IP Library Granted Patent US 6,883,756
Granted Patent B2
US 6,883,756 · App. 10/442,812 · Granted Apr 26, 2005

Method and apparatus for delayed parachute deployment

Assignee: Atair Aerospace, Inc.
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Quick Facts
Patent No.
US 6,883,756
App. No.
10/442,812
Granted
Apr 26, 2005
Kind
B2
Abstract

A hydraulic mechanism is positioned within the drogue bridle of a parachute system. The hydraulic link is slowly moved by tension on the drogue bridle to operate a release. The release operates to release the drogue chute and to deploy the main chute. The movement of the hydraulic link provides a time delay between deployment of the drogue chute and the main chute to allow the load to stabilize before deployment of the main chute.

Claims (27)

1. A parachute system comprising:

a drogue chute;

a main chute; and

a hydraulic timer delayed release for deploying the main chute a predetermined period of time after deployment of the drogue chute.

2. The parachute system of claim 1 , further comprising a drogue bridle connecting the drogue chute to the main chute, and wherein the time delayed release is powered by the tension on the drogue bridle.

3. The parachute system of claim 2 , wherein the hydraulic timer delayed release includes:

a hydraulic link positioned in the drogue bridle which moves from an engaged position to a disengaged position under tension of the drogue bridle, and

a release mechanism operable by the hydraulic link being moved into the disengaged position.

4. The parachute system of claim 3 , wherein the release mechanism includes a three ring release.

5. The parachute system of claim 3 , wherein the release mechanism includes a sacrificial link and a cutter.

6. The parachute system of claim 3 , wherein the hydraulic link includes a body and a piston movable within the body between the engaged position and the disengaged position, and wherein the piston retains triggers the release mechanism when at the end of its stroke.

7. The parachute system of claim 6 , wherein the hydraulic link includes fluid in the body, and a fluid path connected to the piston to control a rate of movement of the piston within the body.

8. The parachute system of claim 7 , wherein the fluid path is adjustable in conductance such that the rate of movement of the piston can be changed.

9. The parachute system of claim 7 , wherein the hydraulic link further comprises a set screw adjustably extending into the fluid path to impede the flow of fluid through the fluid path or an external fluid flow path with a variable conductance valve.

10. A method of deploying chutes in a parachute system having a drogue chute and a main chute, the method comprising the steps of:

deploying the drogue chute;

delaying a predetermined period of time using an hydraulic timer; and

deploying the main chute after the predetermined period of time using a release operated by the hydraulic timer.

11. The method of deploying chutes in a parachute system according to claim 10 , wherein the delaying step includes operating a hydraulic link in a bridle of the drogue chute to provide the predetermined period of time.

12. The method of deploying chutes in a parachute system according to claim 11 , wherein the main chute deploying step includes using a three ring release mechanism operated when a piston of the hydraulic link reaches a disengaged position.

13. The method of deploying chutes in a parachute system according to claim 10 , wherein the predetermined period of time is based upon tension on a bridle of the drogue chute.

14. A parachute system comprising:

a drogue chute;

a main chute;

a bridle, connecting the drogue chute to the main chute;

a hydraulic timer delayed release, for deploying the main chute a predetermined period of time after deployment of the drogue chute, and wherein the hydraulic timer delayed release is actuated by the tension on the bridle, and wherein the hydraulic timer delayed release includes a hydraulic link positioned in the bridle which moves from an engaged position to a disengaged position under tension of the bridle; and

a release mechanism operable by the hydraulic link being moved into the disengaged position, for deploying said main chute.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 4, 2015
From: PRECISION FLIGHT SYSTEMS LLC, D/B/A ATAIR AEROSPACE
To: LUMINATI AEROSPACE LLC
Reel/Frame 037213/0546 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 25, 2005
From: PRESTON, DANIEL J.
To: ATAIR AEROSPACE, INC.
Reel/Frame 016487/0605 →
Continuity (2)
Provisional Application 6038291900 · May 21, 2002
Related Publication 20030218100A1 · Nov 27, 2003