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WO2005094290A2 - Systemes de cablage a longueur reglable - Google Patents

Systemes de cablage a longueur reglable Download PDF

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Publication number
WO2005094290A2
WO2005094290A2 PCT/US2005/010289 US2005010289W WO2005094290A2 WO 2005094290 A2 WO2005094290 A2 WO 2005094290A2 US 2005010289 W US2005010289 W US 2005010289W WO 2005094290 A2 WO2005094290 A2 WO 2005094290A2
Authority
WO
WIPO (PCT)
Prior art keywords
cable
seats
length
conductor
storage unit
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.)
Ceased
Application number
PCT/US2005/010289
Other languages
English (en)
Other versions
WO2005094290A3 (fr
Inventor
Paul C. Burke
Mark Holmes
John A. Runzel
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.)
Telefonix Inc
Original Assignee
Telefonix Inc
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 Telefonix Inc filed Critical Telefonix Inc
Priority to US10/599,359 priority Critical patent/US20070262185A1/en
Priority to EP05733140A priority patent/EP1759442A4/fr
Priority to CA002561261A priority patent/CA2561261A1/fr
Priority to AU2005228208A priority patent/AU2005228208B2/en
Publication of WO2005094290A2 publication Critical patent/WO2005094290A2/fr
Anticipated expiration legal-status Critical
Publication of WO2005094290A3 publication Critical patent/WO2005094290A3/fr
Ceased legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/72—Means for accommodating flexible lead within the holder
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G11/00—Arrangements of electric cables or lines between relatively-movable parts
    • H02G11/02—Arrangements of electric cables or lines between relatively-movable parts using take-up reel or drum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0624—Arrangements of electrical connectors, e.g. for earphone, internet or electric supply
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
    • H02G1/06—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for laying cables, e.g. laying apparatus on vehicle
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G11/00—Arrangements of electric cables or lines between relatively-movable parts
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R2201/00—Connectors or connections adapted for particular applications
    • H01R2201/26—Connectors or connections adapted for particular applications for vehicles
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Definitions

