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US4853555A Expired / Lapsed US ⏱️ 0.0 years remaining

Electrical power transfer system for aircraft passenger entertainment system

Assignee: Boeing Co
•
Filing: 1988-04-21
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Granted: 1989-08-01
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Expires: 2008-04-21
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Abstract

Abstract A conductor rail assembly parallel to an aircraft passenger seat track is coupled by direct electrical connection to the aircraft passenger entertainment system power supply. Passenger seat entertainment system power connectors are inserted into and retained in the conductor rail assembly to distribute power to the individual seat receivers.

Inventors

  • 👤 Lawrence M. Wheat

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 08:29
CPC Classifications
B; B64; B64C; B64C1/00; B64C1/18; B64C1/20; B64D; B64D11/00; B64D11/06; B64D11/0624; H; H01; H01R; H01R25/00; H01R25/16

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 146 words
An electrical power transfer system for an aircraft Passenger entertainment system comprising in combination: an aircraft passenger seat track having a plurality of apertures distributed there along for insertion of passenger seat legs; said seat track having a rectangularly shaped cross section; a plurality of passenger seat entertainment system power connectors; a conductor rail assembly having a plurality of apertures distributed there along for receiving said plurality of passenger seat entertainment system power connectors, said conductor rail assembly having a rectangularly shaped cross section; a passenger entertainment system power supply; said conductor rail assembly having an enclosed conductive strip extending along the length thereof in electrically insulated relationship with respect to said seat track; said passenger entertainment system power supply coupled between said conductive strip and said seat track; and, said plurality of passenger seat entertainment system power connectors making electrical contact with said conductive strip.
Claim 2
Dependent Claim 146 words
An electrical power transfer system for an aircraft Passenger entertainment system comprising in combination: an aircraft passenger seat track having a plurality of apertures distributed there along for insertion of passenger seat legs; said seat track having a rectangularly shaped cross section; a plurality of passenger seat entertainment system power connectors; a conductor rail assembly having a plurality of apertures distributed there along for receiving said plurality of passenger seat entertainment system power connectors, said conductor rail assembly having a rectangularly shaped cross section; a passenger entertainment system power supply; said conductor rail assembly having an enclosed conductive strip extending along the length thereof in electrically insulated relationship with respect to said seat track; said passenger entertainment system power supply coupled between said conductive strip and said seat track; and, said plurality of passenger seat entertainment system power connectors making electrical contact with said conductive strip.
Claim 3
Dependent Claim 19 words
The electrical power transfer system according to claim 1 wherein said conductor rail assembly comprises an electrically insulative material.
Claim 4
Dependent Claim 16 words
The electrical power transfer system according to claim 2 wherein said electrically insulative material comprises polycarbonate.
Claim 5
Dependent Claim 39 words
The electrical power transfer system according to claim 1 wherein each of said plurality of passenger seat entertainment power connectors comprises an electrically insulative housing enclosing a carbon electrical contact for making spring pressure contact with said conductive strip.
Claim 6
Dependent Claim 30 words
The electrical power transfer system according to claim 4 wherein rotation through 90 degrees of said electrically insulative housing causes wiping of said conductive strip by said carbon electrical contact.

References Cited (Backward Citations)

US3401469A Cited
US3553675A Cited
US4428078A Cited
US4736452A Cited
US4763360A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-07-31 1993-01-30 1993-08-01 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-07-31 1997-01-30 1997-08-01 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-07-31 2001-01-30 2001-08-01 $7700.00 Window Closed / Lapsed

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