BR102017019667A8 - Método e sistema para instalação de fixador - Google Patents

Método e sistema para instalação de fixador

Info

Publication number
BR102017019667A8
BR102017019667A8 BR102017019667A BR102017019667A BR102017019667A8 BR 102017019667 A8 BR102017019667 A8 BR 102017019667A8 BR 102017019667 A BR102017019667 A BR 102017019667A BR 102017019667 A BR102017019667 A BR 102017019667A BR 102017019667 A8 BR102017019667 A8 BR 102017019667A8
Authority
BR
Brazil
Prior art keywords
fastener
dies
less
hole
millimeters
Prior art date
Application number
BR102017019667A
Other languages
English (en)
Other versions
BR102017019667A2 (pt
BR102017019667B1 (pt
Inventor
Donald Hood William
Brian Peterson Donald
Leon Hayes Curtis
michael haworth Paul
James Kumley Tyler
Original Assignee
Boeing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of BR102017019667A2 publication Critical patent/BR102017019667A2/pt
Publication of BR102017019667A8 publication Critical patent/BR102017019667A8/pt
Publication of BR102017019667B1 publication Critical patent/BR102017019667B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/02—Riveting procedures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/02—Riveting procedures
    • B21J15/04—Riveting hollow rivets mechanically
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/10—Riveting machines
    • B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
    • B21J15/142—Aerospace structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/10—Riveting machines
    • B21J15/36—Rivet sets, i.e. tools for forming heads; Mandrels for expanding parts of hollow rivets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/38—Accessories for use in connection with riveting, e.g. pliers for upsetting; Hand tools for riveting
    • 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
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0605—Carbon
    • C23C14/0611—Diamond
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/221—Ion beam deposition
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/24—Vacuum evaporation
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/34—Sputtering
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/26—Deposition of carbon only
    • C23C16/27—Diamond only

Abstract

“MÉTODO, SISTEMA, E, APARELHO” Sistemas e métodos são providos para instalar fixadores. Uma modalidade de exemplo é um método que inclui inserir um fixador em um furo, e preender extremidades do fixador por intermédio de matrizes. Pelo menos uma das matrizes inclui um revestimento permanente tendo um coeficiente de fricção estático inferior a 0,2 em uma superfície contactando o fixador. O método inclui adicionalmente deformar plasticamente o fixador por intermédio de força a partir das matrizes, expandindo assim o fixador para a interferência com o furo ao longo de um comprimento do fixador de forma que uma quantidade de interferência entre o fixador e o furo ao longo do comprimento do fixador é maior que 0,0381 milímetros e menor que 0,0508 milímetros (um e meio milésimos de uma polegada e menor que vinte milésimos de uma polegada).
BR102017019667-4A 2016-11-29 2017-09-14 Método e sistema para instalação de fixador BR102017019667B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US15/364,208 US10377508B2 (en) 2016-11-29 2016-11-29 Enhanced tooling for interference-fit fasteners
US15/364,208 2016-11-29
US15/364208 2016-11-29

Publications (3)

Publication Number Publication Date
BR102017019667A2 BR102017019667A2 (pt) 2018-06-19
BR102017019667A8 true BR102017019667A8 (pt) 2022-08-30
BR102017019667B1 BR102017019667B1 (pt) 2023-01-31

Family

ID=60569633

Family Applications (1)

Application Number Title Priority Date Filing Date
BR102017019667-4A BR102017019667B1 (pt) 2016-11-29 2017-09-14 Método e sistema para instalação de fixador

Country Status (7)

Country Link
US (1) US10377508B2 (pt)
EP (1) EP3326730B1 (pt)
JP (1) JP7113610B2 (pt)
CN (1) CN108115076B (pt)
BR (1) BR102017019667B1 (pt)
ES (1) ES2874666T3 (pt)
RU (1) RU2750927C2 (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021191584A (ja) 2020-06-05 2021-12-16 三菱重工業株式会社 加締め装置および加締め方法
JP2022002857A (ja) * 2020-06-23 2022-01-11 三菱重工業株式会社 加締め装置および加締め方法
CN111977020B (zh) * 2020-07-06 2022-08-09 西安飞机工业（集团）有限责任公司 一种起落架减震支柱静摩擦力测试方法
CN113182483B (zh) * 2021-03-04 2023-02-10 浙江锦泰电子有限公司 一种降低内阻用的铆接机构

