Aircraft data networks

Patent metadata

Field	Value
Publication number	US-9838436-B2
Application number	US-201514672639-A
Country	US
Kind code	B2
Filing date	Mar 30, 2015
Priority date	Mar 30, 2015
Publication date	Dec 5, 2017
Grant date	Dec 5, 2017

Abstract

An aircraft data network is provided that can include a first Remote Data Concentrator (RDC), a network switch and a second RDC. The first RDC can receive one or more input signals comprising data from a transmitting system, and translate the data per a network protocol to generate translated data having a format in accordance with the network protocol. The network switch can receive the translated data from the first RDC, determine a destination for at least some of the translated data, and route at least some of the translated data toward a first receiving system. The second RDC can receive at least some of the translated data from the network switch, convert at least some of the translated data to generate converted data having a format designed for use by the first receiving system, and communicate the converted data to the first receiving system.

First claim

What is claimed:

1. An aircraft data network, comprising:
a first communication path between a first transmitting system and a first receiving system, comprising:
a first Remote Data Concentrator (RDC) configured to: receive one or more input signals comprising data from the first transmitting system; and translate the data to generate translated data;
a network switch, communicatively coupled to the first RDC via a bus, the network switch being configured to: receive the translated data from the first RDC; determine a destination for at least some of the translated data from the first RDC; and route the at least some of the translated data from the network switch toward the first receiving system;
a second RDC configured to: receive the at least some of the translated data from the network switch; convert the at least some of the translated data from the network switch to generate converted data having a format designed for use by the first receiving system; and communicate the converted data from the second RDC to the first receiving system;
wherein the first RDC, the network switch, and the second RDC collectively define a first hardware and software of the first communication path; and
a second communication path between the first transmitting system and the first receiving system, comprising:
a first remote interface unit (RIU) configured to: receive the one or more input signals comprising the data from the first transmitting system; and translate the data to generate translated data;
a processing unit, communicatively coupled to the first RIU, the processing unit being configured to: receive the translated data from the first RIU; determine a destination for at least some of the translated data from the first RIU; and route the at least some of the translated data from the processing unit toward the first receiving system; and
a second RIU configured to: receive the at least some of the translated data from the processing unit; convert the at least some of the translated data from the processing unit to generate converted data for use by the first receiving system; and communicate the converted data from the second RIU to the first receiving system,
wherein the first RIU, the processing unit, and the second RIU collectively define a second hardware and software of the second communication path, and
wherein the first hardware and software of the first communication path is different from the second hardware and software of the second communication path.

2. The aircraft data network according to claim 1 , further comprising:
a second receiving system communicatively coupled to the second RDC, wherein the second receiving system is separate and distinct from the first receiving system; and
wherein the second RDC is configured to: receive other translated data from the network switch; convert the other translated data to generate other converted data having a format designed for use by the second receiving system, and communicate the other converted data to the second receiving system.

3. The aircraft data network according to claim 2 , further comprising:
a third communication path between the first transmitting system and the first receiving system, comprising:
a first wired connection that carries the data from the first transmitting system directly to the first receiving system; and
a fourth communication path between the first transmitting system and the second receiving system, the fourth communication path comprising: a second wired connection that carries the data from the first transmitting system directly to the second receiving system.

4. The aircraft data network according to claim 3 , further comprising:
a second transmitting system configured to transmit one or more input signals comprising a redundant version of the data, wherein the second transmitting system is separate and distinct from the first transmitting system; and
a fifth communication path to the first receiving system, comprising: a third wired connection that carries the redundant version of the data directly from the second transmitting system to the first receiving system; and a sixth communication path between the second transmitting system and the first receiving system, comprising: the first RDC, the network switch and the second RDC.

5. The aircraft data network according to claim 4 , further comprising:
a seventh communication path to the second receiving system, comprising:
a fourth wired connection that carries the redundant version of the data from the second transmitting system directly to the second receiving system; and
an eighth communication path between the second transmitting system and the second receiving system, comprising: the first RDC, the network switch and the second RDC.

6. The aircraft data network according to claim 1 , further comprising: wherein the first RDC comprises hardware and software, and wherein the first RIU comprises hardware and software that is different than the hardware and the software of the first RDC;
wherein the network switch comprises hardware and software, and wherein the processing unit comprises hardware and software that is different than the hardware and the software of the network switch; and
wherein the second RDC comprises hardware and software, and wherein the second RIU comprises hardware and software that is different than the hardware and the software of the second RDC.

7. The aircraft data network according to claim 1 , wherein the data comprises critical data, wherein the critical data comprises:
communication data that is used by the first receiving system;
navigation data that is used by the first receiving system; or
aviation data that is used by the first receiving system.

8. The aircraft data network according to claim 1 , wherein the first receiving system comprises: a flight control computer.

9. The aircraft data network according to claim 1 , wherein the first receiving system comprises: an avionics system.

10. The aircraft data network according to claim 1 , wherein the first receiving system comprises: a display.

11. The aircraft data network according to claim 1 , wherein the first transmitting system comprises: a communication system.

12. The aircraft data network according to claim 1 , wherein the first transmitting system comprises: an inertial reference system (IRS).

13. The aircraft data network according to claim 1 , wherein the first transmitting system comprises: an attitude heading and reference system (AHRS).

14. The aircraft data network according to claim 1 , wherein the first transmitting system comprises: an air data system (ADS).

15. An aircraft, comprising:
an aircraft data network, comprising:
a plurality of transmitting systems each being configured to generate signals comprising data, the plurality of transmitting systems comprising: a first transmitting system; a plurality of receiving systems that consume the data, comprising: a first receiving system;
a first communication path between the first transmitting system and the first receiving system, comprising
a first Remote Data Concentrator (RDC) configured to: receive one or more input signals comprising the data from the first transmitting system; and translate the data per a network protocol to generate translated data having a format in accordance with the network protocol;
a network switch, communicatively coupled to the first RDC via a bus, the network switch being configured to: receive the translated data from the first RDC; determine a destination for at least some of the translated data from the first RDC; and route the at least some of the trans

Assignees

• Gulfstream Aerospace Corp

Inventors

• Michaels Charles

Classifications

• H04L12/462

  LAN interconnection over a bridge based backbone · CPC title

• H04L2012/4028

  the transportation system being an aircraft · CPC title

• H04L65/1013 Primary

  Network architectures, gateways, control or user entities · CPC title

• H04L67/12 Primary

  specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks · CPC title

• H04L12/40 Primary

  Bus networks · CPC title