JP2018069335A - モノリシックな取り付け部材を有する多層構造を超塑性成形する方法 - Google Patents
モノリシックな取り付け部材を有する多層構造を超塑性成形する方法 Download PDFInfo
- Publication number
- JP2018069335A JP2018069335A JP2017157817A JP2017157817A JP2018069335A JP 2018069335 A JP2018069335 A JP 2018069335A JP 2017157817 A JP2017157817 A JP 2017157817A JP 2017157817 A JP2017157817 A JP 2017157817A JP 2018069335 A JP2018069335 A JP 2018069335A
- Authority
- JP
- Japan
- Prior art keywords
- precursor panel
- panel
- precursor
- multilayer structure
- edge
- 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.)
- Granted
Links
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
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
-
- 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
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/021—Deforming sheet bodies
-
- 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
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
- B21D26/055—Blanks having super-plastic properties
-
- 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
- B21D31/00—Other methods for working sheet metal, metal tubes, metal profiles
- B21D31/04—Expanding other than provided for in groups B21D1/00 - B21D28/00, e.g. for making expanded metal
-
- 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
- B21D47/00—Making rigid structural elements or units, e.g. honeycomb structures
- B21D47/04—Making rigid structural elements or units, e.g. honeycomb structures composite sheet metal profiles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
- B23K20/122—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
- B23K20/127—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding friction stir welding involving a mechanical connection
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/20—Bonding
- B23K26/21—Bonding by welding
- B23K26/22—Spot welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/20—Bonding
- B23K26/32—Bonding taking account of the properties of the material involved
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/36—Removing material
- B23K26/38—Removing material by boring or cutting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/36—Removing material
- B23K26/40—Removing material taking account of the properties of the material involved
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/006—Vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/08—Non-ferrous metals or alloys
- B23K2103/10—Aluminium or alloys thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/08—Non-ferrous metals or alloys
- B23K2103/14—Titanium or alloys thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/16—Composite materials, e.g. fibre reinforced
- B23K2103/166—Multilayered materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/18—Dissimilar materials
- B23K2103/26—Alloys of Nickel and Cobalt and Chromium
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Plasma & Fusion (AREA)
- Fluid Mechanics (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Abstract
【解決手段】縁部を有する前駆体パネルから多層構造10を形成する方法であって、取り付け部材20の縁部が前駆体パネルの縁部34と一線上に揃うように、取り付け部材を前駆体パネルに接続するステップと、熱およびガス圧を加えて、前駆体パネルを膨張させるステップと、を含む方法。
【選択図】図2
Description
Claims (14)
- 縁部(60,312)を有する前駆体パネル(50,300)から多層構造(10,350)を形成するための方法(100,200)であって、
取り付け部材(20)を前記前駆体パネルに接続することであって、前記取り付け部材の縁部(58)が前記前駆体パネルの前記縁部と一線上に揃うように、接続すること(108,206)と、
熱およびガス圧を加えて、前記前駆体パネルを膨張させること(112,210)と
を含む方法。 - 前記取り付け部材(20)を前記前駆体パネル(50,300)に接続すること(108,206)が、モノリシック本体(36,314)を含む取り付け部材を接続することを含む、請求項1に記載の方法(100,200)。
- 前記取り付け部材(20)を前記前駆体パネル(50,300)に接続すること(108,206)が、層状構造(52,302)を含む前駆体パネルを接続することを含む、請求項1または2に記載の方法(100,200)。
