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1. 发明申请

US20060124114A1 Bypass for exhaust gas cooler 有权
标题翻译：旁路排气冷却器
公开(公告)号：US20060124114A1
公开(公告)日：2006-06-15
申请号：US11011844
申请日：2004-12-14
申请人： Jon Sayers , Stephane Reymondet , Angus Lemon , Willi Smith
发明人： Jon Sayers , Stephane Reymondet , Angus Lemon , Willi Smith
IPC分类号： F02M25/07 , F28F27/02
CPC分类号： F28D9/005 , F02M26/26 , F28F27/02 , F28F2250/06
摘要： An exhaust gas recirculation cooler, typically of the drawn cup design, with a bypass and control valve is disclosed. The control valve can direct a proportion of the exhaust gas to the cooler and a proportion to bypass the cooler depending on the input temperature of the exhaust gas and the required temperature of the exhaust gas. The proportion of the exhaust gas directed to the cooler/bypassing the cooler can be varied as required and so the temperature of the exhaust gas can be controlled. One benefit of certain embodiments of the invention is that engine damaging chemicals, such as sulphuric acid, which result from over-cooling the exhaust gas are reduced.
摘要翻译：公开了一种排气再循环冷却器，典型地具有抽吸杯设计，具有旁路和控制阀。控制阀可以根据废气的输入温度和所需的废气温度将一部分废气引导到冷却器，并且一定比例的旁路冷却器。引导到冷却器/旁路冷却器的废气的比例可以根据需要而改变，因此可以控制废气的温度。本发明的某些实施方案的一个好处是减少了由过度冷却废气引起的发动机损坏的化学物质，例如硫酸。

2. 发明授权

US07198037B2 Bypass for exhaust gas cooler 有权
标题翻译：旁路排气冷却器
公开(公告)号：US07198037B2
公开(公告)日：2007-04-03
申请号：US11011844
申请日：2004-12-14
申请人： Jon A Sayers , Stephane Reymondet , Angus Lemon , Willi J Smith
发明人： Jon A Sayers , Stephane Reymondet , Angus Lemon , Willi J Smith
IPC分类号： F02M25/07 , F02B47/08 , F16K11/09 , F28R27/02 , F28F1/10
CPC分类号： F28D9/005 , F02M26/26 , F28F27/02 , F28F2250/06
摘要： An exhaust gas recirculation cooler, typically of the drawn cup design, with a bypass and control valve is disclosed. The control valve can direct a proportion of the exhaust gas to the cooler and a proportion to bypass the cooler depending on the input temperature of the exhaust gas and the required temperature of the exhaust gas. The proportion of the exhaust gas directed to the cooler/bypassing the cooler can be varied as required and so the temperature of the exhaust gas can be controlled. One benefit of certain embodiments of the invention is that engine damaging chemicals, such as sulphuric acid, which result from over-cooling the exhaust gas are reduced.
摘要翻译：公开了一种排气再循环冷却器，典型地具有抽吸杯设计，具有旁路和控制阀。控制阀可以根据废气的输入温度和所需的废气温度将一部分废气引导到冷却器，并且一定比例的旁路冷却器。引导到冷却器/旁路冷却器的废气的比例可以根据需要变化，因此可以控制排气的温度。本发明的某些实施方案的一个好处是减少了由过度冷却废气引起的发动机损坏的化学物质，例如硫酸。

3. 发明授权

US07001155B2 Compressor impeller with stress riser 有权
标题翻译：压缩机叶轮与应力提升
公开(公告)号：US07001155B2
公开(公告)日：2006-02-21
申请号：US10439075
申请日：2003-05-14
申请人： Jose Cabrales , Gerald Duane LaRue , John M. Wilson , Angus Lemon
发明人： Jose Cabrales , Gerald Duane LaRue , John M. Wilson , Angus Lemon
IPC分类号： F04B35/00
CPC分类号： F01D21/045 , F01D5/025 , F01D5/048 , F04D25/04 , F04D29/266 , F05D2250/281 , F05D2260/941
摘要： A compressor impeller for use with a boreless turbocharger is provided in accordance with this invention. The compressor impeller comprises an integral hub projecting axially therefrom that includes a partial bore therein that extends from an open to a close bore end. The bore includes a threaded portion that is configured to accommodate threaded engagement with an end of a common shaft disposed through a turbocharger housing and attached at an opposite end to a turbine wheel. The hub is specially configured so that the threaded portion has a relatively increased wall thickness when compared to a remaining portion of the bore disposed between the threaded portion and the end of the bore. The bore is configured providing a section having a reduced wall thickness, between the threaded portion and the bore closed end, for purposes of providing a preferential stress relief mechanism. Configured in this manner, the compressor impeller operates to ensure that, in the event of a stress-related compressor impeller failure, the shaft will be contained in its proper placement within the turbocharger.
摘要翻译：根据本发明提供了一种与无孔涡轮增压器一起使用的压缩机叶轮。压缩机叶轮包括从其轴向突出的整体式轮毂，其包括其中从一开放到一孔径端延伸的部分孔。所述孔包括螺纹部分，所述螺纹部分被配置为容纳与通过涡轮增压器壳体设置的公共轴的端部的螺纹接合，并且在相对端附接到涡轮机叶轮。轮毂是特别构造的，使得与设置在螺纹部分和孔的端部之间的孔的剩余部分相比，螺纹部分具有相对增加的壁厚。为了提供优先的应力消除机构，孔被配置成在螺纹部分和孔封闭端之间提供具有减小的壁厚的部分。以这种方式配置，压缩机叶轮操作以确保在压力相关的压缩机叶轮故障的情况下，轴将被包含在其在涡轮增压器内的适当位置。

