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1. 发明申请

US20200281095A1 SYSTEMS AND METHODS FOR USING ADDITIVE MANUFACTURING FOR THERMAL MANAGEMENT 审中-公开
公开(公告)号：US20200281095A1
公开(公告)日：2020-09-03
申请号：US16845381
申请日：2020-04-10
申请人： General Electric Company
发明人： Brian Magann Rush , William Dwight Gerstler , Stefano Angelo Mario Lassini , Todd Garrett Wetzel
IPC分类号： H05K7/20 , F28D15/02 , G06F1/20 , F28D15/04
摘要： According to one embodiment, a thermal management system for electronic devices, including a heat frame, a conformal slot portion, chassis frame, and heat fins wherein the heat frame, conformal slot, chassis frame, and heat fins are integrally formed as a unitary structure by additive manufacturing. In another example, there is a modular vapor assembly for electronic components having a vapor chamber comprising a component surface and a top surface with a vapor channel formed therebetween with at least one liquid receptacle and having a wick structure on at least some of an interior of the component surface. In operation, there is a circuit card with at least some of the electronic components coupled to the vapor chamber component surface and the wick structures transfer at least some of the liquid from the receptacle towards the electronic components, wherein the liquid turns to a vapor that moves towards the receptacle.

2. 发明授权

US09592523B2 Low frequency synthetic jet actuator and method of manufacturing thereof 有权
标题翻译：低频合成射流致动器及其制造方法
公开(公告)号：US09592523B2
公开(公告)日：2017-03-14
申请号：US14490755
申请日：2014-09-19
申请人： General Electric Company
发明人： Todd Garrett Wetzel , Thomas Elliot Stecher , Charles Erklin Seeley , Charles Franklin Wolfe, Jr. , Yogen Vishwas Utturkar , Bryan Patrick Whalen
IPC分类号： B05B3/04 , H05K7/20 , B05B17/06 , F15D1/00 , F15D1/02 , F15D1/08
CPC分类号： B05B17/0607 , F15D1/00 , F15D1/025 , F15D1/08 , Y10T29/49401
摘要： A system and method for lowering the structural natural frequency of a synthetic jet actuator is disclosed. A synthetic jet actuator is provided that includes a first plate, a second plate spaced apart from the first plate and arranged parallelly thereto, and a spacer element configured to space the first plate apart from the second plate and define a chamber along with the first and second plates. The spacer element includes at least one orifice formed therein such that the chamber is in fluid communication with an environment external to the chamber, and the spacer element is constructed to deform in a bending motion in response to a deflection of at least one of the first and second plates.
摘要翻译：公开了一种用于降低合成射流致动器的结构固有频率的系统和方法。提供合成射流致动器，其包括第一板，与第一板间隔开并平行布置的第二板，以及间隔元件，其构造成将第一板与第二板隔开并且与第一板和第一板一起限定腔室第二盘。间隔元件包括形成在其中的至少一个孔，使得腔室与腔室外部的环境流体连通，并且间隔元件构造成响应于第一和第二腔中的至少一个的偏转而在弯曲运动中变形和第二盘。

3. 发明申请

US20150289413A1 SYSTEMS AND METHODS FOR USING ADDITIVE MANUFACTURING FOR THERMAL MANAGEMENT 审中-公开
标题翻译：用于热管理的添加剂制造的系统和方法
公开(公告)号：US20150289413A1
公开(公告)日：2015-10-08
申请号：US14592387
申请日：2015-01-08
申请人： GENERAL ELECTRIC COMPANY
发明人： Brian Magann Rush , William Dwight Gerstler , Stefano Angelo Mario Lassini , Todd Garrett Wetzel
IPC分类号： H05K7/20
摘要： According to one embodiment, a thermal management system for electronic devices, including a heat frame, a conformal slot portion, chassis frame, and heat fins wherein the heat frame, conformal slot, chassis frame, and heat fins are integrally formed as a unitary structure by additive manufacturing. In another example, there is a modular vapor assembly for electronic components having a vapor chamber comprising a component surface and a top surface with a vapor channel formed therebetween with at least one liquid receptacle and having a wick structure on at least some of an interior of the component surface. In operation, there is a circuit card with at least some of the electronic components coupled to the vapor chamber component surface and the wick structures transfer at least some of the liquid from the receptacle towards the electronic components, wherein the liquid turns to a vapor that moves towards the receptacle.
摘要翻译：根据一个实施例，一种用于电子设备的热管理系统，包括加热框架，保形槽部分，底架框架和散热片，其中加热框架，保形槽，底架框架和散热片整体形成为一体结构通过添加剂制造。在另一示例中，存在用于电子部件的模块化蒸汽组件，其具有包括部件表面的蒸气室和具有形成在其间的蒸气通道的顶表面，其具有至少一个液体容器，并且在至少一个液体容器的至少一部分的内部具有芯结构组件表面。在操作中，存在电路卡，其中至少一些电子部件耦合到蒸气室部件表面，并且芯结构将至少一些液体从容器转移到电子部件，其中液体转变为蒸汽，朝向插座移动。