- 前記取り付け部材(20)を前記前駆体パネル(50,300)に接続すること(108,206)が、第1の表面層(14,306)と第2の表面層(16,308)との間に配置されたコア層(18,304)を含む前駆体パネルを接続することを含む、請求項1から3のいずれか一項に記載の方法(100,200)。
- 前記取り付け部材(20)を前記前駆体パネル(50,300)に接続すること(108,206)が、周囲(34,310)を含む前駆体パネルを接続することを含み、前記前駆体パネルの前記縁部(60)が、前記周囲の周りに延在する、請求項1から4のいずれか一項に記載の方法(100,200)。
- 前記取り付け部材(20)を前記前駆体パネル(50)に接続すること(108)が、凹部(54)を含む前駆体パネルを接続することを含み、前記前駆体パネルの前記縁部(60)が、前記凹部によって画定される、請求項1から5のいずれか一項に記載の方法(100,200)。
- 前記前駆体パネル(50)に前記凹部(54)を形成するステップ(104)をさらに含む、請求項6に記載の方法(100,200)。
- 前記熱およびガス圧を加えること(112,210)が、前記前駆体パネル(50,300)を加熱して、前記前駆体パネルを超塑性にすることを含む、請求項1から7のいずれか一項に記載の方法(100,200)。
- 前記熱およびガス圧を加えること(112,210)が、前記前駆体パネル(50,300)の内部容積(22)にガスを導入することを含む、請求項1から8のいずれか一項に記載の方法(100,200)。
- 前記熱およびガス圧を加えること(112,210)が、前記前駆体パネル(50,300)をツール(72,74)に押し付けることを含む、請求項1から9のいずれか一項に記載の方法(100,200)。
- 前記取り付け部材(20)にボア(40,352)を機械加工すること(114,212)をさらに含む、請求項1から10のいずれか一項に記載の方法(100,200)。
- 層状構造(52)を有する前駆体パネル(50)を含む多層構造(10)を形成するための方法(100)であって、
縁部(60)を画定する凹部(54)を前記前駆体パネルに形成すること(104)と、
モノリシック本体(36)を含む取り付け部材(20)を前記凹部に配置することであって、前記取り付け部材の縁部(58)が前記前駆体パネルの前記縁部と一線上に揃うように、配置すること(106)と、
前記取り付け部材を前記前駆体パネルに接続すること(108)と、
熱およびガス圧を加えて、前記前駆体パネルを膨張させること(112)と
を含む方法。 - 前記熱およびガス圧を加えること(112)が、前記前駆体パネル(50)を加熱して、前記前駆体パネルを超塑性にすることを含む、請求項12に記載の方法(100)。
- 請求項1から13のいずれか一項に記載の方法(100,200)により形成された多層構造(10,350)。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/256,958 | 2016-09-06 | ||
US15/256,958 US10189071B2 (en) | 2016-09-06 | 2016-09-06 | Method for superplastic forming a multilayer structure having a monolithic attachment member |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2018069335A true JP2018069335A (ja) | 2018-05-10 |
JP7001391B2 JP7001391B2 (ja) | 2022-01-19 |
Family
ID=61281834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2017157817A Active JP7001391B2 (ja) | 2016-09-06 | 2017-08-18 | モノリシックな取り付け部材を有する多層構造を超塑性成形する方法 |
Country Status (3)
Country | Link |
---|---|
US (1) | US10189071B2 (ja) |
JP (1) | JP7001391B2 (ja) |
CN (1) | CN107790540B (ja) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109227045B (zh) * | 2018-10-15 | 2020-06-23 | 中国航空制造技术研究院 | 三层空心结构成形方法 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002514975A (ja) * | 1998-04-07 | 2002-05-21 | ビーエイイー システムズ パブリック リミテッド カンパニー | 超塑性成形パネル |
US6419146B1 (en) * | 1996-01-12 | 2002-07-16 | The Boeing Company | Metal sandwich structure with integral hardpoint |
US20060249560A1 (en) * | 2005-05-06 | 2006-11-09 | The Boeing Company | Superplastically forming of friction welded structural assemblies |
JP2006334625A (ja) * | 2005-06-01 | 2006-12-14 | Fuji Heavy Ind Ltd | 超塑性・拡散接合パネルの成形方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6211497B1 (en) | 1991-04-05 | 2001-04-03 | The Boeing Company | Induction consolidation system |
US5728309A (en) | 1991-04-05 | 1998-03-17 | The Boeing Company | Method for achieving thermal uniformity in induction processing of organic matrix composites or metals |
US5645744A (en) | 1991-04-05 | 1997-07-08 | The Boeing Company | Retort for achieving thermal uniformity in induction processing of organic matrix composites or metals |
US5118026A (en) * | 1991-04-05 | 1992-06-02 | Rockwell International Corporation | Method for making titanium aluminide metallic sandwich structures |
US6180932B1 (en) | 1998-12-30 | 2001-01-30 | The Boeing Company | Brazing honeycomb panels with controlled net tooling pressure |
US6914225B2 (en) | 2003-06-18 | 2005-07-05 | The Boeing Company | Apparatus and methods for single sheet forming using induction heating |
GB2453308B (en) * | 2007-10-03 | 2012-07-25 | Acell Group Ltd | Composite products |
