JP6611384B1 - Mounting member for rotor blade - Google Patents

Mounting member for rotor blade Download PDF

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JP6611384B1
JP6611384B1 JP2018118796A JP2018118796A JP6611384B1 JP 6611384 B1 JP6611384 B1 JP 6611384B1 JP 2018118796 A JP2018118796 A JP 2018118796A JP 2018118796 A JP2018118796 A JP 2018118796A JP 6611384 B1 JP6611384 B1 JP 6611384B1
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contact
pressure surface
pair
blade
dovetail
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JP2019217613A (en
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烈 淺沼
烈 淺沼
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株式会社エム・アンド・ジェイ
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Abstract

【課題】ジェットエンジン等の軸流式圧縮機の回転翼又はジェットエンジンのタービン若しくは舶用タービンの回転翼を加工機や計測器に取付け部材を介して装着して加工や計測を行う際に、安価、簡易であって、回転翼を高精度かつ安定にクランプすることができる回転翼の取付け部材を提供する。【解決手段】回転翼1の根元部2の一対の圧力面4a、4bの一方の圧力面4aに当接可能な一対の対向面22a、22bと、他方の圧力面4bに当接可能な1つ又は一対の対向面22a、22bと、を備える。【選択図】図3An object of the present invention is to inexpensively perform machining and measurement by mounting a rotor blade of an axial-flow compressor such as a jet engine or a rotor blade of a jet engine or a marine turbine to a processing machine or a measuring instrument via an attachment member. The present invention provides a mounting member for a rotating blade that is simple and can clamp the rotating blade with high accuracy and stability. A pair of pressure surfaces 4a and 4b of a root portion 2 of a rotary blade 1 is contactable with one pressure surface 4a and a pair of opposing surfaces 22a and 22b and 1 is contactable with the other pressure surface 4b. One or a pair of opposing surfaces 22a, 22b. [Selection] Figure 3

Description

本発明は、ジェットエンジン等の軸流式圧縮機の回転翼又はジェットエンジンのタービンや舶用タービンの回転翼の加工や計測(新規製造時に限らず、補修や修理時も含む。)を行う際に使用される、回転翼の取付け部材(クランプホルダーないし取付け冶具)に関する。 The present invention is used when processing and measuring rotor blades of an axial-flow compressor such as a jet engine or rotor blades of a jet engine turbine or a marine turbine (not only during new manufacturing but also during repair and repair). The present invention relates to a rotary blade mounting member (clamp holder or mounting jig) used.

ジェットエンジン等の軸流式圧縮機の回転翼又はジェットエンジンのタービンや舶用タービンの回転翼の翼面の加工や計測は、回転翼の根元に形成されたダブテール部2(図1参照)やクリスマスツリーがホルダーと呼ばれる取付け部材にクランプされて加工装置や計測装置に装着されて行われている。 Machining and measurement of rotor blades of axial flow compressors such as jet engines or rotor blades of jet engine turbines and marine turbines, dovetail part 2 (see Fig. 1) formed at the root of rotor blades and Christmas The tree is clamped to an attachment member called a holder and attached to a processing apparatus or a measuring apparatus.

ここで、従来のホルダーの構造概念およびホルダーによるダブテール部2のクランプ概念を図2に基づいて説明する。 Here, the structure concept of the conventional holder and the clamp concept of the dovetail part 2 by the holder will be described with reference to FIG.

ダブテール部2は、左右一対の張り出し部9a、9bを有しており、張り出し部9a、9bのそれぞれ上面には、圧力面4a、4bが形成されている(図1参照)。ホルダー11は、正面側及び背面側(正面側及び背面側は、それぞれ正面図(図2(a))の紙面手前(表面)側及び紙面向こう(裏面)側をいい、以下同様とする。)が開放され、圧力面4a、4bにそれぞれ覆いかぶさるようにホルダー11の両側部から中央部に向かって庇状に張り出した一対の当接部15a、15bが配設され、ダブテール部2がホルダー11の正面側又は背面側からホルダー11内に挿入できる構造となっている。当接部15a、15bの底面には、それぞれ、ダブテール部2の圧力面4a、4bにそれぞれ対向する平面状の対向面12a、12bが形成されている。ダブテール部2は、ホルダー11の正面側又は背面側からホルダー11内に挿入された後、ネジ機構や空圧・油圧シリンダー等の直動機構(図示省略)により押付け部16の上面をダブテール部2の底面に当接しかつダブテール部2を上方へ押し上げて圧力面4a、4bをそれぞれ対向面12a、12bに嵌合させることによりホルダー11に把持(クランプ)される。 The dovetail portion 2 has a pair of left and right protruding portions 9a and 9b, and pressure surfaces 4a and 4b are formed on the upper surfaces of the protruding portions 9a and 9b, respectively (see FIG. 1). The holder 11 is a front side and a back side (the front side and the back side refer to the front side (front surface) side and the other side (back side) side of the front surface of the front view (FIG. 2A), respectively, and so on). Is opened, and a pair of contact portions 15a, 15b projecting from both side portions of the holder 11 toward the center portion so as to cover the pressure surfaces 4a, 4b are disposed, and the dovetail portion 2 is provided with the holder 11 It can be inserted into the holder 11 from the front side or the back side. On the bottom surfaces of the contact portions 15a and 15b, planar opposing surfaces 12a and 12b are formed which respectively oppose the pressure surfaces 4a and 4b of the dovetail portion 2. After the dovetail part 2 is inserted into the holder 11 from the front side or the back side of the holder 11, the dovetail part 2 is placed on the upper surface of the pressing part 16 by a linear mechanism (not shown) such as a screw mechanism or a pneumatic / hydraulic cylinder. And the dovetail part 2 is pushed upward and the pressure surfaces 4a and 4b are fitted to the opposing surfaces 12a and 12b, respectively, so that the holder 11 holds (clamps).

そして、回転翼の翼部3等の加工や計測においては、ホルダーに回転翼の基準となる積重点が設定されており、ホルダー11に設定された基準(ホルダー上の基準)が回転翼1自身に内包する基準(ブレード内基準)を代用して行われている。 In the processing and measurement of the blade portion 3 etc. of the rotor blade, the product weight as a reference of the rotor blade is set in the holder, and the reference (reference on the holder) set in the holder 11 is the rotor blade 1 itself. This is done by substituting the standard included in the blade (blade internal standard).

