专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO2008094465A1 SYNTHESIS OF CARBON NANOTUBES BY SELECTIVELY HEATING CATALYST 审中-公开
标题翻译：通过选择性加热催化剂合成碳纳米管
公开(公告)号：WO2008094465A1
公开(公告)日：2008-08-07
申请号：PCT/US2008/001004
申请日：2008-01-25
申请人： CFD RESEARCH CORPORATION , VASENKOV, Aleksey
发明人： VASENKOV, Aleksey
IPC分类号： D01F9/127 , B82B3/00
CPC分类号： C23C16/0281 , B82Y30/00 , C23C16/26 , C23C16/503 , C30B25/10 , C30B25/18 , C30B29/602 , Y10S977/742
摘要： The present invention is a catalytic chemical vapor deposition method and apparatus for synthesizing carbon nanotubes and/or carbon nanofibers (CNTs) on a substrate by selectively heating a catalyst for CNT synthesis on or near the surface of the substrate. Selective heating of the catalyst is achieved using an exothermic oxidation reaction on the surface of the catalyst, inductive heating from a radio frequency source, or both. Selective heating of the catalyst prevents heating of the substrate and enables the synthesis of CNTs on temperature sensitive substrates.
摘要翻译：本发明是一种催化化学气相沉积方法和装置，用于通过在衬底的表面上或附近选择性地加热用于CNT合成的催化剂，在衬底上合成碳纳米管和/或碳纳米纤维（CNT）。催化剂的选择性加热通过催化剂表面上的放热氧化反应，来自射频源的感应加热或两者来实现。催化剂的选择性加热防止了基材的加热，并且能够在温度敏感的基材上合成CNT。

2. 发明申请

WO2014127250A1 CELL CULTURE DEVICE WITH AN ARRAY OF MICROFLUIDIC NETWORKS 审中-公开
标题翻译：具有微流控网络阵列的细胞培养装置
公开(公告)号：WO2014127250A1
公开(公告)日：2014-08-21
申请号：PCT/US2014/016506
申请日：2014-02-14
申请人： CFD RESEARCH CORPORATION
发明人： PANT, Kapil , PRABHAKARPANDIAN, Balabhaskar
IPC分类号： C12N5/071
CPC分类号： G01N33/5008 , B01L3/5025 , B01L3/502715 , B01L2300/0829 , B01L2300/0861 , B01L2300/0874 , B01L2400/0487 , C12M23/16 , C12M23/34 , C12M25/14 , C12M29/00 , C12M29/04 , C12M35/08 , C12M41/00 , C12M41/48
摘要： A cell culture assay device can include: a substrate having a plurality of discrete microfluidic networks and a plurality of wells over the discrete microfluidic networks, each discrete microfluidic network having one or more wells fluidly coupled thereto, the wells extending upward from the discrete microfluidic networks; and a manifold body coupled with the substrate and having at least one fluid conduit pair for each microfluidic network and/or each well, each fluid conduit pair including a fluid inlet conduit and a fluid outlet conduit fluidly coupled to a corresponding microfluidic network and/or well. The substrate can be formed from a substrate base having the microfluidic networks coupled to a well plate having the wells associated with the microfluidic networks.
摘要翻译：细胞培养测定装置可以包括：具有多个离散的微流体网络的衬底和离散的微流体网络上的多个阱，每个离散微流体网络具有一个或多个与其流体耦合的阱，所述阱从离散微流体网络向上延伸 ; 以及与所述基底联接并具有用于每个微流体网络和/或每个孔的至少一个流体导管对的歧管主体，每个流体导管对包括流体连接到相应的微流体网络的流体入口导管和流体出口导管，和/或好。衬底可以由具有耦合到具有与微流体网络相关联的阱的阱板的微流体网络的衬底基底形成。

