Data request method without using dedicated connections

• US 6,918,134 B1
• Filed: 09/27/2000
• Issued: 07/12/2005
• Est. Priority Date: 09/27/2000
• Status: Expired due to Term

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Preston, Robert W., Sherlock, Daniel J.
• Primary Examiner(s): BUI, KIEU OANH T
• Application Number:
  US09/670,972
• Time in Patent Office: 1,749 Days
• Field of Search: 725/76, 725/130, 725/150, 348/837
• US Class Current: 725/76
• CPC Class Codes: B64D 11/0015 Arrangements for entertainment or communications, e.g. radio, television
• CPC Class Codes: B64D 11/00155 Individual entertainment or communication system remote controls therefor, located in or connected to seat components, e.g. to seat back or arm rest
• CPC Class Codes: H04N 21/2146 located in mass transportation means, e.g. aircraft, train or bus flight-deck installations for entertainment or communications B64D11/0015; arrangements specially adapted for transportation systems in broadcast systems H04H20/62; moving wireless networks H04W84/005
• CPC Class Codes: H04N 21/25833 involving client hardware characteristics, e.g. manufacturer, processing or storage capabilities allocation of resources considering hardware capabilities in multiprogramming arrangements G06F9/5044; allocation of resources considering software capabilities in multiprogramming arrangements G06F9/5055
• CPC Class Codes: H04N 21/6118 involving cable transmission, e.g. using a cable modem
• CPC Class Codes: H04N 21/6168 involving cable transmission, e.g. using a cable modem

Abstract

In-flight entertainment systems provide entertainment for passengers on commercial airline flights. Presently, usually on longer flights, video entertainment is commonly available on in-flight passenger entertainment systems. In-flight entertainment systems can display video on a variety of display monitors ranging from a conventional CRT display to a more modern Liquid Crystal Display (LCD). Generally most displays are connected to the aircraft electronic system via a ARINC 722 connector. The ARINC 722 connector commonly provides an electrical interface between the aircraft and the video system, whether the video system is a CRT or LCD type monitor. With the increasing use of LCD monitors there is a greater need for the ability of the display monitor to be able to report its status. The need for status reporting is increased because the LCD monitors are often greater in number than the prior art CRT monitors and because malfunctions are less obvious. Several methods for providing status information from video displays have been proposed. Embodiments of the present invention comprise a system in which data can be requested by repeating commands, such as turn on, a number of times within a predetermined time interval. Because embodiments of the invention use an existing command, which can be the repeated without affecting the functioning of legacy systems, the need for modification of the airline and monitor systems is greatly reduced.

Claims

1. A system for gathering data from a commercial airline display unit, the system comprising:

an electronic unit for requesting and receiving said data, said electronic unit requesting said data by providing a first signal to the commercial airline display unit a predetermined number of times within a predetermined time interval;

said airline display unit receiving said first signal and providing superimposed said data upon a static status signal, said superimposed data being provided to said electronic unit; and

a receiver within the electronic unit receiving and decoding the superimposed data.

2. A system as recited in claim 1, wherein the electronic unit comprises a commercial aircraft tapping unit.

3. A system as recited in claim 1 wherein the static status signal comprises the “

on indicator”

on pin 8 of an ARINC 722 connector.

4. A system as recited in claim 1 wherein the first signal is the power control on signal.

5. A system as recited in claim 1 wherein the first signal is provided to pin 6, the power control on input, of an ARINC 722 connector on said commercial airline display unit.

6. A system as recited in claim 1 wherein the display is part of an in-flight entertainment system.

7. A system as recited in claim 1 wherein said airline display unit further comprises:

an ARINC connector,

a power on detection circuit coupled to receive a power-on signal along pin 6 of said ARINC connector and providing an output signal in response to detection of said power-on signal;

a delay circuit connected to an output of said detection circuit and responsive to said power-on signal to generate a delayed signal; and

said airline display unit responsive to said delay signal for transmitting a plurality of additional status signals.

8. A system as recited in claim 7 wherein said airline display unit responds to a predetermined sequence of additional signals along pin 6 of said ARINC connector to transmit current values of said plurality of additional status signals.

9. A system as recited in claim 7 wherein said airline display unit further comprises a memory device for storing said plurality of additional status signals upon the occurrence of said built-in-test signal indicating a failure of said display unit.

10. A system for gathering data from a commercial airline display unit, the system comprising:

electronic unit means for requesting and receiving said data, said electronic unit requesting said data by providing a first signal to the commercial airline display unit;

said airline display unit receiving said first signal and providing said data as superimposed data in the form of a serial or modulated data stream upon a static status signal, said superimposed data being provided to said electronic unit; and

receiver means within the electric unit for receiving and decoding the superimposeed data.

11. A system as recited in claim 10 wherein the electronic unit means comprises a commercial aircraft tapping unit.

12. A system as recited in claim 11 wherein the static status signal comprises the “

on indicator”

on pin 8 of an ARINC 722 connector.

13. A system as recited in claim 12 wherein the first signal is the power control on signal.

14. A system as recited in claim 10 wherein the first signal is coupled to pin 6, of an ARINC 722 connector on said commercial airline display unit.

15. A system as recited in claim 10 wherein said airline display unit further comprises:

an ARINC connector;

a power on detection means for receiving a power-on signal along pin 6 of said ARINC connector and providing an output signal in response to detection of said power-on signal;

a delay circuit means for responding to said output signal to generate a delayed signal; and

said airline display unit responsive to said delay signal for transmitting a plurality of additional stats signals, wherein the additional status signals are provided as superimposed data.

16. A system as recited in claim 15 wherein said airline display unit responds to a predetermined sequence of additional signals along pin 6 of said ARINC connector to transmit current values of said plurality of addition status signals.

17. A system as recited in claim 16 wherein said airline display unit further comprises a memory means for storing said plurality of additional status signals upon the occurrence of said built-in-test signal indicating a failure of said display unit.

18. A method of gathering data from a commercial airline display unit, the method comprising:

requesting said data with an electronic unit from a commercial airline display unit, said electronic unit requesting said data by providing a first signal to the commercial airline display unit;

providing superimposed data in the form of a serial or modulated data stream upon a static status signal said superimpose data being provided to said electronic unit; and

receiving and decoding the superimposed data.

19. A system as recited in claim 18 wherein the static status signal comprises the “

on indicator”

on pin 8 of an ARINC 722 connector.

20. A system as recited in claim 19 wherein the first signal is the power control on signal.