Ground manipulation system and method for fixing an aircraft

Patent metadata

Field	Value
Publication number	US-10875644-B2
Application number	US-201715856301-A
Country	US
Kind code	B2
Filing date	Dec 28, 2017
Priority date	Dec 28, 2017
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

Disclosed herein are aircraft and landing gear systems configured to fix an aircraft to the ground. For example, the aircraft and aircraft systems configured for ground manipulation. In one aspect, an aircraft with an arm and end-effector may be fixed a ground surface to facilitate ground-based robotic manipulation tasks.

First claim

What is claimed is:

1. An aircraft for providing ground manipulation of a target objective at a ground surface, the aircraft comprising:
an airframe;
a plurality of rigid struts configured to support the airframe when the aircraft is on the ground surface;
a plurality of rotor booms extending radially from the airframe;
a plurality of propulsors, each of said plurality of propulsors positioned at a distal end of one of said plurality of rotor booms, wherein the plurality of propulsor are configured to be controlled by an aircraft processor;
an articulating arm coupled at its proximal end to the airframe;
an end-effector coupled to a distal end of the articulating arm configured to engage the target objective; and
a ground-fixing system coupled to at least one of the plurality of rigid struts and configured to secure the airframe relative to the ground surface, wherein the ground-fixing system includes two or more laterally displaceable gripping devices configured to clamp onto a protruding feature of the ground surface.

2. The aircraft of claim 1 , wherein the aircraft is configured to charge via a second aircraft.

3. The aircraft of claim 1 , wherein each of the two or more laterally displaceable gripping devices a rod-driving actuator and a threaded rod having a foot pivotally attached thereto.

4. The aircraft of claim 3 , wherein the foot includes a gripping material to increase friction with, or conform to, a surface of the protruding feature.

5. The aircraft of claim 1 , wherein the ground-fixing system is configured to assess ground stability of the ground surface via a robotic leg before landing the aircraft on the ground surface.

6. The aircraft of claim 1 , wherein the ground-fixing system is configured to provide feedback data relating to the ground surface.

7. The aircraft of claim 6 , wherein the ground-fixing system comprises a vision system that is configured to generate feedback data, wherein the vision system is coupled to the articulating arm or the end effector.

8. The aircraft of claim 1 , further comprising an intelligence, surveillance, and reconnaissance (ISR) payload configured to provide ISR data relating to the ground surface before landing the aircraft on the ground surface.

9. An unmanned aircraft for providing ground manipulation of a target objective at a ground surface, the unmanned aircraft comprising:
an airframe;
a plurality of rigid struts configured to support the airframe when the aircraft is on the ground surface;
a plurality of rotor booms extending radially from the airframe, wherein each of the plurality of rotor booms includes a propulsor;
an aircraft control system configured to navigate and land the unmanned aircraft at the ground surface;
an articulating arm coupled at its proximal end to the airframe;
an end-effector coupled to a distal end of the articulating arm and configured to engage the target objective at the ground surface; and
a ground-fixing system coupled to at least one of the plurality of rigid struts and configured to secure the airframe to the ground surface via a protruding feature of the ground surface, wherein the ground-fixing system comprises a laterally displaceable gripping device having a foot pivotally attached thereto.

10. The unmanned aircraft of claim 9 , wherein the ground-fixing system includes a pair of first and second laterally displaceable gripping devices configured to secure the protruding feature below the airframe.

11. The unmanned aircraft of claim 10 , wherein each of the first and second laterally displaceable gripping devices includes a threaded rod and a rod-driving actuator.

12. The unmanned aircraft of claim 11 , wherein each of the first and second laterally displaceable gripping devices is configured to drive its threaded rod to secure the protruding feature therebetween.

13. The unmanned aircraft of claim 12 , wherein each of the first and second laterally displaceable gripping devices is configured to contact the protruding feature via the feet.

14. A method of manipulating a target objective via a multi-rotor vertical take-off and landing (VTOL) aircraft, the method comprising:
navigating the multi-rotor VTOL aircraft to a waypoint associated with the target objective;
landing the multi-rotor VTOL aircraft on a ground surface at the waypoint, wherein the multi-rotor VTOL comprises a plurality of rigid struts configured to support an airframe of the multi-rotor VTOL aircraft when the multi-rotor VTOL is on the ground surface;
securing the multi-rotor VTOL aircraft to the ground surface via a ground-fixing system coupled to at least one of the plurality of rigid struts, wherein the ground-fixing system includes two or more laterally displaceable gripping devices configured to clamp onto a protruding feature of the ground surface; and
engaging the target objective via an end-effector coupled to a distal end of an articulating arm, wherein the articulating arm is coupled at its proximal end to the multi-rotor VTOL aircraft.

15. The method of claim 14 , wherein each of the two or more laterally displaceable gripping device includes a rod-driving actuator and a threaded rod having a foot pivotally attached thereto.

16. The method of claim 14 , further comprising the step of controlling a propulsor of the multi-rotor VTOL aircraft to generate a force that pushes the multi-rotor VTOL aircraft against the ground surface.

17. The aircraft of claim 9 , wherein the foot includes a gripping material to increase friction with, or conform to, a surface of the protruding feature.

Assignees

• Aurora Flight Sciences Corp

Inventors

• Bosworth William

Classifications

• B64U70/60

  Take-off or landing of UAVs from a runway using their own power · CPC title

• B64U2101/00

  UAVs specially adapted for particular uses or applications · CPC title

• B64U60/50

  with landing legs · CPC title

• B64U30/20

  Rotors; Rotor supports · CPC title

• B64U10/13 Primary

  Flying platforms · CPC title