Wireless data concentrators for aircraft data networks

• US 9,521,678 B2
• Filed: 03/12/2015
• Issued: 12/13/2016
• Est. Priority Date: 03/12/2015
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Dame, Stephen G., Ibrahim, Yakentim M.
• Primary Examiner(s): WILSON, ROBERT W
• Application Number:
  US14/656,623
• Publication Number:
  US 20160270052A1
• Time in Patent Office: 642 Days
• US Class Current: 1/1
• CPC Class Codes: H01Q 1/2291 used in bluetooth or WI-FI devices of Wireless Local Area Networks [WLAN] H01Q1/241 takes precedence; WLAN in general H04W
• CPC Class Codes: H01Q 1/38 formed by a conductive layer on an insulating support patch antennas H01Q9/0407; microstrip dipole antennas H01Q9/065; microstrip slot antennas H01Q13/106; transmission line microstrip antennas H01Q13/206; manufacturing reflecting surfaces using insulating material for supporting the reflecting surface H01Q15/142
• CPC Class Codes: H01Q 1/521 reducing the coupling between adjacent antennas
• CPC Class Codes: H01Q 1/526 Electromagnetic shields
• CPC Class Codes: H01Q 21/28 Combinations of substantially independent non-interacting antenna units or systems multiple beam H01Q25/00
• CPC Class Codes: H01Q 9/04 Resonant antennas
• CPC Class Codes: H01Q 9/0421 with a shorting wall or a shorting pin at one end of the element H01Q9/0414 takes precedence
• CPC Class Codes: H04B 1/40 Circuits
• CPC Class Codes: H04W 4/70 Services for machine-to-machine communication [M2M] or machine type communication [MTC]
• CPC Class Codes: H04W 72/51 based on terminal or device properties

Abstract

Embodiments described herein provide for a four-channel Wireless Data Concentrator (WDC) for a data network of an aircraft. One embodiment of a WDC includes a Printed Circuit Board (PCB), and a controller. The controller is electrically coupled to a top surface of the PCB and is proximate to a centerline of the PCB. The WDC further includes four Radio Frequency (RF) transceivers electrically coupled to the top surface of the PCB that are disposed orthogonally to each other around the controller. Each RF transceiver communicates with at least one wireless sensor that measures an environment of the aircraft. The WDC further includes four inverted-F PCB trace antennas fabricated along the top surface of the PCB. Each inverted-F PCB trace antenna is electrically coupled to one of the RF transceivers and is disposed orthogonally to each other around the controller.

Claims

1. A wireless data concentrator for a data network of an aircraft, the wireless data concentrator comprising:

a Printed Circuit Board (PCB) having a top surface and a bottom surface;

a controller electrically coupled to the top surface of the PCB and proximate to a centerline of the PCB;

four Radio Frequency (RF) transceivers electrically coupled to the top surface of the PCB that are disposed orthogonally to each other around the controller, each configured to communicate with the controller and at least one wireless sensor that measures an environment of the aircraft; and

four inverted-F PCB trace antennas fabricated along the top surface of the PCB, each electrically coupled to one of the RF transceivers and disposed orthogonally to each other around the controller;

the controller configured to receive sensor data about the environment of the aircraft from the at least one wireless sensor utilizing at least one of the RF transceivers, and to provide the sensor data to an application server of the data network of the aircraft utilizing a data backbone of the data network.

2. The wireless data concentrator of claim 1 further comprising:

a connector coupled to the bottom surface of the PCB proximate to the centerline of the PCB that electrically couples the controller to the application server.

3. The wireless data concentrator of claim 1 further comprising:

an RF transparent radome configured to mechanically shield the top surface of the PCB.

4. The wireless data concentrator of claim 1 further comprising:

a metal shield proximate to the top surface of the PCB that is configured to surround the RF transceivers and the controller, and to expose the inverted-F PCB trace antennas.

5. The wireless data concentrator of claim 1 further comprising:

a metal shield proximate to the bottom surface of the PCB that is configured to surround PCB traces for the RF transceivers and the controller, and to expose the bottom surface of the PCB that is adjacent to the inverted-F PCB trace antennas.

6. The wireless data concentrator of claim 1 wherein the sensor data about the environment of the aircraft comprises at least one of a temperature of the environment, a pressure of the environment, and a vibration of the environment.

7. The wireless data concentrator of claim 6 wherein:

the controller is configured to forward the at least one measurement to the application server utilizing the data backbone of the network.

8. The wireless data concentrator of claim 1 wherein:

each of the inverted-F PCB trace antennas are located along an outside edge of the PCB.

9. The wireless data concentrator of claim 8 wherein:

an area along the outside edge of the PCB between each of the inverted-F PCB trace antennas is devoid of PCB traces.

10. The wireless data concentrator of claim 9 wherein:

the PCB is fabricated in a shape of a cross, with each of the inverted-F PCB trace antennas located in one of four ends of the cross.

11. A wireless data concentrator for a data network of an aircraft, the wireless data concentrator comprising:

a Printed Circuit Board (PCB);

a controller electrically coupled to the PCB;

four Radio Frequency (RF) transceivers electrically coupled to the PCB that are disposed around the controller, each configured to communicate with the controller and at least one wireless sensor that measures an environment of the aircraft; and

four inverted-F PCB trace antennas fabricated into the PCB, each electrically coupled to one of the RF transceivers and disposed orthogonally to each other around the controller;

the controller configured to receive sensor data about the environment of the aircraft from the at least one wireless sensor utilizing at least one the RF transceivers, and to provide the sensor data to the data network of the aircraft utilizing a data backbone of the data network.

12. The wireless data concentrator of claim 11 further comprising:

a connector coupled to the bottom surface of the PCB proximate to the controller that electrically couples the wireless data concentrator to the data backbone.

13. The wireless data concentrator of claim 12 wherein:

the controller is configured to forward the at least one measurement to the data network of the aircraft utilizing the data backbone.

14. The wireless data concentrator of claim 11 wherein:

each of the inverted-F PCB trace antennas are located along an outside edge of the PCB.

15. A wireless data concentrator for a data network of an aircraft, the wireless data concentrator comprising:

a controller electrically coupled to a Printed Circuit Board (PCB);

four Radio Frequency (RF) transceivers electrically coupled to the PCB that are disposed around the controller, each configured to communicate with the controller and at least one wireless sensor that measures an environment of the aircraft; and

four PCB trace antennas fabricated into the PCB, each electrically coupled to one of the RF transceivers and disposed orthogonally to each other around the controller;

the controller configured to receive sensor data about the environment of the aircraft from the at least one wireless sensor utilizing at least one of the RF transceivers, and to provide the sensor data to the data network of the aircraft.

16. The wireless data concentrator of claim 15 wherein:

the PCB trace antennas comprise inverted-F antennas.

17. The wireless data concentrators of claim 16 wherein:

each of the inverted-F antennas are located along an outside edge of the PCB.