Home station for unmanned aerial vehicle

Patent metadata

Field	Value
Publication number	US-10239638-B1
Application number	US-201514619673-A
Country	US
Kind code	B1
Filing date	Feb 11, 2015
Priority date	May 10, 2014
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

Described herein are apparatuses that provided various features related to unmanned aerial vehicles (UAVs). An example apparatus may include, among other features, (i) a launch system for a UAV, (ii) a landing feature that is arranged on the apparatus so as to receive the UAV when the UAV returns from a flight, and (iii) a mechanical battery-replacement system that is configured to (a) remove a first battery from the UAV, and (b) after removal of the first battery, install a second battery in the UAV.

First claim

What is claimed is:

1. An apparatus comprising:
a launch system for an unmanned aerial vehicle (UAV);
a landing feature that is arranged on the apparatus so as to receive the UAV when the UAV returns from a flight;
a mechanical battery-replacement system that is configured to:
(a) remove a first battery from the UAV, and
(b) after removal of the first battery, install a second battery in the UAV; and

a frame structure comprising:
a roof, and
a chamber beneath the roof,

wherein the launch system is arranged to:
couple to the UAV at a location inside the chamber, and
move the UAV out of the chamber during a launch process, and

wherein the landing feature is arranged on the roof of the frame structure.

2. The apparatus of claim 1 , wherein the launch system comprises a UAV attachment feature within a compartment,
wherein the UAV attachment feature connects to a launch mechanism, and
wherein a panel that is moveable to a first position to provide access to the compartment such that the UAV attachment feature is accessible at the coupling location within the chamber, and is moveable to a second position to restrict access to the compartment.

3. The apparatus of claim 2 , wherein the launch system requires the moveable panel to be in the second position in order for a launch process to be initiated.

4. The apparatus of claim 2 ,
wherein the launch system further comprises a launch tube, and
wherein the launch mechanism comprises:
a rail, and
a motor configured to move the attachment feature upward through the launch tube such that when the UAV that is attached to the attachment feature the UAV is propelled through an opening at a top end of the launch tube.

5. The apparatus of claim 4 , wherein the launch system further comprises a hatch at the top end of the launch tube, wherein the hatch is configured to open as part of a launch process, and to otherwise remain closed.

6. The apparatus of claim 1 , wherein the landing feature comprises at least one visible feature to assist a UAV in landing on the landing feature.

7. The apparatus of claim 1 , wherein the landing feature comprises a zero-impact grass surface on which a UAV can land.

8. The apparatus of claim 1 ;
wherein the landing feature comprises a recovery net adjacent to a landing pad, and
wherein the recovery net is arranged such that when the UAV is in the process of landing, the recovery net guides the UAV towards the landing pad.

9. The apparatus of claim 1 , further comprising a diagnostics system for the UAV, wherein the diagnostics system comprises at least:
(a) an onboard integrated computer, and
(b) one or more communication interfaces for acquiring data from the UAV.

10. The apparatus of claim 9 , wherein the onboard integrated computer is programmed to generate vehicle log data.

11. The apparatus of claim 1 , further comprising one or more communication systems.

12. The apparatus of claim 11 , wherein the one or more communication systems comprise a long-range communication system configured for communications with the UAV after the UAV has been launched from the apparatus and is in flight to a target location.

13. The apparatus of claim 11 , wherein the one or more communication systems comprise a radar system that is operable to receive air-traffic control data.

14. The apparatus of claim 1 , wherein the apparatus is operable for self-service UAV delivery of a package, the apparatus further comprising:
one or more user-interface components, wherein the one or more user-interface components are operable to:
(a) receive information to facilitate delivery of a package to a target location, and
(b) receive payment for the delivery of the package to the target location; and

a package-reception feature configured to receive the package; and
wherein the launch system is operable to launch the UAV with received package loaded thereon.

15. An apparatus comprising:
a launch system for an unmanned aerial vehicle (UAV);
a landing feature that is arranged on the apparatus so as to receive the UAV when the UAV returns from a flight;
a frame structure that comprises:
a roof, and
one or more side sections, wherein the one or more side sections and the roof form a human-sized chamber that is at least partially enclosed;

one or more human-operable control interfaces that are physically accessible from within the human-sized chamber, wherein the one or more human-operable control interfaces are operable to control at least the launch system;
wherein at least a portion of the launch system is disposed within the human-sized chamber such that the UAV can be loaded onto the launch system at a coupling location within the human-sized chamber,
wherein the launch system is operable for a launch process in which the UAV moved out of the chamber, and
wherein the landing feature is at least partially disposed on the roof.

16. The apparatus of claim 15 , further comprising a diagnostics system for the UAV, wherein the diagnostics system comprises at least:
(a) an onboard integrated computer, and
(b) one or more communication interfaces for acquiring data from a UAV.

17. The apparatus of claim 15 , wherein the apparatus is configured as a self-service kiosk.

Assignees

• Wing Aviation Llc

Inventors

• Cohen Joanna
• Dormiani Parsa
• Fleck Mathias Samuel
• Burgess James Ryan
• Mullaney Sean

Classifications

• B64U2201/20

  Remote controls · CPC title

• B64U10/25

  Fixed-wing aircraft (VTOL aircraft B64U10/20) · CPC title

• B64U70/70

  Launching or landing using catapults, tracks or rails (launching from storage containers B64U70/50) · CPC title

• B64U2201/104

  using satellite radio beacon positioning systems, e.g. GPS · CPC title

• B64U2201/10

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