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公开(公告)号：US12257787B2
公开(公告)日：2025-03-25
申请号：US17484985
申请日：2021-09-24
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich , Georgios S. Zafiris , Joyel M. Schaefer
Abstract: In accordance with at least one aspect of this disclosure, a composite structure can be formed of or including a plurality of composite strips. The plurality of composite strips include one or more filler strips which can have at least one filler edge having a filler edge geometry between a first surface and second surface, the second surface being opposite the first surface. The filler edge geometry can be configured to prevent formation of one or more gaps between one or more adjacent composite strips.
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公开(公告)号：US12209620B2
公开(公告)日：2025-01-28
申请号：US17573722
申请日：2022-01-12
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich , Brayton Reed , Michael King , Joyel M. Schaefer
Abstract: A flexible coupling includes a first flange having an outer edge, a first surface, a second surface opposite the first surface, and a first plurality of passages. A second flange including an outer edge section, a first surface section, a second surface section opposite the first surface section, and a second plurality of passages. A connecting element extends between and connecting the first flange and the second flange through one of the first plurality of passages and one of the second plurality passages. The connecting element includes a connecting member having a first stop element and a second stop element. A compliant component is arranged on the connecting element. The compliant component is positioned on the connecting member between one of: the first stop element and the first surface; the second stop element and the second surface section; and between the second surface and the first surface section.
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公开(公告)号：US20230099452A1
公开(公告)日：2023-03-30
申请号：US17485013
申请日：2021-09-24
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich , Georgios S. Zafiris , Joyel M. Schaefer
Abstract: In accordance with at least one aspect of this disclosure, a composite structure can be formed of or including a plurality of composite strips. The plurality of composite strips include one or more filler strips which can have at least one filler edge having a filler edge geometry between a first surface and second surface, the second surface being opposite the first surface. The filler edge geometry can be configured to prevent formation of one or more gaps between one or more adjacent composite strips.
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公开(公告)号：US20210361800A1
公开(公告)日：2021-11-25
申请号：US17327057
申请日：2021-05-21
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich
Abstract: An antiviral system comprises, an interior space, and an ultra-violet (UV) illuminator system fixedly mounted within the interior space for illumination of surfaces within the interior space for destruction of pathogens on the surfaces. A plurality of seats can be arranged within the interior space such that the UV illuminator system is configured to illuminate full or partial surfaces of individual seats of the plurality of seats.
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公开(公告)号：US20170369157A1
公开(公告)日：2017-12-28
申请号：US15190978
申请日：2016-06-23
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich , Rony Giovanni Ganis
IPC: B64C25/00
CPC classification number: B64C25/00 , B29C70/72 , B32B3/06 , B64C25/60 , F16C7/026 , F16C2326/05 , F16C2326/43
Abstract: A composite metallic joint assembly may include a composite metal rod having a metal liner and a composite material disposed around the metal liner. A first portion of the composite metal rod may comprise the composite material and the metal liner and a second portion of the composite metal rod may comprise the metal liner exposed at a radially outer surface of the composite metal rod. The metal liner may have a first radial thickness at a first axial position corresponding to the first portion of the composite metal rod and a second radial thickness at a second axial position corresponding to the second portion of the composite metal rod. The second thickness may be greater than the first thickness.
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Patent Agency Ranking
公开(公告)号：US20170238369A1
公开(公告)日：2017-08-17
申请号：US15428072
申请日：2017-02-08
Applicant: Goodrich Corporation
Inventor： George F. Owens , Kevin E. Roach , James Mullen , Michael J. Giamati , Jon Shearer , James Van Twisk , David L. Brittingham , Tommy M. Wilson, JR. , Jin Hu , William A. Veronesi , Mark R. Gurvich , Joseph Winesdoerffer , Jason Gesner
CPC classification number: H05B3/26 , B32B3/12 , B32B7/12 , B32B15/20 , B32B2255/00 , B32B2307/202 , B32B2605/18 , B64C1/18 , B64D13/08 , F24D13/024 , H01C17/06 , Y02B30/26
Abstract: An aircraft heated floor panel includes a first face sheet, a second face sheet opposite the first face sheet, and core with an electrically conductive core portion. The electrically conductive core portion supports the first face sheet and the second face sheet, and is electrically insulated from the external environment to receive electrical power, resistively generate heat, and communicate heat to the first face sheet.
