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1. 发明申请

WO2003065360A1 DISK-BASED ARCHIVAL DATA STORAGE SYSTEM AND METHOD 审中-公开
标题翻译：基于磁盘的存档数据存储系统和方法
公开(公告)号：WO2003065360A1
公开(公告)日：2003-08-07
申请号：PCT/US2003/002785
申请日：2003-01-28
申请人： DATA DOMAIN, INC , LI, Kai , LEE, Howard
发明人： LI, Kai , LEE, Howard
IPC分类号： G11B11/00
CPC分类号： G06F3/0647 , G06F3/0614 , G06F3/0625 , G06F3/0634 , G06F3/0683 , G06F11/1076 , G06F2211/1088 , G11B19/20 , Y02D10/154
摘要： A disk-based archival storage system (20) including a storage unit (26) configured to store archival data, including at least one spindle of disks to magnetically store archival data, an interconnect (24) to either archive to or retrieve data from the storage unit. In one embodiment, the system includes a plurality of the storage units each including at least one spindle of disks. The control unit (22) controls the storage commands to selectively cause the storage unit(s) to shut down or power up, enter a running mode or a standby mode, cause the spindle of disk(s) to either spin up or spin down, and to perform a data integrity check of all the archival data stored in the storage system. In various other embodiments, the control unit runs algorithms that expand the lifetime and longevity of the disk spindles, optimizes power consumption, and performs data migration when a data integrity check identifies correctable errors.
摘要翻译：一种基于磁盘的档案存储系统（20），包括存储单元（26），存储单元（26）被配置为存储归档数据，包括至少一个磁盘主轴以磁性地存储档案数据;互连（24）存储单元。在一个实施例中，系统包括多个存储单元，每个存储单元包括至少一个盘轴。控制单元（22）控制存储命令以选择性地使存储单元关闭或上电，进入运行模式或待机模式，使盘的主轴旋转或旋转并且对存储在存储系统中的所有归档数据执行数据完整性检查。在各种其它实施例中，当数据完整性检查识别可校正错误时，控制单元运行扩展磁盘主轴的寿命和寿命的算法，优化功耗并执行数据迁移。

2. 发明申请

WO2005019503A2 SUB-MICRON-SCALE PATTERNING METHOD AND SYSTEM 审中-公开
标题翻译：亚微米尺度图案方法与系统
公开(公告)号：WO2005019503A2
公开(公告)日：2005-03-03
申请号：PCT/US2004/026650
申请日：2004-08-19
申请人： NANOOPTO CORPORATION , WANG, Jian , CHEN, Lei , LEE, Howard
发明人： WANG, Jian , CHEN, Lei , LEE, Howard
IPC分类号： C25D
CPC分类号： G03F7/0002 , B82Y10/00 , B82Y40/00 , H01L51/0014 , H01L51/56 , H01L2251/105
摘要： A method for replicating a nanopattern is disclosed. This method includes identifying a substrate; coating a surface of the substrate with a liquid layer; positioning a mold having a plurality of recesses defining a negative of the nanopattern in sufficient proximity with the coated liquid layer to cause the liquid layer to self-fill at least a portion of the plurality of recesses of the mold; and, chemically transforming the liquid layer to enable the transformed film to substantially retain the nanopattern.
摘要翻译：公开了一种复制纳米图案的方法。该方法包括识别基底; 用液体层涂覆基材的表面; 定位具有限定所述纳米图案的负极的多个凹部的模具，其与所述涂覆的液体层足够接近，以使所述液体层自动填充所述模具的所述多个凹部的至少一部分; 并且化学转化液体层以使转化膜能够基本上保持纳米图案。

3. 发明申请

WO2005065071A2 SUPERSONIC AIRCRAFT 审中-公开
标题翻译：超级飞机
公开(公告)号：WO2005065071A2
公开(公告)日：2005-07-21
申请号：PCT/US2004/027693
申请日：2004-08-25
申请人： SUPERSONIC AEROSPACE INTERNATIONAL, LLC , LEE, Howard , MORGENSTERN, John, M. , ANDERSON, Thomas, J. , FRANKLIN, Walter, M., III , WILKINSON, Todd , PEDERSON, Darrell , SMITH, Christopher, J.R. , AMINPOUR, Hossein
发明人： LEE, Howard , MORGENSTERN, John, M. , ANDERSON, Thomas, J. , FRANKLIN, Walter, M., III , WILKINSON, Todd , PEDERSON, Darrell , SMITH, Christopher, J.R. , AMINPOUR, Hossein
IPC分类号： B64C17/10 , B64C30/00
CPC分类号： B64C30/00 , B64C17/10
摘要： An aircraft (100) designed for transonic speed comprises an airfoil (102), a nacelle (122), an engine (116), and an inverted V-tail (114). The nacelle is mounted on the lower aerodynamic airfoil surface and behind the trailing edge of the airfoil. The engine is enclosed within and structurally supported by the nacelle. The inverted-V tail is coupled to the airfoil at a position on the upper aerodynamic surface directly across the airfoil surface so that the inverted-V tail structurally supports the nacelle and engine in combination with support from the airfoil.
摘要翻译：设计用于跨音速的飞行器（100）包括翼型件（102），机舱（122），发动机（116）和倒V型尾翼（114）。机舱安装在下部空气动力学翼面上和翼型的后缘后面。发动机被机舱包围并在结构上由机舱支撑。倒V尾部直接穿过翼型表面在上空气动力学表面上的一个位置处联接到翼型件，使得倒V尾翼结构地支撑机舱和发动机与来自翼型的支撑。

