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公开(公告)号：US08409954B2
公开(公告)日：2013-04-02
申请号：US11386927
申请日：2006-03-21
申请人： The-Tu Chau , Sharon Shi , Qufei Chen , Martin Hernandez , Deva Pattanayak , Kyle Terrill , Kuo-In Chen
发明人： The-Tu Chau , Sharon Shi , Qufei Chen , Martin Hernandez , Deva Pattanayak , Kyle Terrill , Kuo-In Chen
IPC分类号： H01L21/336
CPC分类号： H01L29/0878 , H01L29/167 , H01L29/7813
摘要： Ultra-low drain-source resistance power MOSFET. In accordance with an embodiment of the preset invention, a semiconductor device comprises a plurality of trench power MOSFETs. The plurality of trench power MOSFETs is formed in a second epitaxial layer. The second epitaxial layer is formed adjacent and contiguous to a first epitaxial layer. The first epitaxial layer is formed adjacent and contiguous to a substrate highly doped with red Phosphorous. The novel red Phosphorous doped substrate enables a desirable low drain-source resistance.
摘要翻译： 超低漏源电阻功率MOSFET。 根据本发明的实施例，半导体器件包括多个沟槽功率MOSFET。 多个沟槽功率MOSFET形成在第二外延层中。 第二外延层形成为与第一外延层相邻并邻接。 第一外延层与高度掺杂有红磷的衬底相邻并邻接地形成。 新型红磷掺杂衬底能够实现所需的低漏源电阻。
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2.发明授权公开(公告)号：US07907382B2
公开(公告)日：2011-03-15
申请号：US12069574
申请日：2008-02-11
IPC分类号： H05F3/00
CPC分类号： B64D45/02 , F16B33/004 , F16B37/14 , F16B43/001
摘要： The invention relates to an integrated device (1) for the protection against electrical discharges of conductive fixing elements (2) between one another or of a fixing element and another conductive element of aircraft, comprising a cap (3) and an o-ring gasket (4) made of non-conductive insulating material, the mentioned integrated device (1) comprising a modified fixing element (2) working together with the cap (3) and the o-ring gasket (4), the fixing element (2) surrounding the cap (3) and the o-ring gasket (4) in a non-conductive manner, thus preventing the possibility of electrical discharges such that in the device (1) the number of necessary components is minimized, the impact in weight for the aircraft being minimum, the modified fixing element (2) further comprising a thread (5) on the outer face of the area that has to be protected.
摘要翻译： 本发明涉及一种用于防止导电固定元件（2）彼此之间或固定元件与飞机另一导电元件的放电的集成装置（1），其包括盖（3）和O形圈垫圈 （4）由不导电绝缘材料制成，所述集成装置（1）包括与盖（3）和O形环垫圈（4）一起工作的改进的固定元件（2），固定元件（2） 以不导电的方式围绕盖（3）和O型圈垫圈（4），从而防止放电的可能性，使得在装置（1）中所需部件的数量最小化，对于 所述飞行器是最小的，所述修改的固定元件（2）还包括在所述区域的外表面上必须被保护的螺纹（5）。
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3.发明授权Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser 有权机身与机身可定向水平稳定器电梯之间存在的间隙的密封系统，用空气动力整流罩延伸，用于密封机身和可定向水平稳定器之间的开口公开(公告)号：US07850119B2
公开(公告)日：2010-12-14
申请号：US11790401
申请日：2007-04-25
IPC分类号： B64C7/00
摘要： Sealing system for the gap (2) between the fuselage (3) and the elevator (4) of the orientable horizontal stabiliser (5) of an aircraft, extended with an aerodynamic fairing (8) for sealing of the opening (24) between the fuselage (3) and said orientable horizontal stabiliser (5) which comprises a main body (1) and an aerodynamic fairing (8) which is extended from the main body (1) in continuity with the latter, and a plurality of first elastic sealing profiles (9) between the first surface (11) of the main body (1) including the aerodynamic fairing (8) and the outer surface of the fuselage (3) and making contact with them, and a plurality of second elastic sealing profiles (13) between the second surface (12) of the main body (1) and the first end of the elevator (15) and making contact with them, in such a way that the sealing takes place of the gap (2) and the opening (24) and an aerodynamic continuity is produced between the orientable horizontal stabiliser (5), the fuselage (3) and the elevator (4) when the elevator (4) is at rest in the plane of the orientable horizontal stabiliser (5) for any of the orientation positions of the orientable horizontal stabiliser (5).
