公开(公告)号：USD636048S1

公开(公告)日：2011-04-12

申请号：US29361190

申请日：2010-05-06

申请人： Mark Larson ,  Lester Larson, Jr.

设计人： Mark Larson ,  Lester Larson, Jr.

公开(公告)号：USD636047S1

公开(公告)日：2011-04-12

申请号：US29361189

申请日：2010-05-06

申请人： Mark Larson ,  Lester Larson, Jr.

设计人： Mark Larson ,  Lester Larson, Jr.

公开(公告)号：US06272618B1

公开(公告)日：2001-08-07

申请号：US09275826

申请日：1999-03-25

申请人： Benjamen G. Tyner ,  Mark Larson

发明人： Benjamen G. Tyner ,  Mark Larson

IPC分类号： G06F948

CPC分类号： G06F9/4812 ,  G06F13/4068

摘要： A system and method for handling system management interrupts in a multi-processor computer is disclosed. When the computer enters system management mode, the method uses the registers of each processor to get currently executing opcode to determine what each processor was doing before the interrupt. The method may have to first translate address information to locate the actual physical location of the currently executing opcode. The registers are stored in memory and the contents of the registers can be used to determine if the current processor caused the system management interrupt. If so, then the method now knows which processor caused the interrupt and can handle the interrupt accordingly. If, however, the processor was not the one that caused the interrupt, or if another processor also caused an interrupt, the method then repeats the above steps for the next processor of the multiprocessor system.

摘要翻译： 公开了一种用于处理多处理器计算机中的系统管理中断的系统和方法。 当计算机进入系统管理模式时，该方法使用每个处理器的寄存器来获取当前正在执行的操作码，以确定中断前每个处理器正在做什么。 该方法可能必须首先翻译地址信息以定位当前执行的操作码的实际物理位置。 寄存器存储在存储器中，寄存器的内容可用于确定当前处理器是否导致系统管理中断。 如果是这样，那么该方法现在知道哪个处理器引起中断并且可以相应地处理中断。 然而，如果处理器不是导致中断的处理器，或者如果另一个处理器也引起中断，则该方法然后针对多处理器系统的下一个处理器重复上述步骤。

公开(公告)号：US5904407A

公开(公告)日：1999-05-18

申请号：US958947

申请日：1997-10-28

申请人： Mark Larson ,  Michael Oleson

发明人： Mark Larson ,  Michael Oleson

IPC分类号： B64D11/06 ,  A47C7/02

CPC分类号： B64D11/0696 ,  B64D11/06 ,  B64D11/064

摘要： An aircraft seat pan assembly to be mounted on an aircraft seat foundation including a pair of spaced side rail supports and a pair of spaced apart cross supports disposed in spanning relating between the side rail supports, the seat pan assembly including a seat panel with a primary surface, a pair of opposite side edges, a front edge, and a rear edge. The side edges and front edge of the seat panel are structured to be secured directly to the side rail supports and a front cross support of the seat foundation in generally planar relation thereto, and a rear edge of the seat panel is structured to be secured to the rear cross support in a generally elevated, spaced apart position there above such that a quantity of a downward spine load exerted on the seat panel will be absorbed at the connection between the rear edge and the rear cross support. Accordingly, the panel will resist the downward spine load thereon to a satisfaction of FAA guidelines with a minimum initial stroking distance between the primary surface of the seat panel and any underlying seat frame portions being maintained.