4. 发明申请

WO2005044661A2 SUPERSONIC AIRCRAFT WITH AERODYNAMIC CONTROL 审中-公开
标题翻译：超音速飞行器，带有空气动力学控制
公开(公告)号：WO2005044661A2
公开(公告)日：2005-05-19
申请号：PCT/US2004/027562
申请日：2004-08-25
申请人： SUPERSONIC AEROSPACE INTERNATIONAL, INC. , MORGENSTERN, John, M. , ARSLAN, Alan, E. , LEE, Howard , CUCCIAS, Robert, S.
发明人： MORGENSTERN, John, M. , ARSLAN, Alan, E. , LEE, Howard , CUCCIAS, Robert, S.
IPC分类号： B64C
CPC分类号： B64C9/326 , B64C3/16 , B64C5/02 , B64C5/04 , B64C5/12 , B64C7/00 , B64C9/22 , B64C9/32 , B64C9/36 , B64C13/503 , B64C23/04 , B64C30/00 , B64C39/12 , Y02T50/12 , Y02T50/32 , Y02T50/44
摘要： A supersonic aircraft (900) comprises a fuselage (901), a wing (904), and a canard (920) coupled onto the fuselage (901) forward of the wing (904) at an elevated position that enables stretching forward of the aircraft lifting length, forming an effective area distribution and a shaped sonic boom signature.
摘要翻译：超音速飞机（900）包括机身（901），机翼（904）和鸭翼（920），所述机身（901）在机翼（904）能够在飞机提升长度前方伸展，形成有效的区域分布和成型的音爆标志。

5. 发明申请

WO2005062743A2 SUPERSONIC AIRCRAFT WITH AERODYNAMIC TAIL STRUCTURE 审中-公开
标题翻译：具有航空尾部结构的超级飞机
公开(公告)号：WO2005062743A2
公开(公告)日：2005-07-14
申请号：PCT/US2004/027699
申请日：2004-08-25
申请人： SUPERSONIC AEROSPACE INTERNATIONAL, LLC , MORGENSTERN, John, M. , ARSLAN, Alan, E. , CHANG, Ming , MEZA, Victor , FRANKLIN III, Walter, M. , LEE, Howard , HAJIC, Ken, J. , SCARCELLO, John
发明人： MORGENSTERN, John, M. , ARSLAN, Alan, E. , CHANG, Ming , MEZA, Victor , FRANKLIN III, Walter, M. , LEE, Howard , HAJIC, Ken, J. , SCARCELLO, John
IPC分类号： B64C3/16 , B64C5/02 , B64C9/00 , B64C13/50 , B64C23/04 , B64C30/00 , B64C39/06
CPC分类号： B64C25/12 , B64C3/16 , B64C5/02 , B64C9/00 , B64C13/503 , B64C23/04 , B64C30/00 , B64C39/068 , Y02T50/12 , Y02T50/32 , Y02T50/44
摘要： A supersonic aircraft (100) comprises a wing (104) and at least two engine nacelles (122) coupled to the lower surface of the wing on the trailing edge (107). The supersonic aircraft further comprises an inverted V-tail (108) abutting to the upper side of the wing comprising a central vertical stabilizer (112), at least two inverted stabilizers (114) coupled to sides of the central vertical stabilizer (112) and coupled to the wing and supporting at least two engine nacelles (122), and at least two ruddervators (116) respectively pivotally coupled to at least two inverted stabilizers (114). The supersonic aircraft also comprises a controller coupled to at least two ruddervators (116) and capable of adjusting the aircraft longitudinal lift distribution throughout a flight envelope to maintain a reduced sonic boom and reduced drag trim condition.
摘要翻译：超音速飞机（100）包括机翼（104）和耦合到后缘（107）上机翼下表面的至少两个引擎机舱（122）。超音速飞机还包括邻接翼的上侧的倒V形尾部（108），其包括中心垂直稳定器（112），耦合到中心垂直稳定器（112）侧面的至少两个倒置的稳定器（114）和耦合到机翼并且支撑至少两个发动机机舱（122），以及分别枢转地联接到至少两个倒立的稳定器（114）的至少两个舵机（116）。超音速飞机还包括耦合到至少两个舵机（116）的控制器，并且能够调整整个飞行信封处的飞行器纵向升力分布，以保持降低的声波起重臂和减小的拖曳修剪状况。

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