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公开(公告)号：US20180363490A1
公开(公告)日：2018-12-20
申请号：US16037708
申请日：2018-07-17
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Gregory Di Vincenzo , Francis P. Marocchini , Bhupindar Singh
CPC classification number: F01D17/02 , F01D17/14 , F01D17/20 , F01D21/003
Abstract: A measuring system for sensing vane positions that comprises a turbine, a target, and a sensor. The turbine includes a plurality of articulating vanes, with each vane being coupled to a sync ring that is configured to position the plurality of articulating vanes in accordance with a degree of rotation by the sync ring. The target is coupled to a first position of the turbine within a first region that is associated with a first vane of the plurality of articulating vanes. The sensor is coupled via a bracket to a second position of the turbine within the first region. The sensor is configured to detect an orientation of the target that corresponds to a vane position of the first vane.
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公开(公告)号：US10145261B2
公开(公告)日：2018-12-04
申请号：US15814089
申请日：2017-11-15
Applicant: Hamilton Sundstrand Corporation
Inventor： Gregory Di Vincenzo , Francis P. Marocchini , Bhupindar Singh
Abstract: A measuring system for sensing vane positions that comprises a turbine, a target, and a sensor. The turbine includes a plurality of articulating vanes, with each vane being coupled to a sync ring that is configured to position the plurality of articulating vanes in accordance with a degree of rotation by the sync ring. The target is coupled to a first position of the turbine within a first region that is associated with a first vane of the plurality of articulating vanes. The sensor is coupled via a bracket to a second position of the turbine within the first region. The sensor is configured to detect an orientation of the target that corresponds to a vane position of the first vane.
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公开(公告)号：US20170241762A1
公开(公告)日：2017-08-24
申请号：US15588125
申请日：2017-05-05
Applicant: Hamilton Sundstrand Corporation
Inventor： Bhupindar Singh , Gary M. McBrien
Abstract: A tip clearance measurement system (TCMS) includes a probe and sensing circuitry. The probe directs microwave signals toward a turbine blade and receives microwave signals reflected by the turbine blade. The sensing circuitry includes a switch having a first state in which a main frequency is provided at an output of the switch and a second state in which a reference frequency is provided at an output of the switch. The sensing circuitry further includes a first conditioning circuit that receives a frequency provided at the output of the switch and provides a conditioned frequency to the probe and a second conditioning circuit that receives both the conditioned frequency provided by the first conditioning circuit and a reflected frequency received by the probe, and provides a conditioned output based on the conditioned frequency and reflected frequency.
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公开(公告)号：US09970315B2
公开(公告)日：2018-05-15
申请号：US14621009
申请日：2015-02-12
Applicant: Hamilton Sundstrand Corporation
Inventor： Gregory DiVincenzo , Bhupindar Singh , Francis P. Marocchini
CPC classification number: F01D17/162 , F01D9/041 , F01D17/02 , F01D21/003 , F04D27/001 , F04D27/002 , F04D29/563 , F05D2250/25
Abstract: A movable vane control system is disclosed for use with a gas turbine engine having a turbine axis of rotation. The system includes a plurality of rotatable turbine vanes in a gas flow path within a turbine case of the gas turbine engine. A first vane position sensor having a first distance sensor is configured to sense the distance between the first distance sensor and a surface portion of a first of said plurality of vanes or a first movable target connected to the first vane. Additionally, the first distance sensor, the first vane surface portion, the first movable target, or a combination thereof is configured to provide a variable distance between the first distance sensor and the first vane surface portion or first movable target that varies as a function of a position of the first vane.
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公开(公告)号：US20160123844A1
公开(公告)日：2016-05-05
申请号：US14529819
申请日：2014-10-31
Applicant: Hamilton Sundstrand Corporation
Inventor： Gregory Di Vincenzo , Francis P. Marocchini , Bhupindar Singh
CPC classification number: F01D17/02 , F01D17/14 , F01D17/20 , F01D21/003
Abstract: A measuring system for sensing vane positions that comprises a turbine, a target, and a sensor. The turbine includes a plurality of articulating vanes, with each vane being coupled to a sync ring that is configured to position the plurality of articulating vanes in accordance with a degree of rotation by the sync ring. The target is coupled to a first position of the turbine within a first region that is associated with a first vane of the plurality of articulating vanes. The sensor is coupled via a bracket to a second position of the turbine within the first region. The sensor is configured to detect an orientation of the target that corresponds to a vane position of the first vane.
Abstract translation: 一种用于感测叶片位置的测量系统，包括涡轮，目标和传感器。 涡轮机包括多个铰接叶片，其中每个叶片耦合到同步环，该同步环被配置成根据同步环的旋转程度来定位多个铰接叶片。 目标在与多个关节式叶片中的第一叶片相关联的第一区域内联接到涡轮机的第一位置。 传感器经由托架连接到第一区域内的涡轮机的第二位置。 传感器被配置为检测对应于第一叶片的叶片位置的目标的方向。
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Patent Agency Ranking
公开(公告)号：US20160010491A1
公开(公告)日：2016-01-14
申请号：US14328252
申请日：2014-07-10
Applicant: Hamilton Sundstrand Corporation
Inventor： Bhupindar Singh , Gregory DiVincenzo
CPC classification number: F01D21/003 , F01D9/02 , F01D17/00 , F01D17/02 , F01D17/10 , F01D17/12 , F01D17/14 , F01D17/16 , F01D17/162 , F01D25/24 , F05D2260/74
Abstract: A turbine is provided and includes an outer duct, a turbine casing formed to define a turbine interior, the turbine casing being disposed within the outer duct to define an annulus, a vane element pivotably coupled to the turbine casing via a spindle to extend spanwise into the turbine interior and a sensor element supportively coupled to the outer duct and configured to sense a characteristic of the spindle within the annulus from which a pivot angle of the vane element is derivable.
