記のような種々の優れた効果を奏し
得る。
【００２６】（１）翼背部形成用電極部、翼腹部形成用
電極部に突出部を設けているので、強度が高くなり、電
解液の流通による電極部に振動を回避でき、翼部を所定
の形状に形成することができる。
【００２７】（２）相互に接する両電極部の突設部によ
って流路から外部への電解液の漏洩が抑止され、加工対
象の金属部材と両電極部の形成曲面との間の空隙に、充
分な流量の電解液を供給できるので、一体型翼車を電解
加工により効率よく形成することが可能なり、これに加
えて、間隔が変化し得る両形成曲面に翼の先端側から基
端側へ延びる流路を形成させるで、金属部材と両形成曲
面の間隔が狭まって、両形成曲面の転写精度が向上し、
高精度の翼前縁形状及び後縁形状を得ることができる。
【００２８】（３）前記両電極部の厚さを厚くして強度
向上を図らなくてもよいので、形成すべき一体型翼の翼
部間の寸法が小さい場合でも対応することができる。Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an electrode for machining a wing portion of an integrated impeller. [0002] In recent years, as the performance of gas turbine engines for aircraft has been improved, the weight of impellers (rotor disks) used for compressors of gas turbine engines has been reduced.
In order to protect the wings and the blade roots of the vehicle plate from stress concentration, an integrated impeller integrally formed with the wings and the vehicle plate is used. As one means for efficiently manufacturing the above-mentioned integral impeller without cutting, Japanese Patent Application Laid-Open No. 1-222282 is known.
No. 0 discloses a method of machining an integrated impeller by electrolytic machining. [0004] The wing processing electrode disclosed in the above publication will be described below with reference to FIGS. 5 and 6. [0005] 1 is a wing back portion forming electrode portion having a wing back portion forming curved surface 2 having substantially the same shape as the back surface of the wing portion to be formed. 3 is a wing abdomen forming curved surface 4 having substantially the same shape as the abdominal surface of the wing portion to be formed. A wing abdomen forming electrode portion having a wing back portion forming electrode portion 1,
The base end of the wing abdomen forming electrode portion 3 is attached to electrode supports 5 and 6 for mounting the wing abdomen forming electrode portion 1 and the wing abdomen forming electrode portion 3 to an electrolytic processing apparatus. When the curved surface 2 for forming the back of the wing and the curved surface 4 for forming the abdomen of the wing are opposed to the end of one electrode support 6 on the side opposite to the electrode B, it projects toward the other electrode support 5. A protruding portion 8 is provided, and a cutout 7 into which the protruding portion 8 can be fitted is formed at the opposite electrode side end of the other electrode support 5. When the curved surface 2 for forming the back of the wing and the curved surface 4 for forming the abdomen of the wing are opposed to each other, reference numerals 9 and 10 extend toward the tip A of the electrode provided on the opposed surfaces of the electrode supports 5 and 6. The liquid guide grooves 11 and 12 are liquid guide holes formed so as to penetrate from the end surfaces of the electrode supports 5 and 6 on the side opposite to the electrode B to the liquid guide grooves 9 and 10, and 13 and 14 are the liquid guide holes 11. , 12 (see FIG. 5). Further, a liquid guide plate 15 is provided on one surface of the electrode support 5 so as to be in contact with one surface of the electrode support 6 and the leading edge side end of each of the electrodes 1 and 3. A liquid guide plate 16 is provided on the other surface of the electrode support 5 and the other electrode portions 1 and 2.
The electrode tip A for forming a wing by the liquid guide plates 15 and 16, the wing back-forming electrode portion 1, and the wing abdomen forming electrode portion 3 is attached so as to abut on the trailing edge side end of the wing 3. The opened electrolyte flow path 18 is connected to the liquid guide plates 15, 1.
6. Electrolyte flow paths 17 communicating with the electrolyte flow paths 18 are formed by the electrode supports 5 and 6 (see FIG. 6). [0009] When forming an integral impeller using the wing processing electrode having the above-described configuration, a pair of side rams that are arranged on the Y axis so as to be opposed to each other and that can approach and separate from each other are provided;
Using an electrolytic processing apparatus having a front ram arranged on the X axis and capable of moving toward and away from the Y axis and rotatable about the X axis, an electrode portion 1 for forming a blade back portion is provided on one of the side rams. An electrode portion 3 for forming a blade abdomen is attached to the other of the side rams so that the curved surface 2 for forming the back of the wing and the curved surface 4 for forming the wing abdomen face each other. Further, a metal member 19, which is a material of an integrated impeller, is attached to the front ram. Attach. Next, the electrode portion 1 for forming the blade back portion and the electrode portion 3 for forming the blade abdomen are maintained at a predetermined interval, and the metal member 19 is set to the positive pole and the metal members 1 and 3 are set to the negative pole. 19 and a voltage is applied between the electrode parts 1 and 3 and the liquid supply pipe 1
The electrolytic solution is supplied to the electrodes 3 and 14 and the electrolytic solution is supplied to the outside through the liquid guide holes 11 and 12, the liquid guide grooves 9 and 10, and the electrolyte channel 18 through the opening on the electrode tip A side of the electrolyte channel 18. When the metal member 19 is caused to flow out and brought close to the tips of the electrodes 1 and 3, the surface layer of the metal member 19 is electrolyzed and electrolytic processing is performed.
