-
公开(公告)号：US10920621B2
公开(公告)日：2021-02-16
申请号：US16250287
申请日：2019-01-17
Applicant: United Technologies Corporation
Inventor： Gabrielle Murphy , Robert M. Lewis , Gregory E. Reinhardt
Abstract: A horizontal support tool for an engine build stand, the horizontal support tool includes a support tube along an axis and a tie shaft between a handle and a puck assembly, the puck assembly including a puck selectively extendable and retractable transverse to the axis in response to rotation of the handle. A method of horizontally assembling a portion of a gas turbine engine including mounting a first module to an engine build stand; installing a horizontal support tool into the first module, the horizontal support tool supported in a spherical bearing supported by the engine build stand; and installing a second module to the first module, the horizontal support tool operable to at least partially support second module.
-
公开(公告)号：US20190153900A1
公开(公告)日：2019-05-23
申请号：US16250287
申请日：2019-01-17
Applicant: United Technologies Corporation
Inventor： Gabrielle Murphy , Robert M. Lewis , Gregory E. Reinhardt
Abstract: A horizontal support tool for an engine build stand, the horizontal support tool includes a support tube along an axis and a tie shaft between a handle and a puck assembly, said puck assembly including a puck selectively extendable and retractable transverse to the axis in response to rotation of the handle. A method of horizontally assembling a portion of a gas turbine engine including mounting a first module to an engine build stand; installing a horizontal support tool into the first module, the horizontal support tool supported in a spherical bearing supported by the engine build stand; and installing a second module to the first module, the horizontal support tool operable to at least partially support second module.
-
Patent Agency Ranking
公开(公告)号：US10533498B2
公开(公告)日：2020-01-14
申请号：US15889259
申请日：2018-02-06
Applicant: United Technologies Corporation
Inventor： Gabrielle Murphy , Gregory E. Reinhardt , Robert M. Lewis , Scott L. Peterson
Abstract: An assembly system for assembling a gas turbine engine including a support beam defining a horizontal plane for assembly of engine components along a horizontal axis substantially parallel with the support beam. A forward arm is supported on the support beam for supporting a forward portion of an engine component. An aft arm is supported on the support beam for supporting an aft portion of the engine component. An aft mounting ring is attachable to an aft end of an engine assembly. A forward mounting ring is attachable to a forward end of the engine assembly. A drive is mounted to the aft arm engageable to the aft mounting ring for rotating the engine assembly about the horizontal axis. A roller is supported on the forward arm and engageable to the forward mounting ring to support the first end of the engine assembly during rotation about the horizontal axis. A method is also disclosed.
-
公开(公告)号：US09885286B2
公开(公告)日：2018-02-06
申请号：US14737671
申请日：2015-06-12
Applicant: United Technologies Corporation
Inventor： Gabrielle Murphy , Gregory E. Reinhardt , Robert M. Lewis , Scott L. Peterson
CPC classification number: F02C7/20 , B66C11/04 , B66C11/12 , F01D25/285 , F05D2230/68 , Y10T29/49236
Abstract: An assembly system for assembling a gas turbine engine including a support beam defining a horizontal plane for assembly of engine components along a horizontal axis substantially parallel with the support beam. A forward arm is supported on the support beam for supporting a forward portion of an engine component. An aft arm is supported on the support beam for supporting an aft portion of the engine component. An aft mounting ring is attachable to an aft end of an engine assembly. A forward mounting ring is attachable to a forward end of the engine assembly. A drive is mounted to the aft arm engageable to the aft mounting ring for rotating the engine assembly about the horizontal axis. A roller is supported on the forward arm and engageable to the forward mounting ring to support the first end of the engine assembly during rotation about the horizontal axis. A method is also disclosed.
