WO2017130787A1 - Method for producing blisk intermediate product, and forging die unit - Google Patents

Method for producing blisk intermediate product, and forging die unit Download PDF

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Publication number
WO2017130787A1
WO2017130787A1 PCT/JP2017/001351 JP2017001351W WO2017130787A1 WO 2017130787 A1 WO2017130787 A1 WO 2017130787A1 JP 2017001351 W JP2017001351 W JP 2017001351W WO 2017130787 A1 WO2017130787 A1 WO 2017130787A1
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WIPO (PCT)
Prior art keywords
forging die
blisk
intermediate product
disk
forging
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PCT/JP2017/001351
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French (fr)
Japanese (ja)
Inventor
落合 宏行
将成 奥田
類 近藤
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株式会社Ihi
株式会社遠藤製作所
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Publication of WO2017130787A1 publication Critical patent/WO2017130787A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/02Die forging; Trimming by making use of special dies ; Punching during forging
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/06Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/06Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
    • B21J5/08Upsetting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00Making machine elements
    • B21K1/28Making machine elements wheels; discs
    • B21K1/36Making machine elements wheels; discs with blades

Definitions

  • the present disclosure relates to a method for manufacturing a blisk intermediate product and a forging die unit.
  • a compressor or turbine constituting a gas turbine engine that can be employed in an aircraft engine or the like may include a blisk (integrated impeller) as a rotor.
  • This blisk is formed of titanium alloy or nickel alloy (one of metal materials).
  • the blisk has a disk-shaped disk and a plurality of moving blades installed on the outer peripheral surface of the disk at equal intervals along the circumferential direction.
  • blisks are manufactured by the following method. Using a cutting tool for a disk such as a bite, turning the metal block (material block) of a disk-shaped or cylindrical metal block (material block) made of titanium alloy etc. Finish the product in the center of the product (final shape). Further, by using a cutting tool for moving blades such as an end mill, by performing rolling (one of cutting) along the circumferential direction of the metal block with respect to the outer edge portion (peripheral side portion) of the metal block, The outer edge of the metal block is finished into a plurality of blades of product shape. Thereby, a blisk can be manufactured from a disk-shaped or columnar metal block.
  • Patent Document 1 The prior art related to the present disclosure is disclosed in Patent Document 1.
  • the volume of the metal block as the input material is blisk. It becomes considerably larger than the volume.
  • the surplus as the cutting allowance of the metal block increases, and the cutting amount (cutting amount of the input material) necessary for manufacturing the blisk increases. Therefore, the material cost of the blisk increases, and it may be difficult to reduce the cost of the blisk. Further, the manufacturing time of blisk becomes long, the blisk productivity decreases, and the consumption of cutting tools such as end mills may become severe.
  • the present disclosure aims to reduce the cost of blisks and sufficiently increase the productivity of blisks, and at the same time, a method for producing blisk intermediate products and a forging die that are advantageous for sufficiently suppressing the consumption of cutting tools.
  • the purpose is to provide units.
  • the manufacturing method of the blisk intermediate product of the present disclosure includes a circular disk equivalent part including a machining allowance and corresponding to a blisk disk, and an outer peripheral surface of the disk equivalent part arranged at intervals along the circumferential direction and This is a method for manufacturing a blisk intermediate product including a machining allowance and having a plurality of blade equivalent parts corresponding to the blades of a blisk.
  • the manufacturing method of the blisk intermediate product of the present disclosure includes a first forging die having a first molding surface having a shape corresponding to the shape of one side in the axial direction of the blisk intermediate product, and the other side in the axial direction of the blisk intermediate product.
  • a forging die unit including a second forging die having a second forming surface having a shape corresponding to the shape, and a first forming surface of the first forging die and a second forming surface of the second forging die.
  • the forging die unit of the present disclosure includes a circular disk equivalent portion including a machining allowance and corresponding to a disc of a blisk, and an outer peripheral surface of the disk equivalent portion with an interval along the circumferential direction and a machining allowance. And a forging die unit used for manufacturing a blisk intermediate product having a plurality of blade equivalent parts corresponding to the blades of the blisk.
  • the forging die unit of the present disclosure has a first forging die having a first molding surface having a shape corresponding to the shape on one side in the axial direction of the blisk intermediate product, and the shape on the other side in the axial direction of the blisk intermediate product.
  • a second forging die having a second molding surface of a corresponding shape.
  • FIG. 1 is a perspective view of the product shape (final shape) of blisk.
  • FIG. 2 is a perspective view of a blisk intermediate product according to an embodiment of the present disclosure.
  • Drawing 3 is a mimetic diagram explaining the setting process in the manufacturing method of the blisk intermediate goods concerning the embodiment of this indication.
  • FIG. 4 is a schematic diagram illustrating an extrusion forging process in the method for manufacturing a blisk intermediate product according to the embodiment of the present disclosure.
  • FIG. 5 is a schematic diagram illustrating an extrusion forging process in the method for manufacturing a blisk intermediate product according to the embodiment of the present disclosure.
  • Drawing 6 is a mimetic diagram explaining an extraction process in a manufacturing method of a blisk intermediate article concerning an embodiment of this indication.
  • FIG. 7A is an enlarged cross-sectional view in the circumferential direction along the line VII-VII in FIG.
  • FIG. 7B is a diagram corresponding to FIG. 7A in a modified example of the extrusion forging process.
  • FIG. 8 is a perspective view of a blisk intermediate product according to a modification of the embodiment of the present disclosure.
  • a manufacturing method of a blisk intermediate product according to an embodiment of the present disclosure, a forging die unit, and the like will be described with reference to the drawings.
  • “U” is the upward direction (upper vertical direction)
  • “D” is the downward direction (lower vertical direction)
  • “AD” is the axial direction of blisk or blisk intermediate product
  • “CD” is , Indicates the direction of rotation of the blisk.
  • the “pressing direction” refers to a direction in which the first forging die and the second forging die are close to each other (on the first forging die side with respect to the second forging die).
  • the “opposite direction (the direction opposite to the pressing direction)” is a direction in which the first forging die and the second forging die are separated from each other (on the basis of the second forging die, Means the other side.
  • the blisk 10 in which the present embodiment can be adopted is an integrated impeller having a shape as shown in FIG. 1 and formed integrally as a whole.
  • the blisk 10 is used for a compressor (not shown) or a turbine (not shown) constituting a gas turbine engine that can be employed in an aircraft engine or the like.
  • the blisk 10 is formed of a titanium alloy or a nickel alloy (one of metal materials).
  • the blisk 10 has a circular (disc-shaped) disk 12.
  • the disk 12 has an insertion hole 14 for inserting a rotor shaft (not shown) of a compressor or turbine in the center thereof.
  • the insertion hole 14 passes through the disk 12 along the axial direction of the blisk 10.
  • a plurality of rotor blades 16 are disposed on the outer peripheral surface 12 c of the disk 12 at equal intervals along the circumferential direction of the outer peripheral surface 12 c of the disk 12.
  • the leading edge 16 a of the preceding moving blade 16 of each adjacent pair of moving blades 16 is located on the rotational direction side of the blisk 10 relative to the trailing edge 16 p of the following moving blade 16.
  • the preceding moving blade 16 refers to the moving blade 16 that precedes the rotation direction of the blisk 10.
  • the trailing blade 16 refers to the trailing blade 16 that follows the rotation direction of the blisk 10.
  • the blisk intermediate product 18 is an intermediate product before being finished into the product shape blisk 10 shown in FIG.
  • the blisk intermediate product 18 is formed by performing an extrusion forging process on an annular metal block (material block) M (see FIG. 3) made of a titanium alloy, a nickel alloy, or the like (material constituting the blisk).
  • the blisk intermediate product 18 has a circular (disk-shaped) disk equivalent portion 20 including the disk 12.
  • a machining allowance (remaining) 20e for finishing is included on the surface side of the disk equivalent portion 20.
  • An insertion hole equivalent part 22 corresponding to the insertion hole 14 is formed at the center of the disk equivalent part 20.
  • a cutting allowance 24e for finishing is included on the surface side of each rotor blade equivalent portion 24, a cutting allowance 24e for finishing is included.
  • the front edge 24a of the preceding blade equivalent portion 24 of each pair of adjacent blade equivalent portions 24 is located on the rotational direction side of the blisk 10 with respect to the rear edge 24p of the subsequent blade equivalent portion 24.
  • the preceding moving blade equivalent portion 24 refers to the moving blade equivalent portion 24 corresponding to the preceding moving blade 16 (see FIG. 1).
