EP0089953A1 - Befestigungsvorrichtung und verfahren für kompositstrukturen. - Google Patents

Befestigungsvorrichtung und verfahren für kompositstrukturen.

Info

Publication number
EP0089953A1
EP0089953A1 EP82900055A EP82900055A EP0089953A1 EP 0089953 A1 EP0089953 A1 EP 0089953A1 EP 82900055 A EP82900055 A EP 82900055A EP 82900055 A EP82900055 A EP 82900055A EP 0089953 A1 EP0089953 A1 EP 0089953A1
Authority
EP
European Patent Office
Prior art keywords
electrically conductive
fastener
composite structure
conically shaped
central axis
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.)
Granted
Application number
EP82900055A
Other languages
English (en)
French (fr)
Other versions
EP0089953A4 (de
EP0089953B1 (de
Inventor
Glenn Oliver Olson
Leland Edward Thomson
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.)
Boeing Co
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 EP0089953A1 publication Critical patent/EP0089953A1/de
Publication of EP0089953A4 publication Critical patent/EP0089953A4/de
Application granted granted Critical
Publication of EP0089953B1 publication Critical patent/EP0089953B1/de
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/28Clamped connections, spring connections
    • H01R4/30Clamped connections, spring connections utilising a screw or nut clamping member
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/58Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation characterised by the form or material of the contacting members
    • H01R4/64Connections between or with conductive parts having primarily a non-electric function, e.g. frame, casing, rail
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R9/00Structural associations of a plurality of mutually-insulated electrical connecting elements, e.g. terminal strips or terminal blocks; Terminals or binding posts mounted upon a base or in a case; Bases therefor
    • H01R9/16Fastening of connecting parts to base or case; Insulating connecting parts from base or case

Definitions

  • This invention relates to fastener arrangements for composite structures and more particularly to methods and associated fastener arrangements for establishing electrical continuity between fasteners and composite structures.
  • FIGURE 1 is illustrative of prior art fastener connection installed in a composite panel structure
  • FIGURE 2 is a sectional view illustrative of an apparatus and method in accordance with a preferred embodiment of the present invention for providing increased conductivity between fastener and composite structure;
  • FIGURE 3 is a view of the assembly of Figure 2 blown apart to show the manner of assembly of the fastener arrangement of Figure 2;
  • FIGURE 4 is an expanded and enlarged view of the crosssection of the present fastener assembly shown in Figure 2 deemed helpful in understanding the manner in which increased conductivity is achieved,
  • the stud assembly indicated generally by the numeral 10 includes a bolt having a head portion 14 and a shank portion 16 passing through the composite panel structure 12, The usual washers and locking nut 18 complete the assembly of grounding stud 10 to composite panel structure 12.
  • countersunk insert device 22 comprises a generally tubular shaped body of corrosion resistant stainless steel or titanium having two continuous integral coaxial portions 30 and 32 disposed about the central axis 40 of the fastener 10 shown in place in Figure 4.
  • Countersunk insert device 22, being of tubular shape about coaxial hole 31 comprises an upper frustro conical shaped portion 30 and a lower cylindrically shaped flange-like portion 32.
  • Graphite epoxy structures such as panel member 12 shown in Figure 4 have much better conductivity in a longitudinal direction (the current flow stays in the plies), than in the transverse direction, such as in the direction 40 along the central axis of a fastener inserted in the graphite epoxy structure.
  • the reason for this is that the currents must cross, the epoxy boundary between plies and run transverse to the graphite filaments which lie along the longitudinal direction 42 of current flow within the graphite epoxy structure 12.
  • This difference in conductivity can be as high as 200:1.
  • the countersunk insert devices 20 and 22 in accordance with a preferred embodiment of the present invention provide the increased conductivity between shank of a fastener, such as the grounding stud 20 shown in Figure 4, and the longitudinal fibers of the conductive structure running in the direction of current flow represented by the numerals 42 in Figure 4.
  • edge-to-edge resistivity is approximately 200;1 for a graphite epoxy type composite structure 12.
  • resistivity of graphite epoxy composite structures varies from 10 3 to 10 6 that of an equivalent aluminum sheet. Therefore, the optimum bonding and ground resistance for a fastener such as a ground stud 20 shown in Figure 4 in a composite panel structure 12 can be successfully realized by utilization of countersunk insert devices 20 and 22 which provide electrical contact between shaft portion 16 of a fastener and an increased number of the longitudinal fibers of the composite structure 12. This is due to the frustro conical shaped portion 30 of countersunk insert 22. Transverse conductivity is also improved between the faying surface of countersunk insert device 22 and the outer plies of composite structure 12.
  • Countersunk insert device 20 is shaped identical to countersunk insert device 22 hereinbefore described, and is located in a complementary-shaped countersunk hole on the other side of composite structure 12,
  • the hereinabove described embodiment of the present invention teaches a method and structures including the utilization of countersunk insert devices which, will achieve the maximum transfer of currents between the shanks of fastening deyices and transversely extending fibers in composite panel structures in which, fasteners are utilized.
  • the longitudinal conductivity property of these advanced composites such as graphite epoxy composites may be utilized in accordance with further embodiments of the invention by those skilled in the art, recognizing that the aforementioned countersunk insert devices may be utilized where, for example, fasteners such as self-locking nuts, shear collars, fixed nut plates or floating nut plates are utilized.
  • the present countersunk insert devices may be utilized on either side of a pair of composite panel members being secured together by standard types of fasteners having shank portions 16 which must be connected to longitudinally extending fibers in the composite panel members utilizing the increase conductivity teachings of the preferred embodiment of the present invention.