Further, when the electrodes 1 and 3 are brought close to each other and the metal member 19 is rotated to a predetermined angle around the X axis while the metal member 19 is brought close to the electrodes 1 and 3, a substantially wing-back portion is formed on the metal member 19. A wing portion 20 having a back surface and an abdominal surface that matches the curved surface 2 and the wing abdomen forming curved surface 4 is formed. However, the wing portion to be formed by vibrating the wing back portion forming electrode portion 1 and the wing abdomen portion forming electrode portion 3 by the electrolyte flowing through the electrolyte solution flow path 18. 20 cannot be formed in a predetermined shape, or the liquid guide plates 15, 16 vibrate, so that the liquid guide plates 15, 1 are vibrated.
In some cases, a gap is formed between the electrode 6 and the electrode portions 1 and 3, and a part of the electrolyte leaks from the gap to the outside, so that the integrated impeller cannot be formed efficiently by electrolytic processing. On the other hand, each of the electrode portions 1, 3 and the liquid guide plates 15, 1
In order to prevent the vibration of 6, the thickness of the electrode portions 1 and 3 and the thickness of the liquid guide plates 15 and 16 may be increased to improve the strength. The thickness of the electrode portions 1 and 3 is increased when the size between the wing portions 20 of the integrated wing is small because it is determined by the size between adjacent wing portions 20 of the integrated wing wheel to be formed. I couldn't do that. The present invention has been made in view of the above circumstances, and has as its object to provide an electrode for processing a wing portion of an integrated impeller, which can prevent vibration of each electrode portion. According to the present invention, there is provided an electrode for machining a wing portion of an integrated impeller, wherein the width of the electrode portion having a curved surface on the entire surface thereof having substantially the same shape as the back surface of the wing to be formed is provided. to both edges of the direction, those
An electrode portion for forming a wing back portion provided with a protruding portion extending from the tip end side to the base end side of the wing to be formed over the entire length from the tip end to the base end of the electrode portion, and substantially the same shape as the abdominal surface of the wing to be formed On both edges in the width direction of the electrode portion having the wing abdomen forming curved surface on one surface,
An electrode portion for forming a wing abdomen provided with a protruding portion extending from the distal end side to the proximal end side of the wing to be formed over the entire length from the distal end to the proximal end of the electrode portion, and the wing back portion forming electrode portion; when it was confronted wings abdominal forming electrode portions, projecting portions of both electrode portion proximal side from the distal end side of the blade between the blade back portion forming curved surface with blade abdominoplasty songs surfaces in contact with each other over its entire length Are formed so as to be able to change the facing distance between the two electrode portions. In the electrode for processing a wing portion of the integrated impeller according to the present invention, the strength of the electrode portion for forming the wing back portion and the electrode portion for forming the wing abdominal portion is increased by providing a protruding portion. Even when the electrolyte flows through the curved surface formed by the back surface of the blade, the curved surface of the blade abdomen, and the protruding portion, the two electrode portions do not vibrate. Embodiments of the present invention will be described below with reference to the drawings. FIGS. 1 to 4 show an embodiment of an electrode for processing a wing portion of an integral impeller according to the present invention. Reference numeral 21 denotes a wing-back forming surface 22 having substantially the same shape as the back surface of the wing to be formed. An electrode portion for forming a blade back portion provided with projecting portions 26 and 27 at both ends of an electrode portion 25 on one surface, and an electrode portion 23 having a curved surface 24 for forming a blade abdominal portion having substantially the same shape as the abdominal surface of the blade to be formed. An electrode portion for forming a blade abdomen provided with protruding portions 29 and 30 at the other ends of both ends of 28. When the wing back portion forming electrode portion 21 and the wing abdomen portion forming electrode portion 23 face each other, the wing back portion forming curved surface 22, the wing belly portion forming curved surface 24, and the projecting portions 26, 27 of both the electrode portions 21, 23. , 29 and 30 surrounded by electrolyte channel 31
Are formed, and both electrode portions 21,
The wing back portion forming curved surface 23 and the wing abdominal portion forming curved surface 24 can be moved closer to and away from each other. Further, 32 and 33 are electrode portions 2 for forming the back of the blade.
