-
公开(公告)号：US20210025527A1
公开(公告)日：2021-01-28
申请号：US16521122
申请日：2019-07-24
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Todd A. Davis , Brad E. Flore
Abstract: A compliant jumper tube fitting assembly may comprise an outer housing comprising a first annular cylindrical structure including a first opening defined by a base wall, and an inner housing comprising a second annular cylindrical structure including a second opening defined by an annular wall, wherein the inner housing is configured to generate a seal between an inner diameter wall of the outer housing and an outer diameter wall of the inner housing in response to inserting the inner housing into a mouth end of the outer housing, wherein the inner housing is configured to receive an end fitting and generate a seal between an inner diameter wall of the inner housing in response to inserting the end fitting into the inner housing.
-
公开(公告)号：US20200291818A1
公开(公告)日：2020-09-17
申请号：US16353331
申请日：2019-03-14
Applicant: United Technologies Corporation
Inventor： Todd A. Davis , Gianna E. Sabino
Abstract: A rotating structure provides a first annular array of first radial scoops and a second annular array of second radial scoops arranged axially with respect to the first annular array of first radial scoops. A first component is arranged in an axially forward direction relative to the first annular array of first radial scoops. A second component is arranged in an axially aft direction relative to the second annular array of second radial scoops. A lubrication system includes at least one nozzle aimed at the first and second annular arrays of first and second radial scoops. A first lubrication delivery path fluidly connects the first annular array of first radial scoops to the first component along the axially forward direction. A second lubrication delivery path fluidly connects the second annular array of second radial scoops to the second component along the axially aft direction.
-
公开(公告)号：US10767867B2
公开(公告)日：2020-09-08
申请号：US15927285
申请日：2018-03-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Todd A. Davis , Christopher M. Valva , Daniel Rosen , Armando Amador , Aneil S. Hegde , Ramin M. Rafatpanah
Abstract: A bearing support may include a central shaft, a flange shaft, and a tube boss. The central shaft may include a central longitudinal axis extending between a first end and a second end of the bearing support. The flange shaft may extend radially outward of the central shaft at an acute angle, relative to the central longitudinal axis from the first end to the second end, and the flange shaft may include a rim defining an aperture. The tube boss extends from the central shaft radially outward through the aperture, according to various embodiments. An annular channel may be between the rim and the tube boss.
-
公开(公告)号：US20200248585A1
公开(公告)日：2020-08-06
申请号：US16269071
申请日：2019-02-06
Applicant: United Technologies Corporation
Inventor： Armando Amador , Todd A. Davis , Jorn Axel Glahn
Abstract: A seal seat includes an annular body and an extension. The annular body is disposed about a centerline axis. The extension is connected to and extends radially outward from the annular body. The extension includes first, second, and third portions. The first portion is connected to the annular body and is defined by axially opposed upstream and downstream wall faces. The first portion includes a fin connected to the upstream wall face. The second portion is connected to the first portion and extends substantially parallel to the annular body. The third portion is connected to the second portion and extends substantially parallel to the second portion.
-
公开(公告)号：US10156158B2
公开(公告)日：2018-12-18
申请号：US15137690
申请日：2016-04-25
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Todd A. Davis
Abstract: An oil supply assembly for a bearing damper of a gas turbine engine includes an oil supply tube configured to supply oil in a first direction. The assembly also includes a bearing support having a bearing damper path connecting the bearing damper to the oil supply tube and a bearing compartment path connecting a bearing compartment to the oil supply tube. The assembly also includes a check valve disposed within the bearing damper path and configured to allow fluid communication in the first direction from the oil supply tube to the bearing damper and block fluid communication in a second direction opposite the first direction.
-
Patent Agency Ranking
公开(公告)号：US20160273389A1
公开(公告)日：2016-09-22
申请号：US15032233
申请日：2014-05-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Todd A. Davis , Mark Ronski , David Allen Stachowiak
CPC classification number: F01D25/28 , F01D25/18 , F02C7/06 , F02C7/32 , F05D2220/32 , F05D2230/60 , F05D2250/41 , F05D2250/411 , F05D2250/42 , F05D2250/43 , F05D2260/30 , F16M13/02
Abstract: An oil tank mounting system for use on a structure of a turbine engine, includes three mounts with each mount configured to constrain the oil tank with a different number of degrees of freedom of movement. A first mount may have fix the oil tank in one degree of freedom, a second mount may fix the oil tank in two degrees of freedom, and a third mount may fix the oil tank in three degrees of freedom. This allows limited rotational and expansion movement while coupling the oil tank to the engine. The mount attachments may be embodied in rubber, with pins, or with spherical joints in a variety of configurations. Frangible pins may be used to absorb energy but still retain the oil tank in the event of a high energy event.