摘要翻译： 一种安装在飞行器座椅基座上的飞行器座椅盘组件，包括一对间隔开的侧轨道支撑件和一对间隔开的交叉支架，该横向支架设置成横跨在侧轨道支撑件之间，座椅盘组件包括座板和主座 表面，一对相对的侧边缘，前边缘和后边缘。 座椅面板的侧边缘和前边缘被构造成直接固定到侧轨道支撑件和与其基本平面的座椅基座的前横向支撑件，并且座椅面板的后边缘被构造成固定到 所述后交叉支撑件在其上方大致高度间隔开的位置，使得施加在所述座椅面板上的向下的脊柱负载的量将在所述后边缘和所述后交叉支撑件之间的连接处被吸收。 因此，面板将抵抗其上的向下的脊柱负载以满足FAA指南，其中座椅面板的主表面和任何下面的座椅框架部分之间的最小初始抚摸距离保持不变。

公开(公告)号：US5836547A

公开(公告)日：1998-11-17

申请号：US630009

申请日：1996-04-08

申请人： Roger Koch ,  Ronald Grilliot ,  Mark Larson

发明人： Roger Koch ,  Ronald Grilliot ,  Mark Larson

IPC分类号： B60N2/42 ,  B60R21/04 ,  B64D11/06 ,  B64D25/04 ,  B60R21/055 ,  B64D25/00

CPC分类号： B64D11/0619 ,  B60N2/4221 ,  B60N2/4249 ,  B64D11/06 ,  B64D11/0649 ,  B64D25/04 ,  B60R21/04

摘要： An attenuated aircraft seat back assembly for use on an aircraft passenger seat of the type which includes a seat back frame with a front side and a rear side, the attenuated assembly comprising a mount assembly structured to be secured at the rear side of the seat back frame, preferably at an upper end thereof, and an impact absorbent, generally rigid material panel fixedly secured thereto. The mount assembly is structured to securely maintain the rigid material panel in a generally parallel orientation relative to the seat back frame, and spaced apart from the seat back frame by a predetermined distance. The rigid material panel, which is sized and configured to shield an upper region of the seat back frame, is substantially lightweight and includes a honeycomb interior core structured and disposed to substantially resist the force of a direct impact thereto, while still yielding sufficiently so that an object impacting the rigid material panel will have a Head Injury Criteria (HIC) value which is acceptable under current Federal Aviation Administration regulations. Preferably, an energy absorbent, resilient material panel is adhered to a front face of the rigid material panel, and together have a combined thickness of generally about two inches, while being spaced apart from the seat back frame in assembled form so as to minimize an overall thickness of the assembly.

摘要翻译： 一种用于在包括具有前侧和后侧的座椅靠背框架的类型的飞机乘客座椅上的减弱的飞行器座椅靠背组件，所述减弱组件包括安装组件，该安装组件构造成固定在座椅靠背的后侧 框架，优选地在其上端，以及抗冲击吸收剂，通常为刚性的材料面板固定地固定到其上。 安装组件构造成将刚性材料面板相对于座椅靠背框架以大致平行的方向牢固地保持，并且与座椅靠背框架隔开预定距离。 尺寸和构造以屏蔽座椅靠背框架的上部区域的刚性材料面板基本上是轻质的，并且包括被构造和设置为基本上抵抗直接冲击力的蜂窝内部芯，同时仍充分产生，使得 影响刚性材料面板的物体将具有头部损伤标准（HIC）值，这在当前的联邦航空管理局法规中是可以接受的。 优选地，吸收能量的弹性材料板粘附到刚性材料板的前表面，并且一起具有大致约2英寸的组合厚度，同时以组装的形式与座椅靠背框架间隔开，以便最小化 组件的总厚度。

公开(公告)号：US10258930B2

公开(公告)日：2019-04-16

申请号：US15738117

申请日：2016-06-19

申请人： Mark Larson ,  Erik Bard ,  Michael Lines

发明人： Mark Larson ,  Erik Bard ,  Michael Lines

IPC分类号： H01L27/146 ,  B01D69/10 ,  G21K1/10 ,  H01J5/18 ,  H01J35/18 ,  B01D63/08 ,  G01T7/00

摘要： A support structure for a membrane comprises a plurality of support members and at least one flange, including: (a) a first set of spoke-like support members that extend generally from at least one flange toward a common hub and that have a distal end joined to at least one flange and a proximal end joined to the common hub; and (b) at least one subsequent set of spoke-like support members that are distributed between circumferentially adjacent pairs of spoke-like support members from the prior sets and that extend generally from at least one flange toward the hub, each having a distal end joined to at least one flange and a proximal end connected to the nearest circumferentially adjacent pair of spoke-like support members from the prior sets via a pair of approximately straight anchoring support members which join together and form an angular joint at or near said proximal end, with the vertex of said angular joint pointing generally away from the hub.

