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1. 发明授权

US09586807B2 Maintaining an operational temperature range 有权
标题翻译：维持工作温度范围
公开(公告)号：US09586807B2
公开(公告)日：2017-03-07
申请号：US11863102
申请日：2007-09-27
申请人： Patrick Zuzek , Mark Justin Johnson
发明人： Patrick Zuzek , Mark Justin Johnson
IPC分类号： F23L99/00 , B67D7/84 , B67D7/08 , G06Q50/06 , G06Q20/18 , B67D7/06
CPC分类号： B67D7/84 , B67D7/06
摘要： Maintaining an operational temperature range of a fuel dispenser component may be accomplished by a variety of systems, devices, and techniques. In one aspect, a fuel dispenser temperature maintenance system includes a centrifugal fan and an airflow separator. The centrifugal fan is detachably mounted to a fuel dispenser and adapted to circulate an airflow from an exterior to an interior of the fuel dispenser; separate the airflow into a conditioning airflow and an ejected airflow; and direct the conditioning airflow directly to a fuel dispenser component. The ejected airflow includes a plurality of particulates. The airflow separator includes a separator inlet adapted to receive the ejected airflow. The airflow separator is adapted to guide the ejected airflow from the separator inlet directly to an exterior of the fuel dispenser through an outlet channel, where the outlet channel is disposed between the airflow separator and the exterior of the fuel dispenser.
摘要翻译：保持燃料分配器部件的工作温度范围可以通过各种系统，装置和技术来实现。一方面，燃料分配器温度维持系统包括离心风扇和气流分离器。离心风扇可拆卸地安装到燃料分配器上并且适于使来自外部的气流循环到燃料分配器的内部; 将气流分离成调节气流和排出的气流; 并将调节空气直接引导到燃料分配器部件。喷出的气流包括多个微粒。气流分离器包括适于接收喷射气流的分离器入口。气流分离器适于通过出口通道将排出的气流从分离器入口直接引导到燃料分配器的外部，其中出口通道设置在气流分离器和燃料分配器的外部之间。

2. 发明申请

US20090087806A1 MAINTAINING AN OPERATIONAL TEMPERATURE RANGE 有权
标题翻译：维持操作温度范围
公开(公告)号：US20090087806A1
公开(公告)日：2009-04-02
申请号：US11863102
申请日：2007-09-27
申请人： Patrick Zuzek , Mark Justin Johnson
发明人： Patrick Zuzek , Mark Justin Johnson
IPC分类号： F23L99/00
CPC分类号： B67D7/84 , B67D7/06
摘要： Maintaining an operational temperature range of a fuel dispenser component may be accomplished by a variety of systems, devices, and techniques. In one aspect, a fuel dispenser temperature maintenance system includes a centrifugal fan and an airflow separator. The centrifugal fan is detachably mounted to a fuel dispenser and adapted to circulate an airflow from an exterior to an interior of the fuel dispenser; separate the airflow into a conditioning airflow and an ejected airflow; and direct the conditioning airflow directly to a fuel dispenser component. The ejected airflow includes a plurality of particulates. The airflow separator includes a separator inlet adapted to receive the ejected airflow. The airflow separator is adapted to guide the ejected airflow from the separator inlet directly to an exterior of the fuel dispenser through an outlet channel, where the outlet channel is disposed between the airflow separator and the exterior of the fuel dispenser.
摘要翻译：保持燃料分配器部件的工作温度范围可以通过各种系统，装置和技术来实现。一方面，燃料分配器温度维持系统包括离心风扇和气流分离器。离心风扇可拆卸地安装到燃料分配器上并且适于使来自外部的气流循环到燃料分配器的内部; 将气流分离成调节气流和排出的气流; 并将调节空气直接引导到燃料分配器部件。喷出的气流包括多个微粒。气流分离器包括适于接收喷射气流的分离器入口。气流分离器适于通过出口通道将排出的气流从分离器入口直接引导到燃料分配器的外部，其中出口通道设置在气流分离器和燃料分配器的外部之间。

