Unmanned air and underwater vehicle

Patent metadata

Field	Value
Publication number	US-10858100-B2
Application number	US-201916393151-A
Country	US
Kind code	B2
Filing date	Apr 24, 2019
Priority date	May 21, 2014
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

An unmanned vehicle including a body and a frame structure extending from the body and supporting a plurality of propeller assemblies, each propeller assembly including at least one propeller and a corresponding motor with the motor housed in a watertight housing or coated and made corrosion resistant. The propellers comprise a first subset of propellers of the propeller assemblies and a second subset of propellers of the propeller assemblies which rotate in a plane positioned below a plane in which the first subset of propellers rotate, wherein said first and second subset of propellers are configured for independent operation of one another as the vehicle transitions from an air medium to a water medium.

First claim

What is claimed is:

1. An unmanned vehicle comprising:
at least one propeller assembly, wherein the at least one propeller assembly comprises:
at least one upper propeller driven by at least one upper electric motor such that the

at least one upper propeller rotates in a first plane, and
at least one lower propeller driven by at least one lower electric motor such that the

at least one lower propeller rotates in a second plane below the first plane; and
a control system operably coupled to the at least one upper electric motor and the at least one lower electric motor of the at least one propeller assembly,
wherein the control system is configured to independently operate the at least one upper electric motor and the at least one lower electric motor so that the at least one upper propeller and the at least one lower propeller (i) operate simultaneously to control propulsion when the unmanned vehicle is fully immersed and being propelled in either one of both an air medium and a water medium, and (ii) operate sequentially when the unmanned vehicle transitions between the air medium and the water medium.

2. The unmanned vehicle of claim 1 , wherein the at least one upper propeller and the at least one lower propeller are positioned coaxially.

3. The unmanned vehicle of claim 1 , wherein the control system is configured to slow or stop rotation of the at least one lower propeller when the at least one lower propeller is at a transition between the air medium and the water medium, and further wherein the control system is configured to continue rotation of the at least one upper propeller when the at least one lower propeller is at a transition between the air medium and the water medium.

4. The unmanned vehicle of claim 3 , the control system is configured to slow or stop rotation of the at least one upper propeller when the at least one upper propeller is at a transition between the air medium and the water medium, and further wherein the control system is configured to continue rotation of the at least one lower propeller when the at least one upper propeller is at a transition between the air medium and the water medium.

5. The unmanned vehicle of claim 2 , further comprising at least one sensor configured to determine when the at least one upper propeller, the at least one lower propeller, or both are at the transition between the air medium and the water medium.

6. The unmanned vehicle of claim 1 , wherein the at least one upper propeller is longer and has a lower pitch angle than the at least one lower propeller so as to provide lift force in the air medium.

7. The unmanned vehicle of claim 1 , wherein the at least one lower propeller is shorter and has a higher pitch angle than the at least one upper propeller so as to provide lift force in the water medium.

8. The unmanned vehicle of claim 1 , wherein the at least one upper propeller of the at least one propeller assembly comprises more than one upper propeller.

9. The unmanned vehicle of claim 1 , wherein the at least one lower propeller of the at least one propeller assembly comprises more than one lower propeller.

10. The unmanned vehicle of claim 1 , wherein the at least one propeller assembly comprises a greater number of upper propellers than lower propellers.

11. The unmanned vehicle of claim 1 , wherein the at least one propeller assembly comprises a plurality of propeller assemblies.

12. The unmanned vehicle of claim 11 , further comprising a frame structure, wherein each of the plurality of propeller assemblies is coupled to the frame structure by a respective arm.

13. The unmanned vehicle of claim 12 , wherein the frame structure includes two, three, four or eight arms.

14. The unmanned vehicle of claim 11 , further comprising a body coupled to the frame structure.

15. The unmanned vehicle of claim 14 , wherein the body is configured to house one or more batteries and one or more speed controllers of the control system.

16. The unmanned vehicle of claim 14 , further comprising a heat sink associated with the body.

17. The unmanned vehicle of claim 1 , wherein, when the at least one upper propeller is determined to be submerged in the water medium, the control system is configured to drive at least one upper electric motor at a higher torque as compared to the torque at which the at least one upper electric motor is driven when the at least one upper propeller is determined to be in the air medium.

18. The unmanned vehicle of claim 1 , wherein, when the at least one lower propeller is determined to be submerged in the water medium, the control system is configured to rotate the drive the at least one lower electric motor at a higher torque as compared to the torque at which the at least one lower electric motor is driven when the at least one lower propeller is determined to be in the air medium.

19. A method of operating an unmanned vehicle having at least one first propeller rotating in a first plane and at least one second propeller rotating in a second plane different from the first plane, the method comprising:
while in either one of both of a first medium and a second medium, controlling the unmanned vehicle to simultaneously operate the at least one first propeller and the at least one second propeller; and
while transitioning between the first medium and the second medium, controlling the unmanned vehicle to sequentially operate the at least one first propeller and the at least one second propeller so that the one of the at least one first propeller and the at least one second propeller that is located at a boundary between the first medium and the second medium operates at a slow or stopped rotation,
wherein the first medium is water or air, and
wherein the second medium is water or air and is different from the first medium.

20. The method of claim 19 , further comprising sensing, by one or more sensors, when the at least one first propeller, the at least one second propeller, or both are at a transition between the first medium and the second medium.

Assignees

• Univ Rutgers

Inventors

• Diez-Garias Francisco J
• Maia Marco M

Classifications

• B64U30/20

  Rotors; Rotor supports · CPC title

• B64U20/00

  Constructional aspects of UAVs (of lift-producing means B64U30/00) · CPC title

• B64U2101/30

  for imaging, photography or videography · CPC title

• B64U2101/64

  for parcel delivery or retrieval · CPC title

• B64U10/13 Primary

  Flying platforms · CPC title