摘要翻译： 用于机身（3）与飞机的可定向水平稳定器（5）的电梯（4）之间的间隙（2）的密封系统，其延伸有空气动力学整流罩（8），用于密封开口（24） 机身（3）和所述可定向水平稳定器（5），其包括从主体（1）延伸的与主体（1）延伸的主体（1）和空气动力整流罩（8），以及多个第一弹性密封 主体（1）的包括气动整流罩（8）和机身外表面（3）的第一表面（11）与其接触并且与多个第二弹性密封型材 13）在主体（1）的第二表面（12）和电梯（15）的第一端之间并与它们接触，使得密封发生在间隙（2）和开口 （24），并且在可定向水平稳定器（5），机身（3）a之间产生空气动力学连续性 d电梯（4）在可定向水平稳定器（5）的任何取向位置处于可定向水平稳定器（5）的平面中静止时。
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4.发明授权Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabilizer 失效密封系统存在于具有可定向水平稳定器的飞机机身和电梯之间的差距公开(公告)号：US07699266B2
公开(公告)日：2010-04-20
申请号：US11790453
申请日：2007-04-25
摘要： A sealing system for a gap (2) existing between the fuselage (3) and the elevator (4) of a orientable horizontal stabilizer (5) of an aircraft, comprises a main body (1) formed by an upper surface (18) and a lower surface (19) and at least one longitudinal vertical element (22) arranged between the two surfaces (18,19) which grants rigidity to the main body (1), and a plurality of first elastic sealing profiles (9) between the first surface (11) of the main body (1) and the outer surface of the fuselage (3) and making contact with them, and a plurality of second elastic sealing profiles (13) between the second surface (12) of the main body (1) and the first end of the elevator (15) and making contact with them, in such a way that the sealing of the gap (2) takes place and an aerodynamic continuity is produced between the fuselage (3) and the elevator (4) when the elevator (4) is at rest in the plane of the orientable horizontal stabilizer (5) for any of the orientation positions of the orientable horizontal stabilizer (5).
摘要翻译： 存在于飞机的可定向水平稳定器（5）的机身（3）和电梯（4）之间的间隙（2）的密封系统包括由上表面（18）形成的主体（1）和 布置在两个表面（18,19）之间的至少一个纵向垂直元件（22）的下表面（19）和至少一个纵向垂直元件（22），其向主体（1）提供刚性;以及多个第一弹性密封型材（9） 主体（1）的第一表面（11）和机身（3）的外表面与它们接触，以及在主体的第二表面（12）之间的多个第二弹性密封型材（13） （1）和电梯（15）的第一端并与其接触，使得间隙（2）的密封发生并且在机身（3）和电梯（3）之间产生空气动力学连续性 4）当电梯（4）在可定向的水平稳定器（5）的平面中静止时，用于任何取向位置 可定向水平稳定器（5）。
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5.发明申请Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabiliser 失效密封系统存在于具有可定向水平稳定器的飞机机身和电梯之间的差距公开(公告)号：US20080169382A1
公开(公告)日：2008-07-17
申请号：US11790453
申请日：2007-04-25
IPC分类号： B64C1/00
摘要： Sealing system for the gap (2) existing between the fuselage (3) and the elevator (4) of the orientable horizontal stabiliser (5) of an aircraft which comprises a main body (1) formed by an upper surface (18) and a lower surface (19) and at least one longitudinal vertical element (22) arranged between the two surfaces (18,19) which grants rigidity to the main body (1), and a plurality of first elastic sealing profiles (9) between the first surface (11) of the main body (1) and the outer surface of the fuselage (3) and making contact with them, and a plurality of second elastic sealing profiles (13) between the second surface (12) of the main body (1) and the first end of the elevator (15) and making contact with them, in such a way that the sealing of the gap (2) takes place and an aerodynamic continuity is produced between the fuselage (3) and the elevator (4) when the elevator (4) is at rest in the plane of the orientable horizontal stabiliser (5) for any of the orientation positions of the orientable horizontal stabiliser (5).
