IP Library Granted Patent US 11,225,330
Granted Patent B2
US 11,225,330 · App. 16/744,602 · Granted Jan 18, 2022

Bimodal parachute deployment system

Inventors: Damon Vander Lind (Alameda, CA); Cameron Robertson (San Mateo, CA)
Assignee: Kitty Hawk Corporation
B64D17/54B64D17/343B64D17/386B64D17/62B64D17/80
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Quick Facts
Patent No.
US 11,225,330
App. No.
16/744,602
Granted
Jan 18, 2022
Kind
B2
Abstract

A parachute deployment system is disclosed. In various embodiments, the system includes an interface configured to receive sensor information; a parachute load limiting device; and a parachute load limiting device state controller. The parachute load limiting device state controller sets a state of the parachute load limiting device to a state associated with a corresponding amount of load based at least in part on the sensor information.

Claims (29)

1. A parachute load limiting device comprising:

a tether configured to be coupled to a parachute line at an end and to be coupled to an aircraft at an opposite end, wherein in an initial state the tether is folded to decrease a length of the tether;

a fastener configured to:

hold folds of the tether in place in the initial state, and open to permit the tether to extend in length and decrease a load delivered to a parachute; and

a reefing device configured to be situated around a mid-section of a canopy of the parachute to constrain a size of the parachute in the initial state, wherein the reefing device is configured to slide down the canopy to a bottom of the parachute to hold one or more tethers of the parachute together.

2. The device of claim 1 , wherein the parachute load limiting device is configured to be inserted between sections of the parachute line to decrease load to the parachute.

3. The device of claim 1 , further comprising a severing tool configured to break the fastener to permit the tether to extend in length.

4. The device of claim 1 , further comprising a blade configured to break the fastener to permit the tether to extend in length.

5. The device of claim 1 , comprising one or more additional parachute load limiting devices or one or more additional fasteners.

6. The device of claim 1 , further comprising a state controller that engages the parachute load limiting device prior to deployment of the parachute.

7. The device of claim 1 , further comprising a state controller that disengages the parachute load limiting device prior to deployment of the parachute.

8. The device of claim 1 , further comprising a state controller that engages the parachute load limiting device after deployment of the parachute.

9. The device of claim 1 , further comprising a state controller that disengages the parachute load limiting device after deployment of the parachute.

10. The device of claim 1 , further comprising a state controller that operates the fastener based on a timer.

11. The device of claim 1 , wherein the force is below the threshold when a vehicle in which the parachute load limiting device is provided does not exceed a threshold altitude or a threshold speed.

12. The device of claim 1 , wherein the force meets the threshold when a vehicle in which the parachute load limiting device is provided exceeds a threshold altitude or a threshold speed.

13. The device of claim 1 , wherein the parachute load limiting device state controller severs a component of the parachute load limiting device in the event the parachute load limiting device state controller sets the parachute load limiting device to a disengaged state.

14. The device of claim 1 , further comprising a state controller configured to instruct the fastener to permit the tether to extend in length in response to sensor information including at least one of: environmental factors, obstacles, wind speed, altitude, or velocity.

15. The device of claim 14 , wherein the state controller is controlled automatically based on the sensor information.

16. The device of claim 1 , wherein the parachute load limiting device has an engaged state in which the fastener is operated and a disengaged state in which the fastener is not operated.

17. The device of claim 16 , wherein the parachute load limiting device is engaged as a default state.

18. A method, comprising:

providing a tether that couples to a parachute line at an end and couples to an aircraft at an opposite end, wherein in an initial state the tether is folded to decrease a length of the tether;

providing a fastener that:

holds folds of the tether in place in the initial state, and

opens to permit the tether to extend in length and decrease a load delivered to a parachute; and

providing a reefing device that is situated around a mid-section of a canopy of the parachute to constrain a size of the parachute in an initial state, wherein the reefing device slides down the canopy to a bottom of the parachute to hold one or more tethers of the parachute together.

19. The method of claim 18 , further comprising: providing a severing tool that breaks the fastener to permit the tether to extend in length.

20. The method of claim 18 , further comprising: providing a state controller that instructs the fastener to permit the tether to extend in length in response to sensor information including at least one of: environmental factors, obstacles, wind speed, altitude, or velocity.

Assignments (4)
RELEASE OF SECURITY INTEREST Recorded May 22, 2023
From: ONE AERO, LLC
To: KITTY HAWK CORPORATION
Reel/Frame 063713/0367 →
SECURITY INTEREST Recorded Mar 25, 2022
From: KITTY HAWK CORPORATION
To: ONE AERO, LLC
Reel/Frame 059503/0382 →
SECURITY INTEREST Recorded Nov 4, 2021
From: KITTY HAWK CORPORATION
To: ONE AERO, LLC
Reel/Frame 058029/0610 →
SECURITY INTEREST Recorded Oct 22, 2020
From: KITTY HAWK CORPORATION
To: ONE AERO, LLC
Reel/Frame 054206/0714 →
Continuity (2)
Continuation 15338086 · Oct 28, 2016
Related Publication 20200207480A1 · Jul 2, 2020