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公开(公告)号：US10087785B2
公开(公告)日：2018-10-02
申请号：US14617323
申请日：2015-02-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Alexander Broulidakis , Anthony P. Cherolis , Jonathan Lemoine , Kalpendu J. Parekh , Steven W. Trinks , Christopher Treat , Kevin Zacchera , Alberto A. Mateo
Abstract: A tie rod assembly for a mid-turbine frame includes at least one tie rod for connecting an outer frame case to an inner frame case. At least one tie rod includes an inlet passage that branches into a first branch and a second branch. A plug is located in the first branch to block flow through a portion of the first branch.
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公开(公告)号：US09896939B2
公开(公告)日：2018-02-20
申请号：US14656230
申请日：2015-03-12
Applicant: United Technologies Corporation
Inventor： Alberto A. Mateo , Anthony P. Cherolis
CPC classification number: F01D5/08 , F01D5/081 , F01D5/082 , F01D5/085 , F01D5/087 , F01D5/088 , F01D9/02 , F01D25/08 , F01D25/12 , F01D25/162 , F02C7/18 , F05D2220/32 , F05D2260/14 , F05D2260/202 , F05D2260/209 , F05D2260/2212 , F05D2270/3062 , Y02T50/676
Abstract: A swirler tube is disclosed. A swirler is provided comprising a flange defining a first surface, a tube extending away from the first surface, a flow surface defined by a flange inner surface and a tube inner surface, the flange inner surface having an inlet diameter, and a metering feature disposed on the flow surface, wherein the metering feature is integral to the tube, the metering feature have a metering feature diameter that is less than the inlet diameter.
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公开(公告)号：US20160290167A1
公开(公告)日：2016-10-06
申请号：US14679305
申请日：2015-04-06
Applicant: United Technologies Corporation
Inventor： Steven D. Porter , Anthony P. Cherolis , Alberto A. Mateo , Joshua Daniel Winn , Seth A. Max
CPC classification number: F01D25/243 , F01D9/00 , F01D9/02 , F01D9/065 , F01D25/00 , F01D25/162 , F01D25/246 , F16B39/101 , F16B39/108 , F16B39/24 , F16B43/00
Abstract: A washer includes a hub and a first lobe connected to the hub. The first lobe includes a first hole. A second lobe is also connected to the hub and includes a second hole. A third lobe is also connected to the hub and includes a third hole. The first lobe extends from the hub at least partially in a first direction opposite the second lobe and the third lobe.
Abstract translation: 垫圈包括毂和连接到轮毂的第一瓣。 第一个瓣包括第一个孔。 第二凸角还连接到毂并且包括第二孔。 第三凸耳也连接到轮毂并且包括第三孔。 所述第一凸耳至少部分地从所述轮毂延伸到与所述第二凸角和所述第三凸角相对的第一方向。
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公开(公告)号：US20160265439A1
公开(公告)日：2016-09-15
申请号：US14644541
申请日：2015-03-11
Applicant: United Technologies Corporation
Inventor： Joshua Daniel Winn , Anthony P. Cherolis
CPC classification number: F02C7/18 , F01D9/065 , F01D25/125 , F01D25/162 , F02C7/06 , Y02T50/675
Abstract: A mid-turbine frame for a gas turbine engine includes an inner frame case. A bearing support member is located adjacent the inner frame case. At least one spoke is attached to the inner frame case. At least one spoke includes a cooling airflow passage that extends through the inner frame case and the bearing support member.
Abstract translation: 用于燃气涡轮发动机的中涡轮机框架包括内框架壳体。 轴承支撑构件邻近内框架壳体定位。 至少一个辐条连接到内框架。 至少一个辐条包括延伸穿过内框架壳体和轴承支撑构件的冷却气流通道。
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公开(公告)号：US20160208646A1
公开(公告)日：2016-07-21
申请号：US14598474
申请日：2015-01-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Joshua Daniel Winn , Anthony P. Cherolis
CPC classification number: F01D25/14 , F01D9/065 , F01D25/12 , F01D25/162 , F01D25/24 , F05D2220/32
Abstract: A mid-turbine frame for a gas turbine engine includes an outer frame case and an inner frame case. At least one spoke connects the outer frame case to the inner frame case. The spoke includes a cooling airflow passage that extends in a radial direction and an axial direction.