  • the present disclosure relates generally to cabling and, more particularly, to adjustable length cable systems.
  • Seating arrangements associated with transportation such as, for example, busses, trains, aircraft, etc. typically provide multiple rows of seats for passengers. Each row may include one or more adjacent seats, which may be joined via a mounting rail assembly, base unit, or any other suitable frame or structure that facilitates attachment of the seats to the transport.
  • the rows of seats are typically arranged to provide a walkway or aisle, which is often located along the longitudinal axis of the transport. Thus, rows of seats may be disposed on each side and along the length of such an aisle or walkway.
  • passenger seats typically provide a variety of electronic functions that require power signals, communication signals, etc.
  • aircraft passenger seats typically provide access to in-flight entertainment such as audio programming, video programming, etc., communication systems such as, for example, telephone service, etc.
  • in-flight entertainment such as audio programming, video programming, etc.
  • communication systems such as, for example, telephone service, etc.
  • fixed length cables or wiring harnesses electrically couple one row of seats to a next row of seats. In this manner, rows of passenger seats may be daisy-chained together with these fixed length cables or wiring harnesses to provide electrical power signals, communication signals, etc. to all of the seats.
  • Fig. 1 depicts a row of aircraft seats.
  • Fig. 2 depicts a known manner in which fixed length cable assemblies are used to provide power, data and other signals to aircraft seats and to electrically couple one row of seats to another.
  • Fig. 3 depicts an example adjustable length cable system.
  • Fig. 4 depicts another example adjustable length cable system.
  • Fig. 5 depicts an example manner in which the adjustable length cable systems of Figs. 3 and 4 may be used to couple signals between aircraft seats.
  • Fig. 6 is a detailed depiction of one manner in which the cabling used in the examples of Figs. 3 and 4 may be implemented.
  • Fig. 7 is a detailed depiction of one manner in which the Ethernet cable shown in Fig. 6 may be implemented.
  • DETAILED DESCRIPTION [0015]
  • Fig. 1 depicts a row of aircraft seats. While the row of seats depicted in Fig. 1 shows three adjacent seats, any other number of seats could be used instead.
  • the example adjustable cable systems described herein are described as being used in connection with aircraft seats, the example adjustable cables systems are more generally applicable.
  • the adjustable cable systems described herein may be used in connection with any other types of seats.
  • the adjustable cable systems described herein may be used in any other applications desired.
  • Fig. 2 depicts a known manner in which fixed length cable assemblies are used to provide power, data and other signals to aircraft seats and to electrically couple one row of seats to another.
  • cables having extra length are used to enable the rows of seats to be moved apart without having to replace the cable assemblies.
  • the extra length of cabling is loosely placed underneath the seat and, as a result, presents a potential hazard and/or failure if the excess cabling is dislodged and falls onto the floor underneath the seat.
  • Fig. 3 depicts an example adjustable length cable system. The example system depicted in Fig.
  • the cable storage unit 300 includes a cable storage unit 300 and a cable assembly 302 having connectors or terminations 304, 306, 308 and 310.
  • the cable storage unit 300 includes a spool or reel 312 upon which a portion of the length of the cable assembly 302 is wound.
  • the cable storage unit 300 also includes a base or housing 314.
  • the housing 314 includes a plurality of circumferentially spaced tabs 316 configured to enable the reel 312 to be rotatable relative to the housing 314. Additionally, the tabs 316 may be further configured to retain the wound portion of the cable assembly 302 against the reel 312.
  • the housing 314 may also provide mounting holes 318 to facilitate mounting of the cable storage unit 300 underneath a seat, or in some other location.
  • the connectors 304, 306, 308 and 310 may include any desired combination of DIN connectors, RCA connectors, or any other types of electrical connectors.
  • the effective length of the adjustable cabling system shown in Fig. 3 may be changed by rotating the reel 312 relative to the housing 314. In the example of Fig. 3, rotating the reel 312 clockwise reduces the effective (e.g., overall) length of the cabling system and rotating the reel 312 counter-clockwise increases the effective length of the cabling system.
  • Fig. 4 depicts another example adjustable length cable system. Similar to the example adjustable cabling system depicted in Fig. 3, the example adjustable cabling system of Fig. 4 includes a cable storage unit 400 and a cable assembly 402 having connectors or terminations 404, 406, 408 and 410. In contrast to the example system of Fig. 3, the cable storage unit 400 depicted in Fig. 4 does not include a reel or spool to enable rotatable retraction and/or extension of a length of the cable assembly.
  • Fig. 5 depicts an example manner in which the adjustable length cable systems of Figs. 3 and 4 may be used to couple signals between aircraft seats.
  • the adjustable length cable systems described herein may be used to eliminate loose lengths of cable (e.g., as depicted in Fig. 2) that facilitate changes in the distances between rows of seats (e.g., in aircraft).
  • Fig. 2 depicts an example manner in which the adjustable length cable systems of Figs. 3 and 4 may be used to couple signals between aircraft seats.
  • the adjustable length cable systems described herein may be used to eliminate loose lengths of cable (e.g., as depicted in Fig. 2) that facilitate changes in the distances between rows of seats (e.g., in aircraft).
  • Fig. 6 is a detailed depiction of one manner in which the cabling used in the examples of Figs. 3 and 4 may be implemented. As depicted in the example implementation of Fig.
  • the cabling may be a multi-conductor cable 600 configured to convey various power, data (e.g., Ethernet), and other electrical signals in conformance with commercial aircraft requirements.
  • the example cabling of Fig. 6 utilizes Litz wire, which meets the voltage (e.g., 600 VAC), temperature (e.g., 200 °C) and flammability requirements (e.g., FAA FAR 25.869) of commercial aircraft.
  • voltage e.g., 600 VAC
  • temperature e.g., 200 °C
  • flammability requirements e.g., FAA FAR 25.869
  • other specifications may be met as well.
  • Litz wire is constructed of individual film insulated wires bunched or braided together in a uniform pattern of twists and length of lay.
  • the example multi- conductor cable 600 of FIG. 6 includes an Ethernet cable (e.g., a 26 AWG 100 ohm cable) 602, five Litz wire conductors (e.g., 16 AWG 19/29), one of which is shown at reference number 604, and a single smaller gauge (e.g., 24 AWG, 19/36) Litz wire conductor 606.
  • Ethernet cable e.g., a 26 AWG 100 ohm cable
  • five Litz wire conductors e.g., 16 AWG 19/29
  • reference number 604 e.g., 24 AWG, 19/36
  • Fig. 7 is a detailed depiction of one manner in which the Ethernet cable 602 shown in Fig. 7 may be implemented.
  • the example Ethernet cable 602 is fabricated using Litz wire (e.g., 26 AWG, 19/38) to minimize weight, maximize mechanical flexibility while meeting the environmental requirements associated with commercial aircraft.
  • the example Ethernet cable 602 includes four conductors (one of which is shown at reference number 700), which may be wrapped around an optional filler (not shown).
  • the example cable 602 includes a double shield 704 and may include a PTFE binder between the conductors 700, the shield 704, and the outside of the shield 704. Using the example cabling construction depicted in Figs.
  • a seventy-five inch long cable may weigh approximately .73 pounds.
  • known fixed length cables for use in commercial aircraft seat-to- seat cabling having a length of about 47 inches may weigh more than .85 pounds.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Insulated Conductors (AREA)
  • Multi-Conductor Connections (AREA)
  • Coupling Device And Connection With Printed Circuit (AREA)
  • Electric Cable Installation (AREA)

