National marine electronics association protocol converter

• US 20020188776A1
• Filed: 04/06/2001
• Published: 12/12/2002
• Est. Priority Date: 04/06/2001
• Status: Active Grant

• Current Assignee: Houlberg, Christian L.
• Original Assignee: Houlberg, Christian L.
• Inventors: Houlberg, Christian L.
• Granted Patent: US 6,718,409 B2
• Time in Patent Office: Days
• US Class Current: 710/62
• CPC Class Codes: H04L 67/12 specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
• CPC Class Codes: H04L 69/08 Protocols for interworking; Protocol conversion
• CPC Class Codes: H04L 69/329 in the application layer [OSI layer 7]

Abstract

A protocol converter for use on board an aircraft with space limitations which converts navigation data from one format to another format for use by the aircraft'"'"'s moving map display. The navigation data is supplied by an aircraft inertial navigation unit to the protocol converter in the ARINC-429 protocol which converts the data to the NMEA-0183 protocol. The converted data is then supplied to a moving map display on board the aircraft. An interface board receives ARINC navigational data from the aircraft navigation unit and stores the data prior to its transfer to a digital computer. The computer reads the data stored in the interface board including a status word which indicates the validity of the data. A computer software program within the computer converts the ARINC-429 navigational data to NMEA-0183 protocol data. The NMEA-0183 protocol data is transmitted through an RS-232 serial port to the moving map display.

Claims

1. A protocol converter for use on board aircraft comprising:

a housing having a front panel;

a computer board positioned in a stack within said housing;

an interface board positioned in said stack within said housing, said interface board being connected to said computer board;

a power board positioned in said stack within said housing, said power board being connected to said interface board and said interface board to provide electrical power to said interface board and said computer board;

said interface board having a pair of data inputs, one of said pair of data inputs receiving ARINC-429 navigation data from a source within said aircraft, said interface board storing said ARINC-429 navigation data therein;

said computer board including a computer software program for operating said computer board, said computer board, responsive to said computer software program, reading said ARINC-429 navigation data from said interface board and then converting said ARINC-429 navigation data to NMEA-0183 navigation data;

said computer board providing a request to send signal to a moving map display located on board said aircraft to effect a transfer of said NMEA-0183 navigation data to said moving map display;

said computer board, responsive to a clear to send signal from said moving map display transferring said NMEA-0183 navigation data to said moving map display.

2. The protocol converter of claim 1 wherein said housing comprises a box shape structure having a length of 6.97 inches, a width of 4.95 inches and a height of 4.16 inches.

3. The protocol converter of claim 2 wherein said housing has a first flange attached to said front panel and a second flange attached to a rear panel of said housing, said first and second flanges being adapted for mounting said protocol converter on said aircraft, said first and said second flanges each having a pair of mounting holes, said protocol converter including said first and said second flanges having an overall length of 7.95 inches.

4. The protocol converter of claim 1 wherein said provides said electrical power to said interface board and said computer board at power levels of +5 VDC, −

5 VDC, +12 VDC and −

12 VDC.

5. The protocol converter of claim 1 wherein said ARINC-429 navigation data comprises 32 bit data words, each of said 32 bit data words has an eight bit label field, twenty one data bits, a pair of status bits and a parity bit.

6. The protocol converter of claim 5 wherein said computer board reads said pair of parity bits of each of said 32 bit data words to determine when said 32 bit data words contain valid navigation data, said valid navigation data occurring whenever said pair of parity bits consist of a pair of logic ones

7. The protocol converter of claim 1 further comprising a fan board positioned in said stack within said housing.

8. The protocol converter of claim 1 further comprising first, second, third and fourth indicator lights located on the front panel of said housing, said first, second, third and fourth indicator lights being connected to said interface board, said first and second indicator lights when activated indicating which one of said pair of data inputs on said interface board is receiving ARINC-429 navigation data from a source.

9. The protocol converter of claim 8 wherein said third and fourth indicator lights when activated indicating which of a pair of serial outputs on said computer board is transferring said NMEA-0183 navigation data to said moving map display.

10. The protocol converter of claim 1 further comprising a circuit breaker connected to said power board, said circuit breaker including a reset button to reset said circuit breaker after circuit breaker deactivates said protocol converter, said circuit breaker being mounted on the front panel of said housing.

11. The protocol converter of claim 1 further comprising a reset switch connected to said computer board, said reset switch being mounted on the front panel of said housing.

13. The protocol converter of claim 12 wherein said housing comprises a box shape structure having a length of 6.97 inches, a width of 4.95 inches and a height of 4.16 inches.