公开(公告)号：US20150016593A1

公开(公告)日：2015-01-15

申请号：US14384383

申请日：2013-03-11

申请人： Mark LARSON ,  Michael LINES ,  Erik BARD

发明人： Mark Larson ,  Michael Lines ,  Erik Bard

IPC分类号： G21K1/00

CPC分类号： G21K1/00 ,  H01J5/18 ,  H01J35/18

摘要： An improved radiation window comprises a film permeable to radiation disposed on a support structure. The support structure comprises a primary transmissive area comprising a plurality of support members defining a plurality of apertures for radiation to pass through; a flange disposed around the periphery of the primary transmissive area having generally greater mechanical rigidity than the primary transmissive area; and a transition region disposed between, and contiguous with, the primary transmissive area and the flange; the transition region having generally greater mechanical rigidity than the primary transmissive area and generally lesser mechanical rigidity than the flange, thereby providing an intermediate rigidity transition between the dissimilar rigidities of the primary transmissive area and the flange. A radiation detection system comprises a sensor configured to detect radiation, disposed behind such an improved radiation window.

摘要翻译： 改进的辐射窗口包括设置在支撑结构上的可透射辐射的膜。 支撑结构包括主要透射区域，其包括限定用于辐射通过的多个孔的多个支撑构件; 围绕主透射区域的周边布置的凸缘具有比主透光区域大的更大的机械刚度; 以及设置在所述主透射区域和所述凸缘之间并与所述主透射区域和所述凸缘邻接的过渡区域; 所述过渡区具有比所述主透射区域大的机械刚度，并且与所述凸缘相比通常具有较小的机械刚性，从而在所述主透射区域和所述凸缘的不同刚性之间提供中间刚性过渡。 辐射检测系统包括配置成检测辐射的传感器，设置在这种改进的辐射窗口之后。

公开(公告)号：US08801527B2

公开(公告)日：2014-08-12

申请号：US13719951

申请日：2012-12-19

申请人： Mark Larson

发明人： Mark Larson

IPC分类号： A63D15/08

CPC分类号： A63D15/08

摘要： A pool cue shaft assembly includes a thermoplastic support body extending along a shaft axis from a tip end to a collar end. The support body defines at least three fin members extending radially from a geometric center of the support body. Spaces between the radially extending fin members define at least three longitudinal grooves. At least three inlay members are coupled to the thermoplastic support body. Each inlay member is disposed within a respective longitudinal groove and extends from the tip end to the collar end.

摘要翻译： 池提示轴组件包括沿轴线从尖端延伸到轴环端部的热塑性支撑体。 支撑体限定从支撑体的几何中心径向延伸的至少三个翅片构件。 在径向延伸的翅片构件之间的空间限定至少三个纵向凹槽。 至少三个镶嵌构件联接到热塑性支撑体。 每个嵌体构件设置在相应的纵向凹槽内并从尖端延伸到套环端。

公开(公告)号：USD699313S1

公开(公告)日：2014-02-11

申请号：US29430316

申请日：2012-08-23

申请人： Mark Larson ,  Lester Larson, Jr.

设计人： Mark Larson ,  Lester Larson, Jr.

公开(公告)号：USD696375S1

公开(公告)日：2013-12-24

申请号：US29430319

申请日：2012-08-23

申请人： Mark Larson ,  Lester Larson, Jr.

设计人： Mark Larson ,  Lester Larson, Jr.