公开(公告)号：US20250144862A1

公开(公告)日：2025-05-08

申请号：US19018415

申请日：2025-01-13

Applicant: CORNING INCORPORATED

Inventor： Patrick W. Albor ,  Roy Joseph Bourcier ,  Eric Hamilton Starns

IPC: B29C48/00 ,  B29C51/00 ,  B29C51/02 ,  B29C64/165 ,  B29C64/188 ,  B29C64/194 ,  B29C64/209 ,  B29C64/321 ,  B29C64/336 ,  B29C70/12 ,  B29C70/20 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y80/00

Abstract: The disclosure relates to embodiments of an apparatus for producing polymer composite panels. The polymer composite panels include one or more layers of a polymeric matrix having discontinuous fibers embedded therein. The apparatus has a frame, a deposition bed, and a deposition head configured to move relative to the frame and over the deposition bed. The deposition head includes at least one extruder and a nozzle array. The extruder is configured to force the polymeric matrix and discontinuous fibers through the nozzle array and onto the deposition bed. The deposition head is configured to deposit an entire layer of a polymer composite panel on the deposition bed in a single pass so that the discontinuous fibers are oriented in the direction of the single pass. The disclosure also relates to embodiments of a method of forming a polymer composite panel and to embodiments of a polymer composite panel.

公开(公告)号：US20250019288A1

公开(公告)日：2025-01-16

申请号：US18711990

申请日：2022-11-08

Applicant: CORNING INCORPORATED

Inventor： Roy Joseph Bourcier ,  Benedict Yorke Johnson ,  Aniello Mario Palumbo

IPC: C03B11/06 ,  C03B40/02

Abstract: In one aspect, a pressing unit is provided, comprising: a mold and a plunger, and a coating configured on at least one of: the surface of the mold and/or the surface of the plunger, where the coating is configured adjacent to the areas where molten or hot glass or glass ceramic touches; wherein the coating comprises: a mold release coating, configured as the gob-contacting surface, wherein the mold release coating comprises: at least two solid lubricants selected from tungsten disulfide, boron nitride, glassy carbon and graphite; and a thermal barrier coating comprising barrier material components and an organo-silica binder.

公开(公告)号：US12226942B2

公开(公告)日：2025-02-18

申请号：US16809071

申请日：2020-03-04

Applicant: CORNING INCORPORATED

Inventor： Patrick W Albor ,  Roy Joseph Bourcier ,  Eric Hamilton Starns

IPC: B32B3/10 ,  B29C48/00 ,  B29C51/00 ,  B29C51/02 ,  B29C64/165 ,  B29C64/188 ,  B29C64/194 ,  B29C64/209 ,  B29C64/321 ,  B29C64/336 ,  B29C70/12 ,  B29C70/20 ,  B32B3/14 ,  B32B3/18 ,  B32B5/02 ,  B32B5/12 ,  B32B5/26 ,  B32B5/28 ,  B32B27/00 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y80/00

Abstract: The disclosure relates to embodiments of an apparatus for producing polymer composite panels. The polymer composite panels include one or more layers of a polymeric matrix having discontinuous fibers embedded therein. The apparatus has a frame, a deposition bed, and a deposition head configured to move relative to the frame and over the deposition bed. The deposition head includes at least one extruder and a nozzle array. The extruder is configured to force the polymeric matrix and discontinuous fibers through the nozzle array and onto the deposition bed. The deposition head is configured to deposit an entire layer of a polymer composite panel on the deposition bed in a single pass so that the discontinuous fibers are oriented in the direction of the single pass. The disclosure also relates to embodiments of a method of forming a polymer composite panel and to embodiments of a polymer composite panel.

公开(公告)号：US20150131949A1

公开(公告)日：2015-05-14

申请号：US14334839

申请日：2014-07-18

Applicant: Corning Incorporated

Inventor： Venkata Adiseshaiah Bhagavatula ,  Roy Joseph Bourcier ,  Satish Chandra Chaparala ,  John Himmelreich

IPC: G02B6/255

CPC classification number: G02B6/2551 ,  B29C65/1406 ,  B29C65/16 ,  B29C65/1616 ,  B29C65/1619 ,  B29C65/4815 ,  B29C65/4835 ,  B29C65/484 ,  B29C65/4845 ,  B29C65/72 ,  B29C66/21 ,  B29C66/3452 ,  B29C2035/0822 ,  B29C2035/0827 ,  G02B6/3801 ,  G02B6/4237 ,  G02B6/4239 ,  Y10T428/269 ,  Y10T428/31551 ,  Y10T428/31663 ,  Y10T428/31721

Abstract: A method of assembling optoelectronic and/or photonic components, said method comprising: (i) providing at least two optoelectronic and/or photonic components; (ii) aligning and situating these components relative to one another and in close proximity with one another so as to: (a) provide optical coupling between these components; and (b) maintain the distance d between the adjacent parts of these components, where d is 0 to 100 μm; (iii) adhering these components to one another with while maintaining optical coupling therebetween; and (iv) laser welding these components together while maintaining optical coupling therebetween.