4. 发明授权

US10830060B2 Engine component with flow enhancer 有权
公开(公告)号：US10830060B2
公开(公告)日：2020-11-10
申请号：US15368076
申请日：2016-12-02
申请人： General Electric Company
发明人： Emily Rosette Clark , Julienne LaChance , William Robb Stewart , Todd Garrett Wetzel
IPC分类号： F01D5/18 , F23R3/00 , F01D9/04
摘要： An apparatus for cooling an engine component such as a turbine engine airfoil, including a wall bounding an interior extending axially between a leading edge and a trailing edge and radially between a root and a tip. A cooling circuit it located within the interior of the airfoil can include a flow enhancer permitting a volume of fluid, such as air, to pass around the flow enhancer.

5. 发明授权

US10660236B2 Systems and methods for using additive manufacturing for thermal management 有权
公开(公告)号：US10660236B2
公开(公告)日：2020-05-19
申请号：US14592387
申请日：2015-01-08
申请人： GENERAL ELECTRIC COMPANY
发明人： Brian Magann Rush , William Dwight Gerstler , Stefano Angelo Mario Lassini , Todd Garrett Wetzel
IPC分类号： H05K7/20 , F28D15/02 , G06F1/20 , F28D15/04 , B33Y80/00
摘要： According to one embodiment, a thermal management system for electronic devices, including a heat frame, a conformal slot portion, chassis frame, and heat fins wherein the heat frame, conformal slot, chassis frame, and heat fins are integrally formed as a unitary structure by additive manufacturing. In another example, there is a modular vapor assembly for electronic components having a vapor chamber comprising a component surface and a top surface with a vapor channel formed therebetween with at least one liquid receptacle and having a wick structure on at least some of an interior of the component surface. In operation, there is a circuit card with at least some of the electronic components coupled to the vapor chamber component surface and the wick structures transfer at least some of the liquid from the receptacle towards the electronic components, wherein the liquid turns to a vapor that moves towards the receptacle.

6. 发明申请

US20150001311A1 LOW FREQUENCY SYNTHETIC JET ACTUATOR AND METHOD OF MANUFACTURING THEREOF 有权
标题翻译：低频合成喷嘴致动器及其制造方法
公开(公告)号：US20150001311A1
公开(公告)日：2015-01-01
申请号：US14490755
申请日：2014-09-19
申请人： General Electric Company
发明人： Todd Garrett Wetzel , Thomas Elliot Stecher , Charles Erklin Seeley , Charles Franklin Wolfe, JR. , Yogen Vishwas Utturkar , Bryan Patrick Whalen
IPC分类号： B05B17/06 , F15D1/02 , F15D1/08
CPC分类号： B05B17/0607 , F15D1/00 , F15D1/025 , F15D1/08 , Y10T29/49401
摘要： A system and method for lowering the structural natural frequency of a synthetic jet actuator is disclosed. A synthetic jet actuator is provided that includes a first plate, a second plate spaced apart from the first plate and arranged parallelly thereto, and a spacer element configured to space the first plate apart from the second plate and define a chamber along with the first and second plates. The spacer element includes at least one orifice formed therein such that the chamber is in fluid communication with an environment external to the chamber, and the spacer element is constructed to deform in a bending motion in response to a deflection of at least one of the first and second plates.
摘要翻译：公开了一种用于降低合成射流致动器的结构固有频率的系统和方法。提供合成射流致动器，其包括第一板，与第一板间隔开并平行布置的第二板，以及间隔元件，其构造成将第一板与第二板隔开并且与第一板和第一板一起限定腔室第二盘。间隔元件包括形成在其中的至少一个孔，使得腔室与腔室外部的环境流体连通，并且间隔元件构造成响应于第一和第二腔中的至少一个的偏转而在弯曲运动中变形和第二盘。