  • the subsequent blade equivalent part 24 refers to the blade equivalent part 24 corresponding to the subsequent blade 16 (see FIG. 1).
  • the forging die unit 26 includes a first forging die 30 detachably mounted on the upper surface of a bolster 28 of a press machine (most of which is not shown).
  • the second forging die 34 is detachably mounted on the lower surface of the ram 32 of the press machine and faces the first forging die 30 in the vertical direction.
  • the specific configurations of the first forging die 30 and the second forging die 34 of the forging die unit 26 according to the present embodiment are as follows.
  • the first forging die 30 has a first disc forming surface 30d corresponding to the shape of one side in the axial direction of the disc equivalent portion 20 in the central portion on the upper side of the first forging die 30.
  • the first forging die 30 has a first blade forming surface corresponding to a shape including the back surfaces 24r (see FIG. 2) of the plurality of blade equivalent portions 24 on the outer edge of the first forging die 30.
  • 30b The first rotor blade forming surface 30b is located on the radially outer side of the first disk forming surface 30d, and is formed in a saw blade shape (uneven shape) in a cross section along the circumferential direction of the first forging die 30. (See FIG. 7A).
  • the first disk forming surface 30d and the first rotor blade forming surface 30b constitute a first forming surface corresponding to the shape of one side of the blisk intermediate product 18 in the axial direction. Further, the first forging die 30 has a set pin 36 for setting the annular metal block M at the center of the first disk forming surface 30d.
  • the second forging die 34 has a cylindrical second forging die base 38 that is detachably attached to the lower surface of the ram (slide) 32. Further, the second forging die base 38 has a punch 40 in the central portion below the second forging die base 38.
  • the punch 40 has a second disk forming surface 40 d corresponding to the shape of the other side in the axial direction of the disk corresponding portion 20 at the lower part of the punch 40. Furthermore, the punch 40 has a fitting hole 42 for fitting into the set pin 36 at the center of the second disk forming surface 40d.
  • the movable ring 44 is disposed below the second forging die base 38 so as to be movable in the vertical direction (press direction and the opposite direction).
  • the movable ring 44 is located on the radially outer side of the punch 40.
  • the movable ring 44 is attached to the second forging die base 38 so as not to be detached by an annular stopper plate 46 fixed to the lower end of the second forging die base 38.
  • the movable ring 44 has a second moving blade forming surface 44 b corresponding to a shape including the abdominal surfaces 24 v (see FIG. 2) of the plurality of moving blade corresponding portions 24 at the lower portion of the movable ring 44.
  • the second rotor blade forming surface 44b is located on the radially outer side of the second disk forming surface 40d, and is formed in a saw blade shape (uneven shape) in a cross section along the circumferential direction of the second forging die 34. (See FIG. 7A).
  • the second disk forming surface 40d and the second rotor blade forming surface 44b constitute a second forming surface corresponding to the shape of the other side of the blisk intermediate product 18 in the axial direction.
  • the outer edge portion (the portion radially outside the second moving blade forming surface 44 b) 44 o on the lower surface of the movable ring 44 is formed so as to be able to contact the outer edge portion 30 o on the upper surface of the first forging die 30.
  • the second moving blade forming surface 44b is locally attached to the first moving blade forming surface 30b when the outer edge portion 44o of the lower surface of the movable ring 44 contacts the outer edge portion 30o of the upper surface of the first forging die 30. It forms so that it may contact (refer FIG. 7A).
  • the movable ring 44 has a plurality of guide holes 48 arranged on the upper surface of the movable ring 44 at intervals in the circumferential direction (predetermined circumferential direction).
  • the second forging die base 38 has a plurality of support pins (guide pins) 50 arranged at intervals in the circumferential direction (predetermined circumferential direction).
  • Each support pin 50 is inserted into a corresponding guide hole 48 to support the movable ring 44 so as to be movable in the vertical direction.
  • each support pin 50 has a spring 52 as a biasing member that biases the movable ring 44 downward (press direction) between the second forging die base 38 and the movable ring 44.
  • the outer edge portion 44o of the lower surface of the movable ring 44 contacts the outer edge portion 30o of the upper surface of the first forging die 30, the outer edge portion 44o of the lower surface of the movable ring 44 has a biasing force of the plurality of springs 52 or In this state, the movable ring 44 protrudes downward with respect to the punch 40 due to its own weight.
  • the manufacturing method of the blisk intermediate product 18 includes a heating process, a setting process, an extrusion forging process, and a removal process. And the specific content of each process in the manufacturing method of the blisk intermediate product 18 which concerns on this embodiment is as follows.
  • the metal block M made of a titanium alloy or the like is preheated to a high temperature of, for example, 800 ° C. or higher using a heating furnace (not shown).
  • the first forging die 30 and the second forging die 34 may be preheated to a high temperature of, for example, 200 ° C. or higher using a heater (not shown). Good.
  • a release agent such as graphite is used to form the first disk forming surface 30d, the first blade forming surface 30b, the second disk forming surface 40d, and the second blade forming.
  • a mold release process is performed on the first forging die 30 and the second forging die 34.
  • the set pin 36 is inserted through the hole Mh of the metal block M, and the metal block M is set on the first disk forming surface 30 d of the first forging die 30.
  • the metal block M is set between the first disk forming surface 30 d of the first forging die 30 and the second disk forming surface 40 d of the second forging die 34.
  • the punch 40 is moved in the pressing direction relative to the movable ring 44, and the lower part (second disk forming surface 40 d) of the punch 40 is moved to the movable ring 44. It protrudes in the pressing direction with respect to the outer edge portion 44o of the lower surface.
  • the metal block M was pressed in the pressing direction by the punch 40, and the first blade forming surface 30b and the second blade forming surface 44b were brought into local contact with each other.
  • the metal block M can be extrusion-forged in the radial direction (radial direction) perpendicular to the pressing direction by the cooperation of the first forging die 30 and the second forging die 34.
  • the disk equivalent portion 20 can be formed on the metal block M, and the plurality of blade equivalent portions 24 can be extruded on the metal block M.
  • the blisk intermediate product 18 having the disk equivalent part 20 and the plurality of blade equivalent parts 24 can be manufactured from the metal block M.
  • the manufacturing method of the blisk intermediate product 18 according to the present embodiment is completed, and the blisk intermediate product 18 having the disk equivalent part 20 and the plurality of blade equivalent parts 24 can be manufactured from the metal block M.
  • the disc equivalent portion 20 is turned (using a cutting tool for a disc (for example, a bite)) ( The disk equivalent portion 20 is finished into the disk 12 by performing one of the cutting operations. Further, by using a cutting tool for moving blades (for example, an end mill or the like), each moving blade corresponding portion 24 is moved to the moving blade 16 by performing rolling (one of cutting) on each moving blade corresponding portion 24. Finish. Thereby, the blisk intermediate product 18 can be finally finished into the product-shaped blisk 10.
  • a cutting tool for moving blades for example, an end mill or the like
  • the disk equivalent part 20 is formed on the metal block M, and the plurality of moving blade equivalent parts 24 are extruded on the metal block M. it can.
  • the blisk intermediate product 18 can be manufactured from the metal block M without cutting the metal block M.
  • the difference between the volume of the metal block M as the input material and the volume of the blisk 10 can be reduced, and the cutting amount necessary for manufacturing the blisk 10 (the cutting amount of the input material) can be greatly reduced.
  • the difference between the volume of the metal block M as the input material and the volume of the blisk 10 can be reduced. Therefore, the increase in material cost of the blisk 10 can be suppressed, and the cost of the blisk 10 can be reduced.
  • the amount of cutting necessary for manufacturing the blisk 10 can be greatly reduced. Therefore, the manufacturing time of the blisk 10 can be greatly shortened, the productivity of the blisk 10 can be sufficiently increased, and consumption of the cutting tool can be sufficiently suppressed.
  • the cost of the blisk 10 can be reduced, the productivity of the blisk 10 can be sufficiently increased, and consumption of the cutting tool can be sufficiently suppressed.
  • the first forging die 30 and the second forging die 34 are in contact with each other in a state where the first moving blade forming surface 30b and the second moving blade forming surface 44b are not in contact with each other.
  • the metal block M may be extrusion-forged in the radial direction by cooperation (see FIG. 5).
  • the second moving blade forming surface 44b is not in contact with the first moving blade forming surface 30b when the outer edge portion 44o of the lower surface of the movable ring 44 contacts the outer edge portion 30o of the upper surface of the first forging die 30. You may form so that it may contact (refer FIG. 7B).
  • each adjacent pair It is possible to manufacture the blisk intermediate product 18 ⁇ / b> A further having a bridge 54 between the rotor blade equivalent parts 24.
  • the blisk intermediate product 18A shown in FIG. 8 has the same configuration as the blisk intermediate product 18 shown in FIG.

