Apparatuses for releasing a payload from an aerial tether

Patent metadata

Field	Value
Publication number	US-10899448-B2
Application number	US-202016890548-A
Country	US
Kind code	B2
Filing date	Jun 2, 2020
Priority date	Jun 10, 2016
Publication date	Jan 26, 2021
Grant date	Jan 26, 2021

Abstract

Described herein are apparatuses for passively releasing a payload of an unmanned aerial vehicle (UAV). An example apparatus may include, among other features, (i) a housing; (ii) a swing arm coupled to the housing, wherein the swing arm is operable to toggle between an open position and a closed position; (iii) a spring mechanism adapted to exert a force on the swing arm from the open position toward the closed position; (iv) a receiving system of a UAV adapted to receive the housing, wherein the receiving system causes the swing arm to be arranged in the open position; and (v) a spool operable to unwind and wind a tether coupled to the housing, wherein unwinding the tether causes a descent of the housing from the receiving system, and wherein winding the tether causes an ascent of the housing to the receiving system.

First claim

What is claimed is:

1. An apparatus comprising:
a housing;
a first swing arm coupled to the housing proximate to a first end of the first swing arm, wherein the first swing arm is operable to toggle between a first open position and a first closed position, wherein the first closed position locates a second end of the first swing arm within the housing, wherein the first open position exposes the second end of the first swing arm outside the housing at an acute angle with respect to a first sidewall of the housing such that the first swing arm is positioned to secure a payload to the housing;
a second swing arm coupled to the housing proximate to a first end of the second swing arm, wherein the second swing arm is operable to toggle between a second open position and a second closed position, wherein the second closed position locates a second end of the second swing arm within the housing, wherein the second open position exposes the second end of the second swing arm outside the housing at an acute angle with respect to a second sidewall of the housing such that the second swing arm is positioned to secure the payload to the housing;
a mechanism coupled between the first and second swing arms;
wherein a cam of one of the first or second swing arms, when contacted by a receiving device receiving the housing, causes, via the mechanism, the other of the first or second swing arms to be arranged in its respective open position.

2. The apparatus of claim 1 , wherein the receiving device contacting the cam of the first swing arm causes the mechanism to exert a force on the second swing arm, and wherein the force is in a direction from the second closed position toward the second open position.

3. The apparatus of claim 1 , wherein the mechanism comprises a rigid member coupled between the first and second swing arms, wherein the receiving system contacting the cam of the first swing arm causes the rigid member to exert a force on the second swing arm, and wherein the force is in a direction from the second closed position toward the second open position.

4. The apparatus of claim 1 , wherein the mechanism comprises a spring coupled between the first and second swing arms, wherein the receiving system contacting the cam of the first swing arm causes the rigid member to exert a force on the second swing arm, and wherein the force is in a direction from the second closed position toward the second open position.

5. The apparatus of claim 1 , wherein the housing includes a first alignment feature, wherein the first alignment feature is adapted to interlock with a second alignment feature of the receiving system.

6. The apparatus of claim 5 , wherein interlocking the first and second alignment features causes the housing to be arranged such that the receiving system contacts the cam of one of the first or second swing arms.

7. The apparatus of claim 5 , wherein interlocking the first and second alignment features aligns one of the first or second swing arms with an opening in the receiving system such that the second end of the aligned first or second swing arm extends through the opening when the aligned first or second swing arm is in its respective open position.

8. The apparatus of claim 5 , wherein the first alignment feature includes a helical feature, and wherein the first alignment feature of the housing contacting the second feature of the receiving system causes the housing to rotate around a rotational axis of the housing until the first and second alignment features interlock.

9. The apparatus of claim 1 , wherein the payload comprises at least one tab adapted to couple to at least one of the first or second swing arms to secure the payload before and during descent, and wherein the at least one tab is adapted to decouple from the at least one of the first or second swing arms upon complete descent of the payload.

10. The apparatus of claim 9 , wherein a gravitational force on the housing is sufficient to cause the at least one tab to decouple from the at least one of the first or second swing arms upon complete descent of the payload.

11. The apparatus of claim 9 , wherein the mechanism causes the swing arm to toggle to the closed position when the at least one tab of the payload decouples from the swing arm.

Assignees

• Wing Aviation Llc

Inventors

• Shannon Trevor
• Li Zhefei

Classifications

• B64U2201/20

  Remote controls · 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

• B64U70/30

  for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net · CPC title

• B64U2201/104

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

• B64U2101/30

  for imaging, photography or videography · CPC title