摘要翻译： 存在于飞机的可定向水平稳定器（5）的机身（3）和升降机（4）之间的间隙（2）的密封系统，包括由上表面（18）形成的主体（1） 下表面（19）和布置在两个表面（18,19）之间的至少一个纵向垂直元件（22），其向主体（1）提供刚性;以及多个第一弹性密封型材（9） 主体（1）的表面（11）和机身（3）的外表面与它们接触，以及在主体的第二表面（12）之间的多个第二弹性密封型材（13） 1）和电梯（15）的第一端并与其接触，使得间隙（2）的密封发生并且在机身（3）和电梯（4）之间产生空气动力学连续性 ）当电梯（4）在可定向的水平稳定平面中静止时 ser（5）用于可定向水平稳定器（5）的任何取向位置。
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公开(公告)号：US20070221989A1
公开(公告)日：2007-09-27
申请号：US11386927
申请日：2006-03-21
申请人： The-Tu Chau , Sharon Shi , Qufei Chen , Martin Hernandez , Deva Pattarayak , Kyle Terrill , Kuo-In Chen
发明人： The-Tu Chau , Sharon Shi , Qufei Chen , Martin Hernandez , Deva Pattarayak , Kyle Terrill , Kuo-In Chen
CPC分类号： H01L29/0878 , H01L29/167 , H01L29/7813
摘要： Ultra-low drain-source resistance power MOSFET. In accordance with an embodiment of the preset invention, a semiconductor device comprises a plurality of trench power MOSFETs. The plurality of trench power MOSFETs is formed in a second epitaxial layer. The second epitaxial layer is formed adjacent and contiguous to a first epitaxial layer. The first epitaxial layer is formed adjacent and contiguous to a substrate highly doped with red Phosphorous. The novel red Phosphorous doped substrate enables a desirable low drain-source resistance.
摘要翻译： 超低漏源电阻功率MOSFET。 根据本发明的实施例，半导体器件包括多个沟槽功率MOSFET。 多个沟槽功率MOSFET形成在第二外延层中。 第二外延层形成为与第一外延层相邻并邻接。 第一外延层与高度掺杂有红磷的衬底相邻并邻接地形成。 新型红磷掺杂衬底能够实现所需的低漏源电阻。
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公开(公告)号：US20060249627A1
公开(公告)日：2006-11-09
申请号：US11323146
申请日：2005-12-30
CPC分类号： B64C7/00
摘要： Reinforced cover for cut-outs in an aerodynamic contour of a vehicle, with a first attachment section 1a attachable to a structural element (2,5) of the vehicle (11); a second elastic section 1c which covers the cut-out (4) which is located between a fixed part 5 and a moving part (6, 12) of the vehicle (11), and provided with a low-friction layer (8) on its inner surface (1e), which comprises a first area (1i) in a rectangular configuration and a second area (1j) with a second cross-section smaller than that of the first area (1i); an outer surface (1k) with a fiberglass layer (7a); a main internal body (9) of a flexible material, a transition section (1g) thickened between the first and the second section, (1a, 1c); flushing the outer surface (1k) of the second section (1c) with the outer surface (5a).
