Methods and systems for vehicle communication to a data network

• US 9,876,533 B2
• Filed: 04/19/2013
• Issued: 01/23/2018
• Est. Priority Date: 04/19/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Lee, Donald B., Mitchell, Timothy M., Ward, Brian E.
• Primary Examiner(s): Barnie, Rexford
• Assistant Examiner(s): Chowdhuri, Swarna N
• Application Number:
  US13/866,348
• Publication Number:
  US 20140312682A1
• Time in Patent Office: 1,740 Days
• Field of Search: None
• CPC Class Codes: H04B 2203/5408 using protocols
• CPC Class Codes: H04B 2203/5441 Wireless systems or telephone
• CPC Class Codes: H04B 2203/5445 Local network
• CPC Class Codes: H04B 2203/5454 Adapter and plugs
• CPC Class Codes: H04B 2203/5483 using coupling circuits
• CPC Class Codes: H04B 3/54 Systems for transmission via power distribution lines
• CPC Class Codes: H04B 3/56 Circuits for coupling, blocking, or by-passing of signals

Abstract

Methods, systems, and an integrated Broadband over Power Line (BPL) module cover assembly for communicating data between an aircraft and a ground-based network are provided. The assembly includes a power receptacle cover plate and a BPL module coupled to said power receptacle cover plate.

Claims

1. An integrated Broadband over Power Line (BPL) module cover assembly for communicating between an aircraft and a ground-based network, said integrated BPL module cover assembly comprising:

a power receptacle cover plate configured to be coupled to a stinger connector onboard the aircraft, the stinger connector configured to receive a ground power stinger cable associated with a ground-based power unit, said power receptacle cover plate configured to cover a plurality of electrical leads extending through a power receptacle of the stinger connector to a power bus of the aircraft; and

a BPL module integrated with said power receptacle cover plate and comprising a first phase connector configured to be electrically coupled to a first power receptacle pin of the power receptacle and a neutral connector configured to be electrically coupled to a second power receptacle pin of the power receptacle for electrically coupling directly to at least one of the plurality of electrical leads of the stinger connector, said BPL module configured to receive power and communicate with the ground-based network via the ground power stinger cable.

2. An integrated BPL module cover assembly in accordance with claim 1, wherein said integrated BPL module cover assembly comprises at least one hole defined therein configured to mate with the stinger connector via at least one bolt.

3. An integrated BPL module cover assembly in accordance with claim 1, wherein said first phase connector and said neutral connector are coupled to said BPL module.

4. An integrated BPL module cover assembly in accordance with claim 1, further comprising an Ethernet connector configured to be coupled to an Ethernet interface of the aircraft.

5. A system for communicating between an aircraft and a ground-based network, said system comprising:

a stinger connector onboard the aircraft and configured to be coupled to a ground power stinger cable associated with a ground-based power unit, said stinger connector comprising a power receptacle and a plurality of electrical leads for receiving power from the ground power stinger cable and extending through the power receptacle into the aircraft; and

an integrated Broadband over Power Line (BPL) module cover assembly coupled to said stinger connector and configured to communicate with the ground-based network, said integrated BPL module cover assembly comprising;

a power receptacle cover plate configured to be coupled to said stinger connector, said power receptacle cover plate configured to cover the plurality of electrical leads extending through said power receptacle of said stinger connector to a power bus of the aircraft, said power receptacle comprising a first power receptacle pin and a second power receptacle pin configured to output power received from the ground power stinger cable;

a BPL module integrated with said power receptacle cover plate and comprising a connector for electrically coupling directly to at least one of the plurality of electrical leads of said stinger connector, said BPL module configured to receive power and communicate with the ground-based network via the ground power stinger cable;

a first phase connector configured to be electrically coupled to said first power receptacle pin; and

a neutral connector configured to be electrically coupled to said second power receptacle pin.

6. A system in accordance with claim 5, wherein said BPL module is coupled directly to the ground power stinger cable.

7. A system in accordance with claim 5, wherein said power receptacle comprises:

at least one bolt for engaging with at least one hole defined in said integrated BPL module cover assembly; and

at least one lug for securing said integrated BPL module cover assembly onto said at least one bolt.

8. A system in accordance with claim 5, wherein said power receptacle comprises a first power receptacle pin and said second power receptacle pin are configured to output power received from the ground power stinger cable.

9. A method of communicating between an aircraft and a ground-based network, said method comprising:

providing a stinger connector onboard the aircraft configured to be coupled to a ground power stinger cable associated with a ground-based power unit, the stinger connector including a power receptacle and a plurality of electrical leads for receiving power from the ground power stinger cable and extending through the power receptacle to a power bus of the aircraft;

coupling an integrated Broadband over Power Line (BPL) module cover assembly to the stinger connector within the aircraft, the integrated BPL module cover assembly including a power receptacle cover plate configured to be coupled to said stinger connector, said power receptacle cover plate configured to cover the plurality of electrical leads extending through the power receptacle of the stinger connector into the aircraft, and a BPL module integrated with the power receptacle cover plate and including a first phase connector configured to be electrically coupled to a first power receptacle pin of the power receptacle and a neutral connector configured to be electrically coupled to a second power receptacle pin of the power receptacle for electrically coupling directly to at least one of the plurality of electrical leads of the stinger connector, the BPL module configured to receive power and communicate with the ground-based network via the ground power stinger cable;

initiating a BPL link between the aircraft and the ground-based network when power is supplied to the aircraft; and

updating data stored in the aircraft with data received from the ground-based network.

10. A method in accordance with claim 9, further comprising configuring the integrated BPL module cover assembly to receive power directly from the ground power stinger cable.

11. A method in accordance with claim 10, wherein configuring the integrated BPL module cover assembly to receive power directly from the ground power stinger cable further comprises:

defining at least one hole in the integrated BPL module cover assembly; and

attaching the integrated BPL module cover assembly to the stinger connector by mating at least one bolt of the stinger connector with the at least one hole.

12. A method in accordance with claim 9, wherein updating data further comprises updating data using cached web content.

13. A method in accordance with claim 9, further comprising:

communicatively coupling the BPL module cover assembly to a ground-based unit via one of a wireless connection and the ground power stinger cable; and

communicatively coupling the ground-based unit to the ground-based network.