ES2006356A6 - A system of protection against electrical shock, especially rays, of structural components of aircraft, particularly deposits or fuel tanks manufactured from composite materials. (Machine-translation by Google Translate, not legally binding) - Google Patents

A system of protection against electrical shock, especially rays, of structural components of aircraft, particularly deposits or fuel tanks manufactured from composite materials. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES2006356A6
ES2006356A6 ES8800669A ES8800669A ES2006356A6 ES 2006356 A6 ES2006356 A6 ES 2006356A6 ES 8800669 A ES8800669 A ES 8800669A ES 8800669 A ES8800669 A ES 8800669A ES 2006356 A6 ES2006356 A6 ES 2006356A6
Authority
ES
Spain
Prior art keywords
translation
layer
protection against
legally binding
google translate
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.)
Expired
Application number
ES8800669A
Other languages
Spanish (es)
Inventor
Murciano Felipe Sequeiros
Garcia-Calvillo Garcia-Morato
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space SA
Original Assignee
Construcciones Aeronauticas CASA SA
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 Construcciones Aeronauticas CASA SA filed Critical Construcciones Aeronauticas CASA SA
Priority to ES8800669A priority Critical patent/ES2006356A6/en
Publication of ES2006356A6 publication Critical patent/ES2006356A6/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/712—Containers; Packaging elements or accessories, Packages
    • B29L2031/7172—Fuel tanks, jerry cans

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

A system of protection against electric shock, especially rays of structural components, particularly deposits or fuel tanks manufactured composite consists of a layer of wire mesh (1) covering the outside all the surface exposed to impact ray; a first layer of insulating material (2) placed between the grid (1) and siding (re), made of composite material; a second layer of insulating material (3) placed inside of the inner part (pi), to clamp (specifically the surface where supporting nut (t) element holder (r)) if this piece contains or formed carbon fiber; a strip of wire mesh (4) located outside the line of fasteners elements and introduced in countersunk made for these heads; and a third layer of insulating material (5) placed between coating and internal part a riveting; and finally, an organic finish (ao). (Machine-translation by Google Translate, not legally binding)
ES8800669A 1988-03-07 1988-03-07 A system of protection against electrical shock, especially rays, of structural components of aircraft, particularly deposits or fuel tanks manufactured from composite materials. (Machine-translation by Google Translate, not legally binding) Expired ES2006356A6 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES8800669A ES2006356A6 (en) 1988-03-07 1988-03-07 A system of protection against electrical shock, especially rays, of structural components of aircraft, particularly deposits or fuel tanks manufactured from composite materials. (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES8800669A ES2006356A6 (en) 1988-03-07 1988-03-07 A system of protection against electrical shock, especially rays, of structural components of aircraft, particularly deposits or fuel tanks manufactured from composite materials. (Machine-translation by Google Translate, not legally binding)

Publications (1)

Publication Number Publication Date
ES2006356A6 true ES2006356A6 (en) 1989-04-16

Family

ID=8255195

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8800669A Expired ES2006356A6 (en) 1988-03-07 1988-03-07 A system of protection against electrical shock, especially rays, of structural components of aircraft, particularly deposits or fuel tanks manufactured from composite materials. (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES2006356A6 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2162718A1 (en) * 1998-07-29 2002-01-01 Const Aeronauticas Sa Lightning protection system for composite aircraft structures
ES2163951A1 (en) * 1998-07-29 2002-02-01 Const Aeronauticas Sa Lightning protection system for composite aircraft structures
EP1484245A1 (en) * 2003-06-06 2004-12-08 Airbus Espana, S.L. Lightning strike protection system for aircraft fuel tanks made of low electrical conductivity composite material
WO2007039650A1 (en) * 2005-09-29 2007-04-12 Airbus España, S.L. Method of protecting fuel tanks that are made from composite materials against electric discharges
ES2279664A1 (en) * 2004-12-30 2007-08-16 Airbus España S.L. Protection device against electrical discharges in aircraft
WO2010037991A1 (en) * 2008-10-03 2010-04-08 Short Brothers Plc Fibre reinforced composite structures and method of manufacture
EP2455286A1 (en) 2010-11-22 2012-05-23 EADS Construcciones Aeronauticas, S.A. Lightning protection for composite aircraft structures
RU2775893C1 (en) * 2022-02-16 2022-07-11 Общество с ограниченной ответственностью Научно-производственный центр "Углеродные волокна и композиты" (ООО "НПЦ "УВИКОМ") Lightning-proof bus for attachment of composite panel to metal frame of unit

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2162718A1 (en) * 1998-07-29 2002-01-01 Const Aeronauticas Sa Lightning protection system for composite aircraft structures
ES2163951A1 (en) * 1998-07-29 2002-02-01 Const Aeronauticas Sa Lightning protection system for composite aircraft structures
EP1484245A1 (en) * 2003-06-06 2004-12-08 Airbus Espana, S.L. Lightning strike protection system for aircraft fuel tanks made of low electrical conductivity composite material
ES2264299A1 (en) * 2003-06-06 2006-12-16 Airbus España S.L. Lightning strike protection system for aircraft fuel tanks made of low electrical conductivity composite material
ES2279664A1 (en) * 2004-12-30 2007-08-16 Airbus España S.L. Protection device against electrical discharges in aircraft
WO2007039650A1 (en) * 2005-09-29 2007-04-12 Airbus España, S.L. Method of protecting fuel tanks that are made from composite materials against electric discharges
CN101312879B (en) * 2005-09-29 2010-05-12 空客西班牙公司 Method for manufacturing fuel tank from compound material for discharging protection
WO2010037991A1 (en) * 2008-10-03 2010-04-08 Short Brothers Plc Fibre reinforced composite structures and method of manufacture
US8675335B2 (en) 2008-10-03 2014-03-18 Short Brothers Plc Fibre reinforced composite structures and method of manufacture
EP2455286A1 (en) 2010-11-22 2012-05-23 EADS Construcciones Aeronauticas, S.A. Lightning protection for composite aircraft structures
RU2775893C1 (en) * 2022-02-16 2022-07-11 Общество с ограниченной ответственностью Научно-производственный центр "Углеродные волокна и композиты" (ООО "НПЦ "УВИКОМ") Lightning-proof bus for attachment of composite panel to metal frame of unit

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20080308