Abstract translation: 用于燃气涡轮发动机的中涡轮机架包括外框壳体和内框架壳体。 至少一个辐条将外框架连接到内框架。 辐条包括沿径向和轴向延伸的冷却气流通道。
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Patent Agency Ranking
公开(公告)号：US20160208644A1
公开(公告)日：2016-07-21
申请号：US14598452
申请日：2015-01-16
Applicant: United Technologies Corporation
Inventor： Andrew D. Burdick , Anthony P. Cherolis , Christopher Treat , Jonathan Lemoine , Robert Russell Mayer , Jorge I. Farah , John H. Mosley
CPC classification number: F01D25/12 , F01D5/02 , F01D5/081 , F01D9/065 , F01D25/125 , F01D25/162 , F01D25/26 , F02C7/12 , F05D2220/32 , F05D2260/2212 , Y02T50/673 , Y02T50/676
Abstract: A mid-turbine frame for a gas turbine engine includes an outer frame case and an inner frame case. At least one spoke connects the outer frame case to the inner frame case. The spoke includes an inlet passage with at least one branch that extends in an axial direction.
Abstract translation: 用于燃气涡轮发动机的中涡轮机架包括外框壳体和内框架壳体。 至少一个辐条将外框架连接到内框架。 辐条包括具有沿轴向方向延伸的至少一个分支的入口通道。
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公开(公告)号：US10822980B2
公开(公告)日：2020-11-03
申请号：US14783054
申请日：2014-04-11
Applicant: United Technologies Corporation
Inventor： Anton G. Banks , Anthony P. Cherolis , Donald Kastel
Abstract: A nozzle segment for a gas turbine engine includes an arcuate outer vane platform segment. An arcuate inner vane platform segment spaced from the arcuate outer vane platform segment. A multiple of airfoils between the arcuate inner vane platform segment and the arcuate outer vane platform segment, the arcuate outer vane platform segment includes a scallop slot and a seal that seals the scallop slot.
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公开(公告)号：US10107141B2
公开(公告)日：2018-10-23
申请号：US14685437
申请日：2015-04-13
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Seth A. Max , Anthony P. Cherolis
Abstract: The present disclosure relates to gas turbine engine and seal configurations, and components for a gas turbine engine. In one embodiment, a seal for a gas turbine engine includes a first circumferential seal, a second circumferential seal and a seal support structure configured to retain at least a portion of each of the first and second seals. The seal support structure is mounted between a turbine assembly and bearing compartment, and wherein the first and second seals provide barriers to a cavity between the turbine assembly and bearing compartment.
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公开(公告)号：US09869204B2
公开(公告)日：2018-01-16
申请号：US14640323
申请日：2015-03-06
Applicant: United Technologies Corporation
Inventor： Joshua Daniel Winn , Anthony P. Cherolis , Steven D. Porter , Christopher Treat , Kevin Zacchera
CPC classification number: F01D25/145 , F01D9/065 , F01D25/12 , F01D25/162 , F01D25/24 , F01D25/243 , F01D25/28 , F05D2260/20 , Y02T50/672 , Y02T50/676
Abstract: A mid-turbine frame for a gas turbine engine according to an example of the present disclosure includes, among other things, a first frame case, a flange coupled to the first frame case, and a heat shield adjacent to the flange and between adjacent spokes. A method of cooling a portion of a gas turbine engine is also disclosed.
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公开(公告)号：US09828881B2
公开(公告)日：2017-11-28
申请号：US14662347
申请日：2015-03-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Seth A. Max , Anthony P. Cherolis , Steven D. Porter , Joshua D. Winn , Gregory E. Reinhardt , Jeffrey J. Lienau
CPC classification number: F01D25/28 , F01D11/003 , F01D11/006 , F01D25/24 , F01D25/243 , F05D2220/32 , F05D2230/00 , F05D2230/60 , F05D2240/55 , F05D2240/60 , F05D2260/97
Abstract: A seal support structure for a turbomachine includes a mounting portion shaped to mount to a stationary structure of a turbomachine and a cylindrical leg portion disposed on the mounting portion extending axially from the mounting portion. The cylindrical leg portion can include a radially extending flange. The flange can extend at an angle of 90 degrees from the end of the cylindrical leg portion. The flange can extend at least partially in an axial direction. The cylindrical leg portion can be formed integrally with the mounting portion. In embodiments, the cylindrical leg portion is not integral with the mounting portion, i.e., the cylindrical leg portion is a separate piece joined to the mounting portion.
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