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1. 发明申请

US20110142633A1 SYSTEMS AND METHODS FOR ASSEMBLING AN AIR DISTRIBUTION SYSTEM FOR USE IN A ROTOR BLADE OF A WIND TURBINE 有权
标题翻译：用于组装风力发电机转子叶片的空气分配系统的系统和方法
公开(公告)号：US20110142633A1
公开(公告)日：2011-06-16
申请号：US12635573
申请日：2009-12-10
申请人： Wouter Haans , Jacob Johannes Nies , Ciro Cerretelli
发明人： Wouter Haans , Jacob Johannes Nies , Ciro Cerretelli
IPC分类号： F03D7/04 , B23P15/04 , F03D1/06
CPC分类号： F03D1/0683 , F03D1/0675 , F03D15/05 , F03D80/60 , F05B2240/30 , F05B2260/64 , Y02E10/721 , Y10T29/49339
摘要： A method of assembling an air distribution system for use in a rotor blade of a wind turbine. The rotor blade includes a sidewall at least partially defining a cavity extending from a blade root towards a blade tip. The method includes positioning at least a portion of a manifold within the cavity and coupling the manifold to the sidewall. The manifold extends from the blade root towards the blade tip and has a root end and an opposing tip end. A passage is defined from the root end to the tip end. A flow control device is coupled to the manifold root end and configured to channel air through the manifold. A bypass flow assembly is coupled to the manifold and configured to channel air through the air distribution system with the flow control device in a non-operating configuration.
摘要翻译：一种组装用于风力涡轮机的转子叶片的空气分配系统的方法。转子叶片包括至少部分地限定从叶片根部朝向叶片尖端延伸的空腔的侧壁。该方法包括将歧管的至少一部分定位在空腔内并将歧管连接到侧壁。歧管从叶片根部朝向叶片尖端延伸并且具有根端和相对的末端。通道从根端到尖端定义。流量控制装置联接到歧管根部端并且构造成将空气引导通过歧管。旁路流动组件联接到歧管并且构造成通过流动控制装置以非操作构型将空气引导通过空气分配系统。

2. 发明授权

US08052375B2 Fluidic sealing for turbomachinery 失效
标题翻译：涡轮机械的流体密封
公开(公告)号：US08052375B2
公开(公告)日：2011-11-08
申请号：US12131193
申请日：2008-06-02
申请人： Norman Arnold Turnquist , Kevin L. Bruce , Ciro Cerretelli , John Ernest Tourigny
发明人： Norman Arnold Turnquist , Kevin L. Bruce , Ciro Cerretelli , John Ernest Tourigny
IPC分类号： F04D27/02
CPC分类号： F16J15/442 , F01D11/04 , F16J15/443
摘要： Disclosed is a seal for turbomachinery including a seal face locatable between a first turbomachinery component and a second turbomachinery component. At least one fluid channel extends through the seal. The at least one fluid channel is capable of injecting fluid flow between the first turbomachinery component and the second turbomachinery component at the seal face thereby disrupting a leakage flow between the first turbomachinery component and the second turbomachinery component. Further disclosed is a turbomachine utilizing the seal.
摘要翻译：公开了一种用于涡轮机械的密封件，包括可定位在第一涡轮机械部件和第二涡轮机械部件之间的密封面。至少一个流体通道延伸穿过密封件。所述至少一个流体通道能够在密封面处在第一涡轮机械部件和第二涡轮机械部件之间注入流体流动，从而破坏第一涡轮机械部件和第二涡轮机械部件之间的泄漏流。另外公开了利用密封件的涡轮机。

