SAFETY APPARATUS FOR A MULTI-BLADE AIRCRAFT

• US 20150314881A1
• Filed: 11/25/2013
• Published: 11/05/2015
• Est. Priority Date: 11/26/2012
• Status: Abandoned Application

• Current Assignee: ParaZero Ltd.
• Original Assignee: Wisec Ltd.
• Inventors: Tsaliah, Amir, Krauss, Ran
• Application Number:
  US14/646,912
• Publication Number:
  US 20150314881A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64C 39/028 Micro-sized aircraft
• CPC Class Codes: B64D 17/72 by explosive or inflatable means
• CPC Class Codes: B64D 17/725 by explosive means
• CPC Class Codes: B64D 17/80 in association with aircraft, e.g. for braking thereof
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 70/83 using parachutes, balloons or the like

Abstract

The present invention provides safety apparatus for a multi-blade aircraft, comprising an expandable and collapsible parachute assembly having a plurality of inflatable tubes, a plurality of electrically triggered gas generators connected to a support surface of a multi-blade aircraft, and an on-board control unit for initiating triggering of said plurality of gas generators, wherein an outlet end of each of said plurality of gas generators is connected to, and in fluid communication with, a bottom end of one of said plurality of tubes, allowing said parachute assembly to be fully expanded upon generation of inflating gas by each of said plurality of gas generators.

Claims

1. Safety apparatus for a multi-blade aircraft, comprising:

an expandable and collapsible parachute assembly having a plurality of inflatable tubes,

a plurality of electrically triggered gas generators connected to a support surface of the multi-blade aircraft, and

an on-board control unit operable to initiate triggering of said plurality of gas generators,

wherein an outlet end of each of said plurality of gas generators is connected to, and in fluid communication with, a bottom end of one of said plurality of inflatable tubes, allowing said parachute assembly to be fully expanded upon generation of inflating gas by each of said plurality of gas generators.

2. The safety apparatus according to claim 1, wherein the control unit is also operable to deactivate rotation of blades of the multi-blade aircraft when the inflating gas is being generated.

3. The safety apparatus according to claim 1, wherein the plurality of gas generators are configured to generate gas of a sufficiently high temperature to increase buoyancy of the parachute assembly when fully expanded.

4. The safety apparatus according to claim 1, wherein the control unit is operable to initiating triggering of the plurality of gas generators upon receiving a command signal from a remote flight controller.

5. The safety apparatus according to claim 1, wherein the control unit is operable to initiating triggering of the plurality of gas generators in response to a processed output of a plurality of on-board sensors which is indicative of a duress condition for the aircraft.

6. The safety apparatus according to claim 1, wherein each of the gas generators is releasably connected to a corresponding inflatable tube and to a base connected to the support surface.

7. The safety apparatus according to claim 6, wherein each of the gas generators is directly connected to the corresponding inflatable tube.

8. The safety apparatus according to claim 6, wherein an intermediate tube interfaces between each of the gas generators and the corresponding inflatable tube.

9. The safety apparatus according to claim 1, wherein the parachute assembly is expandable to a fully opened condition within less than a second following a gas generator triggering event.

10. The safety apparatus according to claim 1, wherein the control unit is also operable to initiate inflation of an airbag assembly for absorbing force of impact at a bottom region of the aircraft in synchronization with a triggering event for expanding the parachute assembly.

11. The safety apparatus according to claim 10, wherein the airbag assembly in an undeployed condition is retained in a chamber mounted on landing gear of the aircraft.

12. The safety apparatus according to claim 1, wherein the aircraft is an unmanned aerial vehicle.

13. The safety apparatus according to claim 1, wherein each of the plurality of gas generators has a diameter of less than 2.5 cm and a length of less than 7.5 cm.

14. The safety apparatus according to claim 3, wherein the temperature of the generated gas for increasing buoyancy of the parachute assembly when fully expanded is at least 160°

C.