Abstract translation: 一种组装光电子和/或光子组件的方法，所述方法包括：（i）提供至少两个光电子和/或光子分量; （ii）使这些部件相对于彼此并且彼此紧密地对准和定位，以便：（a）在这些部件之间提供光耦合; 和（b）保持这些组分的相邻部分之间的距离d，其中d为0至100μm; （iii）在保持它们之间的光耦合的同时将这些部件彼此粘合; 和（iv）将这些部件激光焊接在一起，同时保持它们之间的光耦合。

公开(公告)号：US20190186355A1

公开(公告)日：2019-06-20

申请号：US16327950

申请日：2017-08-25

Applicant: CORNING INCORPORATED

Inventor： Dana Craig Bookbinder ,  Roy Joseph Bourcier ,  Wlliam Edward Lock ,  Richard Curwood Peterson ,  Irene Marjorie Slater ,  Pushkar Tandon

IPC: F02B77/02 ,  F02B77/11 ,  F01N13/14 ,  F02B23/08 ,  F02F3/14 ,  F02F3/24 ,  F02F1/00

CPC classification number: F02B77/02 ,  F01N13/14 ,  F02B23/08 ,  F02B77/11 ,  F02F1/004 ,  F02F3/14 ,  F02F3/24 ,  F05C2251/048

Abstract: A thermal barrier for component surfaces of an engine. The thermal barrier includes a plurality of modules, each module includes a shield. An edge of at least one shield in the array is spaced apart from an edge of an adjacent shield in the array.

公开(公告)号：US20220033942A1

公开(公告)日：2022-02-03

申请号：US17279420

申请日：2019-09-20

Applicant: CORNING INCORPORATED

Inventor： Roy Joseph Bourcier ,  Thomas William Brew ,  Antonia Lee McMullan ,  Obiefuna Chukwuemeka Okafor

IPC: C22C38/46 ,  C22C38/44 ,  C22C38/04 ,  C22C38/02 ,  C23C16/30 ,  C23C16/36 ,  C22C33/02

Abstract: An article including a metal having an austenite transformation temperature of 850 degrees C. or more. The metal may be a steel, such as a stainless steel, a martensitic steel, or a martensitic stainless steel. In some embodiments, the metal is a steel including iron, molybdenum, and tungsten, and at least one of the following: manganese, nickel, chromium, and vanadium, where the manganese, nickel, chromium, and vanadium are in the following ranges: manganese: less than 0.1 wt %, nickel: less than 0.7 wt %, chromium: more than 12.5 wt %, and vanadium: more than 0.3 wt %. The article may have a surface coated with inorganic particles. In some embodiments, the article is an extrusion die, such as a honeycomb extrusion die.

公开(公告)号：US20190186356A1

公开(公告)日：2019-06-20

申请号：US16327933

申请日：2017-08-25

Applicant: CORNING INCORPORATED

Inventor： Dana Craig Bookbinder ,  Roy Joseph Bourcier ,  William Edward Lock ,  Richard Curwood Peterson ,  Irene Marjorie Slater ,  Pushkar Tandon

IPC: F02B77/11 ,  F16L59/02 ,  F16L59/07 ,  F16L59/12

CPC classification number: F02B77/11 ,  F02F3/14 ,  F16L59/028 ,  F16L59/07 ,  F16L59/123

Abstract: A segmented thermal barrier for a combustion chamber surface of an internal combustion engine. The segmented thermal barrier includes a plurality of modules, each module with a support and a shield. The edges of shields of at least two adjacent modules are spaced apart by a distance.

公开(公告)号：US10302013B2

公开(公告)日：2019-05-28

申请号：US15278696

申请日：2016-09-28

Applicant: Corning Incorporated

Inventor： Dana Craig Bookbinder ,  Roy Joseph Bourcier ,  William Edward Lock ,  Richard Curwood Peterson ,  Irene Marjorie Slater ,  Pushkar Tandon ,  Christopher John Warren

IPC: F02B77/11 ,  F02F3/00 ,  F02F3/26 ,  B32B7/02 ,  B32B15/00 ,  B32B15/16 ,  B32B3/12 ,  F02F1/18

Abstract: A composite thermal barrier and methods of applying the composite thermal barrier to a metallic surface within a combustion chamber of an engine. The composite thermal barrier includes at least one metallic support structure, a metallic skin, and an insulation material. The metallic support structure is connected to a metallic surface within the combustion chamber of the engine. The metallic skin is disposed adjacent to the metallic support structure to define a void space between the metallic skin and the metallic surface. The insulation material is contained within the volume to form the composite thermal barrier.

公开(公告)号：US20170089260A1

公开(公告)日：2017-03-30

申请号：US15278696

申请日：2016-09-28

Applicant: Corning Incorporated

Inventor： Dana Craig Bookbinder ,  Roy Joseph Bourcier ,  William Edward Lock ,  Richard Curwood Peterson ,  Irene Marjorie Slater ,  Pushkar Tandon ,  Christopher John Warren

IPC: F02B77/11 ,  F02F3/00 ,  F02F3/26

CPC classification number: F02B77/11 ,  B32B3/12 ,  B32B7/02 ,  B32B15/00 ,  B32B15/16 ,  B32B2307/304 ,  B32B2315/02 ,  F02F1/18 ,  F02F3/0015 ,  F02F3/0084 ,  F02F3/26 ,  F02F2200/00

Abstract: A composite thermal barrier and methods of applying the composite thermal barrier to a metallic surface within a combustion chamber of an engine. The composite thermal barrier includes at least one metallic support structure, a metallic skin, and an insulation material. The metallic support structure is connected to a metallic surface within the combustion chamber of the engine. The metallic skin is disposed adjacent to the metallic support structure to define a void space between the metallic skin and the metallic surface. The insulation material is contained within the volume to form the composite thermal barrier.