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  • Mechanical Engineering (AREA)
  • Forging (AREA)

Abstract

This method for producing a blisk intermediate product comprises a setting step for setting a metal block (M) between a first disk-forming surface (30d) of a first forging die (30) and a second disk-forming surface (40d) of a second forging die (34). The method for producing a blisk intermediate product further comprises an extrusion forging step for, by moving the second forging die in a pressing direction, pressing the metal block in the pressing direction by the second forging die and extrusion-forging the metal block in a radial direction perpendicular to the pressing direction through cooperation between the first forging die and the second forging die.

Description

ブリスク中間品の製造方法、及び、鍛造金型ユニットBlisk intermediate product manufacturing method and forging die unit
 本開示は、ブリスク中間品を製造するための方法、及び、鍛造金型ユニットに関する。 The present disclosure relates to a method for manufacturing a blisk intermediate product and a forging die unit.
 航空機エンジン等に採用され得るガスタービンエンジンを構成するコンプレッサ又はタービンは、ロータとしてブリスク(一体型翼車)を含むことがある。このブリスクは、チタン合金又はニッケル合金等(金属材料の1つ)により形成されている。また、ブリスクは、円板状のディスクと、ディスクの外周面にその周方向に沿って等間隔に設置された複数の動翼とを有する。 A compressor or turbine constituting a gas turbine engine that can be employed in an aircraft engine or the like may include a blisk (integrated impeller) as a rotor. This blisk is formed of titanium alloy or nickel alloy (one of metal materials). The blisk has a disk-shaped disk and a plurality of moving blades installed on the outer peripheral surface of the disk at equal intervals along the circumferential direction.
 一般に、ブリスクは、以下の方法で製造される。バイト等のディスク用の切削工具を用いて、チタン合金等からなる円板状又は円柱状の金属ブロック(素材ブロック)の中央部に対して旋削(切削の1つ)を行うことにより、金属ブロックの中央部を製品形状(最終形状)のディスクに仕上げる。また、エンドミル等の動翼用の切削工具を用いて、金属ブロックの外縁部(外周側の部分)に対して金属ブロックの周方向に沿って転削(切削の1つ)を行うことにより、金属ブロックの外縁部を製品形状の複数の動翼に仕上げる。これにより、円板状又は円柱状の金属ブロックからブリスクを製造することができる。 Generally, blisks are manufactured by the following method. Using a cutting tool for a disk such as a bite, turning the metal block (material block) of a disk-shaped or cylindrical metal block (material block) made of titanium alloy etc. Finish the product in the center of the product (final shape). Further, by using a cutting tool for moving blades such as an end mill, by performing rolling (one of cutting) along the circumferential direction of the metal block with respect to the outer edge portion (peripheral side portion) of the metal block, The outer edge of the metal block is finished into a plurality of blades of product shape. Thereby, a blisk can be manufactured from a disk-shaped or columnar metal block.
 本開示に関連する先行技術としては特許文献1に示すものがある。 The prior art related to the present disclosure is disclosed in Patent Document 1.
特開2009-197649号公報JP 2009-197649 A
 前述のように、円板状又は円柱状の金属ブロックの外縁部を転削等の切削によって製品形状の複数の動翼に仕上げているため、一般に、投入材料としての金属ブロックの体積がブリスクの体積に比べてかなり大きくなる。それに伴い、金属ブロックの切削代としての余肉(余肉としての切削代)が増えて、ブリスクの製造に必要な切削量(投入材料の切削量)が多くなる。そのため、ブリスクの材料コストが増大して、ブリスクの低コスト化を図ることが困難になり得る。また、ブリスクの製造時間が長くなって、ブリスクの生産性が低下すると共に、エンドミル等の切削工具の消耗が激しくなり得る。 As described above, since the outer edge of the disk-shaped or columnar metal block is finished into a plurality of moving blades of product shape by cutting such as rolling, generally the volume of the metal block as the input material is blisk. It becomes considerably larger than the volume. Along with this, the surplus as the cutting allowance of the metal block (the cutting allowance as surplus) increases, and the cutting amount (cutting amount of the input material) necessary for manufacturing the blisk increases. Therefore, the material cost of the blisk increases, and it may be difficult to reduce the cost of the blisk. Further, the manufacturing time of blisk becomes long, the blisk productivity decreases, and the consumption of cutting tools such as end mills may become severe.
 そこで、本開示は、ブリスクの低コスト化を図った上で、ブリスクの生産性を十分に高めると共に、切削工具の消耗を十分に抑制するのに有利なブリスク中間品の製造方法及び鍛造金型ユニットを提供することを目的とする。 Accordingly, the present disclosure aims to reduce the cost of blisks and sufficiently increase the productivity of blisks, and at the same time, a method for producing blisk intermediate products and a forging die that are advantageous for sufficiently suppressing the consumption of cutting tools. The purpose is to provide units.
 本開示のブリスク中間品の製造方法は、削り代を含みかつブリスクのディスクに相当する円形状のディスク相当部と、ディスク相当部の外周面にその周方向に沿って間隔を置いて設置されかつ削り代を含みかつブリスクの動翼に相当する複数の動翼相当部とを有するブリスク中間品を製造するための方法である。本開示のブリスク中間品の製造方法は、ブリスク中間品の軸方向の一方側の形状に対応する形状の第1成形面を有する第1鍛造金型と、ブリスク中間品の軸方向の他方側の形状に対応する形状の第2成形面を有する第2鍛造金型とを含む鍛造金型ユニットを用い、第1鍛造金型の第1成形面と第2鍛造金型の第2成形面との間に、ブリスクの構成材料である金属ブロックをセットするセット工程と、セット工程の終了後に、第2鍛造金型をプレス方向へ移動させることにより、第2鍛造金型によって金属ブロックをプレス方向へ押圧し、かつ、第1鍛造金型と第2鍛造金型との協働によって金属ブロックをプレス方向に直交する放射方向へ押出鍛造する押出鍛造工程と、を有する。 The manufacturing method of the blisk intermediate product of the present disclosure includes a circular disk equivalent part including a machining allowance and corresponding to a blisk disk, and an outer peripheral surface of the disk equivalent part arranged at intervals along the circumferential direction and This is a method for manufacturing a blisk intermediate product including a machining allowance and having a plurality of blade equivalent parts corresponding to the blades of a blisk. The manufacturing method of the blisk intermediate product of the present disclosure includes a first forging die having a first molding surface having a shape corresponding to the shape of one side in the axial direction of the blisk intermediate product, and the other side in the axial direction of the blisk intermediate product. A forging die unit including a second forging die having a second forming surface having a shape corresponding to the shape, and a first forming surface of the first forging die and a second forming surface of the second forging die. Between the setting process of setting the metal block which is the constituent material of the blisk, and after the setting process is finished, the second forging die is moved in the pressing direction, so that the metal block is moved in the pressing direction by the second forging die. An extrusion forging step of pressing and forging the metal block in a radial direction orthogonal to the pressing direction by cooperation of the first forging die and the second forging die.