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公开(公告)号：US12253495B2
公开(公告)日：2025-03-18
申请号：US17958866
申请日：2022-10-03
Applicant: Goodrich Corporation
Inventor： Douglas McNeil , Jeffrey J. Allen , Joyel Schaefer , Mark R. Gurvich , Michael J. King , Brayton Reed
IPC: G01N29/04 , G01N29/06 , G01N29/22 , G01N29/265 , G10K11/00
Abstract: A testing device includes a first member to be positioned on one surface of a part to be tested. A second member to be positioned on an opposed surface of the part to be tested. One of the first and second members have an ultrasonic transmitter and the other has an ultrasonic receiver. At least one of the first and second members have at least one magnetic element and the other of the first and second member have at least one magnetic or at least one ferromagnetic metallic element such that when one of the first and second members moves along the surface of the tested part the other of the first and second members will move along an opposed surface with the one of the members.
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公开(公告)号：US12180837B1
公开(公告)日：2024-12-31
申请号：US18238945
申请日：2023-08-28
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich , Leo J. Veilleux, Jr.
IPC: F01B31/28 , B29C70/32 , B29C70/38 , B29C70/68 , B29K705/00
Abstract: In accordance with at least one aspect of this disclosure, a system (e.g., for aircraft systems) includes an actuator cylinder. The actuator cylinder comprises, a composite cylinder body, the composite cylinder body being axi-symmetric across at least a longitudinal axis. In embodiments, the composite cylinder body can include, a first plurality of plies laid in a first direction relative to the longitudinal axis and second plurality of plies laid in a second direction relative to the longitudinal axis different from the first direction to form a hollow chamber. The actuator cylinder can include a first metallic reinforcing ring and a second metallic reinforcing ring disposed at respective axial ends of the cylinder body configured to anchor the first plurality of plies and provide an axial reaction under axial stress and configured to provide load transfer from the cylinder body to one or more adjacent actuator components.
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公开(公告)号：US20240328453A1
公开(公告)日：2024-10-03
申请号：US18127584
申请日：2023-03-28
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich , Michael J. King , Brayton Reed , Joyel M. Schaefer
IPC: F16C3/02
CPC classification number: F16C3/026 , F16C2220/42 , F16C2326/06
Abstract: In accordance with at least one aspect of this disclosure, a composite shaft includes a plurality of composite elements arranged about an axis to form a hollow shaft with at least one undulation. The plurality of composite elements incudes a first group of the composite elements arranged about the axis offset by an angle +α and a second group of the composite elements arranged about the axis offset by an angle −α to form a web with the first group of composite elements. The first and second groups of the plurality of composite elements are configured to cooperate with one another to allow the hollow shaft to be flexible under axial load and stiff under rotational load.
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公开(公告)号：US12090586B2
公开(公告)日：2024-09-17
申请号：US17654389
申请日：2022-03-10
Applicant: Goodrich Corporation
Inventor： Mark R. Gurvich
CPC classification number: B23P11/00 , B29C66/126 , B29C66/3032 , B29C66/5221 , B29C66/721 , B29C66/742 , B29C70/766 , B29C66/534 , B29C66/73751 , B29C66/73753 , B29C66/7392 , B29C66/7394
Abstract: A method of forming a joint between a composite component and a metallic component is disclosed. The method includes forming a first groove in an outer surface of the metallic component on a first end of the metallic component. The first groove extends circumferentially on the outer surface relative to a center axis of the metallic component, and the first groove extends radially inward from the outer surface relative the center axis. The method further includes inserting the first end of the metallic component into a first end of the composite component. A second groove on the composite component over the first groove of the metallic component such that the composite component extends radially inward into the first groove of the metallic component. A composite hoop reinforcement is then applied in the second groove in a circumferential direction and the composite component, and the composite hoop reinforcement are solidified.
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