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公开(公告)号：US20200300180A1
公开(公告)日：2020-09-24
申请号：US16803110
申请日：2020-02-27
Applicant: United Technologies Corporation
Inventor： Neal R. Herring
Abstract: A fuel system for a gas turbine engine includes a fuel pump to provide fuel flow during engine operation and a transmission system that includes an output shaft coupled to drive the fuel pump, and an input shaft driven through a mechanical link to a shaft of the gas turbine engine. The output shaft drives the fuel pump at a variable speed that is independent of a rotational speed of the input shaft.
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公开(公告)号：US12276230B2
公开(公告)日：2025-04-15
申请号：US16803110
申请日：2020-02-27
Applicant: United Technologies Corporation
Inventor： Neal R. Herring
Abstract: A fuel system for a gas turbine engine includes a fuel pump to provide fuel flow during engine operation and a transmission system that includes an output shaft coupled to drive the fuel pump, and an input shaft driven through a mechanical link to a shaft of the gas turbine engine. The output shaft drives the fuel pump at a variable speed that is independent of a rotational speed of the input shaft.
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公开(公告)号：US20150204625A1
公开(公告)日：2015-07-23
申请号：US14507904
申请日：2014-10-07
Applicant: United Technologies Corporation
Inventor： Matthew Robert Pearson , Neal R. Herring
CPC classification number: H01L35/30 , F28F13/00 , F28F2013/006
Abstract: A thermal interface includes a first thermal component and a second thermal component. A fluid filled cushion is disposed between the first thermal component and the second thermal component, and is a thermal joint.
Abstract translation: 热界面包括第一热分量和第二热分量。 流体填充缓冲垫设置在第一热部件和第二热部件之间，并且是热接头。
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公开(公告)号：US20140165570A1
公开(公告)日：2014-06-19
申请号：US13718115
申请日：2012-12-18
Applicant: United Technologies Corporation
Inventor： Neal R. Herring
CPC classification number: F02C7/14 , F05D2260/208 , F28D15/0266 , Y02T50/671 , Y02T50/675
Abstract: An oscillating heat pipe of a gas turbine engine includes a plurality of channels that define a continuous loop through which a fluid flows, and an evaporator of a gas turbine engine. The fluid flows through the evaporator to accept heat from a first fluid. The first fluid is located near or in an engine core. The oscillating heat pipe also includes condenser of the gas turbine engine. The fluid flows through the condenser to reject heat to a second fluid, and the second fluid is located outwardly of the engine core.
Abstract translation: 燃气涡轮发动机的振荡热管包括限定流体流过的连续回路的多个通道和燃气涡轮发动机的蒸发器。 流体流过蒸发器以接受来自第一流体的热量。 第一种流体位于发动机核心附近或内部。 振荡热管还包括燃气轮机的冷凝器。 流体流过冷凝器以将热量排除到第二流体，并且第二流体位于发动机芯的外部。
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公开(公告)号：US11293354B2
公开(公告)日：2022-04-05
申请号：US16745454
申请日：2020-01-17
Applicant: United Technologies Corporation
Inventor： Neal R. Herring
Abstract: A gas turbine engine includes a main compressor section, a combustor, and a main turbine section. A fuel pump delivers fuel to the combustor. A tap taps air compressed by the main compressor section, and is connected for delivering the tapped air through a first heat exchanger and to a boost compressor. Air downstream of the boost compressor is connected to cool a component. Driving compressed air is connected to be delivered to a power turbine. The power turbine is connected to drive both the boost compressor and the fuel pump.