 本開示の鍛造金型ユニットは、削り代を含みかつブリスクのディスクに相当する円形状のディスク相当部と、ディスク相当部の外周面にその周方向に沿って間隔を置いて設置されかつ削り代を含みかつブリスクの動翼に相当する複数の動翼相当部とを有するブリスク中間品を製造するために用いられる鍛造金型ユニットである。本開示の鍛造金型ユニットは、ブリスク中間品の軸方向の一方側の形状に対応する形状の第1成形面を有する第1鍛造金型と、ブリスク中間品の軸方向の他方側の形状に対応する形状の第2成形面を有する第2鍛造金型と、を有する。 The forging die unit of the present disclosure includes a circular disk equivalent portion including a machining allowance and corresponding to a disc of a blisk, and an outer peripheral surface of the disk equivalent portion with an interval along the circumferential direction and a machining allowance. And a forging die unit used for manufacturing a blisk intermediate product having a plurality of blade equivalent parts corresponding to the blades of the blisk. The forging die unit of the present disclosure has a first forging die having a first molding surface having a shape corresponding to the shape on one side in the axial direction of the blisk intermediate product, and the shape on the other side in the axial direction of the blisk intermediate product. A second forging die having a second molding surface of a corresponding shape.
図1は、ブリスクの製品形状(最終形状)の斜視図である。FIG. 1 is a perspective view of the product shape (final shape) of blisk. 図2は、本開示の実施形態に係るブリスク中間品の斜視図である。FIG. 2 is a perspective view of a blisk intermediate product according to an embodiment of the present disclosure. 図3は、本開示の実施形態に係るブリスク中間品の製造方法におけるセット工程を説明する模式図である。Drawing 3 is a mimetic diagram explaining the setting process in the manufacturing method of the blisk intermediate goods concerning the embodiment of this indication. 図4は、本開示の実施形態に係るブリスク中間品の製造方法における押出鍛造工程を説明する模式図である。FIG. 4 is a schematic diagram illustrating an extrusion forging process in the method for manufacturing a blisk intermediate product according to the embodiment of the present disclosure. 図5は、本開示の実施形態に係るブリスク中間品の製造方法における押出鍛造工程を説明する模式図である。FIG. 5 is a schematic diagram illustrating an extrusion forging process in the method for manufacturing a blisk intermediate product according to the embodiment of the present disclosure. 図6は、本開示の実施形態に係るブリスク中間品の製造方法における取出工程を説明する模式図である。Drawing 6 is a mimetic diagram explaining an extraction process in a manufacturing method of a blisk intermediate article concerning an embodiment of this indication. 図7Aは、図5におけるVII-VII線に沿った円周方向の拡大断面図である。FIG. 7A is an enlarged cross-sectional view in the circumferential direction along the line VII-VII in FIG. 図7Bは、押出鍛造工程の変形例における図7Aに対応する図である。FIG. 7B is a diagram corresponding to FIG. 7A in a modified example of the extrusion forging process. 図8は、本開示の実施形態の変形例に係るブリスク中間品の斜視図である。FIG. 8 is a perspective view of a blisk intermediate product according to a modification of the embodiment of the present disclosure.
 本開示の実施形態に係るブリスク中間品の製造方法、及び、鍛造金型ユニット等について図面を参照して説明する。なお、図中、「U」は、上方向(鉛直方向上側)、「D」は、下方向(鉛直方向下側)、「AD」は、ブリスク又はブリスク中間品の軸方向、「CD」は、ブリスクの回転方向をそれぞれ示す。ここで、「プレス方向」とは、第1鍛造金型と第2鍛造金型とが互いに近接する方向(第2鍛造金型を基準とすると、第1鍛造金型側)をいう。「その反対方向(プレス方向の反対方向)」とは、第1鍛造金型と第2鍛造金型とが互いに離反する方向(第2鍛造金型を基準とすると、第1鍛造金型側とは反対側)をいう。 A manufacturing method of a blisk intermediate product according to an embodiment of the present disclosure, a forging die unit, and the like will be described with reference to the drawings. In the figure, “U” is the upward direction (upper vertical direction), “D” is the downward direction (lower vertical direction), “AD” is the axial direction of blisk or blisk intermediate product, and “CD” is , Indicates the direction of rotation of the blisk. Here, the “pressing direction” refers to a direction in which the first forging die and the second forging die are close to each other (on the first forging die side with respect to the second forging die). The “opposite direction (the direction opposite to the pressing direction)” is a direction in which the first forging die and the second forging die are separated from each other (on the basis of the second forging die, Means the other side.
 本実施形態に係るブリスク中間品の製造方法等について説明する前に、最終製品であるブリスク10の構成について図1を参照して説明する。 Before describing the manufacturing method of the blisk intermediate product according to the present embodiment, the configuration of the blisk 10 as the final product will be described with reference to FIG.
 本実施形態が採用され得るブリスク10は、図1に示されるような形状を有し、全体が一体として形成される一体型翼車である。ブリスク10は、航空機エンジン等に採用され得るガスタービンエンジンを構成するコンプレッサ(図示省略)又はタービン(図示省略)に用いられる。また、ブリスク10は、チタン合金又はニッケル合金等(金属材料の1つ)により形成される。 The blisk 10 in which the present embodiment can be adopted is an integrated impeller having a shape as shown in FIG. 1 and formed integrally as a whole. The blisk 10 is used for a compressor (not shown) or a turbine (not shown) constituting a gas turbine engine that can be employed in an aircraft engine or the like. The blisk 10 is formed of a titanium alloy or a nickel alloy (one of metal materials).
 ブリスク10は、円形状(円板状)のディスク12を有する。ディスク12は、その中央部に、コンプレッサ又はタービンのロータ軸(図示省略)を挿通させるための挿通穴14を有する。挿通穴14は、ブリスク10の軸方向に沿ってディスク12を貫通している。また、ディスク12の外周面12cには、複数の動翼16が、ディスク12の外周面12cの周方向に沿って等間隔に設置されている。そして、各隣接する一対の動翼16のうちの先行の動翼16の前縁16aは、後続の動翼16の後縁16pよりもブリスク10の回転方向側に位置している。換言すれば、ブリスク10の軸方向から見たときに、各隣接する一対の動翼16の間は、開放されている。ここで、先行の動翼16とは、ブリスク10の回転方向に対して先行する動翼16のことをいう。後続の動翼16は、ブリスク10の回転方向に対して後続する動翼16のことをいう。 The blisk 10 has a circular (disc-shaped) disk 12. The disk 12 has an insertion hole 14 for inserting a rotor shaft (not shown) of a compressor or turbine in the center thereof. The insertion hole 14 passes through the disk 12 along the axial direction of the blisk 10. A plurality of rotor blades 16 are disposed on the outer peripheral surface 12 c of the disk 12 at equal intervals along the circumferential direction of the outer peripheral surface 12 c of the disk 12. The leading edge 16 a of the preceding moving blade 16 of each adjacent pair of moving blades 16 is located on the rotational direction side of the blisk 10 relative to the trailing edge 16 p of the following moving blade 16. In other words, when viewed from the axial direction of the blisk 10, the space between each pair of adjacent blades 16 is open. Here, the preceding moving blade 16 refers to the moving blade 16 that precedes the rotation direction of the blisk 10. The trailing blade 16 refers to the trailing blade 16 that follows the rotation direction of the blisk 10.
 次に、本実施形態に係るブリスク中間品の製造方法の製造対象であるブリスク中間品18の構成について図2を参照して説明する。 Next, the configuration of the blisk intermediate product 18 that is a manufacturing target of the manufacturing method of the blisk intermediate product according to the present embodiment will be described with reference to FIG.
 図2に示すように、本実施形態に係るブリスク中間品18は、図1に示す製品形状のブリスク10に仕上げる前の中間品である。また、ブリスク中間品18は、チタン合金又はニッケル合金等(ブリスクの構成材料)からなる環状の金属ブロック(素材ブロック)M(図3参照)に押出鍛造加工を行うことによって成形される。 As shown in FIG. 2, the blisk intermediate product 18 according to the present embodiment is an intermediate product before being finished into the product shape blisk 10 shown in FIG. The blisk intermediate product 18 is formed by performing an extrusion forging process on an annular metal block (material block) M (see FIG. 3) made of a titanium alloy, a nickel alloy, or the like (material constituting the blisk).
