JP6618527B2 - ターボマシン部材リング支持体の製造方法 - Google Patents
ターボマシン部材リング支持体の製造方法 Download PDFInfo
- Publication number
- JP6618527B2 JP6618527B2 JP2017510507A JP2017510507A JP6618527B2 JP 6618527 B2 JP6618527 B2 JP 6618527B2 JP 2017510507 A JP2017510507 A JP 2017510507A JP 2017510507 A JP2017510507 A JP 2017510507A JP 6618527 B2 JP6618527 B2 JP 6618527B2
- Authority
- JP
- Japan
- Prior art keywords
- shroud
- manufacturing
- ring support
- conical
- support
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000004519 manufacturing process Methods 0.000 title claims description 21
- 238000000034 method Methods 0.000 title claims description 11
- 238000003754 machining Methods 0.000 claims description 11
- 238000007789 sealing Methods 0.000 claims description 9
- 238000005452 bending Methods 0.000 claims description 8
- 238000005520 cutting process Methods 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 238000003466 welding Methods 0.000 claims description 4
- 238000003801 milling Methods 0.000 claims description 3
- 230000000630 rising effect Effects 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 2
- 238000013461 design Methods 0.000 description 3
- 238000005219 brazing Methods 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/16—Making other particular articles rings, e.g. barrel hoops
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
- B21D22/02—Stamping using rigid devices or tools
- B21D22/06—Stamping using rigid devices or tools having relatively-movable die parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/92—Making other particular articles other parts for aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K3/00—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/25—Manufacture essentially without removing material by forging
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Automatic Assembly (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Forging (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
Description
2 密封ライニング
3 外側取付レール
4,5 突出カラー
6 中間陥没部
7 取付レール
8 平坦プレート
9 円筒シュラウド
10 二重円錐シュラウド
11 ジョー
12 静止リング
12a,12b ステージ
13 内面
14 外面
15 凹部
16 溝部
17 カラー
19 支持体
20 端部
21 中央部
22 作業部
23 中央円錐ブローチ
25,26 プレート
27 スリット
Claims (8)
- タービンのようなターボマシンの部材のためのリング支持体(19)を製造する方法であって、
密封ライニング(2)が内面に装着されて前記内面と反対の外面に取付レールが装着される角度セクタの周囲に前記リング支持体が延在し、前記リング支持体(19)から径方向外向き方向に立ち上がるカラー(17)により限定される陥没部(16)を前記取付レールが含む、前記リング支持体の製造方法であって、
前記内面と前記外面との間の距離に等しい厚さを持つ少なくとも1枚の平面金属プレート(8)から始めることと、
単数または複数の前記平面金属プレートを一緒に曲げて溶接し閉環の円筒シュラウド(9)を形成することと、
前記円筒シュラウドを工具で曲げて円錐シュラウド(10)を形成することと、ここで、前記円錐シュラウド(10)の軸が前記ターボマシンの長手軸方向に沿っており、
前記円錐シュラウドの外面(14)を機械加工して前記取付レールをその上に形成することと、
前記円錐シュラウドを切断して前記リング支持体(19)に対応するセクタに分割することと、
を含むことを特徴とする、製造方法。 - 曲げと成形とで構成されるステップが低温で行われることを特徴とする、請求項1に記載の製造方法。
- 前記円筒シュラウドが成形される前記工具が、径方向拡張部を伴うジョー(11)の円形列と、前記円形列を囲繞する外側静止リング(12)とを包含することを特徴とする、請求項1または2に記載の製造方法。
- 前記円筒シュラウド(9)が、2回のジョー拡張部通過の際に前記工具で成形され、2回の拡張部通過の間に前記ジョー(11)の間の角度ステップにより成形加工されることを特徴とする、請求項3に記載の製造方法。
- 前記ジョーと前記静止リングとが正中面について対称な二重円錐輪郭を有し、前記円錐シュラウド(10)が二重円錐であることを特徴とする、請求項3または4に記載の製造方法。
- 前記リング支持体の前記内面(13)が表面エリアの大部分にわたって機械加工を受けないことを特徴とする、請求項1から5のいずれか一項に記載の製造方法。
- 前記円錐シュラウドの前記外面の機械加工が、前記取付レールを成形する旋削加工と、前記リング支持体(19)の中央部分での不連続なフライス加工作業部(22)とを包含することを特徴とする、請求項1から6のいずれか一項に記載の製造方法。