しかし、ブレード内基準の代わりに、ホルダー上の基準を使用して回転翼の翼部3等の加工や計測を行うと、ダブテール部2をホルダー11でクランプする際の取り付けの不安定や誤差等により、回転翼1の翼部3等の加工や計測結果に誤差を生じて安定しないという問題があった。   However, if processing and measurement of the blade portion 3 of the rotor blade is performed using the reference on the holder instead of the reference in the blade, instability or error in mounting when the dovetail portion 2 is clamped by the holder 11 As a result, there is a problem that an error occurs in the processing or measurement result of the blade portion 3 of the rotary blade 1 and the result is not stable.

また、従来、ホルダー11の対向面12は平面状に形成されていたのに対して、最近、特に、ダブテール2の圧力面4が、回転翼1の回転ディスクへの取り付け構造の変更により、図1(b)に示されるように湾曲した三次元曲面となってきた。このため、ホルダー11の平面状に形成された対向面12a、12bとダブテール2の三次元曲面状に形成された圧力面4a、4bとをそれぞれ嵌合させると、水平断面において(図2(b)における紙面上下方向を鉛直方向とし、鉛直方向に直交する面を水平面とする。以下同様。)、対向面12aと圧力面4a、対向面12bと圧力面4bとの接触部はそれぞれ、図2(c)に示されるように、当接点P1、P2の1点ずつとなる。このため、圧力面4a、4bないし対向面12a、12b全体として、基準となる圧力面上4と対向面12とは、各側部において、面的に接触することができず、それぞれ1本の直線のみにより接触することとなるため、クランプが不安定となる。これにより、高い繰り返し精度を確保して、回転翼1のダブテール部2をホルダー11で安定にクランプすることが困難となってきた。この結果、同一の回転翼製品をホルダー11でクランプしてホルダー上の基準に基づいて加工や計測を行っても、クランプの不安定によるばらつき等が生じ加工寸法のばらつきや計測の精度の安定的繰り返し保障が困難であるという問題も生じるようになった。   Conventionally, the opposed surface 12 of the holder 11 has been formed in a flat shape, but recently, in particular, the pressure surface 4 of the dovetail 2 has been changed due to a change in the mounting structure of the rotating blade 1 to the rotating disk. As shown in 1 (b), it has become a curved three-dimensional curved surface. For this reason, when the opposing surfaces 12a and 12b formed in the planar shape of the holder 11 and the pressure surfaces 4a and 4b formed in the three-dimensional curved shape of the dovetail 2 are respectively fitted, in a horizontal section (FIG. 2 (b 2), the vertical direction is the vertical direction of the paper surface, and the horizontal plane is the surface perpendicular to the vertical direction. The same applies hereinafter.) The contact portions of the opposing surface 12a and the pressure surface 4a, and the opposing surface 12b and the pressure surface 4b are shown in FIG. As shown in (c), there are one contact point P1 and one point P2. For this reason, as the pressure surfaces 4a, 4b or the opposing surfaces 12a, 12b as a whole, the reference pressure surface 4 and the opposing surface 12 cannot be in surface contact with each other, and each of the pressure surfaces 4a, 12b, 12b, 12b Since the contact is made only by a straight line, the clamp becomes unstable. As a result, it has been difficult to stably clamp the dovetail portion 2 of the rotor blade 1 with the holder 11 while ensuring high repeatability. As a result, even if the same rotor blade product is clamped by the holder 11 and processing and measurement are performed based on the standard on the holder, variations due to instability of the clamp occur, and variations in processing dimensions and measurement accuracy are stable. There is also a problem that it is difficult to guarantee repeatedly.

本発明は、前記従来技術の問題点を解決するためになされたものであって、ジェットエンジン等の軸流式圧縮機の回転翼又はジェットエンジンのタービン若しくは舶用タービンの回転翼を加工機や計測器に取付け部材を介して装着して翼部等の加工や計測を行う際に、安価、簡易であって、回転翼を高精度かつ安定にクランプすることができる回転翼の取付け部材を提供することを目的とする。   The present invention has been made in order to solve the above-described problems of the prior art, and is intended to process the rotor blades of an axial flow compressor such as a jet engine or the rotor blades of a jet engine turbine or a marine turbine. Provided is a rotary blade mounting member that is inexpensive and simple and can clamp a rotary blade with high accuracy and stability when mounting and mounting a blade on a device via a mounting member. For the purpose.

前記課題を解決するために、本発明の第1の態様は、加工機又は計測機を使用して軸流式圧縮機の回転翼又はジェットエンジンのタービン若しくは舶用タービンの回転翼を加工又は計測する際に、前記回転翼を前記加工機又は前記計測器に装着されるために使用される、回転翼の取付け部材であって、前記回転翼の根元部の一対の圧力面の一方の圧力面に当接可能な一対の対向面と、他方の圧力面に当接可能な1つ又は一対の対向面と、を備えることを特徴とする。   In order to solve the above-described problems, a first aspect of the present invention processes or measures a rotor blade of an axial-flow compressor, a turbine of a jet engine, or a rotor blade of a marine turbine using a processing machine or a measuring machine. A rotary blade attachment member used to mount the rotary blade on the processing machine or the measuring instrument, and is attached to one pressure surface of a pair of pressure surfaces of a root portion of the rotary blade. It is characterized by comprising a pair of opposing surfaces that can contact and one or a pair of opposing surfaces that can contact the other pressure surface.

本発明の第2の態様は、第1の態様において、前記一対の圧力面が三次元曲面であることを特徴とする。   According to a second aspect of the present invention, in the first aspect, the pair of pressure surfaces are three-dimensional curved surfaces.

本発明によれば、加工機や計測器に取付け部材を介してジェットエンジン等の軸流式圧縮機の回転翼又はジェットエンジンのタービン若しくは舶用タービンの回転翼を装着して翼部等の加工や計測を行う場合において、安価、簡易であって、回転翼を高精度かつ安定にクランプすることができる回転翼の取付け部材を提供することができる。 According to the present invention, a rotating blade of an axial flow compressor such as a jet engine or a rotating blade of a jet engine turbine or a marine turbine is attached to a processing machine or a measuring instrument via an attachment member to process the blade portion or the like. When performing measurement, it is possible to provide an attachment member for a rotating blade that is inexpensive and simple and can clamp the rotating blade with high accuracy and stability.

