IP Library › Granted Patent US 12,252,257
Granted Patent B2
US 12,252,257 · App. 17/809,103 · Granted Mar 18, 2025

Parachute with inflation control and load distributing slider loops

Inventor: Anthony D. Kasher (Duluth, MN)
Assignee: Cirrus Design Corporation
B64D17/025B64D17/16B64D17/18B64D17/24
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Quick Facts
Patent No.
US 12,252,257
App. No.
17/809,103
Granted
Mar 18, 2025
Kind
B2
Abstract

Disclosed herein are parachute canopies and sliders for use with parachutes. The parachute canopies can include one or more deformable vent panels that can be used to control an inflation rate of the canopies based on an internal pressure within the canopies. The sliders can include strips that form through holes that have a width that distributes a radial load on suspension lines and allow for the use of lower weight, high modulus suspension lines.

Claims (17)

1. A slider for use with a parachute, the slider comprising:

an annular body including an edge; and

a plurality of material strips attached to the annular body at or near the edge and extending radially outward from the edge, each of the plurality of material strips forming a through hole beyond the edge configured to slidably receive a suspension line of the parachute, wherein the plurality of material strips each have a width that, during a transition of the slider from a reefing state to a non-reefing state, distributes a radial load along a length of the suspension line.

2. The slider of claim 1 , wherein the plurality of material strips comprise an attachment portion and a securing portion, the through hole being in the securing portion, forming a substantially flat strap in an unloaded or natural position.

3. The slider of claim 2 , wherein in a loaded position, the securing portion rotates approximately 90 degrees about a longitudinal axis of the attachment portion.

4. The slider of claim 1 , wherein the plurality of material strips comprise a textile.

5. The slider of claim 4 , wherein the plurality of material strips are deformable to conform to a curvature of the suspension line.

6. The slider of claim 4 , wherein the textile comprises at least one of a poly-paraphenylene terephthalamide, an aromatic copolyimide, or combination thereof.

7. The slider of claim 1 , wherein each of the plurality of material strips comprise a single strip of material with a fold and a stitch placed at a distance from the fold to form the through hole.

8. The slider of claim 7 , wherein a top and a bottom tail of the single strip are secured to a top and a bottom side of the annular body to form an attachment portion.

9. An airplane comprising the slider of claim 1 .

10. A slider for use with a parachute, the slider comprising:

an annular body including an outer peripheral edge; and

a plurality of flexible loops formed from textile material strips and having a first end and a second end defining a length, the first end attached to the annular body at or near the outer peripheral edge and the second end being folded to form a through hole at a location beyond the outer peripheral edge,

wherein:

the through hole is configured to slidably receive a suspension line of the parachute, and

the strip of material has a width measured generally perpendicular to the length that, during disreefing, distributes a radial load along a length of the suspension line.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 27, 2022
From: KASHER, ANTHONY
To: CIRRUS DESIGN CORPORATION D/B/A CIRRUS AIRCRAFT
Reel/Frame 060321/0065 →
Continuity (1)
Related Publication 20230415901A1 · Dec 28, 2023
References Cited (24)
US 2164122A · Pool · 1939 [cited by applicant]
US 2356493A · Smith · 1944 [cited by applicant]
US 7293742B2 · Sadeck · 2007 [cited by examiner]
US 7997535B2 · Babovka · 2011 [cited by examiner]
US 8100365B2 · Fleming, III · 2012 [cited by applicant]
US 10118707B2 · Homan et al. · 2018 [cited by applicant]
US 10399686B2 · Homan et al. · 2019 [cited by applicant]
US 10414506B2 · Homan et al. · 2019 [cited by applicant]
US 10717538B2 · Homan et al. · 2020 [cited by applicant]
US 20010050323A1 · Brownell · 2001 [cited by examiner]
CN 107618669A · 2018 [cited by applicant]
WO WO2024006118A2 · 2024 [cited by applicant]
WO WO2024006118A3 · 2024 [cited by applicant]
“Application Serial No. PCT/US2023/025758, Invitation to Pay Additional Fees mailed Dec. 22, 2023”, 4 pgs. [cited by applicant]
“International Application Serial No. PCT/US2023/025758, International Search Report mailed Mar. 14, 2024”, 5 pgs. [cited by applicant]
“International Application Serial No. PCT/US2023/025758, Written Opinion mailed Mar. 14, 2024”, 9 pgs. [cited by applicant]
U.S. Appl. No. 15/431,689 U.S. Pat. No. 10,118,707, filed Feb. 13, 2017, Aircraft Parachute Deployment Autopilot. [cited by applicant]
U.S. Appl. No. 15/431,685 U.S. Pat. No. 10,399,686, filed Feb. 13, 2017, Mechanical Timing Connection for Sequencing Airbag Activation with Rocket for Deploying Aircraft Parachute. [cited by applicant]
U.S. Appl. No. 15/431,688 U.S. Pat. No. 10,717,538, filed Feb. 13, 2017, Bridle for Aircraft Parachute Deployment Rocket. [cited by applicant]
U.S. Appl. No. 15/431,687 U.S. Pat. No. 10,414,506, filed Feb. 13, 2017, Aircraft Parachute System Utilizing Airbag to Assist with Parachute Deployment. [cited by applicant]
U.S. Appl. No. 62/294,399, filed Feb. 12, 2016, Aircraft Parachute System. [cited by applicant]
U.S. Appl. No. 15/836,885 RE47,474, Dec. 10, 2017, Intelligent Ballistic Parachute System that Performs Pre-Activation and/or Post-Activation Actions. [cited by applicant]
U.S. Appl. No. 16/422,357 U.S. Pat. No. 8,100,365, Feb. 10, 2009, Intelligent Ballistic Parachute System that Performs Pre-Activation and/or Post-Activation Actions. [cited by applicant]
U.S. Appl. No. 15/836,885 U.S. Pat. No. 8,056,861, Feb. 10, 2009, Intelligent Ballistic Parachute System that Performs Pre-Activation and/or Post-Activation Actions. [cited by applicant]