-
公开(公告)号：US20180156125A1
公开(公告)日：2018-06-07
申请号：US15889259
申请日：2018-02-06
Applicant: United Technologies Corporation
Inventor： Gabrielle Murphy , Gregory E. Reinhardt , Robert M. Lewis , Scott L. Peterson
CPC classification number: F02C7/20 , B66C11/04 , B66C11/12 , F01D25/285 , F05D2230/68 , Y10T29/49236
Abstract: An assembly system for assembling a gas turbine engine including a support beam defining a horizontal plane for assembly of engine components along a horizontal axis substantially parallel with the support beam. A forward arm is supported on the support beam for supporting a forward portion of an engine component. An aft arm is supported on the support beam for supporting an aft portion of the engine component. An aft mounting ring is attachable to an aft end of an engine assembly. A forward mounting ring is attachable to a forward end of the engine assembly. A drive is mounted to the aft arm engageable to the aft mounting ring for rotating the engine assembly about the horizontal axis. A roller is supported on the forward arm and engageable to the forward mounting ring to support the first end of the engine assembly during rotation about the horizontal axis. A method is also disclosed.
-
公开(公告)号：US20170107858A1
公开(公告)日：2017-04-20
申请号：US14883682
申请日：2015-10-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Gabrielle Murphy , Robert M. Lewis , Gregory E. Reinhardt
CPC classification number: F01D25/285 , B25H1/0007 , B64F5/50 , F01D25/162 , F01D25/24 , F02C7/20 , F04D29/522 , F05D2220/32 , F05D2230/60 , F05D2230/68 , F05D2230/70 , F05D2240/60
Abstract: A horizontal support tool for an engine build stand, the horizontal support tool includes a support tube along an axis and a tie shaft between a handle and a puck assembly, said puck assembly including a puck selectively extendable and retractable transverse to the axis in response to rotation of the handle. A method of horizontally assembling a portion of a gas turbine engine including mounting a first module to an engine build stand; installing a horizontal support tool into the first module, the horizontal support tool supported in a spherical bearing supported by the engine build stand; and installing a second module to the first module, the horizontal support tool operable to at least partially support second module.
-
公开(公告)号：US20150361894A1
公开(公告)日：2015-12-17
申请号：US14737671
申请日：2015-06-12
Applicant: United Technologies Corporation
Inventor： Gabrielle Murphy , Gregory E. Reinhardt , Robert M. Lewis , Scott L. Peterson
IPC: F02C7/20
CPC classification number: F02C7/20 , B66C11/04 , B66C11/12 , F01D25/285 , F05D2230/68 , Y10T29/49236
Abstract: An assembly system for assembling a gas turbine engine including a support beam defining a horizontal plane for assembly of engine components along a horizontal axis substantially parallel with the support beam. A forward arm is supported on the support beam for supporting a forward portion of an engine component. An aft arm is supported on the support beam for supporting an aft portion of the engine component. An aft mounting ring is attachable to an aft end of an engine assembly. A forward mounting ring is attachable to a forward end of the engine assembly. A drive is mounted to the aft arm engageable to the aft mounting ring for rotating the engine assembly about the horizontal axis. A roller is supported on the forward arm and engageable to the forward mounting ring to support the first end of the engine assembly during rotation about the horizontal axis. A method is also disclosed.
Abstract translation: 一种用于组装燃气涡轮发动机的组装系统，其包括限定水平面的支撑梁，用于沿着基本上平行于支撑梁的水平轴线组装发动机部件。 前臂支撑在支撑梁上，用于支撑发动机部件的前部。 后臂支撑在支撑梁上，用于支撑发动机部件的后部。 后安装环可附接到发动机组件的后端。 前安装环可附接到发动机组件的前端。 驱动器安装到后臂上，可与后安装环接合，以使发动机组件围绕水平轴线旋转。 辊子被支撑在前臂上并可与前安装环接合，以在围绕水平轴线旋转期间支撑发动机组件的第一端。 还公开了一种方法。
-
-
-
-
-
-
Search Results
7
records
(took 0.012 seconds)