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DE727551C (de) * 1940-08-06 1942-11-05 Krupp Ag Doepper
US2654272A (en) * 1949-07-16 1953-10-06 Warren Walter Wallace Donald Riveting process
JPS4933054A (pt) * 1972-08-01 1974-03-26
JPS5715108A (en) * 1980-06-23 1982-01-26 Boeing Co Combining method of rivet and parts
JP2826827B2 (ja) * 1988-07-11 1998-11-18 ティーディーケイ株式会社 成形用スタンパーとその製造方法
US5680690A (en) * 1996-02-06 1997-10-28 Franklin S. Briles Coated rivet and deformation thereof
CA2301015C (en) * 1997-08-29 2003-06-03 Douglas A. Shore Riveting tool sheath and method to reduce marring of the workpiece
JP2000061706A (ja) * 1998-08-25 2000-02-29 Tokki Corp センタ
DE10018143C5 (de) 2000-04-12 2012-09-06 Oerlikon Trading Ag, Trübbach DLC-Schichtsystem sowie Verfahren und Vorrichtung zur Herstellung eines derartigen Schichtsystems
DE20013526U1 (de) * 2000-08-05 2000-12-07 Avdel Verbindungselemente Vorrichtung zum Verbinden von Blechen durch Stanznieten oder Durchsetzfügen
GB2383106B (en) * 2001-12-14 2004-09-15 Textron Fastening Syst Ltd Method of fastening
US8105660B2 (en) 2007-06-28 2012-01-31 Andrew W Tudhope Method for producing diamond-like carbon coatings using PECVD and diamondoid precursors on internal surfaces of a hollow component
JP5787094B2 (ja) * 2012-02-09 2015-09-30 三菱マテリアル株式会社 プレス加工用金型
CN103256287A (zh) * 2012-02-21 2013-08-21 富泰华工业（深圳）有限公司 铆合结构及其铆合工艺
KR20140021080A (ko) * 2012-07-16 2014-02-20 삼성전자주식회사 반도체 장치 및 그 제조 방법
JP6192521B2 (ja) * 2013-12-06 2017-09-06 三菱重工業株式会社 スウェージツール
DE102014204449A1 (de) * 2014-03-11 2015-09-17 Ejot Gmbh & Co. Kg Verfahren zum Verbinden von Bauteilen von denen eines aus einem faserverstärkten Kunststoff besteht
CN105081111B (zh) * 2015-07-21 2017-03-01 贵州航太精密制造有限公司 一种机械连接挤压装置

Also Published As

Publication number Publication date
ES2874666T3 (es) 2021-11-05
US10377508B2 (en) 2019-08-13
BR102017019667A2 (pt) 2018-06-19
CN108115076B (zh) 2021-02-05
RU2750927C2 (ru) 2021-07-06
EP3326730A1 (en) 2018-05-30
JP7113610B2 (ja) 2022-08-05
RU2017129372A (ru) 2019-02-18
CN108115076A (zh) 2018-06-05
BR102017019667B1 (pt) 2023-01-31
US20180148194A1 (en) 2018-05-31
RU2017129372A3 (pt) 2021-01-27
EP3326730B1 (en) 2021-03-31
JP2018122354A (ja) 2018-08-09

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Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]
B06W Patent application suspended after preliminary examination (for patents with searches from other patent authorities) chapter 6.23 patent gazette]
B03H Publication of an application: rectification [chapter 3.8 patent gazette]

Free format text: REFERENTE A RPI 2476 DE 19/06/2018, QUANTO AO ITEM (54).

B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 14/09/2017, OBSERVADAS AS CONDICOES LEGAIS