ダブテール部の構造概念の一例を示す図であり、(a)が正面図、(b)が右側面図である。It is a figure which shows an example of the structural concept of a dovetail part, (a) is a front view, (b) is a right view. ダブテール部をクランプする従来のホルダーの概念を示す図であり、(a)が正面図、(b)が右側面図、(c)が(a)の断面E―Eの矢視図である。It is a figure which shows the concept of the conventional holder which clamps a dovetail part, (a) is a front view, (b) is a right view, (c) is an arrow directional view of the cross section EE of (a). 本発明に係る回転翼の取付け部材の第一の実施形態を示す図であり、(a)が左側面図、(b)が正面図、(c)が右側面図、(d)が(b)の断面A―A1―A2―Aの矢視図、(e)が(b)の断面F―Fの矢視図である。It is a figure which shows 1st embodiment of the attachment member of the rotary blade which concerns on this invention, (a) is a left view, (b) is a front view, (c) is a right view, (d) is (b) ) Is an arrow view of a section A-A1-A2-A, and (e) is an arrow view of a section FF of (b). 本発明に係る回転翼の取付け部材の第二の実施形態を示す図であり、(a)が左側面図、(b)が正面図、(c)が右側面図、(d)が(b)の断面B―B1―B2―Bの矢視図、(e)が(b)の断面G―Gの矢視図である。It is a figure which shows 2nd embodiment of the attachment member of the rotary blade which concerns on this invention, (a) is a left view, (b) is a front view, (c) is a right view, (d) is (b) ) Is an arrow view of a section B-B1-B2-B, and (e) is an arrow view of a section GG of (b). 本発明に係る回転翼の取付け部材の第三の実施形態を示す図であり、(a)が左側面図、(b)が正面図、(c)が右側面図、(d)が(b)の矢視C―C1―C2―Cの矢視図、(e)が(b)の断面H―Hの矢視図である。It is a figure which shows 3rd embodiment of the attachment member of the rotary blade which concerns on this invention, (a) is a left view, (b) is a front view, (c) is a right view, (d) is (b) (B) is an arrow view of the section C-C1-C2-C, and (e) is an arrow view of the section HH of (b). 本発明に係る回転翼の取付け部材の第四の実施形態を示す図であり、(a)が左側面図、(b)が正面図、(c)が右側面図、(d)が(b)の矢視D―D1―D2―Dの矢視図、(e)が(b)の断面K―Kの矢視図である。It is a figure which shows 4th embodiment of the attachment member of the rotary blade which concerns on this invention, (a) is a left view, (b) is a front view, (c) is a right view, (d) is (b) ) Is an arrow view of the arrow D-D1-D2-D, and (e) is an arrow view of the section KK of (b). 本発明に係る取付け部材を使用してダブテール部が把持された回転翼を三次元加工機に装着したときの概念を示す斜視図である。It is a perspective view which shows the concept when the rotary blade by which the dovetail part was hold | gripped using the attachment member which concerns on this invention was mounted | worn with the three-dimensional processing machine.

以下、本発明に係る取付け部材の実施形態について、図面を参照しつつ説明する。   Embodiments of an attachment member according to the present invention will be described below with reference to the drawings.

図3は、本発明に係る回転翼の取付け部材の第一の実施形態を示す図であり、回転翼1のダブテール部2が取付け部材21により把持された状態を示す図である。   FIG. 3 is a view showing a first embodiment of the attachment member for the rotor blade according to the present invention, and is a view showing a state in which the dovetail portion 2 of the rotor blade 1 is gripped by the attachment member 21.

取付け部材21には、回転翼1のダブテール部2の左右一対の圧力面4a、4bの左側の圧力面4aに庇状に覆いかぶさる前後一対の当接部24a、24bが配設され、一対の当接部24a、24の底面には、それぞれ、左側の圧力面4aに対して平行に対向する平面状の対向面22a、22bが形成されている(左側、右側は、それぞれ図3(b)における紙面の左側、右側を、また、前、後は、それぞれ図3(b)における紙面の手前側、奥側を指し、以下同様とする)。ここで、平行、平面には、それぞれ、製作上の許容誤差範囲内や設計上の許容範囲内(例えば、同様な作用効果が得られる範囲内)の平行、平面を含み、圧力面4aが湾曲した三次元曲面である場合の平行とは、圧力面4aの中央部の接平面に平行をいい、対向面は、平面部のみでなく面取りやフィレット等の端部加工処理がされた端部も含む(以下同様)。また、取付け部材21には、同様に、左右一対の圧力面4a、4bの右側の圧力面4bに庇状に覆いかぶさる前後一対の当接部25a、25bが配設され、一対の当接部25a、25の底面には、それぞれ、右側の圧力面4bに対して平行に対向する平面状の対向面23a、23bが形成されている。当接部24a、24b、25a及び25bは、それぞれ取付け部材21の下部の基台部から上方に向かって伸びている支持部26a、26b、27a及び27bに連結されている。   The attachment member 21 is provided with a pair of front and rear contact portions 24a and 24b that cover the pressure surface 4a on the left side of the pair of left and right pressure surfaces 4a and 4b of the dovetail portion 2 of the rotor blade 1 in a bowl shape. On the bottom surfaces of the contact portions 24a and 24, planar facing surfaces 22a and 22b are formed in parallel with the left pressure surface 4a, respectively (the left side and the right side are shown in FIG. 3B). The left side and the right side of the paper surface in FIG. 3 and the front and the back indicate the front side and the back side of the paper surface in FIG. Here, the parallel surface and the flat surface include parallel and flat surfaces within a manufacturing tolerance range and a design allowable range (for example, within a range in which similar effects can be obtained), and the pressure surface 4a is curved. Parallel in the case of a three-dimensional curved surface means parallel to the tangent plane of the central portion of the pressure surface 4a, and the opposing surface is not only a plane portion but also an end portion subjected to end processing such as chamfering or fillet. Included (the same applies hereinafter). Similarly, the attachment member 21 is provided with a pair of front and rear contact portions 25a and 25b that cover the pressure surface 4b on the right side of the pair of left and right pressure surfaces 4a and 4b in a bowl shape. On the bottom surfaces of 25a and 25, planar facing surfaces 23a and 23b are formed in parallel to the right pressure surface 4b, respectively. The contact portions 24a, 24b, 25a, and 25b are connected to support portions 26a, 26b, 27a, and 27b extending upward from the base portion at the bottom of the attachment member 21, respectively.

