EP1759442A2 - Systemes de cablage a longueur reglable - Google Patents
Systemes de cablage a longueur reglableInfo
- Publication number
- EP1759442A2 EP1759442A2 EP05733140A EP05733140A EP1759442A2 EP 1759442 A2 EP1759442 A2 EP 1759442A2 EP 05733140 A EP05733140 A EP 05733140A EP 05733140 A EP05733140 A EP 05733140A EP 1759442 A2 EP1759442 A2 EP 1759442A2
- Authority
- EP
- European Patent Office
- 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.)
- Withdrawn
Links
- 239000004020 conductor Substances 0.000 claims abstract description 19
- 230000008859 change Effects 0.000 claims description 4
- 230000000712 assembly Effects 0.000 description 7
- 238000000429 assembly Methods 0.000 description 7
- 238000000034 method Methods 0.000 description 4
- 230000032258 transport Effects 0.000 description 4
- 230000007613 environmental effect Effects 0.000 description 3
- 238000009413 insulation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000004810 polytetrafluoroethylene Substances 0.000 description 1
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 1
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)
- Electric Cable Installation (AREA)
- Multi-Conductor Connections (AREA)
- Coupling Device And Connection With Printed Circuit (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US55666604P | 2004-03-26 | 2004-03-26 | |
PCT/US2005/010289 WO2005094290A2 (fr) | 2004-03-26 | 2005-03-28 | Systemes de cablage a longueur reglable |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1759442A2 true EP1759442A2 (fr) | 2007-03-07 |
EP1759442A4 EP1759442A4 (fr) | 2011-05-11 |
Family
ID=35064269
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05733140A Withdrawn EP1759442A4 (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) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007035780A2 (fr) | 2005-09-19 | 2007-03-29 | Telefonix, Incorporated | Systeme de cables souples et legers de liaison entre sieges de cabine et son procede de fabrication |
DE102007062193B4 (de) * | 2007-12-21 | 2010-04-15 | Airbus Deutschland Gmbh | Vorrichtung zur Aufnahme von Leitungen in einem Flugzeug |
FR2931455B1 (fr) | 2008-05-20 | 2010-07-30 | Radiall Sa | Dispositif de raccordement electrique pour des liaisons siege a siege |
ES2580228T3 (es) * | 2009-04-03 | 2016-08-22 | Telefonix, Inc. | Cable USB y procedimiento para producirlo |
DE102009018771B4 (de) | 2009-04-24 | 2018-09-20 | Airbus Operations Gmbh | Vorhangkopfteil und Ausstattungselement für ein Transportmittel |
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 |
US11572177B2 (en) * | 2019-03-27 | 2023-02-07 | The Boeing Company | Seat cable adjustment system and method |
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 |
FR3115408B1 (fr) * | 2020-10-20 | 2022-10-14 | Latelec | Socle de fixation d’équipement électrique avec logement de stockage pour câble |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2790236A1 (fr) * | 1999-02-25 | 2000-09-01 | Faure Bertrand Equipements Sa | Glissiere pour siege amovible de vehicule |
US6287141B1 (en) * | 2000-07-19 | 2001-09-11 | Pi Yun Hsieh Huang | Apparatus for winding and storing communication wire |
US6324285B1 (en) * | 1996-08-30 | 2001-11-27 | Aerotech Ife Limited | Cradle for a handset |
WO2003020588A1 (fr) * | 2001-09-05 | 2003-03-13 | The Boeing Company | Appareil et procede de raccordement d'un ordinateur portable a un reseau de communication de bord |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1977209A (en) * | 1930-12-09 | 1934-10-16 | Macintosh Cable Company Ltd | Electric cable |
US2576335A (en) * | 1946-12-10 | 1951-11-27 | Benjamin O Fanslow | Electric cord adjusting reel |
US3657491A (en) * | 1970-05-28 | 1972-04-18 | Illinois Tool Works | Cord reel |
CA1075331A (fr) * | 1976-02-05 | 1980-04-08 | Western Electric Company, Incorporated | Procede de fabrication de cables a deux gaines |
US4151365A (en) * | 1977-08-22 | 1979-04-24 | Western Electric Company, Inc. | Filled service cable having corrugated shield and methods of making |
US4384688A (en) * | 1981-05-26 | 1983-05-24 | Warren F. B. Lindsley | Self-storing cord and hose reel assemblies |
US4713497A (en) * | 1982-06-03 | 1987-12-15 | Smith John N | Self-storing cord and reel assemblies for shielded cables |