Abstract translation: 涡轮机被设置并且包括外部管道，形成为限定涡轮机内部的涡轮机壳体，涡轮机壳体设置在外部管道内以限定环形空间;叶片元件，经由主轴可枢转地联接到涡轮机壳体，以将翼展方向延伸到 所述涡轮机内部和传感器元件支撑地联接到所述外部管道并且被配置为感测所述主轴在所述环形空间内的特征，所述叶片元件的枢转角度从所述环形空间可导出。
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公开(公告)号：US09732624B2
公开(公告)日：2017-08-15
申请号：US14328252
申请日：2014-07-10
Applicant: Hamilton Sundstrand Corporation
Inventor： Bhupindar Singh , Gregory DiVincenzo
IPC: F01D17/02 , F01D21/00 , F01D9/02 , F01D25/24 , F01D17/10 , F01D17/00 , F01D17/12 , F01D17/16 , F01D17/14
CPC classification number: F01D21/003 , F01D9/02 , F01D17/00 , F01D17/02 , F01D17/10 , F01D17/12 , F01D17/14 , F01D17/16 , F01D17/162 , F01D25/24 , F05D2260/74
Abstract: A turbine is provided and includes an outer duct, a turbine casing formed to define a turbine interior, the turbine casing being disposed within the outer duct to define an annulus, a vane element pivotably coupled to the turbine casing via a spindle to extend spanwise into the turbine interior and a sensor element supportively coupled to the outer duct and configured to sense a characteristic of the spindle within the annulus from which a pivot angle of the vane element is derivable.
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公开(公告)号：US09677868B2
公开(公告)日：2017-06-13
申请号：US14185061
申请日：2014-02-20
Applicant: Hamilton Sundstrand Corporation
Inventor： Bhupindar Singh , Gary M. McBrien
Abstract: A tip clearance measurement system (TCMS) includes a probe and sensing circuitry. The probe directs microwave signals toward a turbine blade and receives microwave signals reflected by the turbine blade. The sensing circuitry includes a switch having a first state in which a main frequency is provided at an output of the switch and a second state in which a reference frequency is provided at an output of the switch. The sensing circuitry further includes a first conditioning circuit that receives a frequency provided at the output of the switch and provides a conditioned frequency to the probe and a second conditioning circuit that receives both the conditioned frequency provided by the first conditioning circuit and a reflected frequency received by the probe, and provides a conditioned output based on the conditioned frequency and reflected frequency.
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公开(公告)号：US20160356172A1
公开(公告)日：2016-12-08
申请号：US14621009
申请日：2015-02-12
Applicant: Hamilton Sundstrand Corporation
Inventor： Gregory DiVincenzo , Bhupindar Singh , Francis P. Marocchini
CPC classification number: F01D17/162 , F01D9/041 , F01D17/02 , F01D21/003 , F04D27/001 , F04D27/002 , F04D29/563 , F05D2250/25
Abstract: A movable vane control system is disclosed for use with a gas turbine engine having a turbine axis of rotation. The system includes a plurality of rotatable turbine vanes in a gas flow path within a turbine case of the gas turbine engine. A first vane position sensor having a first distance sensor is configured to sense the distance between the first distance sensor and a surface portion of a first of said plurality of vanes or a first movable target connected to the first vane. Additionally, the first distance sensor, the first vane surface portion, the first movable target, or a combination thereof is configured to provide a variable distance between the first distance sensor and the first vane surface portion or first movable target that varies as a function of a position of the first vane.
Abstract translation: 公开了一种与具有涡轮机旋转轴线的燃气涡轮发动机一起使用的可动叶片控制系统。 该系统包括在燃气涡轮发动机的涡轮壳体内的气体流动路径中的多个可旋转涡轮机叶片。 具有第一距离传感器的第一叶片位置传感器被配置为感测第一距离传感器与所述多个叶片中的第一叶片的表面部分之间的距离或连接到第一叶片的第一可移动目标。 另外，第一距离传感器，第一叶片表面部分，第一可移动目标物体或其组合构造成在第一距离传感器和第一叶片表面部分或第一可移动目标之间提供可变距离 第一个叶片的位置。
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公开(公告)号：US10294812B2
公开(公告)日：2019-05-21
申请号：US16037708
申请日：2018-07-17
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Gregory Di Vincenzo , Francis P. Marocchini , Bhupindar Singh
Abstract: A measuring system for sensing vane positions that comprises a turbine, a target, and a sensor. The turbine includes a plurality of articulating vanes, with each vane being coupled to a sync ring that is configured to position the plurality of articulating vanes in accordance with a degree of rotation by the sync ring. The target is coupled to a first position of the turbine within a first region that is associated with a first vane of the plurality of articulating vanes. The sensor is coupled via a bracket to a second position of the turbine within the first region. The sensor is configured to detect an orientation of the target that corresponds to a vane position of the first vane.
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