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公开(公告)号:US20150375343A1
公开(公告)日:2015-12-31
申请号:US14316330
申请日:2014-06-26
Applicant: GOODRICH CORPORATION
Inventor: Christopher L. Chapman , Sayan Rakshit , Tommy R. Hawkins , Satya Swaroop Panda
CPC classification number: B23K26/364 , B23K26/0626 , B23K26/0876 , B23K26/402 , B23K2103/36 , B27D5/00 , B27H1/00 , B29K2001/00 , B29L2009/00 , B32B3/085 , B32B3/263 , B32B21/042 , B32B21/13 , B32B21/14 , B32B2307/546 , B32B2317/16
Abstract: Systems and methods are disclosed herein for laser kerfed veneers. A laser may be used to produce kerf lines in thin veneers. The settings of the laser may be adjusted to adjust the width and depth of the kerf lines. The width and depth of the kerf lines may be selected in order to provide sufficient strength to the veneer while decreasing telegraphing.
Abstract translation: 本文公开了用于激光切割单板的系统和方法。 可以使用激光器来生产薄薄单板中的切口线。 可以调节激光器的设置以调整切口线的宽度和深度。 可以选择切口线的宽度和深度,以便在减少通讯的同时向单板提供足够的强度。
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公开(公告)号:US11673674B2
公开(公告)日:2023-06-13
申请号:US17134308
申请日:2020-12-26
Applicant: Goodrich Corporation
Inventor: Skandan Berikai Kuppan , Jeffrey Martin Werbelow , Satya Swaroop Panda , Rohan Rajiv Motewar
CPC classification number: B64D25/14 , B32B5/024 , B32B7/09 , B32B27/12 , B32B27/304 , D03D1/02 , D03D11/00 , D03D15/283 , B32B2262/0284 , B32B2307/7242 , D10B2331/04 , D10B2505/12
Abstract: An evacuation slide may comprise a first side rail, a second side rail, and a sliding structure. The first side rail and the second side rail may each extend from a head end of the evacuation slide to a toe end of the evacuation slide. The sliding structure may be located between the first side rail and the second side rail. The sliding structure may comprise a drop stitch fabric.
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公开(公告)号:US20210180710A1
公开(公告)日:2021-06-17
申请号:US16787554
申请日:2020-02-11
Applicant: GOODRICH CORPORATION
Inventor: Yasasvi Harish Kumar , Skandan Berikai Kuppan , Satya Swaroop Panda
IPC: F16K27/02 , F16K31/122 , F16K17/12 , F16K1/36 , F16K5/10
Abstract: Disclosed is a pressure regulator, comprising: a first cylindrical chamber; a second cylindrical chamber located concentrically within the first cylindrical chamber and in thermal communication with the first cylindrical chamber; and further comprising at least one of: an internal valve, wherein the internal valve is connected at a first end to the first cylindrical chamber and at a second end to the second cylindrical chamber, wherein the internal valve allows the flow of gas from the second cylindrical chamber to the first cylindrical chamber; and an external gas chamber and an external valve, wherein the external gas chamber is located outside the first cylindrical chamber, wherein the external valve is connected at a first end to the first cylindrical chamber and at a second end to the external gas chamber, wherein the external valve allows the flow of gas from the external gas chamber to the first cylindrical chamber.
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公开(公告)号:US10920794B2
公开(公告)日:2021-02-16
申请号:US16207740
申请日:2018-12-03
Applicant: GOODRICH CORPORATION
Inventor: Skandan Berikai Kuppan , Satya Swaroop Panda
Abstract: An aspirator may include an aspirator body comprising an outer wall and an inner wall, the inner wall defining a body channel. The aspirator may include an aspirator body including an outer wall and an inner wall, the inner wall defining a body channel. The aspirator body may include a plenum disposed between the outer wall and the inner wall. The aspirator body may include a plurality of apertures disposed between the outer wall and the inner wall and defined by a side wall and the plenum. The aspirator may include an aspirator barrel comprising a barrel outer wall and a barrel inner wall, the barrel inner wall defining an air channel. The air channel may be in fluid communication with the plenum.
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公开(公告)号:US10220934B2
公开(公告)日:2019-03-05
申请号:US15052515
申请日:2016-02-24
Applicant: Goodrich Corporation
IPC: B64C1/40 , B32B21/08 , B32B7/12 , B32B27/20 , B32B21/14 , B32B27/08 , B32B27/12 , B32B27/18 , B32B27/30 , B32B27/38 , B32B27/42 , B64C1/06 , B64D45/00
Abstract: An aviation laminate includes an intumescent backer sheet covered by a decorative sheet. The aviation laminate is generally fire-resistant, may be structural, and may be used to construct various components within an aircraft cabin that may be held to government/regulatory fire mitigation requirements.
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