1. An electrode base formed at the base end of the wing abdomen forming electrode section 23. When forming an integral impeller using the wing processing electrode having the above-described configuration, the electrode base of the wing back forming electrode section 21 is provided on one side ram of the aforementioned electrolytic processing apparatus. 32 is attached to the other side ram with the electrode base 33 of the wing abdomen forming electrode portion 23 such that the wing back forming surface 22 and the wing abdominal forming surface 24 face each other. In this state, the electrolytic solution is supplied to the electrode bases 32 and 33 in the flow path 31 surrounded by the curved surface 22 and the curved surface 24 and the protruding portions 26, 27, 29 and 30.
Assuming that the air flows from the sides toward the tips of the electrode portions 21 and 23, the electrode portions 21 for forming the blade back portion and the electrode portions 23 for forming the blade abdomen are provided with protruding portions 26, 27, 29, and 30 to increase the strength. The height of the two electrode portions 21 and
3 does not vibrate due to the flow of the electrolytic solution. Therefore, the above-mentioned electrode portion 2 for forming the back of the blade
1. If electrolytic processing of the integrated impeller is performed using the wing processing electrode having the wing abdomen forming electrode portion 23, the wing to be formed can be formed in a predetermined shape.
Since no gap is formed due to the vibrations of 1 and 23, leakage of the electrolyte does not occur, and the integrated impeller can be efficiently formed by electrolytic processing. Further, since it is not necessary to increase the thickness of the two electrode portions 21 and 23 to improve the strength, the above-described configuration can be used even when the dimension between the wing portions of the integral wing to be formed is small. Can be used. The electrode for the wing frame of the integrated impeller according to the present invention is not limited to the above-described embodiment.
It goes without saying that various changes can be made without departing from the spirit of the invention . According to the electrode for processing a wing portion of an integrated impeller of the present invention, various excellent effects as described below can be obtained. (1) Since the protruding portions are provided on the wing back portion forming electrode portion and the wing abdomen portion forming electrode portion , the strength is increased, and
Vibration can be avoided in the electrode part due to the flow of the lysate, and the wing part can be formed in a predetermined shape. (2) Due to the projecting portions of both electrode portions that are in contact with each other
This prevents leakage of the electrolyte from the flow path to the outside,
Fill the gap between the metal member of the elephant and the curved surface of both electrodes.
Can be supplied to the electrolytic solution of the minute flow rate, it can be efficiently formed by electrochemical machining integral impeller, pressurized to
In addition, the two curved surfaces that can change the interval are
By forming a flow path extending to the end side, both the metal member and the
The distance between the surfaces is reduced, and the transfer accuracy of both formed curved surfaces is improved,
A highly accurate blade leading edge shape and trailing edge shape can be obtained. (3) Since it is not necessary to increase the thickness of the two electrode portions to improve the strength, it is possible to cope with the case where the dimension between the wing portions of the integral wing to be formed is small.
【図面の簡単な説明】
【図１】本発明の一体型翼車の翼部加工用電極の一実施
例において、翼背部形成用電極部と翼腹部形成用電極部
を嵌合させた状態を電極先端部側から見た斜視図であ
る。
【図２】本発明の一体型翼車の翼部加工用電極の一実施
例において、翼背部形成用電極部と翼腹部形成用電極部
を嵌合させた状態を電極基端部側から見た斜視図であ
る。
【図３】本発明の一体型翼車の翼部加工用電極の一実施
例において、翼背部形成用電極部と翼腹部形成用電極部
を電極先端部側から見た斜視図である。
【図４】本発明の一体型翼車の翼部加工用電極の一実施
例において、翼背部形成用電極部と翼腹部形成用電極部
を電極基端部側から見た斜視図である。
【図５】従来の一体型翼車の翼部加工用電極の一例の斜
視図である。
【図６】従来の一体型翼車の翼部加工用電極の一例の斜
視図である。
【符号の説明】
２１ 翼背部形成用電極部
２２ 翼背部形成曲面
２３ 翼腹部形成用電極部
２４ 翼腹部形成曲面
２５，２８ 電極部端面
２６，２７，２９，３０ 突設部
