Systems and methods for transmitting data via a contactless cylindrical interface

Patent metadata

Field	Value
Publication number	US-11774559-B2
Application number	US-202217583106-A
Country	US
Kind code	B2
Filing date	Jan 24, 2022
Priority date	Feb 15, 2018
Publication date	Oct 3, 2023
Grant date	Oct 3, 2023

Abstract

Described herein are systems and methods that create a capacitive link based on a rotating cylinder capacitor. A cylindrical rotor rotates around a shaft and maintains an air gap between the cylindrical rotor and the shaft and to create one or more air gap capacitors. A first subsystem, comprising a light detection and ranging components, is coupled to the rotor. A second sub-subsystem, comprising data analysis functions, is coupled to the shaft. The first subsystem and the second subsystem are coupled via capacitive links created by the air gap capacitors. The communication signaling utilized on the capacitive links may be bi-directional and differential signaling. The first subsystem and the second subsystem may comprise a LIDAR light detection and ranging system. The second subsystem may power the first subsystem via inductive coupling.

First claim

We claim:

1. A system comprising:
a rotor having a hole;
a transmitter;
a shaft;
a receiver; and
a capacitive link coupling the transmitter to the receiver via an air gap capacitor positioned between the rotor and the shaft.

2. The system of claim 1 further comprising:
a first ring attached to an inside surface of the hole of the rotor; and
a second ring attached to an outer surface of the shaft, wherein the shaft is positioned inside the hole;
wherein an air gap between the first ring and the second ring creates the air gap capacitor.

3. The system of claim 1 , wherein the transmitter is configured to transmit data to the receiver via the capacitive link.

4. The system of claim 1 , wherein the rotor is configured to rotate around the shaft.

5. A system comprising:
a rotor having a hole;
a first transceiver located on the cylindrical rotor;
a shaft;
a second transceiver located on the shaft;
one or more air gap capacitors created by an air gap between the cylindrical rotor and the shaft; and
one or more capacitive links coupled between the first transceiver and the second transceiver based on the one or more air gap capacitors.

6. The system of claim 5 , further comprising:
one or more rotor rings attached to an inside surface of the hole of the rotor; and
one or more shaft rings attached to an outer surface of the shaft, wherein the shaft is positioned inside the hole;
wherein each of the one or more rotor rings is paired with a corresponding shaft ring of the one or more shaft rings, and
wherein the air gap is between each pair of the rotor rings and the shaft rings.

7. The system of claim 5 , wherein the one or more capacitive links provide one or more corresponding connections between the first transceiver and the second transceiver.

8. The system of claim 5 , further comprising one or more corresponding pairs of rings supporting one or more respective capacitive links.

9. The system of claim 5 , wherein the first transceiver and the second transceiver are configured to transmit and receive a bi-directional differential signal utilizing four of the capacitive links.

10. The system of claim 9 , wherein each of the capacitive links utilizes one or more of the following:
a low voltage differential signalling (LVDS) protocol; or
a Serializer/Deserializer (SERDES) interface.

11. The system of claim 9 , wherein the shaft is positioned inside the hole in the rotor, and wherein the rotor is configured to rotate around the shaft.

12. The system of claim 9 , further comprising one or more processing devices configured to encode and decode the bi-directional differential signal with a Manchester code.

13. The system of claim 9 , further comprising one or more processing devices configured to process the bi-directional differential signal with an error detecting code.

14. The system of claim 5 , wherein the shaft is configured to provide power to the cylindrical rotor via inductive coupling.

15. A method comprising:
rotating a first subsystem around a second subsystem;
creating a set of capacitive links between the first subsystem and the second subsystem based on an air gap between a set of electrodes located on the first subsystem and another corresponding set of electrodes located on the second subsystem; and
transmitting a first set of data from the first subsystem to the second subsystem via the set of capacitive links.

16. The method of claim 15 , wherein the first subsystem comprises a rotor, the second subsystem comprises a shaft, and the rotor and the shaft are part of a LIDAR system.

17. The method of claim 16 , wherein the set of electrodes located on the first subsystem includes a first rotor ring and a second rotor ring, the method further comprising:
decoding a return light signal from the LIDAR system at the rotor;
transmitting the decoded light signal to an inverter and an amplifier;
coupling a first output signal of the inverter to the first rotor ring; and
coupling a second output signal of the amplifier to the second rotor ring.

18. The method of claim 17 , wherein the set of electrodes located on the second subsystem includes a first shaft ring and a second shaft ring, the first shaft ring aligned with the air gap to the first rotor ring to create a first capacitive link, and the second shaft ring aligned with the air gap to the second rotor ring to create a second capacitive link, the method further comprising:
transmitting the first output signal from the first rotor ring to the first shaft ring through the first capacitive link;
transmitting the second output signal from the second rotor ring to the second shaft ring through the second capacitive link; and
using a differential amplifier coupled to the shaft to generate an output signal based on a difference between the first output signal and the second output signal.

19. The method of claim 15 , wherein a number of electrodes in each of the sets of electrodes is equal to a number of communication links in the set of capacitive links.

20. The method of claim 15 , wherein the transmitting is performed with bi-directional differential signalling over a plurality of the capacitive links.

21. The method of claim 20 , further comprising:
encoding and decoding bi-directional differential signals with a Manchester code.

22. The method of claim 16 , further comprising:
powering the rotor by the shaft via inductive coupling.

23. The method of claim 15 , wherein the air gap creates an air gap capacitor and a tolerance of a capacitance of the air gap capacitor is less than 20%.

24. The method of claim 15 , further comprising transmitting a second set of data from the second subsystem to the first subsystem.

Assignees

• Velodyne Lidar Usa Inc

Inventors

• Venkatesan Pravin Kumar
• Goyal Abhilash
• Etheridge William B
• Ramalingam Varadharajan Rajesh

Classifications

• G01S7/4817 Primary

  relating to scanning · CPC title

• G01S17/88

  Lidar systems specially adapted for specific applications · CPC title

• G01S17/89

  for mapping or imaging · CPC title

• H02J50/05 Primary

  using capacitive coupling · CPC title

• H03M5/12

  Biphase level code, e.g. split phase code, Manchester code; Biphase space or mark code, e.g. double frequency code · CPC title