Landscapes

  • Connection Of Plates (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
EP82900055A 1981-09-30 1981-09-30 Befestigungsvorrichtung und verfahren für kompositstrukturen Expired EP0089953B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1981/001318 WO1983001345A1 (en) 1981-09-30 1981-09-30 Fastening device and method for composite structures

Publications (3)

Publication Number Publication Date
EP0089953A1 true EP0089953A1 (de) 1983-10-05
EP0089953A4 EP0089953A4 (de) 1985-11-07
EP0089953B1 EP0089953B1 (de) 1988-06-22

Family

ID=22161454

Family Applications (1)

Application Number Title Priority Date Filing Date
EP82900055A Expired EP0089953B1 (de) 1981-09-30 1981-09-30 Befestigungsvorrichtung und verfahren für kompositstrukturen

Country Status (3)

Country Link
EP (1) EP0089953B1 (de)
DE (1) DE3176798D1 (de)
WO (1) WO1983001345A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107863610A (zh) * 2016-09-21 2018-03-30 利萨·德雷克塞迈尔有限责任公司 电连接设备和用于制造电连接设备的方法

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8263864B2 (en) 2004-12-30 2012-09-11 Airbus Operations S.L. Device for electrical bonding of electrical cables shielding on composite structures

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1083447A (fr) * 1953-02-27 1955-01-10 Boulon indesserrable
DE1020782B (de) * 1954-12-24 1957-12-12 Brueninghaus Gmbh Stahlwerke Geschraubter Stabanschluss in Fachwerken
US2990533A (en) * 1958-04-09 1961-06-27 Stokes D Hughes Terminal post for circuit board
DE2134605A1 (de) * 1970-07-17 1972-01-27 Nuclear Power Group Ltd Klemmverbindung für unterschiedlicher thermischer Ausdehnung ausgesetzte Körper
FR2265194A1 (de) * 1974-03-21 1975-10-17 Boeing Co
DE2651262A1 (de) * 1976-11-10 1978-05-11 Audi Nsu Auto Union Ag Schraubenverbindung von maschinenteilen
US4110904A (en) * 1977-05-19 1978-09-05 Allen-Bradley Company Substrate with terminal connections and method of making the same

