公开(公告)号：US20200094974A1

公开(公告)日：2020-03-26

申请号：US16138336

申请日：2018-09-21

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson ,  Scott R. Patterson

IPC: B64D25/02 ,  B64D25/10 ,  B64D17/24 ,  B64D17/62 ,  B64D17/30

Abstract: A parachute assembly for an ejection seat may comprise a canopy and a first suspension line coupled to the canopy. A first riser may be coupled to the first suspension line. A seat cushion may be coupled to the first riser. The seat cushion may be configured detach from the ejection seat and restrict rearward translation of a head of an occupant of the ejection seat upon deployment of the parachute assembly.

公开(公告)号：US11618576B2

公开(公告)日：2023-04-04

申请号：US17518884

申请日：2021-11-04

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson

IPC: B64D25/10 ,  B64D25/04 ,  B64D17/22 ,  B64D25/18

Abstract: A life preserver head restraint may be configured to inflate in response to deployment of a parachute assembly. The life preserver head restraint may comprise an inflatable volume and a charge tank fluidly coupled to the inflatable volume. In an inflated state, the life preserver head restraint may restrict head movement during line stretch of the parachute assembly.

公开(公告)号：US20220055755A1

公开(公告)日：2022-02-24

申请号：US17518884

申请日：2021-11-04

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson

IPC: B64D25/04 ,  B64D17/22 ,  B64D25/18 ,  B64D25/10

Abstract: A life preserver head restraint may be configured to inflate in response to deployment of a parachute assembly. The life preserver head restraint may comprise an inflatable volume and a charge tank fluidly coupled to the inflatable volume. In an inflated state, the life preserver head restraint may restrict head movement during line stretch of the parachute assembly.

公开(公告)号：US11148815B2

公开(公告)日：2021-10-19

申请号：US16245764

申请日：2019-01-11

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson

IPC: B64D17/34 ,  B64D17/26

Abstract: A suspension line assembly for a parachute may comprise a first set of suspension lines bound together to form a first riser, and a second set of suspension lines bound together to form a second riser. A confluence may be formed by the first set of suspension line and the second set of suspension line. The confluence may comprise interior confluence suspension lines and exterior confluence suspension lines that alternate circumferentially along a perimeter of a parachute canopy.

公开(公告)号：US20210269165A1

公开(公告)日：2021-09-02

申请号：US17321165

申请日：2021-05-14

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Bradley Mastrolia ,  Kassidy L. Carson ,  Scott Seeber

IPC: B64D17/76 ,  B64D17/26 ,  B64D17/38

Abstract: A multi-staged suspension line length parachute may include a suspension line having a primary length and a secondary length. The primary length may be deployable upon a first deployment of the multi-staged suspension line length parachute. The secondary length may be prevented from deployment until the primary length has fully deployed. An attenuator may attach a first portion of the secondary length to a second portion of the secondary length.

公开(公告)号：US10053221B2

公开(公告)日：2018-08-21

申请号：US15153473

申请日：2016-05-12

Applicant: GOODRICH CORPORATION

Inventor： Bradley Mastrolia ,  Kassidy L. Carson

IPC: B64D17/52 ,  B64D17/38 ,  B64D17/34 ,  B64D17/58

CPC classification number: B64D17/386 ,  B64D17/26 ,  B64D17/343 ,  B64D17/346 ,  B64D17/58

Abstract: A multi-staged suspension line length parachute is provided. The parachute may comprise a canopy, a suspension line, a bundle, a bundling confluence, a traditional confluence, and a riser. The parachute may also comprise a cutter and a cutter pin puller configured to activate the cutter. The bundle may comprise a bundling line configured to secure secondary length from the suspension line. The parachute may deploy to a first length. In response to tension on the cutter pin puller, the cutter may activate to sever the bundling line in the bundle, causing the secondary length of the suspension line to release. The parachute may then deploy to a second length.

公开(公告)号：US20200307810A1

公开(公告)日：2020-10-01

申请号：US16369346

申请日：2019-03-29

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson

IPC: B64D25/04 ,  B64D25/10 ,  B64D25/18 ,  B64D17/22

Abstract: A life preserver head restraint may be configured to inflate in response to deployment of a parachute assembly. The life preserver head restraint may comprise an inflatable volume and a charge tank fluidly coupled to the inflatable volume. In an inflated state, the life preserver head restraint may restrict head movement during line stretch of the parachute assembly.

公开(公告)号：US20200156797A1

公开(公告)日：2020-05-21

申请号：US16193869

申请日：2018-11-16

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Bradley Mastrolia ,  Kassidy L. Carson ,  Scott Seeber

IPC: B64D17/76 ,  B64D17/38 ,  B64D17/26

Abstract: A multi-staged suspension line length parachute may include a suspension line having a primary length and a secondary length. The primary length may be deployable upon a first deployment of the multi-staged suspension line length parachute. The secondary length may be prevented from deployment until the primary length has fully deployed. An attenuator may attach a first portion of the secondary length to a second portion of the secondary length.

公开(公告)号：US20200094973A1

公开(公告)日：2020-03-26

申请号：US16138216

申请日：2018-09-21

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson ,  Scott R. Patterson ,  Drew Hartman

IPC: B64D25/02 ,  B64D17/30 ,  B64D25/10

Abstract: An inflatable head restraint system for a parachute assembly may comprise an inflatable volume configured to inflate in response to a deployment of the parachute assembly. The inflatable volume may be located between a left shoulder riser and a right shoulder riser of the parachute assembly. A conduit may be fluidly coupled to the inflatable volume.

公开(公告)号：US20200094972A1

公开(公告)日：2020-03-26

申请号：US16138014

申请日：2018-09-21

Applicant: GOODRICH CORPORATION

Inventor： Jaro S. Volny ,  Kassidy L. Carson ,  Scott R. Patterson

IPC: B64D17/24 ,  B64D17/30

Abstract: A parachute assembly for decelerating an occupant of an ejection seat may comprise a left shoulder riser configured to be located over a left shoulder of the occupant upon deployment of the parachute assembly. A right shoulder riser may be configured to be located over a right shoulder of the occupant upon deployment of the parachute assembly. A head restraint, configured to be behind a head of the occupant upon deployment of the parachute assembly, may be located between the left and right shoulder risers.