3. 发明申请

US20130195608A1 DROPLET CATCHER FOR CENTRIFUGAL COMPRESSOR 有权
标题翻译：离心压缩机DROPLET CATCHER
公开(公告)号：US20130195608A1
公开(公告)日：2013-08-01
申请号：US13504658
申请日：2009-10-27
申请人： Emad Ahmad Obaid Gharaibah , Ciro Cerretelli , Michael Bernhard Schmitz
发明人： Emad Ahmad Obaid Gharaibah , Ciro Cerretelli , Michael Bernhard Schmitz
IPC分类号： F01D5/14
CPC分类号： F01D5/14 , B01D45/14 , F04D27/0292 , F04D29/284 , F04D29/701 , F04D29/706
摘要： A liquid droplet catching device installed in a compressor impeller, the device includes an aperture disposed on a surface of the impeller and configured to receive the liquid droplet, and a channel disposed beneath and in fluid communication with the aperture, wherein in the channel is configured to direct the liquid droplet away from the aperture and out of the compressor impeller.
摘要翻译：一种安装在压缩机叶轮中的液滴捕获装置，该装置包括设置在叶轮的表面上并构造成接收液滴的孔，以及设置在孔的下方并与其流体连通的通道，其中在通道中配置以将液滴引导离开孔并离开压缩机叶轮。

4. 发明申请

US20110005334A1 TUNABLE FLUID FLOW CONTROL SYSTEM 审中-公开
标题翻译：流体流量控制系统
公开(公告)号：US20110005334A1
公开(公告)日：2011-01-13
申请号：US12499152
申请日：2009-07-08
申请人： Joel Meier Haynes , Ciro Cerretelli
发明人： Joel Meier Haynes , Ciro Cerretelli
IPC分类号： G01F1/20
CPC分类号： F23N1/002 , F23D2900/14482 , F23K2900/05001 , F23N5/242 , F23N2025/04 , F23R3/286 , F23R2900/00001 , F23R2900/00013
摘要： A tunable fluid flow control system includes a fluidic oscillator having a movable boundary wall. A pressurized gas source is coupled to the movable boundary wall and configured to supply a stream of pressurized gas to the movable boundary wall to actuate the boundary wall. The boundary wall is actuatable to vary a cavity volume in the fluidic oscillator so as to control frequency of flow of a pulsating fluid generated by the fluidic oscillator. A portion of a fluid is bypassed the fluidic oscillator so as to control amplitude of flow of a pulsating fluid generated by the fluidic oscillator.
摘要翻译：可调流体流量控制系统包括具有可移动边界壁的流体振荡器。加压气体源耦合到可移动边界壁并且构造成将加压气体流供应到活动边界壁以致动边界壁。边界壁可致动以改变流体振荡器中的空腔体积，以便控制由流体振荡器产生的脉动流体的流动频率。流体的一部分旁路流体振荡器，以便控制由流体振荡器产生的脉动流体的流量的振幅。

5. 发明申请

US20090297341A1 FLUIDIC SEALING FOR TURBOMACHINERY 失效
标题翻译：流体密封用于涡轮机
公开(公告)号：US20090297341A1
公开(公告)日：2009-12-03
申请号：US12131193
申请日：2008-06-02
申请人： Norman Arnold Turnquist , Kevin L. Bruce , Ciro Cerretelli , John Ernest Tourigny
发明人： Norman Arnold Turnquist , Kevin L. Bruce , Ciro Cerretelli , John Ernest Tourigny
IPC分类号： F01D5/20
CPC分类号： F16J15/442 , F01D11/04 , F16J15/443
摘要： Disclosed is a seal for turbomachinery including a seal face locatable between a first turbomachinery component and a second turbomachinery component. At least one fluid channel extends through the seal. The at least one fluid channel is capable of injecting fluid flow between the first turbomachinery component and the second turbomachinery component at the seal face thereby disrupting a leakage flow between the first turbomachinery component and the second turbomachinery component. Further disclosed is a turbomachine utilizing the seal.
摘要翻译：公开了一种用于涡轮机械的密封件，包括可定位在第一涡轮机械部件和第二涡轮机械部件之间的密封面。至少一个流体通道延伸穿过密封件。所述至少一个流体通道能够在密封面处在第一涡轮机械部件和第二涡轮机械部件之间注入流体流动，从而破坏第一涡轮机械部件和第二涡轮机械部件之间的泄漏流。另外公开了利用密封件的涡轮机。

