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公开(公告)号：US20180065755A1
公开(公告)日：2018-03-08
申请号：US15258197
申请日：2016-09-07
Applicant: United Technologies Corporation
Inventor： Matthew D. Teicholz , Stewart B. Hatch , Wyatt S. Daentl
IPC: B64D31/06 , F04D27/00 , F04D29/32 , F04D25/04 , F01D5/02 , F01D17/10 , F01D17/14 , F01D17/16 , B64D27/10
CPC classification number: B64D31/06 , B64D27/10 , F01D5/02 , F01D17/105 , F01D17/145 , F01D17/162 , F02C9/18 , F02C9/20 , F04D25/045 , F04D27/001 , F04D29/321 , F05D2220/323 , F05D2260/80 , F05D2270/02 , F05D2270/04 , F05D2270/101 , F05D2270/102 , F05D2270/1024 , F05D2270/301 , F05D2270/303 , F05D2270/304 , F05D2270/309 , F05D2270/54
Abstract: A control system for a gas turbine engine includes a processing system operable to control a speed of the gas turbine engine and a memory system. The memory system is operable to store instructions executable by the processing system to determine at least one performance parameter associated with a stall condition of the gas turbine engine and to incrementally adjust an acceleration rate of the gas turbine engine based on detecting a degraded stall line limit according to the at least one performance parameter.
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公开(公告)号：US20170233103A1
公开(公告)日：2017-08-17
申请号：US15042363
申请日：2016-02-12
Applicant: United Technologies Corporation
Inventor： Matthew D. Teicholz , Jeffrey W. Sutliff , William H. Greene, JR. , Kenneth J. White , Matthew R. Feulner , John P. Virtue, JR. , Jorn A. Glahn , Philip D. Hoover , Victor M. Pinedo , Jason B. Solomonides
CPC classification number: B64F1/34 , B64D27/16 , F02C7/27 , F02C7/277 , F05D2220/323 , F05D2260/85 , F05D2270/303 , F05D2270/71
Abstract: A system for starting a gas turbine engine of an aircraft is provided. The system includes a pneumatic starter motor, a discrete starter valve switchable between an on-state and an off-state, and a controller operable to perform a starting sequence for the gas turbine engine. The starting sequence includes alternating on and off commands to an electromechanical device coupled to the discrete starter valve to achieve a partially open position of the discrete starter valve to control a flow from a starter air supply to the pneumatic starter motor to drive rotation of a starting spool of the gas turbine engine below an engine idle speed.
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公开(公告)号：US20160332743A1
公开(公告)日：2016-11-17
申请号：US15112648
申请日：2014-10-03
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Matthew D. Teicholz , Ethan K. Stearns
CPC classification number: B64D37/34 , B64D27/10 , F02C7/06 , F02C7/14 , F02C7/22 , F02C7/224 , F02C9/28 , F05D2220/323 , F05D2260/213 , F05D2270/20 , F05D2270/313 , Y02T50/675
Abstract: A method of protecting fuel hardware for a gas turbine engine in an aircraft is disclosed. The method may include determining a current altitude of the aircraft, and controlling a temperature of fuel for the gas turbine engine based at least in part on the current altitude. A thermal management system for a gas turbine engine in an aircraft is also disclosed. The thermal management system may include a sensor configured to detect a current altitude of the aircraft, and a controller in operative communication with the sensor. The controller may be configured to manage a fuel temperature for the gas turbine engine based at least in part on the current altitude detected by the sensor.
Abstract translation: 公开了一种保护飞机中的燃气涡轮发动机的燃料硬件的方法。 该方法可以包括确定飞行器的当前高度，以及至少部分地基于当前高度来控制燃气涡轮发动机的燃料的温度。 还公开了一种用于飞机中的燃气涡轮发动机的热管理系统。 热管理系统可以包括被配置为检测飞行器的当前高度的传感器，以及与传感器可操作地通信的控制器。 控制器可以被配置为至少部分地基于由传感器检测到的当前高度来管理燃气涡轮发动机的燃料温度。
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公开(公告)号：US20150003956A1
公开(公告)日：2015-01-01
申请号：US13669510
申请日：2012-11-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Matthew D. Teicholz , Paul H. Spiesman , Kerri A. Wojcik , John R. Gendron , Glenn D. Bartkowski , Sean DJ Blake , William G. Tempelman
CPC classification number: F04D27/0246 , F02C6/08 , F02C9/20 , F04D27/002 , F04D27/009 , F04D27/0215 , F05D2270/10
Abstract: An example variable vane scheduling method includes adjusting variable vanes from a position based on a first schedule to a position based on a different, second schedule in response to a control feature. An example method of controlling flow through a compressor of a turbomachine includes moving variable vanes to positions that allow more flow into the compressor in response to bleed air being communicated away from the compressor.
Abstract translation: 示例性可变叶片调度方法包括响应于控制特征，将来自基于第一调度的位置的可变叶片调整到基于不同的第二调度的位置。 控制通过涡轮机的压缩机的流量的示例性方法包括将可变叶片移动到允许响应于从压缩机远离的排出空气而进入压缩机的位置。
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公开(公告)号：US11142329B2
公开(公告)日：2021-10-12
申请号：US16812862
申请日：2020-03-09
Applicant: United Technologies Corporation
Inventor： Matthew D. Teicholz , James W. Dunn , Christopher P. Kmetz , Louis A. Celiberti
IPC: B64D31/02 , F02C9/42 , F01D19/00 , F01D25/34 , F02C7/275 , F02C7/26 , F01D13/00 , B64D27/12 , F01D21/00 , F02C7/268
Abstract: An aspect includes a system for pre-start motoring control for multiple engines of an aircraft. The system includes a first engine starting system of a first engine and a controller. The controller is operable to control a motoring time of the first engine starting system relative to one or more other engine starting systems of one or more other engines of the aircraft by adjusting the motoring time of the first engine starting system within a tolerance of the motoring time of the one or more other engine starting systems in a pre-start motoring sequence.
