Apparatuses for releasing a payload from an aerial tether

Patent metadata

Field	Value
Publication number	US-10315764-B2
Application number	US-201615179585-A
Country	US
Kind code	B2
Filing date	Jun 10, 2016
Priority date	Jun 10, 2016
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

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 swing arm coupled to the housing proximate to a first end of the swing arm, wherein the swing arm is operable to toggle between an open position and a closed position, wherein the closed position locates a second end of the swing arm within the housing, wherein the open position exposes the second end of the swing arm outside the housing at an acute angle with respect to a sidewall of the housing such that the swing arm is positioned to secure a payload to the housing;
a spring mechanism adapted to exert a force on the swing arm that biases the swing arm to move to the closed position;
a receiving system adapted to receive the housing, wherein the receiving system contacts a cam of the swing arm when receiving the housing, thereby causing the swing arm to be arranged in the open position, and wherein the receiving system is further adapted to be coupled to an aerial vehicle; and
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.

2. The apparatus of claim 1 , wherein the receiving system includes a spring-loaded cam follower adapted to contact the cam when the receiving system receives the housing, thereby causing the swing arm to be arranged in the open position.

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

4. The apparatus of claim 3 , wherein interlocking the first and second alignment features causes the housing to be arranged such that the receiving system contacts the cam.

5. The apparatus of claim 3 , wherein interlocking the first and second alignment features aligns the swing arm with an opening in the receiving system such that the second end of the swing arm extends through the opening when the swing arm is in the open position.

6. The apparatus of claim 3 , wherein the first and second alignment features include opposing helical features, and wherein a helical feature of the housing contacting a helical feature of the receiving system causes the housing to rotate around a rotational axis of the helical features until the first and second alignment features interlock.

7. The apparatus of claim 1 , wherein the payload comprises at least one tab coupled to the swing arm to secure the payload before and during descent, and wherein the at least one tab is adapted to decouple from the swing arm upon complete descent of the payload.

8. The apparatus of claim 7 , wherein a gravitational force on the housing causes the at least one tab to decouple from the swing arm upon complete descent of the payload.

9. The apparatus of claim 7 , wherein the spring 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.

10. The apparatus of claim 1 , wherein an outer surface of the housing is substantially free of protrusions.

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

• B64U50/19

  using electrically powered motors · CPC title

• B64U2201/104

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

• B64U2101/30

  for imaging, photography or videography · CPC title