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1. 发明申请

WO2008105967A3 PROPULSION SYSTEM WITH CANTED MULTINOZZLE GRID 审中-公开
公开(公告)号：WO2008105967A3
公开(公告)日：2008-09-04
申请号：PCT/US2007/083448
申请日：2007-11-02
申请人： RAYTHEON COMPANY , CHASMAN, Daniel , HAIGHT, Stephen D.
发明人： CHASMAN, Daniel , HAIGHT, Stephen D.
IPC分类号： F02K9/97 , F02K9/30 , F42B10/66
摘要： A propulsion system includes a canted multinozzle plate (144), which has a multitude of small nozzles (150) angled (not perpendicular) to major surfaces of the multinozzle grid plate. The multinozzle plate may be a cylindrical section or plate, and the multitude of nozzles may be substantially axisymmetric about the cylindrical plate. The propulsion system includes a pressurized gas source which may be placed either forward or aft of the multinozzle grid plate. The propulsion system may have a conical insert, an internal flow separator cone (180), to aid in changing directions of flow from the pressurized gas source, to divert the flow through the multiple nozzles.

2. 发明申请

WO2008140776A1 POLYMORPHISM IN THE APO (A) GENE PREDICT RESPONSIVENESS TO ACETYLSALICYLIC ACID TREATMENT 审中-公开
标题翻译： APO中的多聚体（A）基因预测对乙酰胆酸治疗的反应
公开(公告)号：WO2008140776A1
公开(公告)日：2008-11-20
申请号：PCT/US2008/005986
申请日：2008-05-09
申请人： THE BRIGHAM AND WOMEN'S HOSPITAL, INC. , APPLERA CORPORATION , RIDKER, Paul , CHASMAN, Daniel , SHIFFMAN, Dov
发明人： RIDKER, Paul , CHASMAN, Daniel , SHIFFMAN, Dov
IPC分类号： C12Q1/68
CPC分类号： C12Q1/6883 , A61K31/616 , C12Q1/6876 , C12Q2600/106 , C12Q2600/136 , C12Q2600/156 , C12Q2600/158 , C12Q2600/172 , G01N33/92 , G01N2333/775 , G01N2500/04 , G01N2800/32 , G01N2800/50 , G01N2800/52
摘要： This invention relates to nucleotide polymorphisms in the human Apo(a) gene and to the use of Apo(a) nucleotide polymorphisms in identifying whether a human subject will respond or not to treatment with acetylsalicylic acid.
摘要翻译：本发明涉及人Apo（a）基因中的核苷酸多态性和Apo（a）核苷酸多态性在鉴定人受试者是否对乙酰水杨酸治疗有反应的用途。

3. 发明申请

WO2004099601A2 MULTI-NOZZLE GRID MISSILE PROPULSION SYSTEM 审中-公开
标题翻译：多级喷射式雷达推进系统
公开(公告)号：WO2004099601A2
公开(公告)日：2004-11-18
申请号：PCT/US2003/035150
申请日：2003-11-04
申请人： CHASMAN, Daniel
发明人： CHASMAN, Daniel
IPC分类号： F02K
CPC分类号： F02K9/30 , F02K9/97 , F05D2240/40 , F05D2300/21 , F05D2300/224 , F05D2300/603 , F05D2300/614 , F42B15/10
摘要： A jet propulsion outlet device is disclosed that has a grid plate having a plurality of densely clustered nozzlettes, the nozzlettes of the grid plate being configured to operably couple to a pressurized gas source to efficiently expand the pressurized gas.
摘要翻译：公开了一种具有多个密集聚集的喷嘴的格栅板的喷射推进出口装置，格栅板的喷嘴构造成可操作地耦合到加压气体源以有效地膨胀加压气体。

4. 发明申请

WO2014058525A1 SLOTTED MULTI-NOZZLE GRID WITH INTEGRATED COOLING CHANNELS 审中-公开
标题翻译：带集成式冷却通道的多孔多孔网
公开(公告)号：WO2014058525A1
公开(公告)日：2014-04-17
申请号：PCT/US2013/054401
申请日：2013-08-09
申请人： RAYTHEON COMPANY
发明人： CHASMAN, Daniel , HAIGHT, Stephen D. , VILLARREAL, James K.
IPC分类号： F02K9/30 , F02K9/97
CPC分类号： F02K9/30 , F02K9/97 , F02K9/972 , Y10T29/49346
摘要： An apparatus includes a slotted multi-nozzle grid with a plate (102) having multiple elongated slotlettes (104) through the plate. At least some of the slotlettes have a convergent input (202), a divergent output (204), and a narrower throat portion (206). At least some of the slotlettes are arranged in multiple rows (106). The plate further includes multiple cooling channels (116). At least some of the cooling channels are located between the rows of slotlettes. Each cooling channel is configured to transport coolant through the plate in order to cool the plate, such as to cool the plate as hot combustion gases pass through the plate. Each of at least some of the rows may include at least two slotlettes, and two adjacent slotlettes in one row may be separated by a structural ligament (108), which may have a tear¬ drop cross-sectional shape.
摘要翻译：一种装置包括一个带槽的多喷嘴格栅，其具有通过该板的具有多个细长槽形件（104）的板（102）。至少一些小缝隙具有收敛输入（202），发散输出（204）和较窄的喉部（206）。至少一些小插槽被布置成多行（106）。板还包括多个冷却通道（116）。至少一些冷却通道位于行槽之间。每个冷却通道被构造成运输冷却剂通过板以便冷却板，例如当热燃气体通过板时冷却板。至少一些行中的每一行可以包括至少两个开槽元件，并且一行中的两个相邻的开槽元件可以由可能具有泪滴横截面形状的结构韧带（108）分开。

5. 发明申请

WO2004044519A1 MISSILE CONTROL SYSTEM AND METHOD 审中-公开
标题翻译： MISSILE控制系统和方法
公开(公告)号：WO2004044519A1
公开(公告)日：2004-05-27
申请号：PCT/US2003/035237
申请日：2003-11-03
申请人： RAYTHEON COMPANY
发明人： CHASMAN, Daniel , HAIGHT, Stephen, D. , FACCIANO, Andrew, B.
IPC分类号： F42B10/66
CPC分类号： F42B10/64 , F42B10/663
摘要： A missile (10) includes a tail section (12) having a multi-nozzle grid (16) with both fixed nozzles (20), and movable, thrust vector nozzles (22). The movable nozzles may be configured in a number of discrete array bars (32a-32d), each containing multiple of the movable nozzles. Movement of one or more array bars may be used to vector the thrust of the missile, providing roll, yaw, or spinning of the missile, for example.
摘要翻译：导弹（10）包括具有具有两个固定喷嘴（20）的多喷嘴格栅（16）和可移动的推力矢量喷嘴（22）的尾部部分（12）。可移动喷嘴可以被配置在多个离散的阵列条（32a-32d）中，每个离散阵列条包含多个可移动喷嘴。例如，可以使用一个或多个阵列杆的运动来矢量导弹的推力，提供导弹的滚转，偏转或旋转。

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