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Patent Agency Ranking
公开(公告)号：US20170045258A1
公开(公告)日：2017-02-16
申请号：US15305807
申请日：2014-04-21
Applicant: United Technologies Corporation
Inventor： Subramanyaravi Annapragada , Ulf J. Jonsson , Thomas D. Radcliff , Andrzej Ernest Kuczek , John P. Wesson , Neal R. Herring , Stuart S. Ochs , Yinshan Feng , Mikhail B. Gorbounov , Ram Ranjan
CPC classification number: F24F12/006 , F24F3/147 , F24F11/30 , F24F2003/1458 , F24F2011/0002 , F24F2012/008 , F25B2321/001 , F28D17/04 , F28D21/0014 , Y02B30/563
Abstract: Embodiments are directed to obtaining a specification comprising at least one requirement associated with a heating, ventilation, and air-conditioning (HVAC) system, and based on the specification, configuring a control system to control a movement of fluid back and forth across at least one regenerator device of the HVAC system and a mixing of the fluid with ambient air.
Abstract translation: 实施例旨在获得包括与加热，通风和空调（HVAC）系统相关联的至少一个要求的规范，并且基于该规范，配置控制系统以至少控制流体的来回运动 HVAC系统的一个再生器装置和流体与环境空气的混合。
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7.发明申请ADDITIVE MANUFACTURED DUCTED HEAT EXCHANGER SYSTEM WITH ADDITIVELY MANUFACTURED HEADER 审中-公开具有附加制造长度的添加剂制造的导热换热器系统公开(公告)号：US20160231068A1
公开(公告)日：2016-08-11
申请号：US14615732
申请日：2015-02-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： John T. Schmitz , Neal R. Herring , John H. Whiton , Joseph Turney , Brian St. Rock , Michael K. Ikeda
CPC classification number: F28F9/026 , B23P15/26 , B33Y80/00 , F28D2021/0021 , F28D2021/0026 , F28F9/02 , F28F9/0265 , F28F2255/18
Abstract: A heat exchanger system includes an additively manufactured inlet header upstream of, and in fluid communication with, the heat exchanger core and an additively manufactured exit header downstream of, and in fluid communication with, the heat exchanger core. A method of manufacturing a header for a ducted heat exchanger system for a gas turbine engine includes additively manufacturing a header with respect to a desired airflow therethrough.
Abstract translation: 热交换器系统包括在热交换器芯的上游并与之流体连通的加法制造的入口集管以及与热交换器芯下游并与热交换器芯流体连通的相加制造的出口集管。 一种制造用于燃气涡轮发动机的管道式热交换器系统的集管的方法包括相对于所需的气流相加地制造集管。
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公开(公告)号：US20210180520A1
公开(公告)日：2021-06-17
申请号：US16815802
申请日：2020-03-11
Applicant: United Technologies Corporation
Inventor： Neal R. Herring
Abstract: A fuel system for a gas turbine engine includes a first electric motor, a main fuel pump driven by the first electric motor to provide a fuel flow, and an actuator operable by a second electric motor. A first motor controller governs operation of the first electric motor. A second motor controller governs operation of the second electric motor. The second motor controller is operable to control operation of the first electric motor in response the first motor controller being incapable of governing operation of the first electric motor.
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公开(公告)号：US11441485B2
公开(公告)日：2022-09-13
申请号：US16815802
申请日：2020-03-11
Applicant: United Technologies Corporation
Inventor： Neal R. Herring
Abstract: A fuel system for a gas turbine engine includes a first electric motor, a main fuel pump driven by the first electric motor to provide a fuel flow, and an actuator operable by a second electric motor. A first motor controller governs operation of the first electric motor. A second motor controller governs operation of the second electric motor. The second motor controller is operable to control operation of the first electric motor in response the first motor controller being incapable of governing operation of the first electric motor.
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公开(公告)号：US20200300168A1
公开(公告)日：2020-09-24
申请号：US16803095
申请日：2020-02-27
Applicant: United Technologies Corporation
Inventor： Neal R. Herring , Michael K. Ikeda , Peter Cocks
IPC: F02C7/236
Abstract: A fuel system for a gas turbine engine includes a primary fuel pump providing fuel flow during engine operation and a primary electric motor coupled to the primary fuel pump for driving the primary fuel pump during engine operation. A secondary system provides fuel flow in the absence of fuel flow from the primary fuel pump.
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