- 2枚または3枚の前記平面金属プレートが設けられることを特徴とする、請求項1から6のいずれか一項に記載の製造方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1458079A FR3025124B1 (fr) | 2014-08-28 | 2014-08-28 | Procede de fabrication de supports d'anneaux d'organe de turbomachine |
FR1458079 | 2014-08-28 | ||
PCT/FR2015/052275 WO2016030632A1 (fr) | 2014-08-28 | 2015-08-26 | Procede de fabrication de supports d'anneaux d'organe de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2017534467A JP2017534467A (ja) | 2017-11-24 |
JP6618527B2 true JP6618527B2 (ja) | 2019-12-11 |
Family
ID=52450264
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2017510507A Active JP6618527B2 (ja) | 2014-08-28 | 2015-08-26 | ターボマシン部材リング支持体の製造方法 |
Country Status (9)
Country | Link |
---|---|
US (1) | US10773296B2 (ja) |
EP (1) | EP3194111B1 (ja) |
JP (1) | JP6618527B2 (ja) |
CN (1) | CN106794506B (ja) |
BR (1) | BR112017003922B1 (ja) |
CA (1) | CA2958662C (ja) |
FR (1) | FR3025124B1 (ja) |
RU (1) | RU2688102C2 (ja) |
WO (1) | WO2016030632A1 (ja) |
Families Citing this family (7)
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US10774670B2 (en) * | 2017-06-07 | 2020-09-15 | General Electric Company | Filled abradable seal component and associated methods thereof |
US10724390B2 (en) * | 2018-03-16 | 2020-07-28 | General Electric Company | Collar support assembly for airfoils |
FR3079151B1 (fr) * | 2018-03-23 | 2020-10-30 | Safran Aircraft Engines | Optimisation des supportages pour la fabrication additive de piece avec un evidement |
CN112122514A (zh) * | 2020-08-18 | 2020-12-25 | 湖北红业建材科技开发有限公司 | 一种钢筋混凝土井盖抱箍定型装置及定型方法 |
CN112276490B (zh) * | 2020-10-22 | 2022-07-19 | 航天科工哈尔滨风华有限公司 | 一种大型铸造不锈钢翼舱融合舱段加工方法 |
CN112475797B (zh) * | 2020-11-13 | 2022-12-09 | 中国船舶重工集团公司第七0七研究所 | 一种面向转子填充块的高效加工工艺方法 |
CN117816882B (zh) * | 2024-03-06 | 2024-05-03 | 江苏圣贤锻造有限责任公司 | 一种石化压力容器管板锻造设备及工艺 |
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2014
- 2014-08-28 FR FR1458079A patent/FR3025124B1/fr active Active
-
2015
- 2015-08-26 CA CA2958662A patent/CA2958662C/fr active Active
- 2015-08-26 JP JP2017510507A patent/JP6618527B2/ja active Active
- 2015-08-26 US US15/505,967 patent/US10773296B2/en active Active
- 2015-08-26 WO PCT/FR2015/052275 patent/WO2016030632A1/fr active Application Filing
- 2015-08-26 EP EP15771168.0A patent/EP3194111B1/fr active Active
- 2015-08-26 BR BR112017003922-2A patent/BR112017003922B1/pt active IP Right Grant
- 2015-08-26 CN CN201580046410.2A patent/CN106794506B/zh active Active
- 2015-08-26 RU RU2017109884A patent/RU2688102C2/ru active
Also Published As
Publication number | Publication date |
---|---|
FR3025124B1 (fr) | 2016-09-30 |
RU2688102C2 (ru) | 2019-05-17 |
WO2016030632A1 (fr) | 2016-03-03 |
US20170274441A1 (en) | 2017-09-28 |
FR3025124A1 (fr) | 2016-03-04 |
BR112017003922A2 (pt) | 2018-03-06 |
CA2958662C (fr) | 2022-07-26 |
RU2017109884A (ru) | 2018-09-28 |
BR112017003922B1 (pt) | 2022-11-01 |
JP2017534467A (ja) | 2017-11-24 |
EP3194111B1 (fr) | 2018-05-16 |
CN106794506A (zh) | 2017-05-31 |
CA2958662A1 (fr) | 2016-03-03 |
US10773296B2 (en) | 2020-09-15 |
RU2017109884A3 (ja) | 2019-01-17 |
EP3194111A1 (fr) | 2017-07-26 |
CN106794506B (zh) | 2019-01-08 |
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