また、圧力面4aにそれぞれ対向する対向面22a、22bは、同一平面内に形成されており、これにより当接部24a、24bを湾曲した三次元曲面の圧力面4aに当接させると、対向面22a、22bは、圧力面4aの中央部側の端部である当接線L1、L2において圧力面4aと直線状に接触する(図3(d)参照)。ここで、同一平面には、製作上の許容誤差範囲内や設計上の許容範囲内(例えば、同様な作用効果が得られる範囲内)の同一平面をいう(以下、同様)。また、当接部25a、25bも、当接部24a、24bと基本的に同様な構造をしており、当接部25a、25bを湾曲した三次元曲面の圧力面4bに当接させると、対向面23a、23bは、圧力面4bの中央部側の端部である当接線L3、L4において圧力面4bと直線状に接触する(図示省略)。   Further, the opposing surfaces 22a and 22b that oppose the pressure surface 4a are formed in the same plane, so that when the abutting portions 24a and 24b are brought into contact with the curved three-dimensional curved pressure surface 4a, the opposing surfaces 22a and 22b are opposed to each other. The surfaces 22a and 22b are in linear contact with the pressure surface 4a at contact lines L1 and L2, which are ends on the central side of the pressure surface 4a (see FIG. 3D). Here, the same plane refers to the same plane within a manufacturing allowable error range or a design allowable range (for example, within a range in which a similar effect can be obtained) (hereinafter the same). Also, the contact portions 25a and 25b have basically the same structure as the contact portions 24a and 24b, and when the contact portions 25a and 25b are brought into contact with the curved pressure surface 4b having a curved shape, The opposing surfaces 23a and 23b are in linear contact with the pressure surface 4b at contact lines L3 and L4 that are ends on the center side of the pressure surface 4b (not shown).

取付け部材21は、さらに、その下部に、ネジ機構17によりダブテール部2の底面に対して前後進(昇降)して当接することができる押付け部16を備えている。なお、ネジ機構17に代えて空圧シリンダーや油圧シリンダー等を使用した他の方式の直動機構であってもよい(以下、他の実施形態を含めて同様)。押付け部16の先端がダブテール部2の底面から適当な距離離れた状態で、正面側(図3(b)における紙面手前側)又は背面側(図3(b)における紙面向こう側)から、ダブテール部2を取付け部材21の内部空間、すなわち対向面22a、22b、23a、23b及び押付け部16の上面に囲まれた空間に挿入する。ダブテール部2を取付け部材21内に挿入後、ネジ機構27により押付け部16をダブテール部2の底面に押し付けて、当接部24a、24b、25a、25b及び押付け部16とによりダブテール部2を挟み込むことにより、ダブテール部2を取付け部材21により把持(クランプ)する。   The attachment member 21 further includes a pressing portion 16 that can be brought into contact with the bottom surface of the dovetail portion 2 by moving back and forth (up and down) by the screw mechanism 17 at a lower portion thereof. Note that another type of linear motion mechanism using a pneumatic cylinder, a hydraulic cylinder, or the like instead of the screw mechanism 17 may be used (hereinafter the same including other embodiments). Dovetail from the front side (the front side of the paper in FIG. 3B) or the back side (the other side of the paper in FIG. 3B) with the front end of the pressing portion 16 separated from the bottom surface of the dovetail portion 2 by an appropriate distance. The portion 2 is inserted into the internal space of the attachment member 21, that is, the space surrounded by the opposing surfaces 22 a, 22 b, 23 a, 23 b and the upper surface of the pressing portion 16. After the dovetail portion 2 is inserted into the mounting member 21, the pressing portion 16 is pressed against the bottom surface of the dovetail portion 2 by the screw mechanism 27, and the dovetail portion 2 is sandwiched between the contact portions 24 a, 24 b, 25 a, 25 b and the pressing portion 16. As a result, the dovetail portion 2 is gripped (clamped) by the mounting member 21.

なお、把持の手順は、圧力面4に当接部24a、24b、25a、25bの全部又は一部に当接させてから押付け部16を押し込んで挟み込んでも、又は圧力面4が当接部24a、24b、25a、25bの全部と離れた状態から押付け部16を押し込んで挟み込んでもよい。   Note that the gripping procedure may be that the pressure surface 4 is brought into contact with all or a part of the contact portions 24a, 24b, 25a, 25b and then the pressing portion 16 is pushed in, or the pressure surface 4 is brought into contact with the contact portion 24a. , 24b, 25a, 25b, and the pressing portion 16 may be pushed in from a state apart from all of them.

以上の構成により、ダブテール部2が取付け部材21により把持され、平面状に形成された対向面12a、12bとダブテール2の三次元曲面状に形成された圧力面4a、4bとをそれぞれ嵌合させると、図3(e)に示されるように、水平断面において、圧力面4aは対向面22a及び対向面22bとそれぞれ当接点P3及びP4において接触し、圧力面4bは対向面23a及び対向面23bとそれぞれP5及びP6において接触することができるため、取付け部材21によりダブテール部2を安定かつ確実に把持できる。   With the above configuration, the dovetail portion 2 is gripped by the attachment member 21, and the opposing surfaces 12a and 12b formed in a planar shape and the pressure surfaces 4a and 4b formed in the three-dimensional curved surface shape of the dovetail 2 are respectively fitted. 3 (e), in the horizontal cross section, the pressure surface 4a contacts the opposing surface 22a and the opposing surface 22b at the contact points P3 and P4, respectively, and the pressure surface 4b includes the opposing surface 23a and the opposing surface 23b. And P5 and P6, respectively, so that the dovetail portion 2 can be gripped stably and reliably by the mounting member 21.

また、上記においては、圧力面4a、4bが湾曲している三次元曲面であるダブテール部2を取付け部材21の把持対象物として説明したが、取付け部材21の把持対象物が平面状の圧力面2を有するダブテール部2であってもよい。例えば圧力面4aに対向する対向面22a、22bが圧力面4aと接触する面積が従来のホルダーに比べて減少し面圧が増すため、ダブテール部2を把持する精度が向上するからである。以下において説明する他の実施形態においても同様である。   In the above description, the dovetail portion 2 that is a three-dimensional curved surface with the pressure surfaces 4a and 4b curved is described as a gripping object of the mounting member 21, but the gripping object of the mounting member 21 is a flat pressure surface. The dovetail part 2 which has 2 may be sufficient. For example, the area where the opposing surfaces 22a and 22b facing the pressure surface 4a are in contact with the pressure surface 4a is reduced as compared with the conventional holder and the surface pressure is increased, so that the accuracy of gripping the dovetail portion 2 is improved. The same applies to other embodiments described below.

以上のとおり、取付け部材21は、ダブテール部2を再現性高く安定かつ確実に把持できる。これにより、ブレード内基準をホルダー上の基準に代用して回転翼1の翼部3等の加工や計測を高精度に行うことができる。   As described above, the attachment member 21 can grip the dovetail portion 2 stably and reliably with high reproducibility. Thereby, it is possible to process and measure the blade portion 3 of the rotor blade 1 with high accuracy by using the reference in the blade instead of the reference on the holder.