6. 发明授权

US07128082B1 Method and system for flow control with fluidic oscillators 有权
标题翻译：用流体振荡器进行流量控制的方法和系统
公开(公告)号：US07128082B1
公开(公告)日：2006-10-31
申请号：US11201914
申请日：2005-08-10
申请人： Ciro Cerretelli , Kevin Richard Kirtley
发明人： Ciro Cerretelli , Kevin Richard Kirtley
IPC分类号： F15C1/08 , B05B1/08
CPC分类号： F15C1/22 , B05B1/08 , B05B7/0075 , F01D5/145 , F05D2260/60 , F15D1/12 , Y02T50/673 , Y10T137/0396 , Y10T137/212 , Y10T137/2185 , Y10T137/2224
摘要： A system for control of a fluid flow. The system includes an array of fluidic oscillators. Each fluidic oscillator carries an oscillating flow of the fluid and includes a throat, an input port connected to the throat, two control ports connected to the throat and two output ports extending from the throat. A feedback line is connected to each of the two output ports and each of the two control ports. The system further includes a plenum connected to the input ports of the fluidic oscillators to supply the fluid to the fluidic oscillators and a feedback chamber disposed along each feedback line of each fluidic oscillator to provide a feedback path for the control fluid to cause oscillatory fluid motion between the first output port and the second output port, the frequency of which may be modulated by adjusting the volume of the feedback chamber.
摘要翻译：用于控制流体流动的系统。该系统包括一组流体振荡器。每个流体振荡器携带流体的振荡流，并且包括喉部，连接到喉部的输入端口，连接到喉部的两个控制端口和从喉部延伸的两个输出端口。反馈线连接到两个输出端口和两个控制端口中的每一个。该系统还包括连接到流体振荡器的输入端口以将流体供应到流体振荡器的增压室和沿每个流体振荡器的每个反馈线布置的反馈室，以提供用于控制流体引起振荡流体运动的反馈路径在第一输出端口和第二输出端口之间，其频率可以通过调节反馈室的体积来调制。

7. 发明授权

US09689263B2 Droplet catcher for centrifugal compressor 有权
公开(公告)号：US09689263B2
公开(公告)日：2017-06-27
申请号：US13504658
申请日：2009-10-27
申请人： Emad Ahmad Obaid Gharaibah , Ciro Cerretelli , Michael Bernhard Schmitz
发明人： Emad Ahmad Obaid Gharaibah , Ciro Cerretelli , Michael Bernhard Schmitz
IPC分类号： B63H1/28 , F03D11/00 , F04D29/22 , F04D29/32 , F04D29/38 , F01B31/28 , F01D25/32 , F01D5/14 , B01D45/14 , F04D29/28 , F04D29/70 , F04D27/02
CPC分类号： F01D5/14 , B01D45/14 , F04D27/0292 , F04D29/284 , F04D29/701 , F04D29/706
摘要： A liquid droplet catching device installed in a compressor impeller, the device includes an aperture disposed on a surface of the impeller and configured to receive the liquid droplet, and a channel disposed beneath and in fluid communication with the aperture, wherein in the channel is configured to direct the liquid droplet away from the aperture and out of the compressor impeller.

8. 发明授权

US08845281B2 Centrifugal compressor for wet gas environments and method of manufacture 有权
标题翻译：用于湿气环境的离心式压缩机及其制造方法
公开(公告)号：US08845281B2
公开(公告)日：2014-09-30
申请号：US12997494
申请日：2009-06-08
申请人： Ciro Cerretelli , Kripa Kiran Varanasi , Michael Bernhard Schmitz , Emad Ahmad Obaid Gharaibah , Christopher Edward Wolfe
发明人： Ciro Cerretelli , Kripa Kiran Varanasi , Michael Bernhard Schmitz , Emad Ahmad Obaid Gharaibah , Christopher Edward Wolfe
IPC分类号： F04D29/70 , F04D29/02 , F04D29/28 , F04D29/42
CPC分类号： F04D29/023 , F04D29/284 , F04D29/4206 , F04D29/701 , F04D29/706 , F05D2300/51 , F05D2300/512
摘要： A centrifugal compressor comprises at least one stage suited to separate a liquid phase and a gas phase with the aid of at least one of a hydrophobic, super-hydrophobic, hydrophilic or super-hydrophilic surface layer, wherein the hydrophobic and/or super-hydrophobic surface layer is disposed on at least one of an inlet guide vane, impeller, return channel straight hub, or exiting hub bend; and the hydrophilic and/or super-hydrophilic surface is disposed on at least one of the impeller casing, diffuser casing, exiting casing bend, return channel straight hub, exiting hub bend, collection point, or drain.
摘要翻译：离心压缩机包括至少一个级，其适用于借助于疏水性，超疏水性，亲水性或超亲水性表面层中的至少一种来分离液相和气相，其中疏水和/或超疏水表面层设置在入口引导叶片，叶轮，返回通道直轮毂或出口轮毂弯曲部中的至少一个上; 并且亲水和/或超亲水表面设置在叶轮壳体，扩散器壳体，出口壳体弯曲部，返回通道直轮毂，离开毂弯曲部，收集点或排出物中的至少一个上。