Abstract translation: 用于涡轮发动机结构的油箱安装系统包括三个安装件，每个安装件构造成用不同数量的运动自由度约束油箱。 第一安装件可以以一个自由度固定油箱，第二安装件可以将油箱固定在两个自由度上，而第三安装件可以将油箱固定在三个自由度上。 这允许在将油箱连接到发动机的同时进行有限的旋转和膨胀运动。 安装附件可以以各种构造的橡胶，带销或球形接头来实现。 可以使用易碎的销来吸收能量，但是在发生高能量事件时仍然保留油箱。
-
公开(公告)号：US08911204B2
公开(公告)日：2014-12-16
申请号：US13732647
申请日：2013-01-02
Applicant: United Technologies Corporation
Inventor： Todd A. Davis , Brian P. Cigal
CPC classification number: F02C3/113 , F01D25/16 , F01D25/285 , F02C3/107 , F05D2230/70 , F05D2230/72 , F05D2230/80 , Y10T29/49318 , Y10T29/49721 , Y10T29/49815
Abstract: A method for servicing a gas turbine engine includes disassembling a bearing compartment, providing access from a forward side of the gas turbine engine to a gearbox contained within said bearing compartment. The gas turbine engine provides a core flow path that extends from the forward side aftward in a core flow direction. The method includes servicing a component located within the bearing compartment. A method for servicing a gas turbine engine includes providing access from a forward side of a front center body assembly, and servicing a component located within a bearing compartment aft of the front center body assembly. The gas turbine engine includes a seal package located aft of a bearing package. A front wall is mounted to the front center body support and is removable from a front center body support to access at least one of the gearbox, the bearing package and the seal package.
Abstract translation: 用于维修燃气涡轮发动机的方法包括拆卸轴承室，提供从燃气涡轮发动机的前侧到包含在所述轴承室内的齿轮箱的通路。 燃气涡轮发动机提供从芯线流动方向向前延伸的芯流动路径。 该方法包括维护位于轴承室内的部件。 用于维修燃气涡轮发动机的方法包括从前中心主体组件的前侧提供通路，以及维修位于前中心主体组件后部的轴承室内的部件。 燃气涡轮发动机包括位于轴承组件后面的密封组件。 前壁安装到前中心主体支撑件，并且可从前中心主体支撑件移除以进入齿轮箱，轴承封装件和密封包装件中的至少一个。
-
公开(公告)号：US20140140818A1
公开(公告)日：2014-05-22
申请号：US13732647
申请日：2013-01-02
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Todd A. Davis , Brian P. Cigal
CPC classification number: F02C3/113 , F01D25/16 , F01D25/285 , F02C3/107 , F05D2230/70 , F05D2230/72 , F05D2230/80 , Y10T29/49318 , Y10T29/49721 , Y10T29/49815
Abstract: A method for servicing a gas turbine engine includes disassembling a bearing compartment, providing access from a forward side of the gas turbine engine to a gearbox contained within said bearing compartment. The gas turbine engine provides a core flow path that extends from the forward side aftward in a core flow direction. The method includes servicing a component located within the bearing compartment. A method for servicing a gas turbine engine includes providing access from a forward side of a front center body assembly, and servicing a component located within a bearing compartment aft of the front center body assembly. The gas turbine engine includes a seal package located aft of a bearing package. A front wall is mounted to the front center body support and is removable from a front center body support to access at least one of the gearbox, the bearing package and the seal package.
Abstract translation: 用于维修燃气涡轮发动机的方法包括拆卸轴承室，提供从燃气涡轮发动机的前侧到包含在所述轴承室内的齿轮箱的通路。 燃气涡轮发动机提供从芯线流动方向向前延伸的芯流动路径。 该方法包括维护位于轴承室内的部件。 用于维修燃气涡轮发动机的方法包括从前中心主体组件的前侧提供通路，以及维护位于前中心主体组件后部的轴承室内的部件。 燃气涡轮发动机包括位于轴承组件后面的密封组件。 前壁安装到前中心主体支撑件，并且可从前中心主体支撑件移除以进入齿轮箱，轴承封装件和密封包装件中的至少一个。
-
公开(公告)号：US11306656B2
公开(公告)日：2022-04-19
申请号：US16662148
申请日：2019-10-24
Applicant: United Technologies Corporation
Inventor： Todd A. Davis , Reade W. James , Peter T. Schutte , Juan Jimenez
Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a passageway configured to permit fluid to drain back into a bearing compartment. The passageway has an inlet outside the bearing compartment and an outlet inside the bearing compartment. The outlet is spaced-apart from a central rotational axis of a towershaft gear.
-
公开(公告)号：US11286990B2
公开(公告)日：2022-03-29
申请号：US16373879
申请日：2019-04-03
Applicant: United Technologies Corporation
Inventor： Todd A. Davis , Dale C. Humphries
IPC: F16C33/76
Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a bearing compartment, a seal runner, a seal configured to cooperate with the seal runner to seal the bearing compartment, and a catcher in contact with the seal runner to minimize deflection of the seal runner. A method is also disclosed.
-
-
-
-
-
-
-
-
-
Search Results
71
records
(took 0.024 seconds)