図4は、本発明に係る取付け部材の第二の実施形態を示す図であり、回転翼1のダブテール部2が取付け部材31により把持された状態を示す図である。なお、以下において、説明を省略した事項については、矛盾等がない限り、第一の実施形態と同様である。   FIG. 4 is a view showing a second embodiment of the attachment member according to the present invention, and is a view showing a state in which the dovetail portion 2 of the rotary blade 1 is gripped by the attachment member 31. In the following description, items that are not described are the same as those in the first embodiment unless there is a contradiction or the like.

取付け部材31には、回転翼1のダブテール部2の左右一対の圧力面4a、4bの左側の圧力面4aに庇状に覆いかぶさる前後一対の当接部34a、34bが配設され、一対の当接部34a、34bの底面には、それぞれ、左側の圧力面4aに対して平行に対向する平面状の対向面32a、32bが形成されている。また、取付け部材31には、左右一対の圧力面4a、4bの右側の圧力面4bに庇状に覆いかぶさる当接部35が配設され、当接部35の底面には、右側の圧力面4bに対して平行に対向する平面状の対向面33が形成されている。当接部34a、34b及び35は、それぞれ取付け部材21の下部の基台部から上方に向かって伸びている支持部36a、36b、37に連結されている。   The attachment member 31 is provided with a pair of front and rear contact portions 34a and 34b that cover the pressure surface 4a on the left side of the pair of left and right pressure surfaces 4a and 4b of the dovetail portion 2 of the rotor blade 1 in a bowl shape. On the bottom surfaces of the abutting portions 34a and 34b, planar opposing surfaces 32a and 32b that are opposed in parallel to the left pressure surface 4a are formed, respectively. Further, the mounting member 31 is provided with a contact portion 35 that covers the right pressure surface 4b of the pair of left and right pressure surfaces 4a and 4b in a bowl shape, and the bottom surface of the contact portion 35 has a right pressure surface. A flat opposed surface 33 is formed in parallel to 4b. The contact portions 34a, 34b, and 35 are connected to support portions 36a, 36b, and 37 that extend upward from the base portion at the bottom of the attachment member 21, respectively.

本実施形態における当接部34a、34bは、第一の実施形態における当接部24a、24bと同様であり、湾曲した三次元曲面の圧力面4aに当接させると、対向面32a、32bは、それらの中央部側の端部である当接線L5、L6において圧力面4aと直線状に接触する(図示省略)。一方、本実施形態における当接部35は、圧力面4aに対向する対向面33の表面が平面であるため、当接部35を湾曲した三次元曲面の圧力面4bに当接させると、対向面33のほぼ中央である当接線L7において圧力面4bと直線状に接触する(図3(d)参照)。   The contact portions 34a and 34b in the present embodiment are the same as the contact portions 24a and 24b in the first embodiment. When the contact portions 34a and 34b are in contact with the curved pressure surface 4a, the opposing surfaces 32a and 32b are The contact surfaces L5 and L6, which are the end portions on the center side, come into linear contact with the pressure surface 4a (not shown). On the other hand, since the surface of the opposing surface 33 that opposes the pressure surface 4a is a flat surface, the contact portion 35 in the present embodiment is opposed when the contact portion 35 is brought into contact with the curved pressure surface 4b having a curved surface. It contacts the pressure surface 4b in a straight line at the contact line L7 which is substantially the center of the surface 33 (see FIG. 3D).

本実施形態における取付け部材31は、実施形態1と同様に、さらに、その下部に、ダブテール部2の底面に対して前後進して当接することができる押付け部16を備えている。押付け部16は、取付け部材31下部に設けられたネジ機構17により先端(上端)をダブテール部2の底面に対して前後進可能となっており、押付け部16の先端がダブテール部2の底面から適当な距離離れた状態で、正面側(図4(b)における紙面手前側)又は背面側(図3(b)における紙面向こう側)から、ダブテール部2を取付け部材31内、すなわち当接部34a、34b、当接部35及び押付け部16に囲まれた空間に挿入する。ダブテール部2を取付け部材31内に挿入後、ネジ機構17により押付け部16をダブテール部2底面に当接し押し付けて、当接部34a、34b、35及び押付け部16とによりダブテール部2を挟み込むことにより、ダブテール部2を取付け部材31により把持(クランプ)する。   As in the first embodiment, the attachment member 31 in the present embodiment further includes a pressing portion 16 that can be moved forward and backward with respect to the bottom surface of the dovetail portion 2 at the lower portion thereof. The pressing portion 16 can be moved forward and backward with respect to the bottom surface of the dovetail portion 2 by a screw mechanism 17 provided at the lower portion of the attachment member 31, and the distal end of the pressing portion 16 is extended from the bottom surface of the dovetail portion 2. The dovetail portion 2 is placed in the attachment member 31 from the front side (the front side of the paper surface in FIG. 4B) or the back side (the other side of the paper surface in FIG. 3B) with an appropriate distance away, that is, the contact portion. It is inserted into a space surrounded by 34 a, 34 b, the contact portion 35 and the pressing portion 16. After the dovetail portion 2 is inserted into the mounting member 31, the pressing portion 16 is abutted against and pressed against the bottom surface of the dovetail portion 2 by the screw mechanism 17, and the dovetail portion 2 is sandwiched between the abutting portions 34 a, 34 b and 35 and the pressing portion 16. Thus, the dovetail portion 2 is gripped (clamped) by the attachment member 31.

以上の構成により、ダブテール部2が取付け部材31により把持され、平面状に形成された対向面32a、32bとダブテール2の三次元曲面状に形成された圧力面4a、4bとをそれぞれ嵌合させると、図4(e)に示されるように、水平断面において、圧力面4aは対向面32a及び対向面32bとそれぞれ当接点P7及びP8で接触し、圧力面4bは対向面33と当接点P9で当接することができるため、取付け部材31によりダブテール部2を安定かつ確実に把持できる。   With the above configuration, the dovetail portion 2 is gripped by the attachment member 31, and the opposing surfaces 32a and 32b formed in a flat shape and the pressure surfaces 4a and 4b formed in the three-dimensional curved surface shape of the dovetail 2 are fitted to each other. As shown in FIG. 4 (e), in the horizontal cross section, the pressure surface 4a contacts the opposing surface 32a and the opposing surface 32b at the contact points P7 and P8, respectively, and the pressure surface 4b contacts the opposing surface 33 and the contact point P9. Therefore, the dovetail portion 2 can be stably and reliably gripped by the attachment member 31.

なお、前記説明においては、取付け部材31は、ダブテール部2の左側の圧力面4aに対向する位置に一対の当接部34a、34b、右側の圧力面4bに対向する位置に1つの当接部35を配設することとしたが、逆に、ダブテール部2の右側の圧力面4bに対向する位置に一対の当接部34a、34b、左側の圧力面4aに対向する位置に1つの当接部35を配設することしてもよい。   In the above description, the attachment member 31 has a pair of contact portions 34a and 34b at a position facing the left pressure surface 4a of the dovetail portion 2, and one contact portion at a position facing the right pressure surface 4b. However, conversely, a pair of contact portions 34a and 34b are disposed at a position facing the right pressure surface 4b of the dovetail portion 2, and one contact is disposed at a position facing the left pressure surface 4a. The part 35 may be provided.

以上のとおり、第二実施形態においても、第一の実施形態と同様に取付け部材31は、ダブテール部2を再現性高く安定かつ確実に把持できる。これにより、ブレード内基準をホルダー上の基準に代用して回転翼の翼部3等の加工や計測を高精度に行うことができる。   As described above, also in the second embodiment, the mounting member 31 can hold the dovetail portion 2 stably and reliably with high reproducibility as in the first embodiment. Thereby, it is possible to process and measure the blade portion 3 of the rotor blade with high accuracy by substituting the reference in the blade with the reference on the holder.

図5は、本発明に係る取付け部材の第三の実施形態を示す図であり、回転翼1のダブテール部2が取付け部材41により把持された状態を示す図である。なお、以下において、説明を省略した事項については、矛盾等がない限り、第一又は第二の実施形態と同様である。   FIG. 5 is a view showing a third embodiment of the attachment member according to the present invention, and is a view showing a state in which the dovetail portion 2 of the rotary blade 1 is gripped by the attachment member 41. In the following description, items that are not described are the same as those in the first or second embodiment unless there is a contradiction or the like.

取付け部材41には、回転翼1のダブテール部2の左右一対の圧力面4a、4bの左側の圧力面4aに庇状に覆いかぶさる当接部44が配設され、当接部44の底面には、左側の圧力面4aに向けて台地状に突き出した一対の突起部48a、48bが前後方向に配設されている(図5(e)参照)(前後方向とは、図5(e)上下方向を指し、同図下側が前方向とする)。また、突起部48a、48bの表面には、それぞれ平面状の対向面42a、42bが形成されている(図5(e)参照)。取付け部材21には、同様に、左右一対の圧力面4a、4bの右側の圧力面4bに庇状に覆いかぶさる当接部45が配設され、当接部45の底面には、右側の圧力面4bに向けて台地状に突き出した一対の突起部49c、49dが前後方向に配設されている。また、突起部49c、49dの表面には、それぞれ平面状の対向面43a、43bが形成されている(図5(e)参照)。なお、当接部44、45はそれぞれ、取付け部材41の下部の基台部から上方に向かって伸びている支持部46、47に連結されている。   The attachment member 41 is provided with a contact portion 44 that covers the pressure surface 4a on the left side of the pair of left and right pressure surfaces 4a and 4b of the dovetail portion 2 of the rotor blade 1 in a bowl shape. Is provided with a pair of protrusions 48a, 48b protruding in a plateau shape toward the left pressure surface 4a (see FIG. 5 (e)) (the front / rear direction refers to FIG. 5 (e)). It points in the vertical direction, and the lower side of the figure is the forward direction). Moreover, planar opposing surfaces 42a and 42b are formed on the surfaces of the protrusions 48a and 48b, respectively (see FIG. 5E). Similarly, the attachment member 21 is provided with a contact portion 45 that covers the right pressure surface 4b of the pair of left and right pressure surfaces 4a and 4b in a bowl shape. A pair of protrusions 49c and 49d protruding in a plateau shape toward the surface 4b are arranged in the front-rear direction. Also, planar opposing surfaces 43a and 43b are formed on the surfaces of the protrusions 49c and 49d, respectively (see FIG. 5E). The contact portions 44 and 45 are connected to support portions 46 and 47 extending upward from the base portion at the bottom of the attachment member 41, respectively.

また、左側の圧力面4aに対向する対向面42a、42bは、図5(e)に示されるように、同一平面内に形成されており、これにより当接部44を湾曲した三次元曲面の圧力面4aに当接させると、水平断面においては、対向面42a、42bは、それぞれ当接部44の中央部側の端部である当接点P10、P11において圧力面4aと接触し(図5(e)参照)、鉛直断面においては、当接部44の中央部側の端部に沿って直線状の当接線L8、L9において圧力面4aと直線状に接触する(図5(d)参照)。同様に、右側の圧力面4bに対向する対向面43a、43bは、同一平面内に形成されており、これにより当接部45を湾曲した三次元曲面の圧力面4bに当接させると、水平断面においては、対向面43a、43bは、それぞれ当接部44の中央部側の端部である当接点P12、P13において圧力面4bと接触し(図5(e)参照)、鉛直断面においては、対向面43a、43bは、それぞれ当接部45の中央部側の端部に沿って直線状の当接線L10、L11において圧力面4bと直線状に接触する。   Further, the facing surfaces 42a and 42b facing the left pressure surface 4a are formed in the same plane as shown in FIG. 5 (e), thereby forming a three-dimensional curved surface in which the contact portion 44 is curved. When brought into contact with the pressure surface 4a, in the horizontal cross section, the opposing surfaces 42a and 42b come into contact with the pressure surface 4a at the contact points P10 and P11, which are the end portions on the center side of the contact portion 44 (FIG. 5). (See (e)), in the vertical cross section, linearly contacts the pressure surface 4a along the linear contact lines L8 and L9 along the end of the contact portion 44 on the center side (see FIG. 5D). ). Similarly, the opposing surfaces 43a and 43b that oppose the right pressure surface 4b are formed in the same plane, so that when the contact portion 45 is brought into contact with the curved three-dimensional curved pressure surface 4b, In the cross section, the opposing surfaces 43a and 43b are in contact with the pressure surface 4b at the contact points P12 and P13, which are the ends on the center side of the contact portion 44 (see FIG. 5E), and in the vertical cross section, The opposed surfaces 43a and 43b are in linear contact with the pressure surface 4b along linear contact lines L10 and L11 along the end of the contact portion 45 on the center side.

取付け部材41は、ネジ機構17によりダブテール部2の底面に向けて前後進可能な押付け部16が配設されており、押付け部16、当接部44、45でダブテール部2を把持すると、対向面42a、42b、43a、43bが、当接線L8、L9、L10、L11において、圧力面4a、4bと接触するため、ダブテール部2を再現性高く安定かつ確実に把持できる。これにより、ブレード内基準をホルダー上の基準に代用して回転翼の翼部3等の加工や計測を高精度に行うことができる。   The mounting member 41 is provided with a pressing portion 16 that can be moved back and forth toward the bottom surface of the dovetail portion 2 by the screw mechanism 17. When the dovetail portion 2 is gripped by the pressing portion 16 and the abutting portions 44 and 45, the mounting member 41 faces. Since the surfaces 42a, 42b, 43a, 43b are in contact with the pressure surfaces 4a, 4b at the contact lines L8, L9, L10, L11, the dovetail portion 2 can be gripped stably and reliably with high reproducibility. Thereby, it is possible to process and measure the blade portion 3 of the rotor blade with high accuracy by substituting the reference in the blade with the reference on the holder.

図6は、本発明に係る取付け部材の第四の実施形態を示す図であり、回転翼1のダブテール部2が取付け部材51により把持された状態を示す図である。なお、以下において、説明を省略した事項については、矛盾等がない限り、第一乃至第三の実施形態と同様である。   FIG. 6 is a view showing a fourth embodiment of the attachment member according to the present invention, and is a view showing a state in which the dovetail portion 2 of the rotary blade 1 is gripped by the attachment member 51. In the following description, items that are not described are the same as those in the first to third embodiments unless there is a contradiction or the like.

取付け部材51には、回転翼1のダブテール部2の左右一対の圧力面4a、4bの左側の圧力面4aに庇状に覆いかぶさる当接部54が配設され、当接部54の底面には、左側の圧力面4aに向けて台地状に突き出した一対の突起部58a、58bが前後方向に配設されている。突起部58a、58bの圧力面4aに対向する表面にはそれぞれ、平面状の対向面42a、42bが形成されている(図6(e)参照)。また、取付け部材21には、左右一対の圧力面4a、4bの右側の圧力面4bに庇状に覆いかぶさる当接部45が配設されており、当接部45の圧力面4bに対向する表面には、平面状の対向面53が形成されている(図6(e)参照)。なお、当接部54、55はそれぞれ、取付け部材41の下部の基台部から上方に向かって伸びている支持部56、57に連結されている。   The attachment member 51 is provided with a contact portion 54 that covers the pressure surface 4a on the left side of the pair of left and right pressure surfaces 4a and 4b of the dovetail portion 2 of the rotor blade 1 in a bowl shape. Are provided with a pair of protrusions 58a, 58b protruding in the front-rear direction so as to protrude toward the left pressure surface 4a. Planar facing surfaces 42a and 42b are formed on the surfaces of the protrusions 58a and 58b facing the pressure surface 4a, respectively (see FIG. 6E). Further, the mounting member 21 is provided with a contact portion 45 that covers the right pressure surface 4b of the pair of left and right pressure surfaces 4a and 4b in a bowl shape, and faces the pressure surface 4b of the contact portion 45. A flat opposing surface 53 is formed on the surface (see FIG. 6E). The contact portions 54 and 55 are connected to support portions 56 and 57 that extend upward from the base portion at the bottom of the attachment member 41, respectively.

左側の圧力面4aに対向する対向面42a、42bは、第三の実施形態と同様に、同一平面内に形成されており、これにより当接部54を湾曲した三次元曲面の圧力面4aに当接させると、水平断面においては、対向面42a、42bは、それぞれ当接部54の中央部側の端部である当接点P14、P15において圧力面4aと接触し(図6(e)参照)、鉛直断面においては、対向面42a、42bは、それぞれ当接部54の中央部側の端部に沿って直線状の当接線L12、L13において圧力面4aと直線状に接触する(図示省略)。   The opposing surfaces 42a and 42b that oppose the left pressure surface 4a are formed in the same plane as in the third embodiment, so that the contact surface 54 is curved to the three-dimensional curved pressure surface 4a. When contacted, in the horizontal cross section, the opposing surfaces 42a and 42b contact the pressure surface 4a at the contact points P14 and P15, which are the ends of the center of the contact portion 54, respectively (see FIG. 6 (e)). In the vertical cross section, the opposing surfaces 42a and 42b are in linear contact with the pressure surface 4a along linear contact lines L12 and L13 along the end of the contact portion 54 on the center side (not shown). ).

一方、右側の圧力面4bに対向する対向面53は、湾曲した三次元曲面の圧力面4bに当接させると、対向面53は、水平断面においては、当接部44の中央部の当接点P16において圧力面4bと接触し(図6(e)参照)、鉛直断面においては、当接部55の中央部において直線状の当接線L14において圧力面4bと直線状に接触する。   On the other hand, when the facing surface 53 facing the right pressure surface 4b is brought into contact with the curved three-dimensional curved pressure surface 4b, the facing surface 53 becomes a contact point at the center of the contact portion 44 in the horizontal section. In P16, the pressure surface 4b is contacted (see FIG. 6E), and in the vertical section, the pressure surface 4b is linearly contacted at a linear contact line L14 at the center of the contact portion 55.

なお、前記説明においては、取付け部材51は、ダブテール部2の左側の圧力面4aに対向する位置に一対の対向面52a、52bを有する当接部54、右側の圧力面4bに対向する位置に1つの対向面53を有する当接部55を配設することとしたが、逆に、ダブテール部2の右側の圧力面4bに対向する位置に一対の対向面52a、52bを有する当接部54、左側の圧力面4aに対向する位置に1つの対向面53を有する当接部55を配設することしてもよい。   In the above description, the attachment member 51 is located at a position facing the pressure surface 4a on the right side and a contact portion 54 having a pair of facing surfaces 52a and 52b at a position facing the pressure surface 4a on the left side of the dovetail portion 2. The abutting portion 55 having one opposing surface 53 is disposed, but conversely, the abutting portion 54 having a pair of opposing surfaces 52a and 52b at a position facing the right pressure surface 4b of the dovetail portion 2. A contact portion 55 having one facing surface 53 may be disposed at a position facing the left pressure surface 4a.