9. 发明授权

US08475129B2 Systems and methods for assembling an air distribution system for use in a rotor blade of a wind turbine 有权
标题翻译：用于组装用于风力涡轮机的转子叶片的空气分配系统的系统和方法
公开(公告)号：US08475129B2
公开(公告)日：2013-07-02
申请号：US12635573
申请日：2009-12-10
申请人： Wouter Haans , Jacob Johannes Nies , Ciro Cerretelli
发明人： Wouter Haans , Jacob Johannes Nies , Ciro Cerretelli
IPC分类号： F01D5/18
CPC分类号： F03D1/0683 , F03D1/0675 , F03D15/05 , F03D80/60 , F05B2240/30 , F05B2260/64 , Y02E10/721 , Y10T29/49339
摘要： A method of assembling an air distribution system for use in a rotor blade of a wind turbine. The rotor blade includes a sidewall at least partially defining a cavity extending from a blade root towards a blade tip. The method includes positioning at least a portion of a manifold within the cavity and coupling the manifold to the sidewall. The manifold extends from the blade root towards the blade tip and has a root end and an opposing tip end. A passage is defined from the root end to the tip end. A flow control device is coupled to the manifold root end and configured to channel air through the manifold. A bypass flow assembly is coupled to the manifold and configured to channel air through the air distribution system with the flow control device in a non-operating configuration.
摘要翻译：一种组装用于风力涡轮机的转子叶片的空气分配系统的方法。转子叶片包括至少部分地限定从叶片根部朝向叶片尖端延伸的空腔的侧壁。该方法包括将歧管的至少一部分定位在空腔内并将歧管连接到侧壁。歧管从叶片根部朝向叶片尖端延伸并且具有根端和相对的末端。通道从根端到尖端定义。流量控制装置联接到歧管根部端并且构造成将空气引导通过歧管。旁路流动组件联接到歧管并且构造成通过流动控制装置以非操作构型将空气引导通过空气分配系统。

10. 发明申请

US20090324382A1 Torque-based sensor and control method for varying gas-liquid fractions of fluids for turbomachines 审中-公开
$Torque-based sensor and control method for varying gas-liquid fractions of fluids for turbomachines$
标题翻译：用于改变涡轮机流体的气液分数的基于扭矩的传感器和控制方法
公开(公告)号：US20090324382A1
公开(公告)日：2009-12-31
申请号：US12151168
申请日：2008-05-05
申请人： Michael Bernhard Schmitz , Sergio Boris , Ciro Cerretelli , Christof Martin Sihler
发明人： Michael Bernhard Schmitz , Sergio Boris , Ciro Cerretelli , Christof Martin Sihler
IPC分类号： F01D17/08
CPC分类号： F04D27/0261 , F04D27/001
摘要： A torque-based sensor and control method for detecting varying gas-liquid fractions of a fluid entering a turbomachine that operates a fluid of varying liquid phases and compositions and using information about the actual gas-liquid fraction to set a control algorithm so that it can change the torque and therefore the rotation speed of the turbomachine to operate at safer conditions or conditions with higher efficiency or higher power output.
摘要翻译：一种基于扭矩的传感器和控制方法，用于检测进入涡轮机的流体的不同气液分数，其操作不同液相和组成的流体，并使用关于实际气液分数的信息来设置控制算法，使得其可以改变扭矩并因此改变涡轮机的旋转速度，以在更高的效率或更高功率输出的更安全的条件或条件下工作。

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