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公开(公告)号：US20170058692A1
公开(公告)日：2017-03-02
申请号：US14630228
申请日：2015-02-24
Applicant: United Technologies Corporation
Inventor： Nicholas W. Kantany , Edward Boucher , Kristine Marie Carnavos , Adam Covino , Melaine Ho , Jorge I. Farah , Donald W. Peters
CPC classification number: F01D17/145 , F01D17/141 , F01D17/143 , F01D17/167 , F01D25/005 , F04D27/0215 , F05D2220/32 , F05D2270/3061 , F16K39/045
Abstract: An air modulating system for a gas turbine engine includes a fixed plate with a fluid passage inlet, a floating plate with a first side adjacent to the fluid passage inlet, an actuated mount configured to move the floating plate relative to the fixed plate, and a linkage element for connecting the floating plate to the actuated mount. The linkage element includes a mounting flange configured to slidably engage the floating plate.
Abstract translation: 用于燃气涡轮发动机的空气调节系统包括具有流体通道入口的固定板，具有与流体通道入口相邻的第一侧的浮动板，构造成使浮动板相对于固定板移动的致动安装板，以及 连接元件，用于将浮动板连接到致动的安装座。 联动元件包括安装凸缘，该安装凸缘被构造成可滑动地接合浮动板。
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Patent Agency Ranking
公开(公告)号：US09835043B2
公开(公告)日：2017-12-05
申请号：US14630228
申请日：2015-02-24
Applicant: United Technologies Corporation
Inventor： Nicholas W. Kantany , Edward Boucher , Kristine Marie Carnavos , Adam Covino , Melaine Ho , Jorge I. Farah , Donald W. Peters
CPC classification number: F01D17/145 , F01D17/141 , F01D17/143 , F01D17/167 , F01D25/005 , F04D27/0215 , F05D2220/32 , F05D2270/3061 , F16K39/045
Abstract: An air modulating system for a gas turbine engine includes a fixed plate with a fluid passage inlet, a floating plate with a first side adjacent to the fluid passage inlet, an actuated mount configured to move the floating plate relative to the fixed plate, and a linkage element for connecting the floating plate to the actuated mount. The linkage element includes a mounting flange configured to slidably engage the floating plate.
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公开(公告)号：US10352248B2
公开(公告)日：2019-07-16
申请号：US14812926
申请日：2015-07-29
Applicant: United Technologies Corporation
Inventor： Nicholas W. Kantany , Edward Boucher , Kristine Marie Carnavos , Robert Russell Mayer , Donald W. Peters
Abstract: A system for modulating air flow in a gas turbine engine is provided. The system may include a seal wall comprising an opening, a seal door configured to slideably engage the seal wall, and an actuator configured to move the seal door over the opening. In various embodiments, the system may include a surface forward of the seal door. The seal door may be configured to seal a passage through the surface and the opening of the seal wall. A track may be disposed under the seal door. The track may comprise cobalt. Rollers may be coupled to the seal door with the rollers on the track. The seal door may comprise a nickel-chromium alloy. A sync ring may be coupled to the seal door. The actuator may be coupled through the sync ring to the seal door.
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公开(公告)号：US11492977B2
公开(公告)日：2022-11-08
申请号：US16431955
申请日：2019-06-05
Applicant: United Technologies Corporation
Inventor： Nicholas W. Kantany , Edward Boucher , Kristine Marie Carnavos , Robert Russell Mayer , Donald W. Peters
Abstract: A system for modulating air flow in a gas turbine engine is provided. The system may include a seal wall comprising an opening, a seal door configured to slideably engage the seal wall, and an actuator configured to move the seal door over the opening. In various embodiments, the system may include a surface forward of the seal door. The seal door may be configured to seal a passage through the surface and the opening of the seal wall. A track may be disposed under the seal door. The track may comprise cobalt. Rollers may be coupled to the seal door with the rollers on the track. The seal door may comprise a nickel-chromium alloy. A sync ring may be coupled to the seal door. The actuator may be coupled through the sync ring to the seal door.
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公开(公告)号：US20190323435A1
公开(公告)日：2019-10-24
申请号：US16431955
申请日：2019-06-05
Applicant: United Technologies Corporation
Inventor： Nicholas W. Kantany , Edward Boucher , Kristine Marie Carnavos , Robert Russell Mayer , Donald W. Peters
Abstract: A system for modulating air flow in a gas turbine engine is provided. The system may include a seal wall comprising an opening, a seal door configured to slideably engage the seal wall, and an actuator configured to move the seal door over the opening. In various embodiments, the system may include a surface forward of the seal door. The seal door may be configured to seal a passage through the surface and the opening of the seal wall. A track may be disposed under the seal door. The track may comprise cobalt. Rollers may be coupled to the seal door with the rollers on the track. The seal door may comprise a nickel-chromium alloy. A sync ring may be coupled to the seal door. The actuator may be coupled through the sync ring to the seal door.
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公开(公告)号：US20160097327A1
公开(公告)日：2016-04-07
申请号：US14812926
申请日：2015-07-29
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Nicholas W. Kantany , Edward Boucher , Kristine Marie Carnavos , Robert Russell Mayer , Donald W. Peters
Abstract: A system for modulating air flow in a gas turbine engine is provided. The system may include a seal wall comprising an opening, a seal door configured to slideably engage the seal wall, and an actuator configured to move the seal door over the opening. In various embodiments, the system may include a surface forward of the seal door. The seal door may be configured to seal a passage through the surface and the opening of the seal wall. A track may be disposed under the seal door. The track may comprise cobalt. Rollers may be coupled to the seal door with the rollers on the track. The seal door may comprise a nickel-chromium alloy. A sync ring may be coupled to the seal door. The actuator may be coupled through the sync ring to the seal door.
Abstract translation: 提供一种用于调节燃气涡轮发动机中的气流的系统。 系统可以包括密封壁，密封壁包括开口，被配置为可滑动地接合密封壁的密封门以及构造成将密封门移动到开口上方的致动器。 在各种实施例中，系统可以包括密封门前面的表面。 密封门可以被构造成密封通过密封壁的表面和开口的通道。 轨道可以设置在密封门下方。 轨道可以包括钴。 辊子可以与轨道上的辊连接到密封门。 密封门可以包括镍 - 铬合金。 同步环可以联接到密封门。 致动器可以通过同步环耦合到密封门。
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