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公开(公告)号：US20160208647A1
公开(公告)日：2016-07-21
申请号：US14598492
申请日：2015-01-16
Applicant: United Technologies Corporation
Inventor： Anthony P. Cherolis , John H. Mosley , Kalpendu J. Parekh , Christopher Treat , Alberto A. Mateo
CPC classification number: F01D25/14 , F01D9/065 , F01D25/12 , F01D25/162 , F01D25/24 , F02C7/12 , F05D2220/32 , F05D2260/20 , Y02T50/676
Abstract: A mid-turbine frame for a gas turbine engine includes an inner frame case that includes a fluid passage. A swirler tube is in fluid communication with the fluid passage and is configured to direct cooling airflow in a radial inward and downstream direction.
Abstract translation: 用于燃气涡轮发动机的中涡轮机框架包括内框架，其包括流体通道。 旋流管与流体通道流体连通，并且构造成在径向向内和向下流动的方向引导冷却气流。
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公开(公告)号：US20160061048A1
公开(公告)日：2016-03-03
申请号：US14779841
申请日：2014-03-24
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Christopher Corcoran , Anthony P. Cherolis
CPC classification number: F01D11/008 , F01D5/02 , F01D5/147 , F01D11/006 , F01D15/12 , F05D2220/30 , F05D2240/30 , F05D2240/55 , F05D2250/71 , F05D2250/75 , F05D2260/97
Abstract: A turbine engine assembly arranged relative to an axis includes a rotor blade and a feather seal with an L-shaped geometry. The rotor blade includes an airfoil and a base. The airfoil extends axially between an upstream leading edge and a downstream trailing edge, and radially out from the base. The base includes a neck and a pocket. The neck extends axially to a downstream surface. The pocket extends laterally into the neck. The feather seal extends laterally into the pocket, and includes a down stream leg that extends substantially along the downstream surface.
Abstract translation: 相对于轴线布置的涡轮发动机组件包括转子叶片和具有L形几何形状的羽毛密封件。 转子叶片包括翼型件和底座。 翼型件在上游前缘和下游后缘之间轴向延伸，并从底座径向延伸。 底座包括一个颈部和一个口袋。 颈部轴向延伸到下游表面。 口袋横向延伸到颈部。 羽毛密封件横向延伸到袋中，并且包括基本上沿着下游表面延伸的下游腿。
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公开(公告)号：US09915170B2
公开(公告)日：2018-03-13
申请号：US14663567
申请日：2015-03-20
Applicant: United Technologies Corporation
Inventor： Joshua Daniel Winn , Alexander Broulidakis , Anthony P. Cherolis
CPC classification number: F01D25/125 , F01D9/065 , F01D25/162 , F02C7/12 , F05D2220/3213 , F05D2230/64 , F05D2260/20 , F05D2260/31 , F05D2260/941 , Y02T50/676
Abstract: A spoke for a mid-turbine frame on a gas turbine engine includes a cylindrical portion. A flange is attached to the cylindrical portion. At least one gusset extends between the cylindrical portion and the flange. At least one gusset extends to a perimeter of the flange.
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公开(公告)号：US09879604B2
公开(公告)日：2018-01-30
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.
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公开(公告)号：US09822667B2
公开(公告)日：2017-11-21
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
IPC: F01D25/00 , F01D25/24 , F16B43/00 , F01D9/06 , F01D25/16 , F16B39/10 , F01D9/02 , F01D9/00 , F16B39/24
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.
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Patent Agency Ranking
公开(公告)号：US20160273384A1
公开(公告)日：2016-09-22
申请号：US14663567
申请日：2015-03-20
Applicant: United Technologies Corporation
Inventor： Joshua Daniel Winn , Alexander Broulidakis , Anthony P. Cherolis
CPC classification number: F01D25/125 , F01D9/065 , F01D25/162 , F02C7/12 , F05D2220/3213 , F05D2230/64 , F05D2260/20 , F05D2260/31 , F05D2260/941 , Y02T50/676
Abstract: A spoke for a mid-turbine frame on a gas turbine engine includes a cylindrical portion. A flange is attached to the cylindrical portion. At least one gusset extends between the cylindrical portion and the flange. At least one gusset extends to a perimeter of the flange.
Abstract translation: 用于燃气涡轮发动机上的中涡轮机架的辐条包括圆柱形部分。 法兰连接到圆柱形部分。 至少一个角撑板在圆柱形部分和凸缘之间延伸。 至少一个角撑板延伸到凸缘的周边。
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公开(公告)号：US20160265360A1
公开(公告)日：2016-09-15
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.
Abstract translation: 公开了一种旋流管。 提供了一种旋流器，其包括限定第一表面的凸缘，远离第一表面延伸的管，由凸缘内表面和管内表面限定的流动表面，凸缘内表面具有入口直径和设置的计量特征 在流动表面上，其中计量特征与管成一体，计量特征具有小于入口直径的计量特征直径。
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公开(公告)号：US20160258322A1
公开(公告)日：2016-09-08
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.
Abstract translation: 根据本公开的示例的用于燃气涡轮发动机的中涡轮机框架包括第一框架壳体，联接到第一框架壳体的凸缘和邻近凸缘的相邻轮辐之间的隔热板 。 还公开了一种冷却燃气涡轮发动机的一部分的方法。
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公开(公告)号：US20160230602A1
公开(公告)日：2016-08-11
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
CPC classification number: F01D25/28 , F01D9/065 , F01D25/162 , F01D25/26 , F02C7/12 , F05D2220/32 , F05D2220/3213 , F05D2230/20 , F05D2230/64 , F05D2260/20 , F05D2260/30 , F05D2260/31 , Y02T50/671 , Y02T50/676
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.
Abstract translation: 用于中涡轮机架的拉杆组件包括用于将外框壳体连接到内框架壳体的至少一个拉杆。 至少一个拉杆包括分支到第一分支和第二分支中的入口通道。 插头位于第一分支中以阻止流过第一分支的一部分。
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公开(公告)号：US20160208701A1
公开(公告)日：2016-07-21
申请号：US14598732
申请日：2015-01-16
Applicant: United Technologies Corporation
Inventor： Anthony P. Cherolis , Jeffrey J. Lienau , Robert Newman , Cheng-Zhang Wang
IPC: F02C7/18
CPC classification number: F02C7/18 , F01D9/065 , F05D2220/3213 , F05D2240/90 , Y02T50/675
Abstract: A gas turbine engine includes a mid-turbine frame that includes an inner frame case. At least one spoke is connected to the inner frame case. At least one spoke includes a fluid passage that is in fluid communication with a channel on a radially inner end of the fluid passage. The channel is directed in a radially inward and circumferential direction. A cavity is located radially inward from the mid-turbine frame and is in fluid communication with the channel.
Abstract translation: 燃气涡轮发动机包括中间涡轮机框架，其包括内框架壳体。 至少一个辐条与内框架连接。 至少一个辐条包括与流体通道的径向内端上的通道流体连通的流体通道。 通道被引导在径向向内和圆周方向。 空腔从中涡轮机框架径向向内定位并与通道流体连通。
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