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB160218A (en) * 1919-11-14 1921-03-14 British Electric Transformer C Improvements in or relating to electric connections
DE2347217A1 (de) * 1973-09-19 1975-03-27 Siemens Ag Verfahren zum durchkontaktieren eines beidseitig metallkaschierten basismaterials fuer gedruckte schaltungen

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1083447A (fr) * 1953-02-27 1955-01-10 Boulon indesserrable
DE1020782B (de) * 1954-12-24 1957-12-12 Brueninghaus Gmbh Stahlwerke Geschraubter Stabanschluss in Fachwerken
US2990533A (en) * 1958-04-09 1961-06-27 Stokes D Hughes Terminal post for circuit board
DE2134605A1 (de) * 1970-07-17 1972-01-27 Nuclear Power Group Ltd Klemmverbindung für unterschiedlicher thermischer Ausdehnung ausgesetzte Körper
FR2265194A1 (de) * 1974-03-21 1975-10-17 Boeing Co
DE2651262A1 (de) * 1976-11-10 1978-05-11 Audi Nsu Auto Union Ag Schraubenverbindung von maschinenteilen
US4110904A (en) * 1977-05-19 1978-09-05 Allen-Bradley Company Substrate with terminal connections and method of making the same

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO8301345A1 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107863610A (zh) * 2016-09-21 2018-03-30 利萨·德雷克塞迈尔有限责任公司 电连接设备和用于制造电连接设备的方法

Also Published As

Publication number Publication date
EP0089953A4 (de) 1985-11-07
DE3176798D1 (en) 1988-07-28
EP0089953B1 (de) 1988-06-22
WO1983001345A1 (en) 1983-04-14

Similar Documents

Publication Publication Date Title
US4671583A (en) Fastening device and method for composite structures
US4502092A (en) Integral lightning protection system for composite aircraft skins
US5326206A (en) Method for compensating for bolt hole misalignment and bolt assemblies therefor
US7554785B2 (en) Lightning damage protection for composite aircraft
US3989984A (en) Aircraft lightning protection means
US4479163A (en) Integral lightning protection system for composite aircraft skins
US20120019973A1 (en) Method and apparatus for grounding a composite aircraft structure
RU2167788C2 (ru) Отказобезопасная рама для подвески двигателя
RU2641404C2 (ru) Топливный бак, основные крылья, корпус летательного аппарата, летательный аппарат и транспортное средство
US4920449A (en) Conductive bonding of composite structures
EP0269458A1 (de) Blitzschutz-Befestigungsmittel für Flugzeugbauteile aus Verbundmaterial
US6309131B1 (en) Redundant clevis pin pair
CA3067469C (en) Aircraft wing composite ribs having electrical grounding paths
EP0089953A1 (de) Befestigungsvorrichtung und verfahren für kompositstrukturen.
US4574325A (en) Lightning protection electrical circuit path for coupling between aircraft structures
CA1055909A (en) Adjustable mounting assembly
US4390153A (en) Apparatus for securing a wing to the body of a craft
EP0666614A1 (de) Zweimetallverbinder
US11273923B2 (en) Fail-safe engine support system
JPS63134368A (ja) ステアリングホイ−ル取付構造
CN110356570B (zh) 发动机附接件、包括其的飞行器及将发动机固定的方法
EP0112333A1 (de) Befestigungsvorrichtung für kompositstrukturen.
US9784132B2 (en) Voltage discharge channelling assembly for a gas turbine engine
US2709795A (en) Electrical cable connector
CN116198554A (zh) 转向架及轨道车辆

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19830506

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB NL SE

17Q First examination report despatched

Effective date: 19861027

R17C First examination report despatched (corrected)

Effective date: 19870424

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB NL SE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Effective date: 19880630

REF Corresponds to:

Ref document number: 3176798

Country of ref document: DE

Date of ref document: 19880728

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19900907

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 19900928

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 19900930

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 19901031

Year of fee payment: 10

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Effective date: 19910930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Effective date: 19920401

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee
GBPC Gb: european patent ceased through non-payment of renewal fee
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Effective date: 19920529

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Effective date: 19920602

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST