Communication system and method for an aircraft cargo/freight handling system

• US 10,518,898 B2
• Filed: 05/13/2016
• Issued: 12/31/2019
• Est. Priority Date: 05/13/2016
• Status: Active Grant

• Current Assignee: Goodrich Corporation (Rtx Corporation)
• Original Assignee: Goodrich Corporation (Rtx Corporation)
• Inventors: Lopez, Daniel Diaz, Agrawal, Piyush, Foley, Raymond, Veronesi, William A., Harms, Scott
• Primary Examiner(s): Skibinski, Tomi
• Application Number:
  US15/153,949
• Publication Number:
  US 20170327242A1
• Time in Patent Office: 1,327 Days
• Field of Search: 307 91, 370276
• CPC Class Codes: B64D 47/00 Equipment not otherwise provided for
• CPC Class Codes: H02M 1/44 Circuits or arrangements for compensating for electromagnetic interference in converters or inverters
• CPC Class Codes: H02M 7/44 by static converters
• CPC Class Codes: H04B 2203/547 via DC power distribution
• CPC Class Codes: H04B 2203/5491 using filtering and bypassing
• CPC Class Codes: H04B 3/548 the power on the line being DC arrangements for feeding power H04L12/10; extracting feeding power from signals H04L25/02
• CPC Class Codes: H04L 2012/2843 Mains power line

Abstract

Systems for exchanging information between a cargo handling system of an aircraft and a Power Drive Unit (PDU) are described herein. The systems include a power source provided within the aircraft and a first PDU provided within the aircraft. The power source is capable of providing DC power to the at least one PDU via an electrical power line. The power source further including a first Power Line Communication (PLC) node and the PDU further including a second Power Line Communication (PLC) node. The first PLC node being capable of communicating with the second PLC node via the electrical power line.

Claims

1. A system for sending a signal between a power source and at least one Power Drive Unit (PDU) of a cargo handling system of an aircraft, comprising:

said power source provided within said aircraft, and

said at least one PDU provided within said aircraft,

said power source being capable of providing DC power to said at least one PDU via an electrical power line;

said power source further comprising a first Power Line Communication (PLC) node;

said at least one PDU further comprising a second Power Line Communication (PLC) node;

said first PLC node being capable of sending said signal between said first PLC node and said second PLC node via said electrical power line, wherein said at least one PDU comprises;

a motor;

a DC/AC power inverter;

a DC EMI filter; and

an input connector; and

wherein;

said motor is connected to said DC/AC power inverter and said DC/AC power inverter is connected to said DC EMI filter; and

wherein said DC EMI filter is connected to said electrical power line via said input connector,

wherein said second PLC node located in said PDU is connected to said electrical power line at said input connector between said electrical power line and said DC EMI filter.

2. The system of claim 1, wherein said first PLC node comprises a first PLC sub-circuit;

and

said second PLC node comprises a second PLC sub-circuit;

and wherein said first and second PLC sub-circuits comprise a PLC modem connected to an analogue front end (AFE).

3. The system of claim 2, wherein said AFE comprises:

a protection circuit; and

coupling capacitors; and

wherein;

said PLC modem is connected to said protection circuit, and said protection circuit is connected, via said coupling capacitors, to said electrical power line.

4. The system of claim 3, wherein said electrical power line comprises first and second power wires and wherein one of said coupling capacitors is connected to each of said power wires.

5. The system of claim 2, wherein said AFE complies with DO-160 requirements for said aircraft.

6. The system of claim 1, wherein said power source is connected to an AC input source, and wherein said power source comprises:

an AC filter;

a rectifier stage;

a DC filter; and

an output connector and wherein;

said AC filter is capable of receiving an AC current from said AC input source; and

wherein;

said AC filter is connected to said rectifier stage, said rectifier stage is connected to said DC filter and said DC filter is connected to said electrical power line via said output connector.

7. The system of claim 6, wherein said first PLC node is located between said DC filter and said output connector.

8. The system of claim 1, wherein the first PLC node is located within the power source and is capable of sending a command signal to the second PLC node located in the at least one PDU to actuate said at least one PDU.

9. The system of claim 1, wherein a communication between the first PLC node and the second PLC node is bidirectional and the second PLC node is located within the at least one PDU and is capable of sending a return signal back to the first PLC node that is located within the power source.

10. The system of claim 1, further comprising a plurality of said PDUs and wherein said first PLC node is capable of individually communicating via said electrical power line with each of said plurality of PDUs.

11. The system of claim 10, wherein said electrical power line comprises a plurality of branches and wherein at least one of said branches comprises at least one PDU.

12. A method for sending a signal between a power source and at least one Power Drive Unit (PDU) of a cargo handling system of an aircraft;

said method comprising;

connecting a first Power Line Communication (PLC) node to said power source;

connecting a second Power Line Communication (PLC) node to said at least one PDU; and

providing DC power from said power source to said at least one PDU via an electrical power line;

said first PLC node being capable of communicating with said second PLC node via said electrical power line, and sending said signal between said first PLC node and said second PLC node via said electrical power line, wherein said at least one PDU comprises;

a motor;

a DC/AC power inverter;

a DC EMI filter; and

an input connector; and

wherein;

said motor is connected to said DC/AC power inverter and said DC/AC power inverter is connected to said DC EMI filter; and

wherein said DC EMI filter is connected to said electrical power line via said input connector,

wherein said second PLC node located in said PDU is connected to said electrical power line at said input connector between said electrical power line and said DC EMI filter.

13. The method of claim 12, further comprising

providing a first PLC sub-circuit in said first PLC node and providing a second PLC sub-circuit in said second PLC node

and further comprising providing a PLC modem connected to an analogue front end (AFE) in each of said PLC sub-circuits, wherein said AFE comprises:

a protection circuit; and

capacitors; and

said method further comprising connecting said modem to said protection circuit and connecting said protection circuit to said electrical power line via said capacitors.