UAV having barometric sensor and method of isolating disposing barometric sensor within UAV

Patent metadata

Field	Value
Publication number	US-11345472-B2
Application number	US-202016838518-A
Country	US
Kind code	B2
Filing date	Apr 2, 2020
Priority date	Jun 1, 2015
Publication date	May 31, 2022
Grant date	May 31, 2022

Abstract

An unmanned aerial vehicle (UAV) includes a housing forming a central body of the UAV and including an internal compartment, one or more electrical components disposed within the internal compartment and configured to affect operation of the UAV, and an inertial measurement unit (IMU) disposed in an external compartment external to the central body. The IMU is isolated from the internal compartment such that a barometric pressure in the external compartment is independent of a barometric pressure in the internal compartment.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV) comprising:
a housing forming a central body of the UAV, the housing comprising an internal compartment;
one or more electrical components disposed within the internal compartment and configured to affect operation of the UAV; and
an inertial measurement unit (IMU) disposed in an external compartment external to the central body,
wherein the IMU is isolated from the internal compartment such that a barometric pressure in the external compartment is independent of a barometric pressure in the internal compartment.

2. The vehicle of claim 1 , wherein the IMU is attached to an exterior surface of the central body.

3. The vehicle of claim 1 , wherein the IMU is supported by one or more extension members extending away from the central body.

4. The vehicle of claim 1 , wherein the IMU is at least partially shielded from ambient air.

5. The vehicle of claim 1 , wherein the one or more electrical components comprise at least one exhaust fan.

6. The vehicle of claim 5 , wherein the at least one exhaust fan generates negative pressure within the internal compartment.

7. The vehicle of claim 1 , wherein the internal compartment is in barometric communication with at least one exhaust fan.

8. The vehicle of claim 1 , wherein the IMU is isolated from an internal circulation system within the internal compartment of the UAV.

9. The vehicle of claim 1 , wherein the IMU experiences a pressure of ambient air of the environment around the UAV.

10. The vehicle of claim 9 , wherein the IMU communicates with the ambient air.

11. The vehicle of claim 1 , wherein the internal compartment communicates with one or more arms of the UAV.

12. The vehicle of claim 11 , wherein air flow into the central body is generated by the one or more arms.

13. The vehicle of claim 12 , wherein the air flow is generated by rotation of one or more rotors supported by the one or more arms.

14. The vehicle of claim 12 , wherein the air flow cools down the one or more electric components within the internal compartment.

15. The vehicle of claim 1 , further comprising a motor having auxiliary airflow generating components.

16. The vehicle of claim 15 , wherein the auxiliary airflow generating components comprise blades within an upper cover of the motor.

17. The vehicle of claim 15 , wherein the auxiliary airflow generating components comprise a fan within an upper cover of the motor.

18. A method of isolating an inertial measurement unit (IMU) within an unmanned aerial vehicle (UAV) comprising:
providing a UAV comprising:
a housing forming a central body of the UAV and including an internal compartment; and
one or more electrical components disposed in the internal compartment and configured to affect operation of the UAV; and

disposing the IMU externally to the central body of the UAV, wherein the IMU is isolated from the internal compartment.

19. The method of claim 18 , wherein the IMU is at least partially shielded from ambient air.

20. The method of claim 18 , wherein the IMU is fully exposed to ambient air.

Assignees

• Sz Dji Technology Co Ltd

Inventors

• Ao Jiyuan
• Wu Xumin
• Wang Tingting
• Feng Zhuang
• Lee Sungki

Classifications

• B64U2201/10

  autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] · CPC title

• B64U2201/20

  Remote controls · CPC title

• B64U20/80

  Arrangement of on-board electronics, e.g. avionics systems or wiring · CPC title

• B64U20/90

  Cooling · CPC title

• B64U30/291

  Detachable rotors or rotor supports · CPC title