Abstract

L'invention concerne des systèmes de câblage à longueur réglable, notamment un système de câblage destiné à un véhicule de tourisme comprenant plusieurs rangées de sièges, et comprenant un câble multiconducteur présentant une longueur donnée et une première et une seconde extrémité couplées à un premier et à un second connecteur correspondants. Ce câble multiconducteur est conçu pour transporter des signaux électriques dans au moins une rangée de sièges. Le système de câblage décrit comprend en outre une unité de stockage de câble conçue pour contenir une portion enroulée du câble multiconducteur. Cette unité de stockage de câble comprend une partie boîtier conçue pour pouvoir être installée sous au moins un des sièges passagers.
PCT/US2005/010289 2004-03-26 2005-03-28 Systemes de cablage a longueur reglable Ceased WO2005094290A2 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US10/599,359 US20070262185A1 (en) 2004-03-26 2005-03-28 Adjustable Length Cabling Systems
EP05733140A EP1759442A4 (fr) 2004-03-26 2005-03-28 Systemes de cablage a longueur reglable
CA002561261A CA2561261A1 (fr) 2004-03-26 2005-03-28 Systemes de cablage a longueur reglable
AU2005228208A AU2005228208B2 (en) 2004-03-26 2005-03-28 Adjustable length cabling systems

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US55666604P 2004-03-26 2004-03-26
US60/556,666 2004-03-26

Publications (2)

Publication Number Publication Date
WO2005094290A2 true WO2005094290A2 (fr) 2005-10-13
WO2005094290A3 WO2005094290A3 (fr) 2009-04-09

Family

ID=35064269

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/010289 Ceased WO2005094290A2 (fr) 2004-03-26 2005-03-28 Systemes de cablage a longueur reglable

Country Status (7)