 ブリスク中間品18は、ディスク12を含む円形状(円板状)のディスク相当部20を有する。ディスク相当部20の表面側には、仕上げ加工のための削り代(余肉)20eが含まれている。ディスク相当部20の中央部に、挿通穴14に相当する挿通穴相当部22が形成されている。ディスク相当部20の外周面20cには、動翼16に相当する複数の動翼相当部24が、ディスク相当部20の外周面20cの周方向に沿って等間隔に設置されている。各動翼相当部24の表面側には、仕上げ加工のための削り代24eが含まれている。 The blisk intermediate product 18 has a circular (disk-shaped) disk equivalent portion 20 including the disk 12. On the surface side of the disk equivalent portion 20, a machining allowance (remaining) 20e for finishing is included. An insertion hole equivalent part 22 corresponding to the insertion hole 14 is formed at the center of the disk equivalent part 20. On the outer peripheral surface 20 c of the disk equivalent portion 20, a plurality of rotor blade equivalent portions 24 corresponding to the moving blades 16 are installed at equal intervals along the circumferential direction of the outer peripheral surface 20 c of the disk equivalent portion 20. On the surface side of each rotor blade equivalent portion 24, a cutting allowance 24e for finishing is included.
 また、各隣接する一対の動翼相当部24のうちの先行の動翼相当部24の前縁24aは、後続の動翼相当部24の後縁24pよりもブリスク10の回転方向側に位置している。ここで、先行の動翼相当部24とは、先行の動翼16(図1参照)に相当する動翼相当部24のことをいう。後続の動翼相当部24とは、後続の動翼16(図1参照)に相当する動翼相当部24のことをいう。 Further, the front edge 24a of the preceding blade equivalent portion 24 of each pair of adjacent blade equivalent portions 24 is located on the rotational direction side of the blisk 10 with respect to the rear edge 24p of the subsequent blade equivalent portion 24. ing. Here, the preceding moving blade equivalent portion 24 refers to the moving blade equivalent portion 24 corresponding to the preceding moving blade 16 (see FIG. 1). The subsequent blade equivalent part 24 refers to the blade equivalent part 24 corresponding to the subsequent blade 16 (see FIG. 1).
 次に、ブリスク中間品18を製造するために用いられる鍛造金型ユニット26の構成について図3から図5を参照して説明する。 Next, the configuration of the forging die unit 26 used for manufacturing the blisk intermediate product 18 will be described with reference to FIGS.
 図3から図5に示すように、本実施形態に係る鍛造金型ユニット26は、プレス機械(大部分を図示省略)のボルスタ28の上面に着脱可能に装着された第1鍛造金型30と、プレス機械のラム32の下面に着脱可能に装着されかつ第1鍛造金型30に上下方向に対向する第2鍛造金型34とを含む。そして、本実施形態に係る鍛造金型ユニット26の第1鍛造金型30及び第2鍛造金型34の具体的な構成は、次の通りである。 As shown in FIGS. 3 to 5, the forging die unit 26 according to the present embodiment includes a first forging die 30 detachably mounted on the upper surface of a bolster 28 of a press machine (most of which is not shown). The second forging die 34 is detachably mounted on the lower surface of the ram 32 of the press machine and faces the first forging die 30 in the vertical direction. The specific configurations of the first forging die 30 and the second forging die 34 of the forging die unit 26 according to the present embodiment are as follows.
 第1鍛造金型30は、第1鍛造金型30の上側の中央部に、ディスク相当部20の軸方向の一方側の形状に対応する第1ディスク成形面30dを有する。また、第1鍛造金型30は、第1鍛造金型30の上側の外縁部に、複数の動翼相当部24の背面24r(図2参照)を含む形状に対応する第1動翼成形面30bを有する。第1動翼成形面30bは、第1ディスク成形面30dの半径方向外側に位置しており、第1鍛造金型30の周方向に沿った断面において鋸刃形状(凹凸形状)に形成されている(図7A参照)。第1ディスク成形面30d及び第1動翼成形面30bは、ブリスク中間品18の軸方向の一方側の形状に対応する第1成形面を構成する。更に、第1鍛造金型30は、第1ディスク成形面30dの中央部に、環状の金属ブロックMをセットするためのセットピン36を有する。 The first forging die 30 has a first disc forming surface 30d corresponding to the shape of one side in the axial direction of the disc equivalent portion 20 in the central portion on the upper side of the first forging die 30. The first forging die 30 has a first blade forming surface corresponding to a shape including the back surfaces 24r (see FIG. 2) of the plurality of blade equivalent portions 24 on the outer edge of the first forging die 30. 30b. The first rotor blade forming surface 30b is located on the radially outer side of the first disk forming surface 30d, and is formed in a saw blade shape (uneven shape) in a cross section along the circumferential direction of the first forging die 30. (See FIG. 7A). The first disk forming surface 30d and the first rotor blade forming surface 30b constitute a first forming surface corresponding to the shape of one side of the blisk intermediate product 18 in the axial direction. Further, the first forging die 30 has a set pin 36 for setting the annular metal block M at the center of the first disk forming surface 30d.
 第2鍛造金型34は、ラム(スライド)32の下面に着脱可能に装着された筒状の第2鍛造金型ベース38を有する。また、第2鍛造金型ベース38は、第2鍛造金型ベース38の下側の中央部に、パンチ40を有する。パンチ40は、パンチ40の下部に、ディスク相当部20の軸方向の他方側の形状に対応する第2ディスク成形面40dを有する。更に、パンチ40は、第2ディスク成形面40dの中央部に、セットピン36に嵌入させるための嵌入穴42を有する。 The second forging die 34 has a cylindrical second forging die base 38 that is detachably attached to the lower surface of the ram (slide) 32. Further, the second forging die base 38 has a punch 40 in the central portion below the second forging die base 38. The punch 40 has a second disk forming surface 40 d corresponding to the shape of the other side in the axial direction of the disk corresponding portion 20 at the lower part of the punch 40. Furthermore, the punch 40 has a fitting hole 42 for fitting into the set pin 36 at the center of the second disk forming surface 40d.
 第2鍛造金型ベース38の下部に、可動リング44が上下方向(プレス方向及びその反対方向)へ移動可能に配置されている。可動リング44は、パンチ40の半径方向外側に位置している。可動リング44は、第2鍛造金型ベース38の下端に固定した環状のストッパプレート46によって、第2鍛造金型ベース38に対して離脱不能に装着されている。可動リング44は、可動リング44の下部に、複数の動翼相当部24の腹面24v(図2参照)を含む形状に対応する第2動翼成形面44bを有する。第2動翼成形面44bは、第2ディスク成形面40dの半径方向外側に位置しており、第2鍛造金型34の周方向に沿った断面において鋸刃形状(凹凸形状)に形成されている(図7A参照)。第2ディスク成形面40d及び第2動翼成形面44bは、ブリスク中間品18の軸方向の他方側の形状に対応する第2成形面を構成する。また、可動リング44の下面の外縁部(第2動翼成形面44bよりも半径方向外側の部分)44oは、第1鍛造金型30の上面の外縁部30oに接触可能に形成されている。そして、第2動翼成形面44bは、可動リング44の下面の外縁部44oが第1鍛造金型30の上面の外縁部30oに接触したときに、第1動翼成形面30bに局所的に接触するように形成されている(図7A参照)。 The movable ring 44 is disposed below the second forging die base 38 so as to be movable in the vertical direction (press direction and the opposite direction). The movable ring 44 is located on the radially outer side of the punch 40. The movable ring 44 is attached to the second forging die base 38 so as not to be detached by an annular stopper plate 46 fixed to the lower end of the second forging die base 38. The movable ring 44 has a second moving blade forming surface 44 b corresponding to a shape including the abdominal surfaces 24 v (see FIG. 2) of the plurality of moving blade corresponding portions 24 at the lower portion of the movable ring 44. The second rotor blade forming surface 44b is located on the radially outer side of the second disk forming surface 40d, and is formed in a saw blade shape (uneven shape) in a cross section along the circumferential direction of the second forging die 34. (See FIG. 7A). The second disk forming surface 40d and the second rotor blade forming surface 44b constitute a second forming surface corresponding to the shape of the other side of the blisk intermediate product 18 in the axial direction. Further, the outer edge portion (the portion radially outside the second moving blade forming surface 44 b) 44 o on the lower surface of the movable ring 44 is formed so as to be able to contact the outer edge portion 30 o on the upper surface of the first forging die 30. The second moving blade forming surface 44b is locally attached to the first moving blade forming surface 30b when the outer edge portion 44o of the lower surface of the movable ring 44 contacts the outer edge portion 30o of the upper surface of the first forging die 30. It forms so that it may contact (refer FIG. 7A).