US4675475A (en) * | 1984-05-02 | 1987-06-23 | Ericsson, Inc. | Electrical cable with reinforcement |
US4769906A (en) * | 1986-06-18 | 1988-09-13 | Switchcraft, Inc. | Round-to-flat cable assembly |
GB8705393D0 (en) * | 1987-03-07 | 1987-04-08 | British Aerospace | Seating arrangement for aircraft |
US4773879A (en) * | 1987-10-13 | 1988-09-27 | Amp Incorporated | Coaxial drop cable |
US4989805A (en) * | 1988-11-04 | 1991-02-05 | Burke Paul C | Retractable reel assembly for telephone extension cord |
US5094396B1 (en) * | 1988-11-04 | 1997-05-27 | Telefonix Inc | Retractable reel assembly for telephone extension cord |
US5128993A (en) * | 1990-11-28 | 1992-07-07 | Gte Airfone, Incorporated | Telephone dispenser with compact cord guide |
US6164582A (en) * | 1994-10-18 | 2000-12-26 | Reel Butler, Inc. | Enhanced storage system for electrical appliances, powercords and adapters |
US5574250A (en) * | 1995-02-03 | 1996-11-12 | W. L. Gore & Associates, Inc. | Multiple differential pair cable |
US6372988B1 (en) * | 1997-01-07 | 2002-04-16 | Paul C. Burke | Seamless flat-round conductive cable for a retractable cord reel |
ES2297877T3 (es) * | 1997-01-07 | 2008-05-01 | Telefonix, Inc. | Carrete retraible con mecanismo de trinquete acanalado. |
US6169251B1 (en) * | 1997-03-31 | 2001-01-02 | The Whitaker Corporation | Quad cable |
US6386906B1 (en) * | 1998-03-16 | 2002-05-14 | Telefonix Inc | Cord management apparatus and method |
AU758261B2 (en) * | 1998-08-06 | 2003-03-20 | Prestolite Wire Corporation | Cable with twisting filler |
DE69923700T2 (de) * | 1998-10-06 | 2006-01-19 | Telefonix, Inc., North Chicago | Zurückziehbare kabelanordnung |
US6578683B1 (en) * | 1999-11-12 | 2003-06-17 | Telefonix, Inc | Miniature retractable cord reel |
US6300573B1 (en) * | 1999-07-12 | 2001-10-09 | The Furukawa Electric Co., Ltd. | Communication cable |
US6439491B1 (en) * | 2000-12-18 | 2002-08-27 | Sheng Hsin Liao | Wire winding box |
US6835068B2 (en) * | 2001-09-19 | 2004-12-28 | The Boeing Company | Apparatus for aircraft seat connector interface to portable electronic devices |
US6434249B1 (en) * | 2001-11-16 | 2002-08-13 | Jose Wei | Earphone wire winding box with coaxial and dual wheels |
US20040149533A1 (en) * | 2003-01-24 | 2004-08-05 | Joanne Milano | Cable management and contact monitoring system |
US7108216B2 (en) * | 2003-04-11 | 2006-09-19 | Telefonix, Inc. | Retractable cord reels for use with flat electrical cable |
-
2005
- 2005-03-28 EP EP05733140A patent/EP1759442A4/fr not_active Withdrawn
- 2005-03-28 WO PCT/US2005/010289 patent/WO2005094290A2/fr active Application Filing
- 2005-03-28 CA CA002561261A patent/CA2561261A1/fr not_active Abandoned
- 2005-03-28 US US10/599,359 patent/US20070262185A1/en not_active Abandoned
- 2005-03-28 CN CNA2005800156076A patent/CN101432939A/zh active Pending
- 2005-03-28 KR KR1020067022326A patent/KR20070041433A/ko not_active Application Discontinuation
- 2005-03-28 AU AU2005228208A patent/AU2005228208B2/en not_active Ceased
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6324285B1 (en) * | 1996-08-30 | 2001-11-27 | Aerotech Ife Limited | Cradle for a handset |
FR2790236A1 (fr) * | 1999-02-25 | 2000-09-01 | Faure Bertrand Equipements Sa | Glissiere pour siege amovible de vehicule |
US6287141B1 (en) * | 2000-07-19 | 2001-09-11 | Pi Yun Hsieh Huang | Apparatus for winding and storing communication wire |
WO2003020588A1 (fr) * | 2001-09-05 | 2003-03-13 | The Boeing Company | Appareil et procede de raccordement d'un ordinateur portable a un reseau de communication de bord |
Non-Patent Citations (1)
Title |
---|
See also references of WO2005094290A2 * |
Also Published As
Publication number | Publication date |
---|---|
CA2561261A1 (fr) | 2005-10-13 |
KR20070041433A (ko) | 2007-04-18 |
EP1759442A4 (fr) | 2011-05-11 |
WO2005094290A2 (fr) | 2005-10-13 |
CN101432939A (zh) | 2009-05-13 |
AU2005228208B2 (en) | 2011-06-16 |
AU2005228208A1 (en) | 2005-10-13 |
WO2005094290A3 (fr) | 2009-04-09 |
US20070262185A1 (en) | 2007-11-15 |
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Legal Events
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A4 | Supplementary search report drawn up and despatched |
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