3. 发明授权

US08668560B2 Shielding electronic components from liquid 失效
标题翻译：屏蔽液体中的电子部件
公开(公告)号：US08668560B2
公开(公告)日：2014-03-11
申请号：US11863054
申请日：2007-09-27
申请人： Patrick Zuzek , Mark Justin Johnson
发明人： Patrick Zuzek , Mark Justin Johnson
IPC分类号： H05K5/00 , H02K7/20 , F24F7/007 , H05K7/20
CPC分类号： B67D7/84
摘要： Shielding liquid from electronic components may be accomplished by a variety of systems, devices, and techniques. A shielding may include a substantially vertical channel mounted to a fuel dispenser component; an airflow inlet; a plurality of arrays of angled protrusions; and a plurality of substantially vertical protrusions. The channel is adapted to guide an airflow. The plurality of arrays of angled protrusions are, disposed within the channel and are substantially parallel in arrangement within each array. The angled protrusions within each array are angularly offset in arrangement relative to the angled protrusions within adjacent arrays. The arrays of angled protrusions are adapted to form a tortuous path for the airflow through the channel. The plurality of substantially vertical protrusions are disposed within the channel and are located between the airflow inlet and the plurality of arrays. The vertical protrusions are adapted to substantially straighten the airflow within the channel.
摘要翻译：来自电子部件的屏蔽液体可以通过各种系统，装置和技术来实现。屏蔽可以包括安装到燃料分配器部件的基本垂直的通道; 气流入口; 多个倾斜突起阵列; 和多个基本垂直的突起。该通道适于引导气流。多个倾斜突起阵列设置在通道内并且在每个阵列内基本上平行布置。每个阵列内的成角度的突起相对于相邻阵列内的成角度的突起成角度地偏移。倾斜突起的阵列适于形成通过通道的气流的曲折路径。多个基本垂直的突起设置在通道内并且位于气流入口和多个阵列之间。垂直突起适于基本上使通道内的气流伸直。

4. 发明申请

US20090088066A1 SHIELDING ELECTRONIC COMPONENTS FROM LIQUID 失效
标题翻译：液体屏蔽电子元件
公开(公告)号：US20090088066A1
公开(公告)日：2009-04-02
申请号：US11863054
申请日：2007-09-27
申请人： Patrick Zuzek , Mark Justin Johnson
发明人： Patrick Zuzek , Mark Justin Johnson
IPC分类号： H05K5/00 , F24F7/06
CPC分类号： B67D7/84
摘要： Shielding liquid from electronic components may be accomplished by a variety of systems, devices, and techniques. A shielding device may include a substantially vertical channel mounted to a fuel dispenser component; an airflow inlet; a plurality of arrays of angled protrusions; and a plurality of substantially vertical protrusions. The channel is adapted to guide an airflow. The plurality of arrays of angled protrusions are, disposed within the channel and are substantially parallel in arrangement within each array. The angled protrusions within each array are angularly offset in arrangement relative to the angled protrusions within adjacent arrays. The arrays of angled protrusions are adapted to form a tortuous path for the airflow through the channel. The plurality of substantially vertical protrusions are disposed within the channel and are located between the airflow inlet and the plurality of arrays. The vertical protrusions are adapted to substantially straighten the airflow within the channel.
摘要翻译：来自电子部件的屏蔽液体可以通过各种系统，装置和技术来实现。屏蔽装置可以包括安装到燃料分配器部件的基本垂直的通道; 气流入口; 多个倾斜突起阵列; 和多个基本垂直的突起。该通道适于引导气流。多个倾斜突起阵列设置在通道内并且在每个阵列内基本上平行布置。每个阵列内的成角度的突起相对于相邻阵列中的成角度的突起成角度地偏移。倾斜突起的阵列适于形成通过通道的气流的曲折路径。多个基本垂直的突起设置在通道内并且位于气流入口和多个阵列之间。垂直突起适于基本上使通道内的气流伸直。

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