 可動リング44は、可動リング44の上面に、円周方向(所定の円周方向)に間隔を置いて配置された複数のガイド穴48を有する。また、第2鍛造金型ベース38は、その下部に、円周方向(所定の円周方向)に間隔を置いて配置された複数の支持ピン(ガイドピン)50を有する。各支持ピン50は、対応するガイド穴48に挿入されて可動リング44を上下方向へ移動可能に支持している。更に、各支持ピン50は、第2鍛造金型ベース38と可動リング44との間に、可動リング44を下方向(プレス方向)へ付勢する付勢部材としてのスプリング52を有する。そして、可動リング44の下面の外縁部44oが第1鍛造金型30の上面の外縁部30oに接触する前には、可動リング44の下面の外縁部44oは、複数のスプリング52の付勢力又は可動リング44の自重によってパンチ40に対して下方向へ突出した状態である。 The movable ring 44 has a plurality of guide holes 48 arranged on the upper surface of the movable ring 44 at intervals in the circumferential direction (predetermined circumferential direction). In addition, the second forging die base 38 has a plurality of support pins (guide pins) 50 arranged at intervals in the circumferential direction (predetermined circumferential direction). Each support pin 50 is inserted into a corresponding guide hole 48 to support the movable ring 44 so as to be movable in the vertical direction. Further, each support pin 50 has a spring 52 as a biasing member that biases the movable ring 44 downward (press direction) between the second forging die base 38 and the movable ring 44. Then, before the outer edge portion 44o of the lower surface of the movable ring 44 contacts the outer edge portion 30o of the upper surface of the first forging die 30, the outer edge portion 44o of the lower surface of the movable ring 44 has a biasing force of the plurality of springs 52 or In this state, the movable ring 44 protrudes downward with respect to the punch 40 due to its own weight.
 次に、本実施形態に係るブリスク中間品18の製造方法について図3から図7Aを参照して説明する。 Next, a method for manufacturing the blisk intermediate product 18 according to this embodiment will be described with reference to FIGS. 3 to 7A.
 本実施形態に係るブリスク中間品18の製造方法は、加熱工程と、セット工程と、押出鍛造工程と、取出工程とを含む。そして、本実施形態に係るブリスク中間品18の製造方法における各工程の具体的な内容は、次の通りである。 The manufacturing method of the blisk intermediate product 18 according to the present embodiment includes a heating process, a setting process, an extrusion forging process, and a removal process. And the specific content of each process in the manufacturing method of the blisk intermediate product 18 which concerns on this embodiment is as follows.
 (i)加熱工程
 チタン合金等からなる金属ブロックMを、加熱炉(図示省略)を用いて、例えば800℃以上の高温に予め加熱する。また、金属ブロックMを予め加熱する他に、第1鍛造金型30及び第2鍛造金型34を、ヒータ(図示省略)を用いて、例えば200℃以上の高温に予め加熱するようにしてもよい。
(i) Heating step The metal block M made of a titanium alloy or the like is preheated to a high temperature of, for example, 800 ° C. or higher using a heating furnace (not shown). In addition to preheating the metal block M, the first forging die 30 and the second forging die 34 may be preheated to a high temperature of, for example, 200 ° C. or higher using a heater (not shown). Good.
 (ii)セット工程
 加熱工程の終了後に、例えば、グラファイト等の離型剤を、第1ディスク成形面30d、第1動翼成形面30b、第2ディスク成形面40d、及び、第2動翼成形面44bに塗布することにより、離型処理を第1鍛造金型30及び第2鍛造金型34に対して施す。そして、図3に示すように、セットピン36を金属ブロックMの穴部Mhに挿通させて、金属ブロックMを第1鍛造金型30の第1ディスク成形面30dにセットする。換言すれば、金属ブロックMを第1鍛造金型30の第1ディスク成形面30dと第2鍛造金型34の第2ディスク成形面40dとの間にセットする。
(ii) Setting step After the heating step, for example, a release agent such as graphite is used to form the first disk forming surface 30d, the first blade forming surface 30b, the second disk forming surface 40d, and the second blade forming. By applying to the surface 44 b, a mold release process is performed on the first forging die 30 and the second forging die 34. Then, as shown in FIG. 3, the set pin 36 is inserted through the hole Mh of the metal block M, and the metal block M is set on the first disk forming surface 30 d of the first forging die 30. In other words, the metal block M is set between the first disk forming surface 30 d of the first forging die 30 and the second disk forming surface 40 d of the second forging die 34.
 (iii)押出鍛造工程
 セット工程の終了後に、図4に示すように、プレス機械を駆動して、ラム32をプレス方向(下方向)へ移動させることにより、第2鍛造金型34をラム32と一体的にプレス方向へ移動させて、第1鍛造金型30に対して近接させる。これにより、可動リング44の下面の外縁部44oを第1鍛造金型30の上面の外縁部30oに接触させて、第2動翼成形面44bを第1動翼成形面30bに局所的に接触させることができる。
(iii) Extrusion forging process After the setting process is completed, the second forging die 34 is moved to the ram 32 by driving the press machine and moving the ram 32 in the pressing direction (downward) as shown in FIG. And move in the pressing direction so as to be close to the first forging die 30. Thereby, the outer edge portion 44o on the lower surface of the movable ring 44 is brought into contact with the outer edge portion 30o on the upper surface of the first forging die 30, and the second blade forming surface 44b is locally in contact with the first blade forming surface 30b. Can be made.
 そして、ラム32をプレス方向へ更に移動させることにより、パンチ40を可動リング44に対して相対的にプレス方向へ移動させて、パンチ40の下部(第2ディスク成形面40d)を可動リング44の下面の外縁部44oに対してプレス方向へ突出させる。すると、図5及び図7Aに示すように、パンチ40によって金属ブロックMをプレス方向へ押圧し、かつ、第1動翼成形面30bと第2動翼成形面44bとを局所的に接触させた状態で、第1鍛造金型30と第2鍛造金型34との協働によって金属ブロックMをプレス方向に直交する放射方向(半径方向)へ押出鍛造することができる。これにより、金属ブロックMにディスク相当部20を成形し、かつ、金属ブロックMに複数の動翼相当部24を押出成形することができる。換言すれば、金属ブロックMから、ディスク相当部20と複数の動翼相当部24とを有するブリスク中間品18を製造することができる。 Then, by further moving the ram 32 in the pressing direction, the punch 40 is moved in the pressing direction relative to the movable ring 44, and the lower part (second disk forming surface 40 d) of the punch 40 is moved to the movable ring 44. It protrudes in the pressing direction with respect to the outer edge portion 44o of the lower surface. Then, as shown in FIGS. 5 and 7A, the metal block M was pressed in the pressing direction by the punch 40, and the first blade forming surface 30b and the second blade forming surface 44b were brought into local contact with each other. In this state, the metal block M can be extrusion-forged in the radial direction (radial direction) perpendicular to the pressing direction by the cooperation of the first forging die 30 and the second forging die 34. As a result, the disk equivalent portion 20 can be formed on the metal block M, and the plurality of blade equivalent portions 24 can be extruded on the metal block M. In other words, the blisk intermediate product 18 having the disk equivalent part 20 and the plurality of blade equivalent parts 24 can be manufactured from the metal block M.
 (iv)取出工程
 押出鍛造工程の終了後に、図6に示すように、プレス機械を駆動して、ラム32をプレス方向の反対方向(上方向)へ移動させることにより、第2鍛造金型34をラム32と一体的にプレス方向の反対方向へ移動させて、第1鍛造金型30に対して離反させる。そして、ブリスク中間品18を動翼相当部24の捻りに応じて回転させながら、ブリスク中間品18を第1鍛造金型30から取り出す。