DE102010053959A1 (de) * | 2010-12-09 | 2012-06-14 | Daimler Ag | Verfahren zum Herstellen eines Verbundbauteils |
DE102012102286A1 (de) * | 2012-03-19 | 2013-09-19 | Thyssenkrupp Steel Europe Ag | Verfahren zum Verbinden eines Verbundblechs mit einem metallischen Substrat |
CN103551444B (zh) * | 2013-11-14 | 2016-05-11 | 深圳智慧能源技术有限公司 | 制造中空结构的方法 |
US10112229B2 (en) * | 2015-08-17 | 2018-10-30 | The Boeing Company | Apparatus and method for forming three-sheet panels |
-
2016
- 2016-09-06 US US15/256,958 patent/US10189071B2/en active Active
-
2017
- 2017-08-04 CN CN201710658884.3A patent/CN107790540B/zh active Active
- 2017-08-18 JP JP2017157817A patent/JP7001391B2/ja active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6419146B1 (en) * | 1996-01-12 | 2002-07-16 | The Boeing Company | Metal sandwich structure with integral hardpoint |
JP2002514975A (ja) * | 1998-04-07 | 2002-05-21 | ビーエイイー システムズ パブリック リミテッド カンパニー | 超塑性成形パネル |
US20060249560A1 (en) * | 2005-05-06 | 2006-11-09 | The Boeing Company | Superplastically forming of friction welded structural assemblies |
JP2006334625A (ja) * | 2005-06-01 | 2006-12-14 | Fuji Heavy Ind Ltd | 超塑性・拡散接合パネルの成形方法 |
Also Published As
Publication number | Publication date |
---|---|
CN107790540A (zh) | 2018-03-13 |
US10189071B2 (en) | 2019-01-29 |
CN107790540B (zh) | 2020-12-18 |
US20180065165A1 (en) | 2018-03-08 |
JP7001391B2 (ja) | 2022-01-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR100622041B1 (ko) | 금속 접합에 의해 부착되고 변형 가능한 격벽을 구비하는허니컴 코어 흡음 유닛 및 그 제조 방법 | |
US7048175B2 (en) | Friction welded structural assembly and preform and method for same | |
US5240376A (en) | SPF/DB hollow core fan blade | |
US7416105B2 (en) | Superplastically forming of friction welded structural assemblies | |
US5692881A (en) | Hollow metallic structure and method of manufacture | |
JP4516469B2 (ja) | 積層部接合方法 | |
US4549685A (en) | Method for superplastic forming and diffusion bonding Y shaped support structures | |
US5723225A (en) | Superplastically formed, diffusion bonded multiple sheet panels with web doublers and method of manufacture | |
US20020036057A1 (en) | Combined superplastic forming and adhesive bonding | |
JP6554263B2 (ja) | 超塑性成形され超音波溶接された金属構造体 | |
US8474684B2 (en) | Segmented mandrel for high temperature bonding of metallic axisymmetric shells having complex curvatures | |
US5289965A (en) | Method of superplastically forming and braze bonding a structure | |
EP3680038A1 (en) | Dual walled titanium tubing and method of manufacturing the tubing | |
JPH1147859A (ja) | アルミ合金パネルの製造方法 | |
JP2018069335A (ja) | モノリシックな取り付け部材を有する多層構造を超塑性成形する方法 | |
JP7025130B2 (ja) | サンドイッチ構造及び関連の圧力ベースの形成する方法 | |
TWM524261U (zh) | 複合空心板結構 | |
TWI609120B (zh) | 複合空心板結構及其製作方法 | |
Smirnov | Promising processes for shaping superplastic materials | |
JPS59178244A (ja) | チタンと他金属との複層体 | |
TWM521542U (zh) | 複合物件 | |
Ascani et al. | New advancements in titanium technology and their cost and weight benefits | |
JPH03204186A (ja) | 1次構造多層荷重保持および絶縁部材 | |
TWM521543U (zh) | 複合金屬件 | |
TW201726275A (zh) | 複合金屬件及其製作方法 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20200812 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20210525 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20210526 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20210823 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20211207 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20211224 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 7001391 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |