MX2020011213A - Sistema de sujecion, y metodos para fabricar y utilizar el sistema. - Google Patents

Sistema de sujecion, y metodos para fabricar y utilizar el sistema.

Info

Publication number
MX2020011213A
MX2020011213A MX2020011213A MX2020011213A MX2020011213A MX 2020011213 A MX2020011213 A MX 2020011213A MX 2020011213 A MX2020011213 A MX 2020011213A MX 2020011213 A MX2020011213 A MX 2020011213A MX 2020011213 A MX2020011213 A MX 2020011213A
Authority
MX
Mexico
Prior art keywords
methods
panel
making
fastening
fastener
Prior art date
Application number
MX2020011213A
Other languages
English (en)
Inventor
Robert J Bingham
Emanuel Guzman
Original Assignee
Rigidcore Group Llc
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 Rigidcore Group Llc filed Critical Rigidcore Group Llc
Publication of MX2020011213A publication Critical patent/MX2020011213A/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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
    • 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
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Laminated Bodies (AREA)

Abstract

Un sistema, que comprende un panel que comprende una retícula de panal tetraédrico-octaédrico, una capa superficial formada sobre un primer lado de la retícula, que tiene una abertura formada ahí mismo configurada para recibir a un sujetador, y un montaje de sujeción que comprende un sujetador configurado para ser montado al panel cuando el panel es fijado a un componente adyacente, y un material endurecedor. También se describen sistemas y métodos correspondientes.
MX2020011213A 2018-04-23 2019-04-22 Sistema de sujecion, y metodos para fabricar y utilizar el sistema. MX2020011213A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201862661205P 2018-04-23 2018-04-23
PCT/US2019/028457 WO2019209683A1 (en) 2018-04-23 2019-04-22 Fastening system, and methods of making and using the system

Publications (1)

Publication Number Publication Date
MX2020011213A true MX2020011213A (es) 2020-11-09

Family

ID=68293588

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2020011213A MX2020011213A (es) 2018-04-23 2019-04-22 Sistema de sujecion, y metodos para fabricar y utilizar el sistema.

Country Status (4)

Country Link
US (1) US20210246922A1 (es)
CA (1) CA3096109A1 (es)
MX (1) MX2020011213A (es)
WO (1) WO2019209683A1 (es)

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US4348442A (en) * 1979-08-17 1982-09-07 Figge Irving E Structural panel
US4650385A (en) * 1983-05-17 1987-03-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Daze fasteners
US4495237A (en) * 1983-06-10 1985-01-22 Patterson Fred R Pyramidal core structure
US4711062A (en) * 1986-12-17 1987-12-08 Gwilliam Tony S Octet structures using tension and compression
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US5070673A (en) * 1988-11-02 1991-12-10 Tetrahex, Inc. Tetrahexagonal truss structure
US5040966A (en) * 1988-11-02 1991-08-20 Tetrahex, Inc. Die for making a tetrahexagonal truss structure
US4973208A (en) * 1989-08-31 1990-11-27 Gauron Richard F Inset panel fastener with floating member
US4981735A (en) * 1989-09-05 1991-01-01 The United States Of America As Represented By The Secretary Of The Army Two piece threaded mounting insert with adhesive for use with honeycomb composite
US5093957A (en) * 1991-07-08 1992-03-10 Atr International, Inc. Compression fitting for use in a two-sided honeycomb panel
JP2640078B2 (ja) * 1993-02-08 1997-08-13 株式会社神戸製鋼所 制振形材及び輸送機用構造体
CA2144295C (en) * 1995-03-09 2005-05-24 Germain Belanger Core-board
US5653078A (en) * 1995-09-29 1997-08-05 Erico International Corporation Variable embedment anchor and method
US5930970A (en) * 1997-03-14 1999-08-03 De Le Fevre; Patrick Y. Panel construction use as a forming device for settable fluids in construction
WO2000009307A2 (en) * 1998-08-11 2000-02-24 Molecular Geodesics, Inc. A mold for making a three-dimensional complex structure, said mold comprising at least three mold portions, method of making said mold, and use of said mold for making three-dimensional complex structures
JP4220606B2 (ja) * 1999-01-26 2009-02-04 櫻護謨株式会社 ハニカムパネル固定構造
US6200664B1 (en) * 1999-11-01 2001-03-13 Ward Figge Explosion barrier
US6488460B1 (en) * 2000-05-02 2002-12-03 Bell Helicopter Textron Inc. Composite panel insert with hold out recess feature
WO2003101722A1 (en) * 2002-05-30 2003-12-11 University Of Virginia Patent Foundation Active energy absorbing cellular metals and method of manufacturing and using the same
US20060010831A1 (en) * 2004-07-16 2006-01-19 Skakie Edward F Insulated concrete form
US8297169B2 (en) * 2006-06-26 2012-10-30 The Boeing Company Ballistic resistant through insert with floating capability for stopping a ballistic projectile
US8650756B2 (en) * 2006-10-27 2014-02-18 University Of Virginia Patent Foundation Manufacture of lattice truss structures from monolithic materials
US7802953B2 (en) * 2007-03-16 2010-09-28 Robert Stephen Inset panel fastener
US8393601B2 (en) * 2008-10-04 2013-03-12 Applied Concepts Aircraft Solutions, Inc. Vibration isolation fastener insert
US9597826B2 (en) * 2012-10-30 2017-03-21 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
WO2015073094A2 (en) * 2013-08-27 2015-05-21 University Of Virginia Patent Foundation Lattice materials and structures and related methods thereof
US9446488B2 (en) * 2014-05-21 2016-09-20 The Boeing Company Self-locking molded-in blind inserts
US10099767B2 (en) * 2015-08-04 2018-10-16 The Boeing Company Sandwich panel inserts and related methods
US9862166B2 (en) * 2016-03-07 2018-01-09 The Boeing Company Adjustable-height inserts and related methods
US9976583B2 (en) * 2016-04-04 2018-05-22 The Boeing Company Threaded adjustable-height inserts and related methods

Also Published As

Publication number Publication date
WO2019209683A1 (en) 2019-10-31
US20210246922A1 (en) 2021-08-12
CA3096109A1 (en) 2019-10-31

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