4. 发明授权

US06932563B2 Apparatus, system and method for minimizing resonant forces in a compressor 有权
标题翻译：用于最小化压缩机中的共振力的装置，系统和方法
公开(公告)号：US06932563B2
公开(公告)日：2005-08-23
申请号：US10430467
申请日：2003-05-05
申请人： Jose Cabrales , Gerald Duane LaRue , Ronren Gu , Angus Lemon , John M. Wilson
发明人： Jose Cabrales , Gerald Duane LaRue , Ronren Gu , Angus Lemon , John M. Wilson
IPC分类号： F04D29/42 , F01D25/24
CPC分类号： F04D29/4213 , Y10S415/914
摘要： A buffer chamber and outlet guide provide an air path from an intake passage in a compressor housing to an upstream position relative to an intake port of the compressor. Surging is minimized during low airflow conditions while cyclic forces on the blades of the impeller are minimized during high airflow conditions. By providing an air path through the buffer chamber and outlet guide, ribs or other supporting structures are eliminated within the air pathway through the intake port and intake passage within the compressor housing.
摘要翻译：缓冲室和出口引导件提供从压缩机壳体中的进气通道到相对于压缩机的进气口的上游位置的空气通路。在低气流条件下，浪涌最小化，而在高气流条件下，叶轮叶片上的循环力最小化。通过提供通过缓冲室和出口引导件的空气路径，在通过压缩机壳体内的进气口和进气通道的空气通路内消除肋或其它支撑结构。

5. 发明授权

US08602733B2 Structural and acoustical vibration dampener for a rotatable blade 有权
公开(公告)号：US08602733B2
公开(公告)日：2013-12-10
申请号：US12163397
申请日：2008-06-27
申请人： Costas Christofi , Quynh Hoang , Sanjay Gupta , Angus Lemon , James T. Vershaw , Nandagopal Nalla , Emile Abi-Habib
发明人： Costas Christofi , Quynh Hoang , Sanjay Gupta , Angus Lemon , James T. Vershaw , Nandagopal Nalla , Emile Abi-Habib
IPC分类号： F03B7/00 , F03D11/02 , F04D29/38 , F01D5/20 , F01D5/08 , F01D5/14 , B63H7/02
CPC分类号： F04D29/668 , F04D29/38
摘要： A structural and acoustical vibration dampener for a rotatable blade comprises a layer of structural/acoustic damping material coupled to at least a portion of the blade. A fan blade comprises a structural layer and a layer of damping material coupled to at least a portion of the structural layer. A method of applying a structural and acoustical vibration dampener to a fan blade comprises identifying a region on the fan blade and securing the structural/acoustical vibration dampener to the fan blade over at least a portion of the region.

6. 发明授权

US08313303B2 Acoustical vibration dampener for a rotatable blade 有权
标题翻译：用于可旋转叶片的声音减振器
公开(公告)号：US08313303B2
公开(公告)日：2012-11-20
申请号：US12169194
申请日：2008-07-08
申请人： Costas Christofi , Quynh Hoang , Sanjay Gupta , Angus Lemon , James T. Vershaw , Nandagopal Nalla , Emile Abi-Habib
发明人： Costas Christofi , Quynh Hoang , Sanjay Gupta , Angus Lemon , James T. Vershaw , Nandagopal Nalla , Emile Abi-Habib
IPC分类号： B63H1/26 , B63H7/02 , B64C11/24 , B64C27/46 , B64C11/16 , F01D5/18 , F01D5/14 , F03B3/12 , F03B7/00 , F03D11/02 , F03D29/38
CPC分类号： F01D5/16 , Y10T29/49337
摘要： An acoustical vibration dampening system for a rotatable blade comprises at least one section of a rotatable blade and a layer of acoustic damping material coupled to a portion of the at least one section of a rotatable blade. A fan blade comprises a first structural section of a fan blade, a second structural section of the fan blade, and a layer of acoustic damping material provided between the first structural section and the second structural section of the fan blade. A method of making a fan blade with acoustic damping comprises forming at least two sections of a fan blade, and disposing an acoustical vibration dampener between the at least two sections of the fan blade.
摘要翻译：用于可旋转叶片的声音减振系统包括可旋转叶片的至少一个部分和耦合到可旋转叶片的至少一个部分的一部分的声阻尼材料层。风扇叶片包括风扇叶片的第一结构部分，风扇叶片的第二结构部分和设置在风扇叶片的第一结构部分和第二结构部分之间的声阻尼材料层。制造具有声阻尼的风扇叶片的方法包括形成风扇叶片的至少两个部分，并且在风扇叶片的至少两个部分之间设置声音减振器。

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