(iv) Extraction Process After the extrusion forging process is completed, as shown in FIG. 6, the press machine is driven to move the ram 32 in the direction opposite to the pressing direction (upward direction), whereby the second forging die 34 is moved. Is moved away from the first forging die 30 by moving the ram 32 in the direction opposite to the pressing direction. Then, the blisk intermediate product 18 is taken out from the first forging die 30 while the blisk intermediate product 18 is rotated according to the twist of the rotor blade equivalent portion 24.
 以上により、本実施形態に係るブリスク中間品18の製造方法が完了し、金属ブロックMから、ディスク相当部20と複数の動翼相当部24とを有するブリスク中間品18を製造することができる。 Thus, the manufacturing method of the blisk intermediate product 18 according to the present embodiment is completed, and the blisk intermediate product 18 having the disk equivalent part 20 and the plurality of blade equivalent parts 24 can be manufactured from the metal block M.
 なお、ブリスク中間品18を第1鍛造金型30から取り出した後(取出工程の終了後)に、ディスク用の切削工具(例えば、バイト等)を用いて、ディスク相当部20に対して旋削(切削の1つ)を行うことにより、ディスク相当部20をディスク12に仕上げる。また、動翼用の切削工具(例えば、エンドミル等)を用いて、各動翼相当部24に対して転削(切削の1つ)を行うことにより、各動翼相当部24を動翼16に仕上げる。これにより、ブリスク中間品18を製品形状のブリスク10に最終的に仕上げることができる。 After the blisk intermediate product 18 is taken out from the first forging die 30 (after the take-out process is completed), the disc equivalent portion 20 is turned (using a cutting tool for a disc (for example, a bite)) ( The disk equivalent portion 20 is finished into the disk 12 by performing one of the cutting operations. Further, by using a cutting tool for moving blades (for example, an end mill or the like), each moving blade corresponding portion 24 is moved to the moving blade 16 by performing rolling (one of cutting) on each moving blade corresponding portion 24. Finish. Thereby, the blisk intermediate product 18 can be finally finished into the product-shaped blisk 10.
 次に、本実施形態の作用及び効果について説明する。 Next, functions and effects of this embodiment will be described.
 鍛造金型ユニット26を用いて、金属ブロックMを押出鍛造することにより、金属ブロックMにディスク相当部20を成形し、かつ、金属ブロックMに複数の動翼相当部24を押出成形することができる。換言すれば、金属ブロックMに対して切削加工を行うことなく、ブリスク中間品18を金属ブロックMから製造することができる。これにより、投入材料としての金属ブロックMの体積とブリスク10の体積との差を小さくすると共に、ブリスク10の製造に必要な切削量(投入材料の切削量)を大幅に減らすことができる。 By forging the metal block M using the forging die unit 26, the disk equivalent part 20 is formed on the metal block M, and the plurality of moving blade equivalent parts 24 are extruded on the metal block M. it can. In other words, the blisk intermediate product 18 can be manufactured from the metal block M without cutting the metal block M. As a result, the difference between the volume of the metal block M as the input material and the volume of the blisk 10 can be reduced, and the cutting amount necessary for manufacturing the blisk 10 (the cutting amount of the input material) can be greatly reduced.
 従って、本実施形態によれば、前述のように、投入材料としての金属ブロックMの体積とブリスク10の体積との差を小さくすることができる。そのため、ブリスク10の材料コストの増大を抑えて、ブリスク10の低コスト化を図ることができる。 Therefore, according to the present embodiment, as described above, the difference between the volume of the metal block M as the input material and the volume of the blisk 10 can be reduced. Therefore, the increase in material cost of the blisk 10 can be suppressed, and the cost of the blisk 10 can be reduced.
 また、本実施形態によれば、前述のように、ブリスク10の製造に必要な切削量を大幅に減らすことができる。そのため、ブリスク10の製造時間を大幅に短縮して、ブリスク10の生産性を十分に高めると共に、切削工具の消耗を十分に抑制することができる。 Further, according to the present embodiment, as described above, the amount of cutting necessary for manufacturing the blisk 10 can be greatly reduced. Therefore, the manufacturing time of the blisk 10 can be greatly shortened, the productivity of the blisk 10 can be sufficiently increased, and consumption of the cutting tool can be sufficiently suppressed.
 つまり、本実施形態によれば、ブリスク10の低コスト化を図った上で、ブリスク10の生産性を十分に高めると共に、切削工具の消耗を十分に抑制することができる。 That is, according to the present embodiment, the cost of the blisk 10 can be reduced, the productivity of the blisk 10 can be sufficiently increased, and consumption of the cutting tool can be sufficiently suppressed.
 次に、本開示の実施形態の変形例について図7B及び図8を参照して説明する。 Next, a modified example of the embodiment of the present disclosure will be described with reference to FIGS. 7B and 8.
 図7Bに示すように、押出鍛造工程では、第1動翼成形面30bと第2動翼成形面44bとが非接触の状態で、第1鍛造金型30と第2鍛造金型34との協働によって金属ブロックMを放射方向へ押出鍛造するようにしてもよい(図5参照)。換言すれば、第2動翼成形面44bは、可動リング44の下面の外縁部44oが第1鍛造金型30の上面の外縁部30oに接触したときに、第1動翼成形面30bに非接触になるように形成されていてもよい(図7B参照)。本開示の実施形態の変形例に係るブリスク中間品18Aの製造方法を実施することにより、図8に示すように、ディスク相当部20及び複数の動翼相当部24に加えて、各隣接する一対の動翼相当部24間にブリッジ54をさらに有するブリスク中間品18Aを製造することが可能になる。 As shown in FIG. 7B, in the extrusion forging process, the first forging die 30 and the second forging die 34 are in contact with each other in a state where the first moving blade forming surface 30b and the second moving blade forming surface 44b are not in contact with each other. The metal block M may be extrusion-forged in the radial direction by cooperation (see FIG. 5). In other words, the second moving blade forming surface 44b is not in contact with the first moving blade forming surface 30b when the outer edge portion 44o of the lower surface of the movable ring 44 contacts the outer edge portion 30o of the upper surface of the first forging die 30. You may form so that it may contact (refer FIG. 7B). By performing the manufacturing method of the blisk intermediate product 18A according to the modification of the embodiment of the present disclosure, as shown in FIG. 8, in addition to the disk equivalent portion 20 and the plurality of blade equivalent portions 24, each adjacent pair It is possible to manufacture the blisk intermediate product 18 </ b> A further having a bridge 54 between the rotor blade equivalent parts 24.
 なお、図8に示すブリスク中間品18Aは、前述の点を除き、図2に示すブリスク中間品18と同様の構成を有する。ブリスク中間品18Aにおける各構成要素については、図中にブリスク中間品18における対応する構成要素と同一符号を付して、その説明を省略している。 The blisk intermediate product 18A shown in FIG. 8 has the same configuration as the blisk intermediate product 18 shown in FIG. About each component in Blisk intermediate product 18A, the same code | symbol as the corresponding component in Blisk intermediate product 18 is attached | subjected in the figure, and the description is abbreviate | omitted.
 そして、本開示の実施形態の変形例においても、本開示の実施形態と同様の作用及び効果を奏するものである。 And also in the modified example of the embodiment of the present disclosure, the same operation and effect as the embodiment of the present disclosure are exhibited.
 このように、本開示は、ここでは記載していない様々な実施の形態などを含むことは勿論である。従って、本開示の技術的範囲は、上述の説明から妥当な特許請求の範囲に係る発明特定事項によってのみ定められる。 Thus, it is needless to say that the present disclosure includes various embodiments that are not described herein. Therefore, the technical scope of the present disclosure is defined only by the invention specifying matters according to the scope of claims reasonable from the above description.