14. The protocol converter of claim 13 wherein said housing has a first flange attached to said front panel and a second flange attached to a rear panel of said housing, said first and second flanges being adapted for mounting said protocol converter on said aircraft, said first and said second flanges each having a pair of mounting holes, said protocol converter including said first and said second flanges having overall length of 7.95 inches.

15. The protocol converter of claim 12 wherein said provides said electrical power to said interface board and said computer board at power levels of +5 VDC, −

5 VDC, +12 VDC and −

12 VDC.

16. The protocol converter of claim 12 further comprising:

first, second, third and fourth indicator lights located on the front panel of said housing, said first, second, third and fourth indicator lights being connected to said interface board;

said first and second indicator lights when activated indicating which one of said pair of data inputs on said interface board is receiving ARINC-429 navigation data from a source.

said third and fourth indicator lights when activated indicating which of a pair of serial outputs on said computer board is transferring said NMEA-0183 navigation data to said moving map display.

17. The protocol converter of claim 12 further comprising a circuit breaker connected to said power board, said circuit breaker including a reset button to reset said circuit breaker after circuit breaker deactivates said protocol converter, said circuit breaker being mounted on the front panel of said housing.

18. The protocol converter of claim 12 further comprising a reset switch connected to said computer board, said reset switch being mounted on the front panel of said housing.

20. The protocol converter of claim 19 wherein said housing comprises a box shape structure having a length of 6.97 inches, a width of 4.95 inches and a height of 4.16 inches, said housing having a first flange attached to said front panel and a second flange attached to a rear panel of said housing, said first and second flanges being adapted for mounting said protocol converter on said aircraft, said first and said second flanges each having a pair of mounting holes, said protocol converter including said first and said second flanges having overall length of 7.95 inches.

12. A protocol converter for use on board aircraft comprising:

a housing having a front panel;

a computer board positioned in a stack within said housing;

an interface board positioned in said stack within said housing, said interface board being connected to said computer board;

a power board positioned in said stack within said housing, said power board being connected to said interface board and said interface board to provide electrical power to said interface board and said computer board;

said interface board having a pair of data inputs, one of said pair of data inputs receiving ARINC-429 navigation data from an inertial navigation unit located within said aircraft, said interface board storing said ARINC-429 navigation data therein;

said computer board including a computer software program for operating said computer board, said computer board, responsive to said computer software program, reading said ARINC-429 navigation data from said interface board and then converting said ARINC-429 navigation data to NMEA-0183 navigation data;

said computer board, responsive to said computer software program, reading a pair of parity bits within each of a plurality of data words within said ARINC-429 navigation data to determine when said data words contain valid navigation data;

said computer board providing a request to send signal to a moving map display located on board said aircraft to effect a transfer of said NMEA-0183 navigation data to said moving map display;

said computer board, responsive to a clear to send signal from said moving map display transferring said NMEA-0183 navigation data to said moving map display.

19. A protocol converter for use on board aircraft comprising:

a housing having a front panel;

a computer board positioned in a stack within said housing;

an interface board positioned in said stack within said housing, said interface board being connected to said computer board;

a power board positioned in said stack within said housing, said power board being connected to said interface board and said interface board to provide electrical power to said interface board and said computer board;

said interface board having a pair of data inputs, one of said pair of data inputs receiving ARINC-429 navigation data from an inertial navigation unit located within said aircraft, said interface board storing said ARINC-429 navigation data therein;

said computer board including a computer software program for operating said computer board, said computer board, responsive to said computer software program, reading said ARINC-429 navigation data from said interface board and then converting said ARINC-429 navigation data to NMEA-0183 navigation data;

said computer board, responsive to said computer software program, reading a pair of parity bits within each of a plurality of data words within said ARINC-429 navigation data to determine when said data words contain valid navigation data, said valid navigation data occurring whenever said pair of parity bits are a binary three;

said computer board providing a request to send signal to a moving map display located on board said aircraft to effect a transfer of said NMEA-0183 navigation data to said moving map display;

said computer board, responsive to a clear to send signal from said moving map display transferring said NMEA-0183 navigation data to said moving map display;

first, second, third and fourth indicator lights located on the front panel of said housing, said first, second, third and fourth indicator lights being connected to said interface board;

said first and second indicator lights when activated indicating which one of said pair of data inputs on said interface board is receiving ARINC-429 navigation data from a source;

said third and fourth indicator lights when activated indicating which of a pair of serial outputs on said computer board is transferring said NMEA-0183 navigation data to said moving map display.