IP Library › Granted Patent US 6,942,185
Granted Patent B2
US 6,942,185 · App. 10/434,319 · Granted Sep 13, 2005

Pneumatic riser release

Assignee: Atair Aerospace, Inc.
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Quick Facts
Patent No.
US 6,942,185
App. No.
10/434,319
Granted
Sep 13, 2005
Kind
B2
Abstract

An automated quick release mechanism for a three ring release includes a pneumatic or hydraulic cylinder with a hardened metal pin. The pin engages a string loop of the three ring release. An internal spring holds the pin in an extended position. A controller external to the automated quick release mechanism provides a gas or fluid pressure to withdraw the pin and disengage the string loop.

Claims (22)

1. A parachute quick release comprising:

a cascading three ring release having a string loop closure;

a pin having a longitudinal axis disposed substantially parallel to a longitudinal axis of said cascading three ring release; and

a pin release mechanism to engage the string loop closure of the cascading three ring release, wherein the pin release mechanism includes a cylinder adapted to move the pin along a direction parallel to said longitudinal axis of said cascading three ring release, whereby in a first position the string loop closure is engage with the pin and whereby in a second position the string loop is disengaged with the pin.

2. The parachute quick release of claim 1 , further comprising:

a cylinder controller selectively providing a source of compressed gas to the cylinder; and

a flexible connector attaching the cylinder to the cylinder such that the source of compressed gas causes the cylinder to move the pin.

3. The parachute quick release of claim 1 , wherein the cylinder comprises a cylinder having a pyrotechnic charge for moving the pin.

4. The parachute quick release of claim 1 , further comprising:

a pin enclosure for supporting the pin, wherein the pin enclosure includes a bore perpendicular to a direction of movement of the pin for receiving a portion of the string loop for engagement by the pin.

5. The parachute quick release of claim 1 , further comprising:

a spring for retaining the pin in the first position.

6. The parachute release of claim 1 , wherein the three ring release is attached to webbing of a parachute.

7. A parachute quick release comprising:

a cascading three ring release having a string loop closure; and

a release mechanism including a piston disposed at least partially within a cylinder such that a longitudinal axis of said piston is disposed substantially parallel to a longitudinal axis of said cascading three ring release, whereby said release mechanism includes a first position wherein said piston is disposed through the string loop closure of the three ring release loop such that said cascading three ring release secures a harness to a parachute and a second position wherein said piston disengages from said string loop closure of the three ring release loop such that said cascading three ring release releases said harness from said parachute.

8. The parachute quick release as claimed in claim 7 wherein said cylinder moves said piston from said first position to said second position along a direction parallel to a longitudinal axis of said cascading three ring release.

9. A method of releasably securing a harness to a parachute, said method comprising:

securing said harness to a largest ring of a cascading three ring release;

securing said parachute to at least said smallest ring of said cascading three ring release;

disposing a string loop through said smallest ring and through an engagement aperture of a release mechanism, said release mechanism secured to said cascading three ring release; and

extending a piston of said release mechanism through a first aperture of said engagement aperture, through said string loop, and into a second aperture of said engagement aperture, wherein said piston secures said string loop which in turn secures said smallest ring.

Assignments (1)
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 6037891300 · May 7, 2002
Related Publication 20040026569A1 · Feb 12, 2004