Country Link
US (1) US20070262185A1 (fr)
EP (1) EP1759442A4 (fr)
KR (1) KR20070041433A (fr)
CN (1) CN101432939A (fr)
AU (1) AU2005228208B2 (fr)
CA (1) CA2561261A1 (fr)
WO (1) WO2005094290A2 (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007062193A1 (de) * 2007-12-21 2009-07-02 Airbus Deutschland Gmbh Vorrichtung zur Aufnahme von Leitungen in einem Flugzeug
FR2931455A1 (fr) * 2008-05-20 2009-11-27 Radiall Sa Dispositif de raccordement electrique pour des liaisons siege a siege
US7692099B2 (en) 2005-09-19 2010-04-06 Telefonix, Inc. Flexible and lightweight seat-to-seat cabin cable system and method of manufacturing same
DE102009018771A1 (de) * 2009-04-24 2010-11-04 Airbus Deutschland Gmbh Ausstattungselement mit einziehbarer Leitung
FR3115408A1 (fr) * 2020-10-20 2022-04-22 Latelec Socle de fixation d’équipement électrique avec logement de stockage pour câble
US11572177B2 (en) * 2019-03-27 2023-02-07 The Boeing Company Seat cable adjustment system and method

Families Citing this family (6)

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Publication number Priority date Publication date Assignee Title
AU2010232980B2 (en) 2009-04-03 2015-06-04 Astronics Connectivity Systems & Certification Corp. USB cable and method for producing the same
CN102866270A (zh) * 2012-09-20 2013-01-09 山东电力集团公司枣庄供电公司 电气试验测试线
US9238416B2 (en) 2013-08-15 2016-01-19 Telefonix, Incorporated Cord reel variable current thermal management and damage detection
US10015281B2 (en) * 2015-07-06 2018-07-03 The Boeing Company Wireless software loader
US9963236B2 (en) * 2016-02-09 2018-05-08 The Boeing Company Modular system for distributing electrical power and data between structures
CN110980440B (zh) * 2019-12-12 2021-11-02 上汽通用汽车有限公司 线束收卷装置及车辆座椅

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7692099B2 (en) 2005-09-19 2010-04-06 Telefonix, Inc. Flexible and lightweight seat-to-seat cabin cable system and method of manufacturing same
DE102007062193A1 (de) * 2007-12-21 2009-07-02 Airbus Deutschland Gmbh Vorrichtung zur Aufnahme von Leitungen in einem Flugzeug
DE102007062193B4 (de) * 2007-12-21 2010-04-15 Airbus Deutschland Gmbh Vorrichtung zur Aufnahme von Leitungen in einem Flugzeug
FR2931455A1 (fr) * 2008-05-20 2009-11-27 Radiall Sa Dispositif de raccordement electrique pour des liaisons siege a siege
EP2128022A1 (fr) * 2008-05-20 2009-12-02 Radiall Dispositif de raccordement électrique pour des liaisons siège à siège
US8087952B2 (en) 2008-05-20 2012-01-03 Radiall Electrical connection device for making seat to seat connections
DE102009018771A1 (de) * 2009-04-24 2010-11-04 Airbus Deutschland Gmbh Ausstattungselement mit einziehbarer Leitung
DE102009018771B4 (de) 2009-04-24 2018-09-20 Airbus Operations Gmbh Vorhangkopfteil und Ausstattungselement für ein Transportmittel
US11572177B2 (en) * 2019-03-27 2023-02-07 The Boeing Company Seat cable adjustment system and method
FR3115408A1 (fr) * 2020-10-20 2022-04-22 Latelec Socle de fixation d’équipement électrique avec logement de stockage pour câble
WO2022084268A1 (fr) * 2020-10-20 2022-04-28 Latelec Socle de fixation d'équipement électrique avec logement de stockage pour câble
US20230391581A1 (en) * 2020-10-20 2023-12-07 Latelec Electrical equipment mounting base plate with cable storage recess

Also Published As

Publication number Publication date
EP1759442A4 (fr) 2011-05-11
CN101432939A (zh) 2009-05-13
CA2561261A1 (fr) 2005-10-13
AU2005228208A1 (en) 2005-10-13
WO2005094290A3 (fr) 2009-04-09
US20070262185A1 (en) 2007-11-15
AU2005228208B2 (en) 2011-06-16
EP1759442A2 (fr) 2007-03-07
KR20070041433A (ko) 2007-04-18

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