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Patent Agency Ranking
公开(公告)号：US20200207482A1
公开(公告)日：2020-07-02
申请号：US16812862
申请日：2020-03-09
Applicant: United Technologies Corporation
Inventor： Matthew D. Teicholz , James W. Dunn , Christopher P. Kmetz , Louis A. Celiberti
IPC: B64D31/02 , F02C7/268 , F01D21/00 , F01D19/00 , B64D27/12 , F01D13/00 , F02C7/26 , F02C7/275 , F01D25/34 , F02C9/42
Abstract: An aspect includes a system for pre-start motoring control for multiple engines of an aircraft. The system includes a first engine starting system of a first engine and a controller. The controller is operable to control a motoring time of the first engine starting system relative to one or more other engine starting systems of one or more other engines of the aircraft by adjusting the motoring time of the first engine starting system within a tolerance of the motoring time of the one or more other engine starting systems in a pre-start motoring sequence.
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公开(公告)号：US10040577B2
公开(公告)日：2018-08-07
申请号：US15042363
申请日：2016-02-12
Applicant: United Technologies Corporation
Inventor： Matthew D. Teicholz , Jeffrey W. Sutliff , William H. Greene, Jr. , Kenneth J. White , Matthew R. Feulner , John P. Virtue, Jr. , Jorn A. Glahn , Philip D. Hoover , Victor M. Pinedo , Jason B. Solomonides
CPC classification number: B64F1/34 , B64D27/16 , F02C7/27 , F02C7/277 , F05D2220/323 , F05D2260/85 , F05D2270/303 , F05D2270/71
Abstract: A system for starting a gas turbine engine of an aircraft is provided. The system includes a pneumatic starter motor, a discrete starter valve switchable between an on-state and an off-state, and a controller operable to perform a starting sequence for the gas turbine engine. The starting sequence includes alternating on and off commands to an electromechanical device coupled to the discrete starter valve to achieve a partially open position of the discrete starter valve to control a flow from a starter air supply to the pneumatic starter motor to drive rotation of a starting spool of the gas turbine engine below an engine idle speed.
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公开(公告)号：US20180156117A1
公开(公告)日：2018-06-07
申请号：US15875279
申请日：2018-01-19
Applicant: United Technologies Corporation
CPC classification number: F02C7/06 , F01D25/20 , F01M1/16 , F01M2013/0472 , F02C3/107 , F02C7/14 , F02C7/36 , F05D2260/53 , F16H57/0435 , F16N2250/08 , Y02T50/671
Abstract: A method of controlling lubrication flow to a first engine component, a second engine component and a lubrication tank of a gas turbine engine according to an example of the present disclosure includes, among other things, determining more than one condition experienced by the gas turbine engine, comparing with a processor on a controller the more than one condition against an engine performance model stored in memory on the controller, wherein the engine performance model includes stored relationship values between the more than one condition and a position of a scheduling valve, the scheduling valve disposed between the lubricant tank and the first engine component and between the lubricant tank and the second engine component, pumping a lubricant from the lubricant tank through a conduit to the scheduling valve using a pump, and controlling the position of the scheduling valve to vary a flow of the lubricant to two or more of the first engine component, the second engine component and the lubrication tank based upon the comparing of the more than one condition experienced by the gas turbine engine.
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公开(公告)号：US20180156116A1
公开(公告)日：2018-06-07
申请号：US15875179
申请日：2018-01-19
Applicant: United Technologies Corporation
CPC classification number: F02C7/06 , F01D25/20 , F01M1/16 , F01M2013/0472 , F02C3/107 , F02C7/14 , F02C7/36 , F05D2260/53 , F16H57/0435 , F16N2250/08 , Y02T50/671
Abstract: A lubrication system for a gas turbine engine according to an example of the present disclosure includes, among other things, a pump that moves a lubricant, a lubricant tank that stores the lubricant, a first engine component and a second engine component each requiring lubrication from the lubricant, a conduit between the lubricant tank and the first engine component and between the lubricant tank and the second engine component, a scheduling valve positioned in the conduit between the lubricant tank, and the first engine component and the second engine component, and a controller including a memory and a processor that controls the scheduling valve, wherein the memory includes an engine performance model, wherein the engine performance model includes stored relationship values between more than one condition experienced by the gas turbine engine during operation and a position of the scheduling valve, and wherein the scheduling valve varies a flow of the lubricant to the first engine component, the second engine component and the lubrication tank based on comparing the more than one condition with the engine performance model.
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公开(公告)号：US20180022463A1
公开(公告)日：2018-01-25
申请号：US15216233
申请日：2016-07-21
Applicant: United Technologies Corporation
Inventor： Matthew D. Teicholz , James W. Dunn , Christopher P. Kmetz , Louis A. Celiberti
CPC classification number: B64D31/02 , B64D27/12 , F01D13/003 , F01D19/00 , F01D21/003 , F01D25/34 , F02C7/26 , F02C7/268 , F02C7/275 , F02C9/42 , F05D2220/323 , F05D2260/85 , F05D2270/14
Abstract: An aspect includes a system for pre-start motoring synchronization for multiple engines of an aircraft. The system includes a first engine starting system of a first engine and a controller. The controller is operable to synchronize a motoring time of the first engine starting system with one or more other engine starting systems of one or more other engines of the aircraft by extending the motoring time of the first engine starting system to match, within a synchronization tolerance, the motoring time of the one or more other engine starting systems in a pre-start motoring sequence.
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