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公开(公告)号:US11021256B2
公开(公告)日:2021-06-01
申请号:US16138336
申请日:2018-09-21
Applicant: GOODRICH CORPORATION
Inventor: Jaro S. Volny , Kassidy L. Carson , Scott R. Patterson
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.
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公开(公告)号:US10946970B2
公开(公告)日:2021-03-16
申请号:US16138415
申请日:2018-09-21
Applicant: GOODRICH CORPORATION
Inventor: Jaro S. Volny , Kassidy L. Carson , Scott R. Patterson
Abstract: A system for translating a head restraint of a parachute assembly away from a head of an occupant supported by the parachute assembly may comprise a chord coupled to the head restraint and at least one of a control line configured to manipulate a canopy of the parachute assembly or a handle coupled to the control line.
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公开(公告)号:US20200094975A1
公开(公告)日:2020-03-26
申请号:US16138415
申请日:2018-09-21
Applicant: GOODRICH CORPORATION
Inventor: Jaro S. Volny , Kassidy L. Carson , Scott R. Patterson
Abstract: A system for translating a head restraint of a parachute assembly away from a head of an occupant supported by the parachute assembly may comprise a chord coupled to the head restraint and at least one of a control line configured to manipulate a canopy of the parachute assembly or a handle coupled to the control line.
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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
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.
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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
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.
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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
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.
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公开(公告)号:US11046444B2
公开(公告)日:2021-06-29
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
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.
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公开(公告)号:US11027851B2
公开(公告)日:2021-06-08
申请号:US16138014
申请日:2018-09-21
Applicant: GOODRICH CORPORATION
Inventor: Jaro S. Volny , Kassidy L. Carson , Scott R. Patterson
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.
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