-
公开(公告)号：US20200149432A1
公开(公告)日：2020-05-14
申请号：US16734965
申请日：2020-01-06
Applicant: United Technologies Corporation
Inventor： Thomas E. Clark , Brian C. McLaughlin
Abstract: A retention device includes a retention block including an opening extending through the retention block in a first direction. A tab also extends from the retention block in the first direction. A fastener extends through the opening and includes a head configured to engage the retention block. A clinch nut is coupled to the fastener with an interface surface of the clinch nut configured to engage the tab of the retention block.
-
公开(公告)号：US10415416B2
公开(公告)日：2019-09-17
申请号：US15260701
申请日：2016-09-09
Applicant: United Technologies Corporation
Inventor： Thomas E. Clark , Brian C. McLaughlin
Abstract: A fluid flow assembly may include an orifice plate having a set of orifices and a plenum defined by a blade outer air seal. The set of orifices may be aligned with and in fluid communication with the plenum. A gas turbine engine may include a vane outer support having an orifice plate, wherein the orifice plate includes a plurality of sets of orifices. The gas turbine engine may also include a blade outer air seal defining a plurality of plenums. Each set of orifices of the plurality of sets of orifices may be forward relative to and substantially axially aligned with a respective plenum of the plurality of plenums.
-
公开(公告)号：US20180017260A1
公开(公告)日：2018-01-18
申请号：US15210090
申请日：2016-07-14
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Thomas E. Clark , Harvey C. Lee , Brian C. McLaughlin , Jonathan Lemoine
CPC classification number: F23R3/60 , F01D25/243 , F02C7/20 , F05B2230/606 , F05D2220/32 , F05D2240/35 , F23R3/002 , F23R2900/00005
Abstract: A combustor assembly for a gas turbine engine comprises a vane support ring; an annular combustor extending around a central axis and being located radially inwards of the vane support ring, the annular combustor including an aft end, a forward end with at least one opening through which at least one fuel nozzle is received, and an annular outer shell and an annular inner shell that define an annular combustion chamber there between, the annular outer shell including a radially-outwardly extending flange including at least one scallop cut; and a stop member integrally formed with the vane support ring.
-
公开(公告)号：US20170350265A1
公开(公告)日：2017-12-07
申请号：US15170451
申请日：2016-06-01
Applicant: United Technologies Corporation
Inventor： Brian C. McLaughlin , Thomas E. Clark
CPC classification number: F01D11/005 , F01D25/12 , F01D25/246 , F02C7/18 , F02C7/28 , F05D2220/32 , F05D2240/55 , F05D2260/202 , Y02T50/676
Abstract: A seal ring includes a disk having a radially outer end and an orifice at a center forming a radially inner end, a plurality of holes extending through the disk, and a rail having an annular shape extending axially away from the disk at a position that is between the radially outer end and the plurality of holes extending through the disk with the rail being configured to direct the flow of fluid.
-
公开(公告)号：US20170306779A1
公开(公告)日：2017-10-26
申请号：US15137395
申请日：2016-04-25
Applicant: United Technologies Corporation
Inventor： Brian C. McLaughlin , Thomas E. Clark , Peter J. Milligan , Dairus Deylan McDowell , Jaimie Schweitzer , Jeremy Drake , Richard K. Hayford
Abstract: Aspects of the disclosure are directed to a seal comprising: a first leg that emanates from a center point of the seal and is configured to contact a first component, a second leg that emanates from the center point and is configured to contact a second component that is operative at a temperature that is within a range of 648 degrees Celsius to 1093 degrees Celsius, and a third leg that emanates from the center point.
-
Patent Agency Ranking
公开(公告)号：US11619136B2
公开(公告)日：2023-04-04
申请号：US16434630
申请日：2019-06-07
Applicant: United Technologies Corporation
Inventor： Brian C. McLaughlin , Paul M. Lutjen , Richard K. Hayford , Anthony B. Swift
Abstract: A blade outer air seal segment including a radially outward surface, a radially inward surface oriented away from the radially outward surface, and a cooling channel located between the radially outward surface and the radially inward surface. The blade outer air seal segment also including a stress-relief boss extending into the cooling channel and an inlet orifice fluidly coupled to the cooling channel through the stress-relief boss. The blade outer air seal segment further including a stress-relief recess. The stress-relief boss being located within the stress relief recess.
-
公开(公告)号：US11591917B2
公开(公告)日：2023-02-28
申请号：US16434630
申请日：2019-06-07
Applicant: United Technologies Corporation
Inventor： Brian C. McLaughlin , Paul M. Lutjen , Richard K. Hayford , Anthony B. Swift
Abstract: A blade outer air seal segment including a radially outward surface, a radially inward surface oriented away from the radially outward surface, and a cooling channel located between the radially outward surface and the radially inward surface. The blade outer air seal segment also including a stress-relief boss extending into the cooling channel and an inlet orifice fluidly coupled to the cooling channel through the stress-relief boss. The blade outer air seal segment further including a stress-relief recess. The stress-relief boss being located within the stress relief recess.
-
公开(公告)号：US10393024B2
公开(公告)日：2019-08-27
申请号：US15250304
申请日：2016-08-29
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Michael S. Stevens , Brian C. McLaughlin
Abstract: A multi-air stream cooling system is provided. The multi-air stream cooling system may comprise an inner vane support, a flow guide, and a fastened inner duct. The inner vane support may partially define a first airflow path. The flow guide may couple to the inner vane support and may partially define a second airflow path. The fastened inner duct may couple to the flow guide and may partially define a third airflow path. The inner vane support may comprise a discharge slot to allow a first airflow into a blade rim cavity. The flow guide may comprise a tangential onboard injector (TOBI) to provide a second airflow through a cover plate. The flow guide may also comprise a bypass passage configured to enable a third airflow from the third airflow path.
-
公开(公告)号：US20180058329A1
公开(公告)日：2018-03-01
申请号：US15250304
申请日：2016-08-29
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Michael S. Stevens , Brian C. McLaughlin
CPC classification number: F02C7/18 , F01D5/082 , F04D29/54 , Y02T50/676
Abstract: A multi-air stream cooling system is provided. The multi-air stream cooling system may comprise an inner vane support, a flow guide, and a fastened inner duct. The inner vane support may partially define a first airflow path. The flow guide may couple to the inner vane support and may partially define a second airflow path. The fastened inner duct may couple to the flow guide and may partially define a third airflow path. The inner vane support may comprise a discharge slot to allow a first airflow into a blade rim cavity. The flow guide may comprise a tangential onboard injector (TOBI) to provide a second airflow through a cover plate. The flow guide may also comprise a bypass passage configured to enable a third airflow from the third airflow path.
-
公开(公告)号：US20170335720A1
公开(公告)日：2017-11-23
申请号：US15161716
申请日：2016-05-23
Applicant: United Technologies Corporation
Inventor： Thomas E. Clark , Brian C. McLaughlin
CPC classification number: F01D25/28 , F01D5/02 , F01D9/023 , F01D25/243 , F02C3/04 , F02C3/14 , F05D2220/32 , F05D2260/30 , F05D2260/31 , F23R3/60
Abstract: A retention device includes a retention block including an opening extending through the retention block in a first direction. A tab also extends from the retention block in the first direction. A fastener extends through the opening and includes a head configured to engage the retention block. A clinch nut is coupled to the fastener with an interface surface of the clinch nut configured to engage the tab of the retention block.
-
-
-
-
-
-
-
-
-
Search Results
20
records
(took 0.016 seconds)