3. 发明申请

WO2005077444A1 SPACER FOR DELIVERY OF MEDICATIONS FROM AN INHALER TO CHILDREN AND BREATHING IMPAIRED PATIENTS 审中-公开
标题翻译：从吸入者向儿童和呼吸困难患者输送药物的间隔
公开(公告)号：WO2005077444A1
公开(公告)日：2005-08-25
申请号：PCT/US2005/002140
申请日：2005-01-25
申请人： CFD RESEARCH CORPORATION , SUNDARAM, Shivshankar , PRABHAKARPANDIAN, Balabhaskar , MAKHIJANI, Vinod , PRZEKWAS, Andrzej
发明人： SUNDARAM, Shivshankar , PRABHAKARPANDIAN, Balabhaskar , MAKHIJANI, Vinod , PRZEKWAS, Andrzej
IPC分类号： A61M11/00
CPC分类号： A61M15/0086 , A61M15/0016
摘要： A spacer (10) for delivering a medication spray from a metered dose inhaler includes a first conical body (16) joined to a second conical body (18), forming a continuous spray conduit (11) through first and second internal chambers (116, 118) of the respective first and second conical bodies. A mouthpiece (28) is formed in the small diameter (proximal) end (30) of the first conical body. A spray inlet (20) for attachment to an MDI or similar device is formed at the large diameter (distal) end (14) of the second conical body. A plurality of air inlets (26) are placed downstream of the medication inlet proximate to, or in, the large diameter distal end surface (22) of the first conical body.
摘要翻译：用于从计量剂量吸入器输送药物喷雾的间隔物（10）包括连接到第二锥形体（18）的第一锥形体（16），通过第一和第二内室（116,116）形成连续的喷射导管（11）相应的第一和第二锥体的第一和第二锥形体。在第一锥形体的小直径（近端）端部（30）形成有接口（28）。在第二锥形体的大直径（远端）（14）处形成用于附接到MDI或类似装置的喷雾入口（20）。多个空气入口（26）被放置在药物入口的下游靠近第一锥形体的大直径远端表面（22）处或其中。

4. 发明申请

WO2001051787A1 PILOTED AIRBLAST LEAN DIRECT FUEL INJECTOR 审中-公开
标题翻译：先导式航空燃料直接燃料喷射器
公开(公告)号：WO2001051787A1
公开(公告)日：2001-07-19
申请号：PCT/US2001/001675
申请日：2001-01-12
申请人： CFD RESEARCH CORPORATION
发明人： CROCKER, David, S. , NICKOLAUS, Daniel, A. , SMITH, Clifford, E.
IPC分类号： F02C3/14
CPC分类号： F02C7/22 , F05D2270/082 , F23D11/107 , F23D2900/00015 , F23D2900/11101 , F23R3/343 , Y02T50/677
摘要： A gas turbine fuel injection system of the lean direction injector type to reduce NOx emissions is provided. The configuration includes a pilot fuel injector (66), a pilot swirler (28), a main injector (68), and inner (22) and outer (24) main swirlers. An air splitter (26) between the pilot (28) and main (22) swirlers is provided to create a bifurcated recirculation zone (52).
摘要翻译：提供了一种用于减少NOx排放的贫油方向喷射器类型的燃气涡轮机燃料喷射系统。该配置包括先导燃料喷射器（66），先导式旋流器（28），主喷射器（68）以及内部（22）和外部（24）主旋流器。在先导阀（28）和主（22）旋流器之间设置空气分流器（26）以形成分叉再循环区（52）。

5. 发明申请

WO2014085498A1 MULTI-CHAMBERED CELL CULTURE DEVICE TO MODEL ORGAN MICROPHYSIOLOGY 审中-公开
标题翻译：多室细胞培养装置模型有机微生物学
公开(公告)号：WO2014085498A1
公开(公告)日：2014-06-05
申请号：PCT/US2013/072081
申请日：2013-11-26
申请人： CFD RESEARCH CORPORATION
发明人： PRABHAKARPANDIAN, Balabhaskar , PANT, Kapil
IPC分类号： C12M3/00
CPC分类号： C12M21/08 , C12M23/20 , C12M23/26 , C12M23/58 , C12M25/06 , C12M29/00 , C12M29/04 , C12M41/48
摘要： A cell culture device can include: a top wall; a bottom wall; one or more perimeter walls coupled with and extending between the top wall and bottom wall; and at least 3 distinct chambers between the top wall, bottom wall. The one or more perimeter walls can include: an internal chamber defined by at least one porous internal wall and having an internal chamber inlet and an internal chamber outlet; one or more boundary layer chambers having at least an inner boundary layer chamber defined by the at least one porous internal wall and at least one porous inner boundary layer wall, the at least one porous internal wall having a plurality of pores fluidically coupling the central internal chamber to the one or more boundary layer chamber; and an outer chamber defined by an outer porous boundary layer wall of the at least one porous boundary layer walls and the one or more perimeter walls and having an outer chamber inlet and an outer chamber outlet, the outer porous boundary layer wall having a plurality of pores that fluidically couple the outer chamber with the one or more boundary layer chambers. In one aspect, wherein the at least three distinct chambers are nonlinear and/or idealized.
摘要翻译：细胞培养装置可以包括：顶壁; 底壁在顶壁和底壁之间耦合并延伸的一个或多个周边壁; 以及在顶壁，底壁之间的至少3个不同的腔室。一个或多个周边壁可以包括：由至少一个多孔内壁限定并具有内部室入口和内部室出口的内部室; 一个或多个边界层室具有至少一个由所述至少一个多孔内壁和至少一个多孔内边界层壁限定的内边界层室，所述至少一个多孔内壁具有多个孔，室到一个或多个边界层室; 以及由所述至少一个多孔边界层壁和所述一个或多个周边壁的外部多孔边界层壁限定的外部室，并且具有外部室入口和外部室出口，所述外部多孔边界层壁具有多个将外室与一个或多个边界层室流体耦合的孔。在一个方面，其中所述至少三个不同的室是非线性和/或理想化的。