7. 发明申请

US20180195896A1 SYSTEM AND METHOD FOR DISPOSABLE INFRARED IMAGING SYSTEM 审中-公开
公开(公告)号：US20180195896A1
公开(公告)日：2018-07-12
申请号：US15401927
申请日：2017-01-09
申请人： General Electric Company
发明人： Guanghua Wang , Naveenan Thiagarajan , Todd Garrett Wetzel , Jason Edward Dees , Bernard Patrick Bewlay
IPC分类号： G01J1/02 , G01N21/35 , F02C7/12
CPC分类号： G01J1/0252 , F02C7/12 , F05D2260/207 , F05D2270/112 , F05D2270/804 , G01J5/0088 , G01J5/042 , G01J5/046 , G01J5/049 , G01J5/061 , G01J2005/0077
摘要： An infrared imaging device includes a plurality of electronic components, a phase change material, and a heat transfer structure. The plurality of electronic components is configured to collect data and have a predetermined temperature parameter. The plurality of electronic components is disposed within the phase change material. The phase change material has a first material phase and a second material phase. The phase change material has a first material phase and a second material phase. The phase change material is configured to absorb heat through changing from the first material phase to the second material phase. The heat transfer structure is disposed within the phase change material. The heat transfer structure is configured to conduct heat within the phase change material. The phase change material and the heat transfer structure are further configured to regulate a temperature of the electronic components below the predetermined temperature parameter.

8. 发明申请

US20180156044A1 ENGINE COMPONENT WITH FLOW ENHANCER 审中-公开
公开(公告)号：US20180156044A1
公开(公告)日：2018-06-07
申请号：US15368076
申请日：2016-12-02
申请人： General Electric Company
发明人： Emily Clark Clark , Julienne LaChance , William Robb Stewart , Todd Garrett Wetzel
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , F01D5/187 , F01D9/04 , F05D2220/32 , F05D2240/126 , F05D2250/12 , F05D2260/22141 , F23R3/002 , F23R3/005 , F23R2900/03045 , Y02T50/676
摘要： An apparatus for cooling an engine component such as a turbine engine airfoil, including a wall bounding an interior extending axially between a leading edge and a trailing edge and radially between a root and a tip. A cooling circuit it located within the interior of the airfoil can include a flow enhancer permitting a volume of fluid, such as air, to pass around the flow enhancer.

9. 发明申请

US20170314464A1 MICRO THERMAL IMAGING SYSTEM FOR TURBINE ENGINES 审中-公开
公开(公告)号：US20170314464A1
公开(公告)日：2017-11-02
申请号：US15142539
申请日：2016-04-29
申请人： General Electric Company
发明人： Guanghua Wang , Todd Garrett Wetzel , Jason Edward Dees
IPC分类号： F02C6/00 , F01D17/02
摘要： A turbine engine includes a compressor section, a combustor section fluidly coupled to the compressor section, a turbine section fluidly coupled to the combustor section, and a drive shaft coupled to the turbine section and the compressor section. The turbine engine also includes a plurality of internal components coupled to one of the compressor section, the combustor section, the turbine section, and the drive shaft. The turbine engine also includes at least one micro infrared sensor coupled to at least one of the plurality of internal components. The micro infrared sensor is configured to detect a surface temperature of the plurality of internal components.

10. 发明申请

US20150049786A1 METHOD AND SYSTEM FOR GAS TEMPERATURE MEASUREMENT 有权
标题翻译：气温测量方法与系统
公开(公告)号：US20150049786A1
公开(公告)日：2015-02-19
申请号：US13969186
申请日：2013-08-16
申请人： General Electric Company
发明人： Guanghua Wang , Nirm Velumylum Nirmalan , Ronald Scott Bunker , Todd Garrett Wetzel , Robert Michael Zacharias , Shawn David Wehe , Robert David Briggs
IPC分类号： G01K13/02 , G01J5/10 , G01M15/14
CPC分类号： G01J5/10 , G01J5/0014 , G01J5/0887 , G01J5/60 , G01M15/14
摘要： A temperature measurement system includes a plurality of filaments. The plurality of filaments are configured to emit thermal radiation in a relatively broad and substantially continuous wavelength band at least partially representative of a temperature of the plurality of filaments. A first and second portion of the filaments has a differing first and a second diameter and/or emissivity, respectively. The system also includes a detector array configured to generate electrical signals at least partially representative of the thermal radiation received from the filaments. The system further includes a controller communicatively coupled to the detector array configured to transform the first electrical signals to a first temperature indication at least partially as a function of the first diameter and/or first emissivity and transform the second electrical signals to a second temperature indication at least partially as a function of the second diameter and/or emissivity.
摘要翻译：温度测量系统包括多个细丝。多根细丝构造成发射至少部分代表多个细丝的温度的相对宽且基本上连续的波长带中的热辐射。长丝的第一和第二部分分别具有不同的第一和第二直径和/或发射率。该系统还包括检测器阵列，该检测器阵列被配置为产生至少部分代表从灯丝接收的热辐射的电信号。所述系统还包括通信地耦合到所述检测器阵列的控制器，所述检测器阵列被配置为至少部分地将所述第一电信号转换为第一温度指示作为所述第一直径和/或第一发射率的函数，并将所述第二电信号转换为第二温度指示至少部分地作为第二直径和/或发射率的函数。

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