公开(公告)号：US20180195551A1

公开(公告)日：2018-07-12

申请号：US15401878

申请日：2017-01-09

Applicant: Hamilton Sundstrand Corporation

Inventor： Steven Poteet ,  David J. Grulke

IPC: F16C17/10 ,  F16C33/10 ,  C10M107/44 ,  C10M125/02 ,  C10M125/26 ,  C10M125/22

CPC classification number: F16C17/102 ,  C10M107/44 ,  C10M125/02 ,  C10M125/22 ,  C10M125/26 ,  C10M2201/041 ,  C10M2201/0413 ,  C10M2201/0613 ,  C10M2201/0623 ,  C10M2201/066 ,  C10M2201/087 ,  C10M2217/0443 ,  C10N2220/082 ,  C10N2240/02 ,  C10N2250/08 ,  F16C17/024 ,  F16C32/0633 ,  F16C33/107 ,  F16C33/1095 ,  F16C2240/48

Abstract: A bearing assembly is disclosed that includes a first component with a first bearing surface, and a second component with a second bearing surface. A fluid is disposed between the first bearing surface and the second bearing surface supporting the first bearing surface and the second bearing surface in a non-contact rotational relationship. The first bearing surface, or the second bearing surface, or both the first bearing surface and the second bearing surface include a surface layer with solid lubricant 2D nanoparticles in a matrix.

公开(公告)号：US20220136559A1

公开(公告)日：2022-05-05

申请号：US17572791

申请日：2022-01-11

Applicant: Hamilton Sundstrand Corporation

Inventor： Steven Poteet ,  David J. Grulke

IPC: F16C17/10 ,  F16C17/02 ,  F16C32/06 ,  C10M107/44 ,  C10M125/02 ,  C10M125/26 ,  F16C33/10 ,  C10M125/22 ,  C10N50/08 ,  C10N40/02 ,  C10N20/06

Abstract: A bearing assembly is disclosed that includes a first component with a first bearing surface, and a second component with a second bearing surface. A fluid is disposed between the first bearing surface and the second bearing surface supporting the first bearing surface and the second bearing surface in a non-contact rotational relationship. The first bearing surface, or the second bearing surface, or both the first bearing surface and the second bearing surface include a surface layer with solid lubricant 2D nanoparticles in a matrix.

公开(公告)号：US20180194966A1

公开(公告)日：2018-07-12

申请号：US15403315

申请日：2017-01-11

Applicant: Hamilton Sundstrand Corporation

Inventor： Steven Poteet ,  Marc E. Gage ,  David J. Grulke

IPC: C09D183/00 ,  C08J3/20 ,  B05D1/02 ,  B05D1/18

CPC classification number: C09D183/00 ,  B05D1/02 ,  B05D1/18 ,  C08J3/203 ,  C08J2383/00 ,  C08K3/346 ,  C08K2201/003 ,  C08K2201/011 ,  C09D183/04

Abstract: A high temperature coating includes a silicone resin, a mass of nanoclay particles dispersed in the silicone resin, a surfactant and water.

公开(公告)号：US11221039B2

公开(公告)日：2022-01-11

申请号：US15401878

申请日：2017-01-09

Applicant: Hamilton Sundstrand Corporation

Inventor： Steven Poteet ,  David J. Grulke

IPC: C07F7/02 ,  F16C33/12 ,  F16C33/04 ,  F16C17/10 ,  F16C33/10 ,  C10M107/44 ,  C10M125/02 ,  C10M125/26 ,  C10M125/22 ,  F16C32/06 ,  F16C17/02 ,  C10N20/06 ,  C10N40/02 ,  C10N50/08

Abstract: A bearing assembly is disclosed that includes a first component with a first bearing surface, and a second component with a second bearing surface. A fluid is disposed between the first bearing surface and the second bearing surface supporting the first bearing surface and the second bearing surface in a non-contact rotational relationship. The first bearing surface, or the second bearing surface, or both the first bearing surface and the second bearing surface include a surface layer with solid lubricant 2D nanoparticles in a matrix.

公开(公告)号：US10760609B2

公开(公告)日：2020-09-01

申请号：US15018076

申请日：2016-02-08

Applicant: HAMILTON SUNDSTRAND CORPORATION

Inventor： Marc E. Gage ,  David J. Grulke ,  Michael E. Folsom ,  Blair A. Smith ,  Mark S. Busha ,  Kerry L. Davis

IPC: F16B11/00 ,  F16B19/00 ,  F16B33/00 ,  F16B33/06 ,  F16B43/00 ,  B29C65/48 ,  B29C65/56 ,  B29C65/72 ,  B29C65/00 ,  B32B15/08 ,  B32B37/00 ,  B29C65/02 ,  F16B39/22 ,  B29L31/00

Abstract: A method of making an assembly is disclosed. According to the method, a curable sealant is applied to a metal surface of a first article, and the curable sealant and first article are stored under conditions to maintain the curable sealant in an at least partially uncured state. The method further includes contacting the curable sealant on the first article metal surface with an electrically conductive surface of a second article, and curing the curable sealant.

公开(公告)号：US20170227041A1

公开(公告)日：2017-08-10

申请号：US15018076

申请日：2016-02-08

Applicant: HAMILTON SUNDSTRAND CORPORATION

Inventor： Marc E. Gage ,  David J. Grulke ,  Michael E. Folsom ,  Blair A. Smith ,  Mark S. Busha ,  Kerry L. Davis

IPC: F16B33/00 ,  B29C65/02 ,  F16B43/00 ,  B29C65/48

Abstract: A method of making an assembly is disclosed. According to the method, a curable sealant is applied to a metal surface of a first article, and the curable sealant and first article are stored under conditions to maintain the curable sealant in an at least partially uncured state. The method further includes contacting the curable sealant on the first article metal surface with an electrically conductive surface of a second article, and curing the curable sealant.

公开(公告)号：US20150246721A1

公开(公告)日：2015-09-03

申请号：US14457671

申请日：2014-08-12

Applicant: Hamilton Sundstrand Corporation

Inventor： Blair A. Smith ,  David J. Grulke

IPC: B64C11/00 ,  B64C11/24 ,  B64C11/30 ,  B64C11/04

CPC classification number: B64C11/008 ,  B64C11/04 ,  B64C11/24 ,  B64C11/30

Abstract: An aircraft propeller taper bore insert apparatus is provided. The apparatus includes a tapered outer surface and an inner surface. The outer surface is dimensioned and configured to fit within and be of substantially a same size and shape as an aircraft propeller taper bore or an aircraft propeller balancing tube. The inner surface defines an inner cavity configured to receive a balancing medium and includes a plurality of retention formations arranged thereon and configured to support the balancing medium.

Abstract translation: 提供了一种飞机螺旋桨锥孔插入装置。 该装置包括锥形外表面和内表面。 外表面的尺寸和构造适合于与飞机螺旋桨锥孔或飞行器螺旋桨平衡管相配合并且具有基本相同的尺寸和形状。 内表面限定了被配置为接收平衡介质并且包括布置在其上并被配置为支撑平衡介质的多个保持结构的内腔。