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MX2017014489A - Fijacion instalada de un solo lado. - Google Patents

Fijacion instalada de un solo lado.

Info

Publication number
MX2017014489A
MX2017014489A MX2017014489A MX2017014489A MX2017014489A MX 2017014489 A MX2017014489 A MX 2017014489A MX 2017014489 A MX2017014489 A MX 2017014489A MX 2017014489 A MX2017014489 A MX 2017014489A MX 2017014489 A MX2017014489 A MX 2017014489A
Authority
MX
Mexico
Prior art keywords
deformable zone
bushing
adjacent
head
length
Prior art date
Application number
MX2017014489A
Other languages
English (en)
Other versions
MX389355B (es
Inventor
Gay Olivier
Pailhories Guy
Villet Antoine
Naretto Nicolas
Original Assignee
Lisi Aerospace
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 Lisi Aerospace filed Critical Lisi Aerospace
Publication of MX2017014489A publication Critical patent/MX2017014489A/es
Publication of MX389355B publication Critical patent/MX389355B/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04—Rivets; Spigots or the like fastened by riveting
    • F16B19/08—Hollow rivets; Multi-part rivets
    • F16B19/10—Hollow rivets; Multi-part rivets fastened by expanding mechanically
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04—Rivets; Spigots or the like fastened by riveting
    • F16B19/08—Hollow rivets; Multi-part rivets
    • F16B19/10—Hollow rivets; Multi-part rivets fastened by expanding mechanically
    • F16B19/1027—Multi-part rivets
    • F16B19/1036—Blind rivets
    • F16B19/1045—Blind rivets fastened by a pull - mandrel or the like
    • F16B19/1072—Blind rivets fastened by a pull - mandrel or the like the pull-mandrel or the like comprising a thread and being rotated with respect to the rivet, thereby mechanically expanding and fastening the rivet

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Clamps And Clips (AREA)
  • Connection Of Plates (AREA)
  • Dowels (AREA)
  • Insertion Pins And Rivets (AREA)

Abstract

El presente invento se trata de una fijación para adherir elementos de estructuras que contienen orificios alineados con un diámetro nominal D. La fijación comprende un plano de sujeción mínima GmÍn y un plano de sujeción máxima Gmáx, y: - un tornillo (12) de cabeza grande en un extremo y una parte roscada (22), - un casquillo (30) de cabeza grande, un cuerpo tubular cilíndrico y una parte horadada (36) en contacto con la parte roscada (22) del tornillo. La parte horadada (36) es adyacente a una parte interior lisa del cuerpo (34) del casquillo, la cual presenta un espesor nominal E, una zona poco deformable (A) adyacente a la cabeza del casquillo y una zona deformable (B) adyacente a la zona poco deformable (A); la zona deformable (B) del casquillo puede deformarse en un bulbo (48) que recibe una cara ciega (46) de los elementos de la estructura. La zona deformable (B) se extiende en una longitud (L) mayor que la longitud mínima (Lmín) y menor que la longitud máxima (Lmáx), tales que: Lmín = D/2 + 2E + (Gmáx - Gmín), Lmáx = (E / 0.092) El invento se aplica, principalmente, al ensamblaje de estructuras de aeronaves.
MX2017014489A 2015-06-11 2016-06-10 Fijacion instalada de un solo lado. MX389355B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1555313A FR3037369B1 (fr) 2015-06-11 2015-06-11 Fixation installee d'un seul cote a douille deformable
PCT/EP2016/063298 WO2016198600A1 (fr) 2015-06-11 2016-06-10 Fixation installée d'un seul côté

Publications (2)

Publication Number Publication Date
MX2017014489A true MX2017014489A (es) 2018-04-10
MX389355B MX389355B (es) 2025-03-20

Family

ID=54007875

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2017014489A MX389355B (es) 2015-06-11 2016-06-10 Fijacion instalada de un solo lado.

Country Status (12)

