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公开(公告)号：US11840986B2
公开(公告)日：2023-12-12
申请号：US16857487
申请日：2020-04-24
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
IPC: F02K1/62 , F02K1/70 , B29C43/18 , B29C65/02 , B29C65/48 , B29C65/00 , B29K101/12 , F02K1/72 , B29L31/00
CPC classification number: F02K1/70 , B29C43/18 , B29C65/02 , B29C65/48 , B29C66/7254 , B29C2043/189 , B29K2101/12 , B29L2031/7504 , F02K1/625 , F02K1/72 , F05D2220/32 , F05D2230/23 , F05D2230/60 , F05D2250/283 , F05D2260/96 , F05D2300/43 , F05D2300/432 , F05D2300/433 , F05D2300/434 , F05D2300/436
Abstract: A blocker door assembly for use in a gas turbine includes a panel, a core integrally formed with the panel, and a plurality of mounting structures extending from at least one of the panel and the core. The plurality of mounting structures are integrally formed with the core and the panel such that the panel, the core, and the mounting structures are co-molded from a thermoplastic material.
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公开(公告)号：US11365705B2
公开(公告)日：2022-06-21
申请号：US16170966
申请日：2018-10-25
Applicant: The Boeing Company
Inventor： Patrick J. Kinlen , Randy J. Grove
Abstract: Disclosed are laminates comprising a carbon fiber reinforced polymer sheet and a layer of polysilazane and methods for producing such laminates.
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公开(公告)号：US20180056554A1
公开(公告)日：2018-03-01
申请号：US15250297
申请日：2016-08-29
Applicant: THE BOEING COMPANY
Inventor： Kevin O'Brien Gaw , Michael A. Nill , Gary Anthony Booker , Stephen Dark , Laura Fournier , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch , Michael H. Larson
Abstract: A compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door is provided. The compression molding assembly includes a ram plate comprising a plurality of openings defined therethrough and a plurality of core inserts coupled to the ram plate such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells.
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公开(公告)号：US10794326B2
公开(公告)日：2020-10-06
申请号：US15250253
申请日：2016-08-29
Applicant: THE BOEING COMPANY
Inventor： Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
Abstract: A blocker door assembly for use in a gas turbine engine includes a facesheet including a plurality of openings to facilitate noise attenuation and a body portion coupled to the facesheet. The body portion includes a backsheet integrally formed with a honeycomb core, wherein the body portion is molded from a thermoplastic material.
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公开(公告)号：US20200291892A1
公开(公告)日：2020-09-17
申请号：US16857487
申请日：2020-04-24
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
Abstract: A blocker door assembly for use in a gas turbine includes a panel, a core integrally formed with the panel, and a plurality of mounting structures extending from at least one of the panel and the core. The plurality of mounting structures are integrally formed with the core and the panel such that the panel, the core, and the mounting structures are co-molded from a thermoplastic material.
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Patent Agency Ranking
公开(公告)号：US11713732B2
公开(公告)日：2023-08-01
申请号：US17745492
申请日：2022-05-16
Applicant: The Boeing Company
Inventor： Patrick J. Kinlen , Randy J. Grove
IPC: C08J7/04 , F02K1/82 , B32B3/12 , B32B3/26 , B32B7/12 , B32B15/08 , B32B15/20 , F02K1/34 , F02K1/54
CPC classification number: F02K1/827 , B32B3/12 , B32B3/266 , B32B7/12 , B32B15/08 , B32B15/20 , B64D33/06 , C08J7/0427 , F02K1/54 , B32B2255/10 , B32B2255/26 , B32B2262/106 , B32B2305/024 , B32B2307/206 , B32B2307/714 , B32B2605/18 , C08J2483/16 , F05D2220/323 , F05D2260/96 , F05D2300/514 , F05D2300/603
Abstract: Disclosed are laminates comprising a carbon fiber reinforced polymer sheet and a layer of polysilazane and methods for producing such laminates.
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公开(公告)号：US20220275772A1
公开(公告)日：2022-09-01
申请号：US17745492
申请日：2022-05-16
Applicant: The Boeing Company
Inventor： Patrick J. Kinlen , Randy J. Grove
Abstract: Disclosed are laminates comprising a carbon fiber reinforced polymer sheet and a layer of polysilazane and methods for producing such laminates.
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公开(公告)号：US10406729B2
公开(公告)日：2019-09-10
申请号：US15250297
申请日：2016-08-29
Applicant: THE BOEING COMPANY
Inventor： Kevin O'Brien Gaw , Michael A. Nill , Garry Anthony Booker , Stephen R. Dark , Laura Fournier , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch , Michael H. Larson
IPC: B29C43/36 , B29C43/18 , B29C43/50 , B29C33/00 , B29C33/30 , B29D99/00 , F02K1/00 , F02K1/72 , B29K101/12 , B29L31/00 , B29C33/44 , B29L31/60 , B64D29/00
Abstract: A compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door is provided. The compression molding assembly includes a ram plate comprising a plurality of openings defined therethrough and a plurality of core inserts coupled to the ram plate such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells.
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公开(公告)号：US09945735B2
公开(公告)日：2018-04-17
申请号：US14856550
申请日：2015-09-16
Applicant: The Boeing Company
Inventor： Gary E. Georgeson , Wesley L. Holman, Jr. , Brandon P. Jamison , Randy J. Grove
CPC classification number: G01K11/12 , B29C35/0288 , B29C73/34 , G01N21/64 , G01N21/71 , G01N2201/061
Abstract: There is provided a system, a method, and a thermochromatic witness assembly to monitor a thermal environment of a composite structure. The thermochromatic witness assembly has a polymeric material and one or more thermochromatic probes mixed into the polymeric material to form a thermochromatic probe mixture. The thermochromatic probe mixture is applied to a transparent polymeric film, or is formed into the transparent polymeric film with a pressure sensitive adhesive (PSA) applied thereto, thus forming the thermochromatic witness assembly in a form of a thermochromatic applique. The thermochromatic applique is configured to be applied directly and continuously to a surface of the composite structure. The thermochromatic applique is further configured to monitor the thermal environment of the composite structure by detecting one or more temperatures and one or more times the surface of the composite structure is exposed to the thermal environment.
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10.发明申请公开(公告)号：US20180058373A1
公开(公告)日：2018-03-01
申请号：US15250253
申请日：2016-08-29
Applicant: THE BOEING COMPANY
Inventor： Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
Abstract: A blocker door assembly for use in a gas turbine engine includes a facesheet including a plurality of openings to facilitate noise attenuation and a body portion coupled to the facesheet. The body portion includes a backsheet integrally formed with a honeycomb core, wherein the body portion is molded from a thermoplastic material.
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