摘要翻译： 具有车辆空气动力学轮廓中的切口的加强盖，具有可附接到车辆（11）的结构元件（2,5）的第一附接部分1a; 覆盖位于车辆（11）的固定部分5和移动部分（6,12）之间的切口（4）的第二弹性部分1c，并且设置有低摩擦层（8） 在其内表面（1e）上，其包括矩形构造的第一区域（1i）和具有小于第一区域（1i）的第二横截面的第二区域（1j）; 具有玻璃纤维层（7a）的外表面（1k）; 柔性材料的主体（9），在第一和第二部分之间增厚的过渡部分（1g）（1a，1c）; 用外表面（5a）冲洗第二部分（1c）的外表面（1k）。
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8.发明申请Holder for Being Positioned in Floating Floor Slabs and Installation System Thereof 有权定位在浮动地板及其安装系统中的持有人公开(公告)号：US20120210656A1
公开(公告)日：2012-08-23
申请号：US13463320
申请日：2012-05-03
摘要： A holder to be placed in floating floor slabs and the installation system thereof, the holder comprising a cubic holder having a pair of tubes on each side thereof, parallel with the supporting base, with facing sides in identical position; within said sides a section designed for placing rods on which the different layers of the rebar mesh are supported and a system for fitting the mesh on the rods, and also the securing of the corners of the different levels of the rebar mesh by means of linking of the holder s using the rods.
摘要翻译： 放置在浮动楼板中的支架及其安装系统，该支架包括一立方体支架，该立方体支架的每侧具有一对平行于支撑底座的一对管，其相对侧面处于相同的位置; 在所述侧面内设有用于放置支撑钢筋网不同层的杆的部分和用于将网格装配到杆上的系统，以及通过连接固定不同级别的钢筋网的角部 的持有人使用杆。
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公开(公告)号：US20100281815A1
公开(公告)日：2010-11-11
申请号：US12668890
申请日：2008-07-01
IPC分类号： E04F15/022
摘要： A device to be placed in floating floor slabs and the installation system thereof, the device comprising a cube having a pair of tubes on each side thereof, parallel with the base, with facing sides in identical position; within said sides a section designed for placing rods on which the different layers of the rebar mesh are supported and a system for fitting the mesh on the rods, and also the securing of the corners of the different levels of the rebar mesh by means of linking of the cubes using the rods.
摘要翻译： 一种放置在浮动楼板中的装置及其安装系统，该装置包括立方体，该立方体的每侧具有与基座平行的一对管，面对侧面处于相同的位置; 在所述侧面内设有用于放置支撑钢筋网不同层的杆的部分和用于将网格装配到杆上的系统，以及通过连接固定不同级别的钢筋网的角部 的立方体使用杆。
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10.发明申请公开(公告)号：US20090147429A1
公开(公告)日：2009-06-11
申请号：US12069574
申请日：2008-02-11
CPC分类号： B64D45/02 , F16B33/004 , F16B37/14 , F16B43/001
摘要： The invention relates to an integrated device (1) for the protection against electrical discharges of conductive fixing elements (2) between one another or of a fixing element and another conductive element of aircraft, comprising a cap (3) and an o-ring gasket (4) made of non-conductive insulating material, the mentioned integrated device (1) comprising a modified fixing element (2) working together with the cap (3) and the o-ring gasket (4), the fixing element (2) surrounding the cap (3) and the o-ring gasket (4) in a non-conductive manner, thus preventing the possibility of electrical discharges such that in the device (1) the number of necessary components is minimized, the impact in weight for the aircraft being minimum, the modified fixing element (2) further comprising a thread (5) on the outer face of the area that has to be protected.
摘要翻译： 本发明涉及一种用于防止导电固定元件（2）彼此之间或固定元件与飞机另一导电元件的放电的集成装置（1），其包括盖（3）和O形圈垫圈 （4）由不导电绝缘材料制成，所述集成装置（1）包括与盖（3）和O形环垫圈（4）一起工作的改进的固定元件（2），固定元件（2） 以不导电的方式围绕盖（3）和O型圈垫圈（4），从而防止放电的可能性，使得在装置（1）中所需部件的数量最小化，对于 所述飞行器是最小的，所述修改的固定元件（2）还包括在所述区域的外表面上必须被保护的螺纹（5）。
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