Country Link
US (1) US10690167B2 (es)
EP (1) EP3308040B1 (es)
JP (1) JP6885879B2 (es)
KR (1) KR20180017002A (es)
CN (1) CN107810338B (es)
BR (1) BR112017026673B1 (es)
CA (1) CA2987870C (es)
ES (1) ES2784934T3 (es)
FR (1) FR3037369B1 (es)
MX (1) MX389355B (es)
RU (1) RU2714661C2 (es)
WO (1) WO2016198600A1 (es)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019104341A1 (en) 2017-11-27 2019-05-31 Sps Technologies, Llc Blind fastener with frangible nut
MX387757B (es) 2017-11-28 2025-03-18 Sps Tech Llc Herramienta automática de instalación de sujetadores de doble acción.
US10774863B2 (en) * 2018-06-18 2020-09-15 The Boeing Company Blind fastener system with electromagnetic effects-protective coating
FR3085448B1 (fr) * 2018-09-04 2020-11-27 Lisi Aerospace Vis avec gorge de rupture, fixation comprenant une telle vis, assemblage et procede d'installation associes
US11152619B2 (en) * 2019-06-28 2021-10-19 City University Of Hong Kong Energy storage device and an electrode for an energy storage device
GB2600415A (en) * 2020-10-27 2022-05-04 Airbus Operations Ltd Blind fastener
GB2600407B (en) * 2020-10-27 2022-12-14 Airbus Operations Ltd Blind fasteners
EP4011558B1 (en) 2020-12-08 2024-10-09 The Boeing Company Method and tool for installing a fastener
CA3142366C (en) * 2020-12-17 2023-11-07 Sps Technologies, Llc Two-piece blind fastener and installation tool
EP4140615B1 (en) * 2021-08-24 2024-02-28 Airbus Operations GmbH Method for installing a blind fastening device, and use of a longitudinal passage of a sleeve of a blind fastening device
US20230160030A1 (en) * 2021-11-24 2023-05-25 Rinngo Technology Co., Ltd. Method of manufacturing blind rivet
CN219828640U (zh) * 2023-02-28 2023-10-13 广州市浩洋电子股份有限公司 一种防止电化学腐蚀的锁紧结构及具有其的舞台灯

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3030705A (en) * 1958-03-05 1962-04-24 Goodrich Co B F Method of securing a structure to a tubular rivet in apertured work
US3236143A (en) 1959-05-15 1966-02-22 Hi Shear Corp Blind fastening device with collapsible tube
US3304830A (en) * 1960-08-09 1967-02-21 Goodrich Co B F Expansible hollow rivet having a polygonal shank
US3322449A (en) * 1964-06-18 1967-05-30 Vsi Corp Blind fastener system
US3345900A (en) * 1964-10-15 1967-10-10 Standard Pressed Steel Co Blind fastener
GB2368889B (en) * 2000-11-09 2004-02-04 Textron Fastening Syst Ltd Method of manufacturing a blind threaded insert
WO2004022260A1 (de) * 2002-09-04 2004-03-18 Newfrey Llc Befestigungselement, insbesondere zum blindnieten
GB2401661B (en) * 2003-05-16 2006-03-29 Textron Fastening Syst Ltd Blind fastener and method of installation thereof
US6868757B2 (en) 2003-05-20 2005-03-22 Huck International, Inc. Blind fastener and nose assembly for installation of the blind fastener
CA2643034A1 (en) * 2006-02-28 2007-09-07 Monogram Aerospace Fasteners, Inc. Mechanically locked blind bolt fastener
CN200952517Y (zh) * 2006-08-17 2007-09-26 何米铃 轮圈钢丝调整孔专用铆钉构造改良
WO2011031805A2 (en) * 2009-09-09 2011-03-17 Toosky Rahmatollah F Self-interlocking sleeve-core shear pin fastener
CN201696420U (zh) * 2010-04-26 2011-01-05 林士荣 拉钉的紧固结构
FR2970309B1 (fr) * 2011-01-07 2012-12-28 Prospection & Inventions Cheville pour materiau support friable
JP2013160321A (ja) * 2012-02-07 2013-08-19 Nippon Pop Rivets & Fasteners Ltd ブラインドナットとその取付け方法
JP5972036B2 (ja) * 2012-05-08 2016-08-17 ポップリベット・ファスナー株式会社 ブラインドナット
US9593706B2 (en) * 2012-11-11 2017-03-14 The Boeing Company Structural blind fastener and method of installation
US10006478B2 (en) * 2015-01-22 2018-06-26 Arconic Inc. Blind fasteners
CN204784052U (zh) * 2015-06-05 2015-11-18 浙江西子航空紧固件有限公司 一种改进的螺纹抽芯铆钉

Also Published As

Publication number Publication date
US10690167B2 (en) 2020-06-23
CA2987870C (fr) 2023-04-04
ES2784934T3 (es) 2020-10-02
US20180238372A1 (en) 2018-08-23
JP2018517105A (ja) 2018-06-28
CN107810338A (zh) 2018-03-16
CN107810338B (zh) 2020-10-16
FR3037369A1 (fr) 2016-12-16
EP3308040A1 (fr) 2018-04-18
WO2016198600A1 (fr) 2016-12-15
BR112017026673A2 (pt) 2018-08-14
RU2018100399A (ru) 2019-07-11
JP6885879B2 (ja) 2021-06-16
FR3037369B1 (fr) 2017-07-21
EP3308040B1 (fr) 2020-02-12
MX389355B (es) 2025-03-20
CA2987870A1 (fr) 2016-12-15
RU2018100399A3 (es) 2019-07-17
KR20180017002A (ko) 2018-02-20
BR112017026673B1 (pt) 2021-10-26
RU2714661C2 (ru) 2020-02-18

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