取付け部材51は、ネジ機構17によりダブテール部2の底面に向けて前後進可能な押付け部16が配設されており、押付け部16、当接部54a、54b、55でダブテール部2を把持すると、当接部54a、54b、55が、当接線L12、L13、L14において、圧力面4a、4bと線状に接触するため、ダブテール部2を再現性高く安定かつ確実に把持できる。これにより、ブレード内基準をホルダー上の基準に代用して回転翼の翼部3等の加工や計測を高精度に行うことができる。   The attachment member 51 is provided with a pressing portion 16 that can be moved forward and backward by the screw mechanism 17 toward the bottom surface of the dovetail portion 2. When the dovetail portion 2 is gripped by the pressing portion 16 and the contact portions 54 a, 54 b, 55, Since the contact portions 54a, 54b, and 55 are in linear contact with the pressure surfaces 4a and 4b at the contact lines L12, L13, and L14, the dovetail portion 2 can be gripped stably and reliably with high reproducibility. Thereby, it is possible to process and measure the blade portion 3 of the rotor blade with high accuracy by substituting the reference in the blade with the reference on the holder.

図7は、ダブテール部を本発明に係る取付け部材により把持された回転翼1を三次元N C加工機71に装着したときの概念を示す斜視図である。   FIG. 7 is a perspective view showing a concept when the rotating blade 1 having the dovetail portion gripped by the mounting member according to the present invention is mounted on the three-dimensional NC processing machine 71.

三次元N C加工機71は、X軸テーブル73、Y軸テーブル74、鉛直V軸テーブル75、Xθテーブル76、Zθ軸テーブル77、水平H軸テーブル78を有し、V軸テーブル75に主軸72が設けられており、ダブテール部2を介して回転翼1を把持した取付け部材81がY軸テーブル74に装着される。   The three-dimensional NC processing machine 71 includes an X-axis table 73, a Y-axis table 74, a vertical V-axis table 75, an Xθ table 76, a Zθ-axis table 77, and a horizontal H-axis table 78. A mounting member 81 that is provided and holds the rotary blade 1 via the dovetail portion 2 is attached to the Y-axis table 74.

主軸72には、加工の種類や内容に応じて適切な加工ツール80が装着されて翼部等の加工が行われる。また、水平H軸テーブル78には、翼部等の三次元形状を測定するための三次元測定器79が装着される。三次元測定器79にはレーザ光を使用した非接触式測定器や触針式測定器等が使用される。   An appropriate machining tool 80 is attached to the main shaft 72 according to the type and content of machining, and the wings and the like are machined. The horizontal H-axis table 78 is equipped with a three-dimensional measuring device 79 for measuring a three-dimensional shape such as a wing. As the three-dimensional measuring device 79, a non-contact type measuring device using a laser beam, a stylus type measuring device, or the like is used.

なお、前記実施形態の説明においては、加工機、測定器としてそれぞれ三次元加工機、三次元測定器を使用したが、より簡略な加工機、測定器(例えば二次元加工機等)であってもよい。   In the description of the embodiment, a three-dimensional processing machine and a three-dimensional measuring instrument are used as a processing machine and a measuring instrument, respectively. However, a simpler processing machine and a measuring instrument (for example, a two-dimensional processing machine) Also good.

1 回転翼
2 ダブテール部
3 翼部
4a、4b 圧力面
9a、9b 張り出し部
11 ホルダー
12a、12b 対向面
15a、15b 当接部
16 押付け部
17 ネジ機構
21 取付け部材
22a、22b、23a、23b 対向面
24a、24b、25a、25b 当接部
26a、26b、27a、27b 支持部
31 取付け部材
32a、32b、33 対向面
34a、34b、35 当接部
36a、36b、37 支持部
41 取付け部材
42a、42b、43a、43b 対向面
44、45 当接部
46、47 支持部
48a、48b、48c、48d 突起部
51 取付け部材
52a、52b、53 対向面
54、55 当接部
56、57 支持部
58a、58b 突起部
81 取付け部材
DESCRIPTION OF SYMBOLS 1 Rotating blade 2 Dovetail part 3 Blade | wing part 4a, 4b Pressure surface 9a, 9b Overhang | projection part 11 Holder 12a, 12b Opposing surface 15a, 15b Abutting part 16 Pressing part 17 Screw mechanism 21 Mounting member 22a, 22b, 23a, 23b Opposing surface 24a, 24b, 25a, 25b Abutting portions 26a, 26b, 27a, 27b Support portion 31 Mounting members 32a, 32b, 33 Opposing surfaces 34a, 34b, 35 Abutting portions 36a, 36b, 37 Support portions 41 Mounting members 42a, 42b , 43a, 43b Opposing surfaces 44, 45 Abutting portions 46, 47 Support portions 48a, 48b, 48c, 48d Protruding portions 51 Mounting members 52a, 52b, 53 Opposing surfaces 54, 55 Abutting portions 56, 57 Supporting portions 58a, 58b Projection 81 Mounting member

Claims (1)

ダブテールの両側部に形成される一対の庇状の張り出し部の翼部側の面が三次元曲面として形成される圧力面を有する軸流式圧縮機の回転翼を加工機又は計測器に装着するために使用される、回転翼の取付け部材であって、
前記一対の張り出し部の一方の張り出し部の前記圧力面に当接可能な一対の対向面と、
前記一対の張り出し部の他方の張り出し部の前記圧力面に当接可能な1つ又は一対の対向面と、
を備える回転翼の取付け部材。
Pressurized KOKI or measuring instruments the rotor blades of the axial compressor having a pressure face in which the pair of eave-shaped surface of the blade portion side of the projecting portion formed on both sides of the dovetail is formed as a three-dimensional curved surface A mounting member for a rotor blade used for mounting to
A pair of opposed surfaces which can come into contact with the pressure surface of one of the projecting portions of the pair of protruding portions,
And one or a pair of opposed surfaces which can come into contact with the pressure surface of the other overhanging portion of the pair of protruding portions,
A mounting member for a rotor blade comprising:
JP2018118796A 2018-06-22 2018-06-22 Mounting member for rotor blade Active JP6611384B1 (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112809576A (en) * 2020-12-30 2021-05-18 德阳六合能源材料有限公司 Positioning fixture device of steam turbine blade
CN113369922A (en) * 2021-06-30 2021-09-10 中国航发动力股份有限公司 Quick-change device for die forging blade machining blade tip center hole

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112809576A (en) * 2020-12-30 2021-05-18 德阳六合能源材料有限公司 Positioning fixture device of steam turbine blade
CN113369922A (en) * 2021-06-30 2021-09-10 中国航发动力股份有限公司 Quick-change device for die forging blade machining blade tip center hole

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