Parachute assemblies with multi-stage reefing

Patent metadata

Field	Value
Publication number	US-12286233-B2
Application number	US-202217902735-A
Country	US
Kind code	B2
Filing date	Sep 2, 2022
Priority date	Sep 2, 2022
Publication date	Apr 29, 2025
Grant date	Apr 29, 2025

Abstract

A parachute assembly may comprise a canopy and one or more reefing lines. The one or more reefing lines may limit inflation of the canopy to attenuate impulse load or otherwise mitigate forces exerted by the parachute assembly on cargo or an occupant during deployment of the canopy. The one or more reefing lines may be broken in stages to selectively limit inflation of the canopy followed by selectively permitting inflation of the canopy in stages.

First claim

What is claimed is:

1. A parachute assembly, comprising:
a parachute canopy;
a first reefing line disposed adjacent an edge of the parachute canopy to restrict inflation of the parachute canopy;
a second reefing line comprising a reefing line insert coupled between a first portion of the first reefing line and a second portion of the first reefing line; and
a first cutter configured to break the second reefing line in response to a passing of a first elapsed period of time after a first triggering event, wherein breaking the second reefing line causes a lengthening of the first reefing line.

2. The parachute assembly according to claim 1 , wherein the first triggering event is an ejection from an aircraft cockpit of an occupant who is connected to the parachute assembly.

3. The parachute assembly according to claim 1 , wherein the first triggering event is a deployment of the parachute canopy.

4. The parachute assembly of claim 1 , wherein at least a portion of the reefing line insert is located within an internal volume of the first reefing line.

5. The parachute assembly of claim 1 , further comprising:
a first stitching coupling a first segment of the reefing line insert to the first portion of the first reefing line; and
a second stitching coupling a second segment of the reefing line insert to the second portion of the first reefing line.

6. The parachute assembly of claim 5 , wherein a third segment of the reefing line insert is located external to the first reefing line, the third segment extending between the first segment and the second segment.

7. The parachute assembly of claim 1 , wherein the reefing line insert includes:
a first segment located within an internal volume of the first reefing line;
a second segment located within the internal volume of the first reefing line; and
a third segment located external to the first reefing line and extending between the first segment and the second segment.

8. The parachute assembly according to claim 1 , further comprising a second cutter configured to break at least one of the first reefing line and the second reefing line in response to a passing of a second elapsed period of time after a second triggering event, wherein the lengthening of the first reefing line is the second triggering event.

9. The parachute assembly according to claim 8 , further comprising a tether line connecting a trigger of the second cutter to the second reefing line to initiate the second triggering event by the lengthening of the first reefing line.

10. The parachute assembly according to claim 1 , wherein the first cutter is a pyrotechnic cutter.

11. The parachute assembly according to claim 1 , wherein the first cutter includes electrically operated cutting blades.

12. A parachute assembly, comprising:
a parachute canopy;
a first reefing line having a first length and disposed adjacent an edge of the parachute canopy to restrict inflation of the parachute canopy;
a second reefing line having a second length and disposed adjacent the first reefing line of the parachute canopy to restrict inflation of the parachute canopy;
a first cutter configured to break the first reefing line in response to a passing of a first elapsed period of time after a first triggering event;
a second cutter configured to break the second reefing line in response to a passing of a second elapsed period of time after the breaking the first reefing line; and
a tether line connecting a trigger of the second cutter to the first reefing line to trigger the second cutter by the breaking of the first reefing line, a first end of the tether line is attached to the first reefing line and a second end of the tether line is attached to the second cutter, and the tether line is configured to be pulled with the first reefing line as the first reefing line breaks.

13. The parachute assembly according to claim 12 , wherein the first triggering event is an ejection from an aircraft cockpit of an occupant who is connected to the parachute assembly.

14. The parachute assembly according to claim 12 , wherein the first cutter and the second cutter are pyrotechnic cutters having fixed time delays corresponding to the first elapsed period of time and the second elapsed period of time, respectively.

15. The parachute assembly according to claim 12 , further comprising a third cutter configured to break the first reefing line in response to the passing of the first elapsed period of time after the first triggering event, the third cutter providing redundancy to the first cutter; and
a fourth cutter configured to break the second reefing line in response to the passing of the second elapsed period of time after the breaking the first reefing line, the fourth cutter providing redundancy to the second cutter.

16. A method of staged parachute deployment comprising:
deploying a parachute canopy of the parachute assembly;
increasing a tensile load applied to a first reefing line having a first length and disposed adjacent an edge of the parachute canopy for restricting of inflation of the parachute canopy;
breaking, by a first cutter, the first reefing line in response to a passing of a first elapsed period of time after a first triggering event;
tensioning a tether line connecting a trigger of a second cutter to the first reefing line to initiate a start of a second elapsed period of time by the breaking of the first reefing line, a first end of the tether line is attached to the first reefing line and a second end of the tether line is attached to the second cutter, and the tensioning the tether line connecting the trigger of the second cutter to the first reefing line includes pulling the tether line with the first reefing line as the first reefing line breaks;
subsequently to the breaking the first reefing line, increasing a tensile load applied to a second reefing line having a second length and disposed adjacent the first reefing line of the parachute canopy for the restricting of inflation of the parachute canopy, wherein the second length is selected to provide less restricting of inflation of the parachute canopy than the first length; and
breaking, by the second cutter, the second reefing line in response to a passing of the second elapsed period of time.

17. The method according to claim 16 , wherein the first cutter and the second cutter are pyrotechnic cutters.

18. The method according to claim 16 , wherein the first cutter and the second cutter each include electrically operated cutting blades.

19. The parachute assembly according to claim 12 , wherein the second reefing line is disposed further from the edge of the canopy than the first reefing line.

Assignees

• Rockwell Collins Inc

Inventors

• Benjamin Jeff
• Carson Kassidy L

Classifications

• B64D17/386

  Devices adapted to cut lines or straps · CPC title

• B64D17/02 Primary

  Canopy arrangement or construction · CPC title

• B64D17/00

  Parachutes (non-canopied parachutes B64D19/00) · CPC title

• B64D17/343 Primary

  by reefing means · CPC title

• B64D17/24 Primary

  Rigging lines · CPC title