Claims (11)

  1.  削り代を含みかつブリスクのディスクに相当する円形状のディスク相当部と、前記ディスク相当部の外周面にその周方向に沿って間隔を置いて設置されかつ削り代を含みかつ前記ブリスクの動翼に相当する複数の動翼相当部とを有するブリスク中間品を製造するための方法であって、
     前記ブリスク中間品の軸方向の一方側の形状に対応する形状の第1成形面を有する第1鍛造金型と、前記ブリスク中間品の軸方向の他方側の形状に対応する形状の第2成形面を有する第2鍛造金型とを含む鍛造金型ユニットを用い、前記第1鍛造金型の前記第1成形面と前記第2鍛造金型の前記第2成形面との間に、前記ブリスクの構成材料である金属ブロックをセットするセット工程と、
     前記セット工程の終了後に、前記第2鍛造金型をプレス方向へ移動させることにより、前記第2鍛造金型によって前記金属ブロックを前記プレス方向へ押圧し、かつ、前記第1鍛造金型と前記第2鍛造金型との協働によって前記金属ブロックを前記プレス方向に直交する放射方向へ押出鍛造する押出鍛造工程と、を有するブリスク中間品の製造方法。
    A circular disk equivalent part including a machining allowance and corresponding to a blisk disk, and an outer peripheral surface of the disk equivalent part disposed at intervals along the circumferential direction and including a machining allowance and the blade of the blisk A method for producing a blisk intermediate product having a plurality of rotor blade equivalent parts corresponding to
    A first forging die having a first molding surface having a shape corresponding to the shape on one side in the axial direction of the blisk intermediate product, and a second molding having a shape corresponding to the shape on the other side in the axial direction of the blisk intermediate product. A forging die unit including a second forging die having a surface, and the blisk between the first forming surface of the first forging die and the second forming surface of the second forging die. A setting step of setting a metal block that is a constituent material of
    After the setting step, the second forging die is moved in the pressing direction to press the metal block in the pressing direction with the second forging die, and the first forging die and the An extrusion forging process for extruding and forging the metal block in a radial direction orthogonal to the pressing direction in cooperation with a second forging die.
  2.  前記第1成形面は、前記ディスク相当部の軸方向の一方側の形状に対応する第1ディスク成形面と、複数の前記動翼相当部の背面又は腹面を含む形状に対応する第1動翼成形面と、を含み、
     前記第2成形面は、前記ディスク相当部の軸方向の他方側の形状に対応する第2ディスク成形面と、複数の前記動翼相当部の腹面又は背面を含む形状に対応する第2動翼成形面と、を含む請求項1に記載のブリスク中間品の製造方法。
    The first molding surface corresponds to a shape including a first disk molding surface corresponding to the shape of one side in the axial direction of the disk equivalent portion, and a back surface or abdominal surface of the plurality of blade equivalent portions. A molding surface, and
    The second molding surface corresponds to a shape including a second disk molding surface corresponding to the shape of the other side in the axial direction of the disk equivalent portion and a plurality of bellows or back surfaces of the plurality of blade equivalent portions. The manufacturing method of the blisk intermediate product of Claim 1 containing a molding surface.
  3.  前記第2鍛造金型は、前記第2ディスク成形面を有するパンチと、前記パンチの半径方向外側に位置しかつ前記パンチに対して前記プレス方向及びその反対方向へ移動可能でありかつ前記第2動翼成形面を有する可動リングと、を有する請求項2に記載のブリスク中間品の製造方法。 The second forging die is located on the radially outer side of the punch having the second disk forming surface and is movable in the pressing direction and the opposite direction with respect to the punch. The method for manufacturing a blisk intermediate product according to claim 2, further comprising a movable ring having a moving blade forming surface.
  4.  前記押出鍛造工程では、前記第2鍛造金型を前記プレス方向へ移動させることにより、前記可動リングを前記第1鍛造金型に接触させ、続いて、前記パンチを前記可動リングに対して相対的に前記プレス方向へ移動させることにより、前記パンチによって前記金属ブロックを前記プレス方向へ押圧する請求項3記載のブリスク中間品の製造方法。 In the extrusion forging process, the movable ring is brought into contact with the first forging die by moving the second forging die in the pressing direction, and then, the punch is relative to the movable ring. The manufacturing method of the blisk intermediate product of Claim 3 which presses the said metal block to the said press direction with the said punch by moving to the said press direction.
  5.  前記押出鍛造工程では、前記第1動翼成形面と前記第2動翼成形面とを局所的に接触させた状態で、前記第1鍛造金型と前記第2鍛造金型との協働によって前記金属ブロックを前記放射方向へ押出鍛造する請求項2から請求項4のうちのいずれか1項に記載のブリスク中間品の製造方法。 In the extrusion forging step, with the first forging die and the second forging die cooperating in a state where the first moving blade forming surface and the second moving blade forming surface are in local contact with each other. The method for manufacturing a blisk intermediate product according to any one of claims 2 to 4, wherein the metal block is extrusion-forged in the radial direction.
  6.  前記押出鍛造工程では、前記第1動翼成形面と前記第2動翼成形面とが非接触の状態で、前記第1鍛造金型と前記第2鍛造金型との協働によって前記金属ブロックを前記放射方向へ押出鍛造する請求項2から請求項4のうちのいずれか1項に記載のブリスク中間品の製造方法。 In the extrusion forging step, the metal block is formed by the cooperation of the first forging die and the second forging die while the first moving blade forming surface and the second moving blade forming surface are not in contact with each other. The method for manufacturing a blisk intermediate product according to any one of claims 2 to 4, wherein the steel is extruded and forged in the radial direction.
  7.  前記押出鍛造工程の終了後に、前記第2鍛造金型を前記プレス方向の反対方向へ移動させることにより、前記第2鍛造金型を前記第1鍛造金型に対して離反させ、続いて、前記第1鍛造金型から前記ブリスク中間品を取り出す取出工程を有する請求項1から請求項6のうちのいずれか1項に記載のブリスク中間品の製造方法。 After completion of the extrusion forging process, the second forging die is moved away from the first forging die by moving the second forging die in the direction opposite to the pressing direction, and then, The method for manufacturing a blisk intermediate product according to any one of claims 1 to 6, further comprising a step of taking out the blisk intermediate product from the first forging die.
  8.  前記セット工程の開始前に、前記金属ブロックを加熱する加熱工程を有する請求項1から請求項7のうちのいずれか1項に記載のブリスク中間品の製造方法。 The manufacturing method of a blisk intermediate product according to any one of claims 1 to 7, further comprising a heating step of heating the metal block before the start of the setting step.
  9.  削り代を含みかつブリスクのディスクに相当する円形状のディスク相当部と、前記ディスク相当部の外周面にその周方向に沿って間隔を置いて設置されかつ削り代を含みかつ前記ブリスクの動翼に相当する複数の動翼相当部とを有するブリスク中間品を製造するために用いられる鍛造金型ユニットであって、
     前記ブリスク中間品の軸方向の一方側の形状に対応する形状の第1成形面を有する第1鍛造金型と、
     前記ブリスク中間品の軸方向の他方側の形状に対応する形状の第2成形面を有する第2鍛造金型と、を有する鍛造金型ユニット。
    A circular disk equivalent part including a machining allowance and corresponding to a blisk disk, and an outer peripheral surface of the disk equivalent part disposed at intervals along the circumferential direction and including a machining allowance and the blade of the blisk A forging die unit used for manufacturing a blisk intermediate product having a plurality of rotor blade equivalent parts corresponding to
    A first forging die having a first molding surface having a shape corresponding to the shape of one side of the blisk intermediate product in the axial direction;
    A forging die unit having a second forging die having a second molding surface having a shape corresponding to the shape of the other side in the axial direction of the blisk intermediate product.
  10.  前記第1鍛造金型の前記第1成形面は、前記ディスク相当部の軸方向の一方側の形状に対応する第1ディスク成形面と、複数の前記動翼相当部の背面又は腹面を含む形状に対応する第1動翼成形面と、を含み、
     前記第2鍛造金型は、前記ディスク相当部の軸方向の他方側の形状に対応する第2ディスク成形面と、複数の前記動翼相当部の腹面又は背面を含む形状に対応する第2動翼成形面と、を含む請求項9に記載の鍛造金型ユニット。
    The first molding surface of the first forging die includes a first disk molding surface corresponding to the shape of one side in the axial direction of the disk equivalent portion and a back surface or abdominal surface of the plurality of blade equivalent portions. A first blade forming surface corresponding to
    The second forging die has a second movement corresponding to a shape including a second disk forming surface corresponding to the shape of the other side in the axial direction of the disk equivalent portion and a plurality of belly surfaces or back surfaces of the plurality of blade equivalent portions. The forged die unit according to claim 9, comprising a blade forming surface.
  11.  前記第2鍛造金型は、前記第2ディスク成形面を有するパンチと、前記パンチの半径方向外側に位置しかつ前記パンチに対してプレス方向及びその反対方向へ移動可能であってかつ前記第2動翼成形面を有する可動リングと、を有する請求項10に記載の鍛造金型ユニット。 The second forging die is a punch having the second disk forming surface, is located on the radially outer side of the punch and is movable in the pressing direction and the opposite direction with respect to the punch, and the second The forging die unit according to claim 10, further comprising a movable ring having a moving blade forming surface.
PCT/JP2017/001351 2016-01-25 2017-01-17 Method for producing blisk intermediate product, and forging die unit WO2017130787A1 (en)

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CN116078989A (en) * 2023-01-03 2023-05-09 合肥工业大学 Double-performance-disc hot die forging-differential temperature compression-torsion composite forming method and die tool

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WO2021038848A1 (en) 2019-08-30 2021-03-04 ヤマザキマザック株式会社 Integrally bladed rotor manufacturing method, blade cutting program for same, and integrally bladed rotor
JP7372217B2 (en) 2020-08-03 2023-10-31 本田技研工業株式会社 Drive disk manufacturing equipment
CN113510207B (en) * 2021-04-27 2023-03-31 中国第二重型机械集团德阳万航模锻有限责任公司 Manufacturing method of TC17 titanium alloy large-size variable-section blisk forged piece

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RU2769333C1 (en) * 2021-04-16 2022-03-30 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Method and device for stamping blings
CN116078989A (en) * 2023-01-03 2023-05-09 合肥工业大学 Double-performance-disc hot die forging-differential temperature compression-torsion composite forming method and die tool

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