Water landing parachute trap and method

Patent metadata

Field	Value
Publication number	US-10532818-B2
Application number	US-201615220335-A
Country	US
Kind code	B2
Filing date	Jul 26, 2016
Priority date	Jul 26, 2016
Publication date	Jan 14, 2020
Grant date	Jan 14, 2020

Abstract

Systems and methods for aerially delivering cargo into a body of water while avoiding parachute entrapment and entanglement are described. The system includes a parachute having a canopy and suspension lines. The system further includes a weight coupled to a first end of the suspension lines and a ring that is configured to float in the body of water. The weight is coupled to the cargo, and the ring is disposed between the weight and the canopy with the suspension lines passing through the center of the ring.

First claim

The invention claimed is:

1. A system comprising:
a parachute comprising a canopy and suspension lines;
a weight coupled to a first end of the suspension lines, the weight being couplable to a cargo;
a ring configured to float in a body of water and being disposed between the weight and the canopy, the suspension lines passing through a center of the ring; and
a weight releasing device coupled to the weight and configured to detach the cargo from the weight such that upon separation, the weight is configured to sink in the body of water while coupled to the first end of the suspension lines.

2. The system of claim 1 , wherein the weight releasing device is configured to attach to a mount on the cargo.

3. The system of claim 2 , wherein the mount comprises a curved surface such that when the cargo is detached from the weight, the weight is adapted to fall off of the mount.

4. The system of claim 2 , wherein the weight is configured to separate from the cargo in response to the weight releasing device detaching the weight from the cargo, wherein the sinking of the weight pulls the suspension lines through the center of the ring.

5. The system of claim 4 , wherein the canopy is coupled to a second end of the suspension lines, the suspension lines and the canopy being adapted to collect at the ring in response to the weight pulling the suspension lines through the center of the ring, the suspension lines and the canopy being separated from the cargo.

6. The system of claim 4 , wherein the ring is an inflatable ring comprising a valve configured to be opened by the sinking of the weight to deflate the ring.

7. The system of claim 6 , wherein the valve is coupled with the weight via a tether.

8. The system of claim 1 , wherein the ring comprises an inner surface along an inner perimeter of the ring and an outer surface along an outer perimeter of the ring, the inner surface comprising a surface coefficient of friction of about 0.05 to about 0.1.

9. The system of claim 1 , wherein the ring comprises an inner surface along an inner perimeter of the ring and an outer surface along an outer perimeter of the ring, the inner surface comprising a polytetrafluoroethylene (PTFE) coated surface.

10. A method of deploying the system of claim 1 , the method comprising:
dropping the system from an aircraft such that the system descends to the body of water with the parachute deployed;
detaching the cargo from the weight after the cargo enters the body of water such that the cargo and the weight separate from each other and the weight sinks into the body of water; and
pulling the suspension lines by the detached weight through the center of the ring.

11. The method of claim 10 , further comprising inflating the ring before the cargo impacts the body of water.

12. A method of assembling the system of claim 1 , the method comprising:
attaching the first end of the suspension lines to the weight;
positioning the ring on the weight between the weight and the parachute; and
packing the parachute and positioning the packed parachute on the ring.

13. The method of claim 12 , further comprising attaching the weight to the cargo with a weight releasing device.

14. The method of claim 13 , wherein the weight is attached to a mount on the cargo with the weight releasing device.

15. The method of claim 12 , wherein the ring is in a deflated form, the ring being configured to inflate before the ring impacts the body of water.

16. The method of claim 12 , wherein the ring is in a deflated form and the ring comprises a device configured to automatically inflate the ring in response to the cargo impacting the body of water.

17. A method for air-dropping cargo to a body of water using a parachute, the method comprising:
releasing the cargo from a weight coupled to suspension lines of a parachute after the cargo enters the body of water;
pulling the suspension lines, by sinking the weight due to gravity, through a center of a ring floating on a surface of the body of water; and
collecting the parachute at the ring.

18. The method of claim 17 , further comprising:
ejecting the cargo from an aircraft utilized for the air-dropping of the cargo;
deploying the parachute to controllably descend the cargo toward the body of water; and
inflating the ring before the cargo impacts the body of water.

19. The method of claim 17 , wherein the releasing of the cargo from the weight comprises automatically activating an actuator configured to detach the weight from the cargo.

Assignees

• Boeing Co

Inventors

• Childress Jamie

Classifications

• B64D1/02

  Dropping, ejecting, or releasing articles (jettisonable fuel reservoirs B64D37/12) · CPC title

• B64D25/20

  Releasing of crash-position indicators · CPC title

• B63B22/00

  Buoys ({floating decoys, e.g. for waterfowl A01M31/06;} means for indicating the location of underwater objects B63C7/26; life-buoys, e.g. rings B63C9/08; {mountings of acoustic transducer in underwater equipment, e.g. sonobuoys G10K11/006; electric cables supported on or from floats H02G9/12}) · CPC title

• B64D17/38

  Releasable fastening devices between parachute and load or pack · CPC title

• B63B22/003 Primary

  adapted for being launched from an aircraft or water vehicle;, e.g. with brakes deployed in the water · CPC title