System and method for providing a simple and reliable inertia measurement unit (IMU)

Patent metadata

Field	Value
Publication number	US-10627233-B2
Application number	US-201816029794-A
Country	US
Kind code	B2
Filing date	Jul 9, 2018
Priority date	Apr 7, 2015
Publication date	Apr 21, 2020
Grant date	Apr 21, 2020

Abstract

An inertia measurement unit including a housing assembly, a weight block assembly, a circuit board, and a signal line. The housing assembly includes a cavity and a first opening in communication with the cavity. The weight block assembly is arranged in the cavity of the housing assembly. The weight block assembly includes an inner chamber and a second opening in communication with the inner chamber. The circuit board is arranged in the inner chamber of the weight block assembly. The signal line is coupled to a first edge of the circuit board and extends out of the weight block assembly through the second opening and out of the housing assembly through the first opening. At least one of the first opening or the second opening is located proximal to a second edge of the circuit board that is different from the first edge of the circuit board.

First claim

The invention claimed is:

1. An inertia measurement unit (IMU) comprising:
a housing assembly including a cavity and a first opening in communication with the cavity;
a weight block assembly arranged in the cavity of the housing assembly, the weight block assembly including an inner chamber and a second opening in communication with the inner chamber;
a circuit board arranged in the inner chamber of the weight block assembly; and
a signal line coupled to a first edge of the circuit board and extending out of the weight block assembly through the second opening and out of the housing assembly through the first opening;
wherein at least one of the first opening or the second opening is located proximal to a second edge of the circuit board that is opposite to the first edge of the circuit board.

2. The IMU of claim 1 , wherein the circuit board includes one or more sensors that are sensitive to vibration.

3. The IMU of claim 2 , wherein the one or more sensors includes an inertia sensor.

4. The IMU of claim 3 , wherein the inertia sensor includes at least one of:
a motion sensor including at least one of a velocity measurement instrument or an acceleration measurement instrument; or
an orientation sensor including at least one of a gyroscope or a gravity gradient sensor.

5. The IMU of claim 1 , wherein the weight block assembly includes a first weight block and a second weight block coupled together to form the inner chamber.

6. The IMU of claim 1 , further comprising:
a thermal interface material filling a gap in the inner chamber.

7. The IMU of claim 6 , wherein the thermal interface material is based on at least one of silica gel, thermal gel, epoxy, a phase change material, polyimide, graphite, an aluminum tape, or a silicone-coated fabric.

8. The IMU of claim 1 , wherein the signal line includes a bent portion near the first edge of the circuit board.

9. The IMU of claim 1 , wherein the signal line includes a portion held on an outside surface of the weight block assembly.

10. The IMU of claim 1 , wherein the housing assembly includes a first housing member and a second housing member locked together to form the cavity.

11. The IMU of claim 1 , further comprising:
at least one of an adhesive layer or a form layer arranged in the cavity and fixing the weight block assembly in the cavity.

12. The IMU of claim 1 ,
wherein the circuit board is a first circuit board;
the IMU further comprising:
a second circuit board arranged outside the housing assembly;
wherein the signal line is further coupled to the second circuit board through a plug-in device.

13. The IMU of claim 12 , wherein the second circuit board includes a control board for an unmanned aircraft, the control board including at least one of a barometer or a heating device.

14. An unmanned aircraft comprising:
a body; and
an inertia measurement unit (IMU) configured to determining a spatial disposition for the unmanned aircraft, the IMU including:
a housing assembly including a cavity and a first opening in communication with the cavity;
a weight block assembly arranged in the cavity of the housing assembly, the weight block assembly including an inner chamber and a second opening in communication with the inner chamber;
a circuit board arranged in the inner chamber of the weight block assembly; and
a signal line coupled to a first edge of the circuit board and extending out of the weight block assembly through the second opening and out of the housing assembly through the first opening;
wherein at least one of the first opening or the second opening is located proximal to a second edge of the circuit board that is opposite to the first edge of the circuit board.

15. The unmanned aircraft of claim 14 , wherein the weight block assembly has a mass that keeps an inherent frequency of the IMU away from an operation frequency of the unmanned aircraft.

16. The unmanned aircraft of claim 15 , wherein the mass of the weight block assembly keeps the inherent frequency of the IMU outside a range from 50 Hz to 200 Hz.

17. The unmanned aircraft of claim 14 , further comprising:
a support base; and
one or more damping elements coupling the IMU to the support base.

18. The unmanned aircraft of claim 14 , further comprising:
one or more motors.

19. The IMU of claim 1 , wherein the signal line extends out of the weight block assembly through the second opening along a first direction and is bent back to extend over the weight block assembly along a second direction that is opposite to the first direction.

Assignees

• Sz Dji Technology Co Ltd

Inventors

• Feng Jiangang
• Tang Yin

Classifications

• G01C25/00

  Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass (testing, calibrating or compensating compasses G01C17/38) · CPC title

• H05K2201/10151

  Sensor · CPC title

• H05K7/20

  Modifications to facilitate cooling, ventilating, or heating · CPC title

• G01C21/265 Primary

  constructional aspects of navigation devices, e.g. housings, mountings, displays (G01C21/3688 takes precedence) · CPC title

• G01C19/00 Primary

  Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects · CPC title