Seat power bus with discrete connection ports

• US 7,207,523 B2
• Filed: 09/08/2004
• Issued: 04/24/2007
• Est. Priority Date: 09/08/2004
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Laib, Trevor M, Mitchell, Bradley J, Henley, James T, Callahan, Kevin S
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US10/936,004
• Publication Number:
  US 20060049311A1
• Time in Patent Office: 958 Days
• Field of Search: 244/129.1, 244/118.1, 244/118.5, 244/118.6, 244/122.R, 439/157, 439/131, 439/210, 439/110, 296/65.13, 361/601, 174/10, 174/70.R, 174/209, 174/74.R, 174/15.7, 297/344.1, 297/217.4
• US Class Current: 244/118.6
• CPC Class Codes: B60R 16/0207 Wire harnesses
• CPC Class Codes: B64D 11/06 Arrangements of seats, or adaptations or details specially adapted for aircraft seats crew seat constructions for emergency purposes B64D25/04
• CPC Class Codes: B64D 11/0624 Arrangements of electrical connectors, e.g. for earphone, internet or electric supply
• CPC Class Codes: H01R 25/16 Rails or bus-bars provided with a plurality of discrete connecting locations for counterparts

Abstract

A power/data bus for conducting at least one of data and power signals to a variety of different locations on a mobile platform. The bus has a plurality of discrete connection ports, and at least one conductive cable. The power/data bus extends across an area where access to at least one of data and electricity is desired. The discrete connection ports are spaced apart at different locations along the power/data bus. The conductive cable extends through the power/data bus and is connected to at least one of the discrete connection ports. The conductive cable conducts at least one of power and data signals between the discrete connection ports and a data/power source. At least one of the connection ports are operable to cooperate with a connector of an external device to supply at least one of power and data signals to the external device. The power/data bus, when used in an aircraft passenger cabin, eliminates the need to extend individual data and/or power cables to or between each passenger seat group.

Claims

1. An apparatus for enabling communication of signals with communication ports associated with a plurality of spaced apart seats supported along a common support track, the apparatus comprising:

a signal bus adapted to be disposed at least approximately parallel to the support track without interfering with support structure of said seats being coupled to said support track;

said signal bus including an elongated jacket extending along at least a major portion of a length of said support track;

said jacket including;

a conductor housed therein for communicating said signals therethrough; and

a plurality of embedded coupling ports at spaced apart locations along said jacket corresponding to approximate locations of said seats, each of said spaced apart coupling ports being in communication with said conductor and adapted to engage with connectors of external cables associated with said communication ports of said seats.

2. The apparatus of claim 1, wherein at least one of said coupling ports comprises a latching member for cooperating with a latching portion on at least one of said connectors of said cables to secure said one connector to said jacket.

3. The device of claim 1, wherein said coupling ports extend from said jacket.

4. The device of claim 1, further comprising a cover operable to mate with said coupling port when said coupling port is not in use.

5. The device of claim 4, wherein said cover is slidably secured to said jacket.

6. The device of claim 1, wherein said bus further comprises a plurality of indentations within said jacket;

wherein said coupling ports each further comprise an outlet; and

wherein said outlets are located within said indentations.

7. The device of claim 1, wherein said coupling port is movable between a first position in which said coupling port is recessed within said jacket and a second position in which said coupling port extends from within said jacket.

8. The device of claim 7, wherein said coupling port further comprises a pin that cooperates with a track;

wherein said track has a first portion and a second portion that extends from said first portion at an angle;

wherein said coupling port is operable to move between said first position and said second position when said pin is in said first portion; and

wherein said coupling port is locked in said second position when said pin is in said second portion.

9. The device of claim 8, further comprising a cover having a release rod;

wherein when said cover mates with said coupling port said release rod contacts said pin to move said pin to said first portion of said track to permit movement of said coupling port to said first position.

10. The device of claim 1, wherein said coupling port is secured to said bus by a flexible cord to permit movement of said coupling port between a storage position and an operable position;

and

wherein said coupling port further comprises an outlet on a first side of said coupling port and a mounting knob on a second side of said coupling port opposite said first side.

11. The device of claim 10, wherein said bus further comprises a support pocket and a stowage pocket;

wherein said outlet of said coupling port is seated within said stowage pocket when said coupling port is in said storage position; and

wherein said mounting knob of said coupling port is seated within said support pocket when said coupling port is in said operable position.

12. The device of claim 10, wherein said bus further comprises a stowage pocket;

and

wherein said mounting knob is seated within said stowage pocket when said coupling port is in said operable position; and

wherein said outlet is seated within said stowage pocket when said coupling port is in said storage position.

13. The device of claim 1, wherein said coupling port is recessed within said bus;

and

wherein said connector includes a recess to receive and store a protective cap.

14. The device of claim 7, wherein said coupling port further comprises a cavity and a movable tab seated within said cavity, said tab movable between a recessed position where said tab is recessed within said cavity and an extended position where said tab extends from within said cavity to contact said jacket;

wherein said tab is positioned in said recessed position when said coupling port is in said first position and said tab is positioned in said extended position when said coupling port is in said second position.

15. The device of claim 14, wherein said tab is moved from said extended position to said recessed position through cooperation between a cover and said tab.

16. The device of claim 15, wherein a rod portion of said cover contracts said tab;

and

wherein both said rod portion and said recessed portion have a dove-tail shape.

17. An aircraft comprising:

an elongated electrical signal bus extending across at least a portion of a passenger cabin thereof;

a plurality of discrete connection ports spaced apart at different locations along said electrical signal bus; and

a conductor extending through said electrical signal bus, said conductor connected to a plurality of said spaced apart discrete connection ports and connected to an electrical signal source;

at least one of said connection ports adapted to be coupled to a connector of a passenger seat to transmit electrical signals between said passenger seat and said electrical signal source.

18. The aircraft of claim 17, wherein said connection ports extend from a body of said electrical signal bus.

19. The aircraft of claim 17, further comprising a plug operable to mate with said connection port when said connection port is not in use.

20. The aircraft of claim 17, wherein said electrical signal bus further comprises a plurality of indentations within a body of said electrical signal bus;

wherein said connection ports each further comprise an outlet; and

wherein said outlets are located within said indentations.

21. The aircraft of claim 17, wherein said connection port is movable between a first position in which said connection port is recessed within said electrical signal bus and a second position in which said connection port extends from within said electrical signal bus.

22. The aircraft of claim 17, wherein said connection port is secured to said electrical signal bus by a flexible cord to permit movement of said connection port between a storage position and an operable position;

and

wherein said connection port further comprises an outlet on a first side of said connection port and a mounting knob on a second side of said connection port opposite said first side.

23. A method for conducting at least one of data and power signals to a plurality of individual locations comprising:

forming an elongated bus extending across an area where access to at least one of data and power is desired;

forming a plurality of discrete connection ports spaced apart at different locations along said bus; and

locating a conductor in said bus and connecting said discrete connection ports to said conductor;

using said conductor to conduct at least one of power and data signals between said discrete connection ports and a signal source; and

using at least one of said connection ports to supply at least one of power and data signals to a connector of an external device.