6. 发明申请

WO2008105853A1 CONSTANT VOLUME COMBUSTION BIPROPELLANT PULSED ROCKET MOTOR 审中-公开
标题翻译：恒定体积燃料BIPROPELLANT PULSED ROCKET MOTOR
公开(公告)号：WO2008105853A1
公开(公告)日：2008-09-04
申请号：PCT/US2007/022754
申请日：2007-10-26
申请人： CFD RESEARCH CORPORATION , DiSALVO, Roberto , OSTRANDER, Mark , ELLIOTT, Adam
发明人： DiSALVO, Roberto , OSTRANDER, Mark , ELLIOTT, Adam
IPC分类号： C06B43/00 , C06D5/00
CPC分类号： F02K9/94 , F02K9/58 , F02K9/805
摘要： The present invention is a constant volume rocket motor that uses a non-detonating constant-volume, bipropellant combustion process in pulse-mode operation. Opening and closing of the combustion chamber exhaust outlet is controlled by an actuated reciprocating thrust valve (RTV). Fuel enters the combustion chamber at low pressure with the RTV closed. The valve opens after or during combustion when combustion chamber pressure is at or near maximum. The motor has applications in reaction control systems and attitude control systems in spacecraft.
摘要翻译：本发明是在脉冲模式操作中使用非引爆恒定体积的双组元推进剂燃烧过程的恒定体积火箭发动机。燃烧室排气出口的打开和关闭由致动往复推力阀（RTV）控制。燃料在RTV关闭时以低压进入燃烧室。当燃烧室压力处于或接近最大值时，阀门或燃烧期间打开阀门。电机在航天器的反应控制系统和姿态控制系统中有应用。

7. 发明申请

WO2007126921A2 SYNTHETIC MICROFLUIDIC MICROVASCULATURE 审中-公开
标题翻译：合成微血管微血管
公开(公告)号：WO2007126921A2
公开(公告)日：2007-11-08
申请号：PCT/US2007/007721
申请日：2007-03-28
申请人： CFD RESEARCH CORPORATION , PRABHAKARPANDIAN, Balabhaskar , PANT, Kapil , SUNDARAM, Shivshankar
发明人： PRABHAKARPANDIAN, Balabhaskar , PANT, Kapil , SUNDARAM, Shivshankar
IPC分类号： C12Q1/00 , G06F19/00
CPC分类号： G01N33/54346
摘要： The present invention is a synthetic microfluidic microvasculature network and associated methods. The synthetic microfluidic microvasculature network mimics the structure, fluid flow characteristics, and physiological behavior of physiological microvasculature networks. Computational methods for simulating flow and particle adherence in synthetic and physiological microvascular systems and methods for determining parameters influencing particle adhesion and drug delivery are also described. The invention has many uses including the optimization of drug delivery and microvascular treatments and in describing disease mechanisms that affect the microvasculature such as inflammation, diabetes and hypertension.
摘要翻译：本发明是合成微流控微血管网络及其相关方法。合成微流体微血管网络模拟生理微血管网络的结构，流体流动特性和生理行为。还描述了用于模拟合成和生理微血管系统中的流动和颗粒粘附的计算方法以及用于确定影响颗粒粘附和药物递送的参数的方法。本发明具有许多用途，包括优化药物递送和微血管治疗，并描述影响微血管的疾病机制，如炎症，糖尿病和高血压。