３１ 電解液流路（流路）BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a view showing an embodiment of an electrode for forming a wing portion of an integrated impeller according to the present invention, in which a wing back portion forming electrode portion and a wing abdomen portion forming electrode portion are fitted to each other. It is the perspective view seen from the electrode tip side. FIG. 2 is a view showing a state in which an electrode portion for forming a wing back portion and an electrode portion for forming a wing abdomen portion are fitted from an electrode base end side in an embodiment of an electrode for processing a wing portion of an integrated impeller according to the present invention. FIG. FIG. 3 is a perspective view of an electrode portion for forming a wing back portion and an electrode portion for forming a wing abdomen viewed from the electrode tip side in one embodiment of the wing portion processing electrode of the integrated type impeller of the present invention. FIG. 4 is a perspective view of an electrode portion for forming a wing back portion and an electrode portion for forming a wing abdomen portion viewed from the electrode base end side in the embodiment of the wing portion processing electrode of the integrated impeller according to the present invention. FIG. 5 is a perspective view of an example of a wing portion processing electrode of a conventional integrated impeller. FIG. 6 is a perspective view of an example of a wing processing electrode of a conventional integrated impeller. DESCRIPTION OF SYMBOLS 21 Blade Back Forming Electrode 22 Blade Back Forming Curved Surface 23 Blade Ventral Forming Electrode 24 Blade Wing Forming Surface 25, 28 Electrode End Surfaces 26, 27, 29, 30 Protrusion 31 Electrolyte Flow Path (Flow path)
───────────────────────────────────────────────────── フロントページの続き (58)調査した分野(Int.Cl.7，ＤＢ名) B23H 9/10 B23H 3/04 ──────────────────────────────────────────────────続 き Continued on front page (58) Field surveyed (Int.Cl. 7 , DB name) B23H 9/10 B23H 3/04
Claims (1)
形成曲面を一面に有する電極部の巾方向の両縁に、当該
電極部の先端から基端までの全長にわたって、形成すべ
き翼の先端側から基端側へ延びる突設部を設けた翼背部
形成用電極部と、形成すべき翼の腹面と略同形状の翼腹
部形成曲面を一面に有する電極部の巾方向の両縁に、当
該電極部の先端から基端までの全長にわたって、形成す
べき翼の先端側から基端側へ延びる突設部を設けた翼腹
部形成用電極部とを備え、前記翼背部形成用電極部と翼
腹部形成用電極部を対峙させた際に、両電極部の突設部
がその全長にわたり相互に接して翼背部形成曲面と翼腹
部形成曲面の間に前記翼の先端側から基端側へ延びる流
路が形成され且つ両電極部の対峙間隔を変化せしめ得る
ように構成したことを特徴とする一体型翼車の翼部加工
用電極。(57) to the Claims 1 Both edges of the width direction of the electrode portion having the rear and one side of the blade back portion forming a curved surface of substantially the same shape of the blade to be formed, the
Over the entire length from the tip end to the base end of the electrode portion, a wing back portion forming electrode portion provided with a protruding portion extending from the tip end side to the base end side of the wing to be formed, and has substantially the same shape as the abdominal surface of the wing to be formed. both edges of the width direction of the electrode portion having on one surface a blade abdominoplasty curved, those
A wing abdomen forming electrode portion provided with a protruding portion extending from the tip side to the base end of the wing to be formed over the entire length from the tip end to the base end of the electrode portion; when it was confronted wings abdominal forming electrode portions, projecting portions of both electrode portion proximal side from the distal end side of the blade between the blade back portion forming curved surface with blade abdominoplasty songs surfaces in contact with each other over its entire length Characterized in that a flow path extending to the wing portion is formed and the facing distance between the two electrode portions can be changed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11498393A JP3362446B2 (en) | 1993-05-17 | 1993-05-17 | Electrode for wing processing of integrated impeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11498393A JP3362446B2 (en) | 1993-05-17 | 1993-05-17 | Electrode for wing processing of integrated impeller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH06320346A JPH06320346A (en) | 1994-11-22 |
| JP3362446B2 true JP3362446B2 (en) | 2003-01-07 |
Family
ID=14651452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11498393A Expired - Lifetime JP3362446B2 (en) | 1993-05-17 | 1993-05-17 | Electrode for wing processing of integrated impeller |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3362446B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103752965A (en) * | 2014-01-13 | 2014-04-30 | 南京航空航天大学 | Electrochemical machining tool and electrochemical machining method with linear feeding and rotary feeding combination for blisk |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0304321D0 (en) | 2003-02-26 | 2003-04-02 | Bladon Jets Ltd | Fans and turbines |
| GB0420022D0 (en) | 2004-09-09 | 2004-10-13 | Bladon Jets Ltd | Fans and turbines |
| CN112191962B (en) * | 2020-09-29 | 2022-07-08 | 中国航发动力股份有限公司 | Electrolytic machining process method of open type blisk |
| GB2601550A (en) * | 2020-12-04 | 2022-06-08 | Texture Jet Ltd | A nozzle |
-
1993
- 1993-05-17 JP JP11498393A patent/JP3362446B2/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103752965A (en) * | 2014-01-13 | 2014-04-30 | 南京航空航天大学 | Electrochemical machining tool and electrochemical machining method with linear feeding and rotary feeding combination for blisk |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH06320346A (en) | 1994-11-22 |
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