IT8423478A0 - Elemento di spessore resistente alla corrosione per unire elettricamente materiali incompatibili. - Google Patents
Elemento di spessore resistente alla corrosione per unire elettricamente materiali incompatibili.Info
- Publication number
- IT8423478A0 IT8423478A0 IT8423478A IT2347884A IT8423478A0 IT 8423478 A0 IT8423478 A0 IT 8423478A0 IT 8423478 A IT8423478 A IT 8423478A IT 2347884 A IT2347884 A IT 2347884A IT 8423478 A0 IT8423478 A0 IT 8423478A0
- Authority
- IT
- Italy
- Prior art keywords
- corrosion
- incompatible materials
- electrically joining
- thick element
- resistant thick
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/043—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
- B32B2307/202—Conductive
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/714—Inert, i.e. inert to chemical degradation, corrosion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12431—Foil or filament smaller than 6 mils
- Y10T428/12438—Composite
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12556—Organic component
- Y10T428/12569—Synthetic resin
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/12743—Next to refractory [Group IVB, VB, or VIB] metal-base component
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Prevention Of Electric Corrosion (AREA)
- Preventing Corrosion Or Incrustation Of Metals (AREA)
- Connections Effected By Soldering, Adhesion, Or Permanent Deformation (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/549,388 US4478915A (en) | 1983-11-07 | 1983-11-07 | Corrosion resistant shim for electrically joining incompatible materials |
Publications (3)
Publication Number | Publication Date |
---|---|
IT8423478A0 true IT8423478A0 (it) | 1984-11-07 |
IT8423478A1 IT8423478A1 (it) | 1986-05-07 |
IT1178622B IT1178622B (it) | 1987-09-09 |
Family
ID=24192820
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT23478/84A IT1178622B (it) | 1983-11-07 | 1984-11-07 | Elemento di spessore resistente alla corrosione per unire elettricamente materiali incompatibili |
Country Status (6)
Country | Link |
---|---|
US (1) | US4478915A (it) |
BR (1) | BR8405632A (it) |
CA (1) | CA1245888A (it) |
DE (1) | DE3440360A1 (it) |
ES (1) | ES8606934A1 (it) |
IT (1) | IT1178622B (it) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4888451A (en) * | 1988-11-29 | 1989-12-19 | United Technologies Corporation | Electrical continuity means for composite joints |
US5489804A (en) * | 1989-08-28 | 1996-02-06 | Lsi Logic Corporation | Flexible preformed planar structures for interposing between a chip and a substrate |
US5299730A (en) * | 1989-08-28 | 1994-04-05 | Lsi Logic Corporation | Method and apparatus for isolation of flux materials in flip-chip manufacturing |
US5504035A (en) * | 1989-08-28 | 1996-04-02 | Lsi Logic Corporation | Process for solder ball interconnecting a semiconductor device to a substrate using a noble metal foil embedded interposer substrate |
US5834799A (en) * | 1989-08-28 | 1998-11-10 | Lsi Logic | Optically transmissive preformed planar structures |
DE69315352T2 (de) * | 1992-09-14 | 1998-04-09 | Cytec Technology Corp., West Paterson, N.J. | Verminderung der galvanischen zersetzung von metall/verbundwerkstoff hybridstrukturen |
US5401914A (en) * | 1993-02-03 | 1995-03-28 | The Curran Company | Vent for shielded enclosures |
FR2740380B1 (fr) * | 1995-10-30 | 1998-01-02 | Eurocopter France | Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere |
FR2740378B1 (fr) * | 1995-10-30 | 1998-01-02 | Eurocopter France | Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere, et pale a pas variable pouvant etre obtenue par un tel procede |
FR2740379B1 (fr) * | 1995-10-30 | 1998-01-02 | Eurocopter France | Procede de fabrication d'une pale en materiau composite pour rotor d'helicoptere, et pale pouvant etre obtenue par un tel procede |
US5770889A (en) * | 1995-12-29 | 1998-06-23 | Lsi Logic Corporation | Systems having advanced pre-formed planar structures |
JP3895437B2 (ja) * | 1997-09-19 | 2007-03-22 | 株式会社ジェイテクト | 動力舵取装置のハウジング構造 |
DE19823008A1 (de) * | 1998-05-22 | 1999-11-25 | Volkswagen Ag | Elektrisches Verbindungselement, insbesondere elektrisches Masseverbindungselement |
GB9919787D0 (en) | 1999-08-21 | 1999-10-27 | British Aerospace | Manufacture and assembly of structures |
EP1081043A1 (en) * | 1999-08-23 | 2001-03-07 | British Aerospace Public Limited Company | Manufacture and assembly of structures |
US6989608B2 (en) * | 2004-04-01 | 2006-01-24 | Atmel Corporation | Method and apparatus to eliminate galvanic corrosion on copper doped aluminum bond pads on integrated circuits |
US7611595B2 (en) * | 2006-02-01 | 2009-11-03 | Lockheed Martin Corporation | System, method, and apparatus for metallic-composite joint with compliant, non-corrosive interface |
US9393761B2 (en) * | 2013-03-15 | 2016-07-19 | The Boeing Company | Hybrid structure and methods for forming the same |
US10359383B2 (en) * | 2016-06-06 | 2019-07-23 | United Technologies Corporation | Method of detecting galvanic insulation integrity |
JP6130089B1 (ja) * | 2017-02-24 | 2017-05-17 | 伸和テクノス株式会社 | 第1部品の開口部を第2部品で覆う方法 |
US9964131B1 (en) * | 2017-04-28 | 2018-05-08 | The Boeing Company | Methods and apparatuses for providing corrosion protection to joined surfaces |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3052331A (en) * | 1959-09-03 | 1962-09-04 | Dow Chemical Co | Joint |
US3337711A (en) * | 1965-05-15 | 1967-08-22 | Janusz L A Garscia | Method of welding metal bodies separated by an adhesive layer |
US3613220A (en) * | 1969-11-25 | 1971-10-19 | Kaiser Aluminium Chem Corp | Method of forming transition insert material |
US4209889A (en) * | 1978-02-27 | 1980-07-01 | Olin Corporation | Corrosion resistant fastening system and method |
JPS56149780A (en) * | 1980-04-21 | 1981-11-19 | Sumitomo Electric Industries | Connecting composite plate |
-
1983
- 1983-11-07 US US06/549,388 patent/US4478915A/en not_active Expired - Lifetime
-
1984
- 1984-08-15 CA CA000461101A patent/CA1245888A/en not_active Expired
- 1984-11-05 DE DE19843440360 patent/DE3440360A1/de not_active Withdrawn
- 1984-11-05 BR BR8405632A patent/BR8405632A/pt not_active IP Right Cessation
- 1984-11-06 ES ES537398A patent/ES8606934A1/es not_active Expired
- 1984-11-07 IT IT23478/84A patent/IT1178622B/it active
Also Published As
Publication number | Publication date |
---|---|
IT8423478A1 (it) | 1986-05-07 |
IT1178622B (it) | 1987-09-09 |
DE3440360A1 (de) | 1985-05-15 |
BR8405632A (pt) | 1985-09-10 |
ES537398A0 (es) | 1986-05-16 |
US4478915A (en) | 1984-10-23 |
ES8606934A1 (es) | 1986-05-16 |
CA1245888A (en) | 1988-12-06 |
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