Unmanned aerial vehicle protection airbag

Patent metadata

Field	Value
Publication number	US-10099786-B1
Application number	US-201815867622-A
Country	US
Kind code	B1
Filing date	Jan 10, 2018
Priority date	Mar 25, 2015
Publication date	Oct 16, 2018
Grant date	Oct 16, 2018

Abstract

An unmanned aerial vehicle (UAV) airbag may protect protection for a UAV or other objects when making contact with one another. The UAV airbag may at least partially surround the UAV while allowing the UAV to remain at least partially operable. In some embodiments, the UAV airbag may be inflated just prior to making contact with another object. After inflation, the UAV airbag may be at least partially sealed to reduce or inhibit deflation of the UAV airbag, but possibly not to completely prevent airflow from the UAV airbag upon contact with another object. The UAV airbag may exhaust some air upon impact, thereby reducing a deceleration of a UAV contained inside of the UAV airbag.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV) assembly comprising:
a frame;
one or more propulsion units coupled to the frame;
a system controller, coupled to the frame, configured to at least adjust power of the one or more propulsion units;
a UAV airbag, coupled to the frame, comprising:
an elongated tubular inflatable vessel, forming a cavity, that at least partially winds around the frame and is located at least partially below the one or more propulsion units to reduce interference with downdraft caused by the one or more propulsion units,
a filling orifice in fluid communication with the elongated tubular inflatable vessel to receive gas to inflate the elongated tubular inflatable vessel, and
an exhaust orifice in fluid communication with the elongated tubular inflatable vessel configured to release air from the elongated tubular inflatable vessel upon an impact to the UAV airbag; and

an inflator, coupled to the frame, to at least partially inflate the elongated tubular inflatable vessel via the filling orifice.

2. The UAV assembly as recited in claim 1 , further comprising a sealer, coupled to the filling orifice, configured to seal the filling orifice after at least partial inflation of the airbag.

3. The UAV assembly as recited in claim 1 , further comprising a one directional valve, coupled to the filling orifice, that allows airflow into the elongated tubular inflatable vessel and inhibits deflation of the elongated tubular inflatable vessel.

4. The UAV assembly as recited in claim 1 , further comprising at least one sensor, coupled to the system controller, configured to detect objects and generate a signal used by the inflator.

5. The UAV assembly as recited in claim 1 , further comprising a wireless network interface, coupled to the system controller, wherein the system controller initiates deployment of the UAV airbag in response to receiving a signal or detection of a triggering event.

6. The UAV assembly as recited in claim 1 , wherein the inflator includes a compressed gas reservoir to selectively exhaust gas into the elongated tubular inflatable vessel to at least partially inflate the elongated tubular inflatable vessel.

7. A system comprising:
an unmanned aerial vehicle (UAV);
an airbag including a continuous inflation chamber that, when at least partially inflated forms a cavity and, at least partially winds around the UAV, the airbag configured to dissipate energy caused by the UAV contacting another object or the ground; and
an inflator to at least partially inflate the airbag after receipt of a signal or detection of a triggering event.

8. The system as recited in claim 7 , wherein the triggering event includes at least one of a loss of power, a loss of control, a detection of a collision, or a detection of an imminent collision.

9. The system as recited in claim 7 , wherein the airbag is formed at least partly by a plurality of compartments that include apertures to provide airflow between adjacent compartments of the plurality of compartments.

10. The system as recited in claim 7 , wherein the inflator includes a compressed gas reservoir to selectively exhaust gas into the airbag to at least partially inflate the airbag.

11. The system as recited in claim 7 , wherein the airbag includes a valve to selectively open and close a filling orifice of the airbag.

12. The system as recited in claim 7 , wherein the UAV includes one or more propulsion units and wherein the airbag extends below the one or more propulsion units to reduce interference with downdraft caused by the one or more propulsion units.

13. The system as recited in claim 7 , wherein the continuous inflation chamber that, when at least partially inflated, creates a helical structure.

14. The system as recited in claim 7 , further comprising one or more sensors to detect obstacles, wherein the one or more sensors include at least one of an image sensor, a thermal sensor, an infrared sensor, a time of flight sensor, an accelerometer, a pressure sensor, a weather sensor, or an airflow sensor, and wherein the one or more sensors are configured to generate the signal used by the inflator.

15. A method comprising:
receiving a signal or detecting a triggering event; and
inflating, at least partially, an airbag in response to receiving the signal or detecting the triggering event, wherein the airbag includes a continuous inflation chamber that, when at least partially inflated, forms a cavity and at least partially winds around an unmanned aerial vehicle (UAV), the airbag configured to dissipate energy caused by the UAV contacting another object or the ground.

16. The method as recited in claim 15 , wherein the airbag includes a valve to selectively open and close a filling orifice of the airbag, and further comprising manipulating the valve to close the filling orifice.

17. The method as recited in claim 15 , wherein receiving a triggering event comprises detecting at least one of a loss of power, a loss of control, a collision, or an imminent collision.

18. The method as recited in claim 15 , wherein inflating the airbag includes using a compressed gas reservoir to selectively exhaust gas into the airbag to at least partially inflate the airbag.

19. The method as recited in claim 15 , further comprising sealing the airbag to inhibit, at least temporarily, deflation of the airbag.

20. The method as recited in claim 15 , further comprising releasing air through at least one orifice of the airbag upon an impact to the airbag.

Assignees

• Amazon Tech Inc

Inventors

• Bar-Zeev Avi
• Kimchi Gur

Classifications

• B64C27/006

  Safety devices · CPC title

• B64C25/56

  inflatable · CPC title

• B64D2201/00

  Airbags mounted in aircraft for any use · CPC title

• B64D1/14 Primary

  Absorbing landing shocks · CPC title

• B64C2201/128

  Operations & Transport · mapped topic