8. 发明申请

WO2007064965A2 HIGH ENERGY, LOW TEMPERATURE GELLED BI-PROPELLANT FORMULATION 审中-公开
标题翻译：高能，低温凝胶双螺旋配方
公开(公告)号：WO2007064965A2
公开(公告)日：2007-06-07
申请号：PCT/US2006/046137
申请日：2006-12-02
申请人： CFD RESEARCH CORPORATION
发明人： DISALVO, Roberto
IPC分类号： F17C5/00 , F25C1/00 , F25C1/18 , D03D23/00
CPC分类号： C06B47/12 , C06B47/04 , F17C2221/03 , F17C2227/0348 , F17C2227/0388 , F17C2265/025 , F17C2270/0194
摘要： The present invention is a bi-propellant system comprising a gelled liquid propane (GLP) fuel and a gelled MON-30 (70% N 2 O 4 + 30% NO) oxidizer. The bi-propellant system is particularly well-suited for outer planet missions greater than 3 AU from the sun and also functions in earth and near earth environments. Additives such as powders of boron, carbon, lithium, and/or aluminum can be added to the fuel component to improve performance or enhance hypergolicity. The gelling agent can be silicon dioxide, clay, carbon, or organic or inorganic polymers. The bi-propellant system may be, but need not be, hypergolic.
摘要翻译：本发明是一种双推进剂系统，其包括凝胶液态丙烷（GLP）燃料和凝胶状MON-30（70％N 2 O 4+ + 30％NO）氧化剂。双推进剂系统特别适用于大于3 AU的太阳外部行星任务，并且在地球和近地环境中也起作用。可以将添加剂如硼，碳，锂和/或铝的粉末加入到燃料组分中，以改善性能或增加超高性。胶凝剂可以是二氧化硅，粘土，碳或有机或无机聚合物。双推进剂系统可以是但不一定是高通量的。

9. 发明授权

US12121889B2 Variable three dimensional convergent-divergent nozzle 有权
公开(公告)号：US12121889B2
公开(公告)日：2024-10-22
申请号：US17502517
申请日：2021-10-15
申请人： CFD RESEARCH CORPORATION , Garry Lynn Freeman, Jr.
发明人： Joseph Roger Herdy, Jr. , Garry Lynn Freeman, Jr.
IPC分类号： G01M9/04 , B01J4/00 , B01J6/00 , C01B13/02 , C01B21/02
CPC分类号： B01J4/002 , B01J6/00 , C01B13/0203 , C01B21/02 , G01M9/04 , B01J2204/007
摘要： A variable 3D CD nozzle includes: a flexible body defining a flow path having an inlet extending through a narrowed throat to an expanded outlet, wherein the flexible body comprises a plurality of flexible members movably interconnected together; and at least one means for changing a shape of the flexible body to change a dimension or location of the throat plane relative to at least one of the inlet plane or outlet plane. A method of changing airflow in a nozzle includes operating at least one means for changing the shape of the flexible nozzle body to change the dimension or the location of the throat plane. A method of testing an object includes placing a test object in the test region of the test cell and passing a test gas from the outlet opening of the nozzle onto the test object.

10. 发明申请

US20210338664A1 COMPOSITIONS AND METHODS FOR MITIGATING AFLATOXIN B1-INDUCED LIVER INJURY 有权
公开(公告)号：US20210338664A1
公开(公告)日：2021-11-04
申请号：US16862500
申请日：2020-04-29
申请人： CFD Research Corporation
发明人： Narender Singh
IPC分类号： A61K31/497 , A61P1/16
摘要： A method for providing a therapy to a subject that has been exposed to an Aflatoxin B1 can include administering a compound having a structure of Formula 1 to the subject after exposure to the Aflatoxin B1: wherein: R1, R2, R3, R4, R5 and/or R6 are each individually a chemical moiety and n is 1, 2, 3, 4, or 5. The compound can be Amprenavir or a derivative thereof, prodrug thereof, salt thereof, or stereoisomer thereof, or having any chirality at any chiral center, or tautomer, polymorph, solvate, or combination thereof. The prodrug can be Amprenavir phosphate.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式