Integrated approach navigation system, method, and computer program product
    1.
    发明授权
    Integrated approach navigation system, method, and computer program product 有权
    综合导航系统,方法和计算机程序产品

    公开(公告)号:US08027756B2

    公开(公告)日:2011-09-27

    申请号:US11608064

    申请日:2006-12-07

    IPC分类号: G05D1/06

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。

    Integrated approach navigation system, method, and computer program product
    2.
    发明授权
    Integrated approach navigation system, method, and computer program product 有权
    综合导航系统,方法和计算机程序产品

    公开(公告)号:US08423207B2

    公开(公告)日:2013-04-16

    申请号:US13218978

    申请日:2011-08-26

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。

    INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT
    3.
    发明申请
    INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT 有权
    综合方法导航系统,方法和计算机程序产品

    公开(公告)号:US20080140270A1

    公开(公告)日:2008-06-12

    申请号:US11608064

    申请日:2006-12-07

    IPC分类号: G01C21/00 G05D1/00

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。

    INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT
    4.
    发明申请
    INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT 有权
    综合方法导航系统,方法和计算机程序产品

    公开(公告)号:US20110313600A1

    公开(公告)日:2011-12-22

    申请号:US13218978

    申请日:2011-08-26

    IPC分类号: G01C23/00 G05D1/00

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。

    Integral tensioning member for variable sheetmetal thickness carrier attachment
    5.
    发明授权
    Integral tensioning member for variable sheetmetal thickness carrier attachment 有权
    用于可变钣金厚度载体附件的整体张紧构件

    公开(公告)号:US08348581B2

    公开(公告)日:2013-01-08

    申请号:US11654799

    申请日:2007-01-18

    IPC分类号: F16B19/00

    CPC分类号: B60R13/0206

    摘要: A carrier for engaging a panel and a method of making a carrier for engaging a panel are disclosed. The carrier generally includes a base portion, an attachment member disposed on the base portion which is operable to engage a panel, and a springbar disposed on the base portion. The method generally includes forming a base portion, forming an attachment member, and forming a springbar on the base portion. The attachment member cooperates with the base portion to define a maximum panel thickness, and the springbar engages panels having a thickness less than or equal to the maximum panel thickness to provide tension between the base portion and a panel.

    摘要翻译: 公开了一种用于接合面板的托架和制造用于接合面板的托架的方法。 载体通常包括基部,设置在基部上的可操作以接合面板的附接构件和设置在基部上的弹簧杆。 该方法通常包括形成基部,形成附接构件,以及在基部上形成弹簧杆。 附接构件与基部配合以限定最大面板厚度,并且弹簧杆接合厚度小于或等于最大面板厚度的面板,以在基部和面板之间提供张力。

    Current amplifier having multiple selectable outputs
    6.
    发明授权
    Current amplifier having multiple selectable outputs 失效
    电流放大器具有多个可选输出

    公开(公告)号:US4501979A

    公开(公告)日:1985-02-26

    申请号:US413054

    申请日:1982-08-30

    IPC分类号: G05F3/26 H03K17/62 H03F3/04

    CPC分类号: H03K17/6285 G05F3/265

    摘要: A current amplifier is provided having a single control amplifier and a plurality of output stages. The desired output stage is digitally selected. The ratios of the output stage currents may be selected during the metalization process. A single capacitor compensates for all output stages regardless of which output stage is selected.

    摘要翻译: 提供了具有单个控制放大器和多个输出级的电流放大器。 所需的输出级数字选择。 可以在金属化处理期间选择输出级电流的比率。 单个电容器补偿所有输出级,无论选择哪个输出级。

    Heart valve prosthesis
    7.
    发明授权
    Heart valve prosthesis 失效
    心脏瓣膜假体

    公开(公告)号:US4297749A

    公开(公告)日:1981-11-03

    申请号:US125121

    申请日:1980-02-27

    IPC分类号: A61F2/24 A61F1/22

    摘要: A frame system for heart valve prosthesis. A first frame has at least three generally parallel legs each comprising a pair of rod portions connected at one end and diverging at the other end as lobes respectively connecting with rod portions of others of said legs. The lobes form an aperture therebetween and the legs are adapted to receive the margin of a valve leaflet between the rod portions thereof. Thus, the leaflet may be secured to two adjacent legs and the interconnecting lobe so as to have a free edge extending between said adjacent legs. A second frame is adapted to nest with the first frame and comprises a rod formed to be substantially congruent with the interconnecting lobes, whereby the leaflets may be secured to and between the frames.

    摘要翻译: 心脏瓣膜假体的框架系统。 第一框架具有至少三个大致平行的腿,每个腿包括一对杆部分,该杆部分在一端连接并且在另一端处以分别与所述腿部中的其他杆的杆部分连接的凸起分开。 叶片在它们之间形成孔,并且腿部适于在其杆部之间容纳瓣膜小叶的边缘。 因此,小叶可以固定到两个相邻的腿和互连瓣,以便具有在所述相邻腿之间延伸的自由边缘。 第二框架适于与第一框架嵌套并且包括形成为与互连凸角基本一致的杆,由此传单可以固定到框架之间并且在框架之间。

    Method of fabricating a hollow filament separator module
    8.
    发明授权
    Method of fabricating a hollow filament separator module 失效
    制造中空丝分离器模块的方法

    公开(公告)号:US4220489A

    公开(公告)日:1980-09-02

    申请号:US956032

    申请日:1978-10-30

    摘要: A hollow filament separatory module utilizing an annulus of semi-permeable hollow filaments with open ends encased in a potting compound and a collection chamber communicating with said open ends adjacent the potting compound with access surface means formed in the potting compound wherein the open ends appear, said filaments having ends thereof encapsulated by the introduction of potting medium into the interfilament interstices under the urging of vibratory energy and thereafter creating said open ends by cutting of ends and potting medium at a time in the curring cycle of the potting compound prior to its final cure.

    摘要翻译: 一种中空丝分离模块,其利用封闭在灌封化合物中的开放端部的半透空心细丝的环形空间,以及与封闭化合物相邻的所述开口端连通的收集室,其中形成在灌封化合物中的入口表面装置, 所述长丝的端部通过在振动能量的推动下将灌封介质引入到间隙间隙中而封装,然后通过在灌封混合物的最终卷绕循环之前一次切割端部和灌封介质来形成所述开口端 治愈。

    Orifice sealing physical barrier
    9.
    发明授权
    Orifice sealing physical barrier 失效
    孔眼密封物理屏障

    公开(公告)号:US06708979B2

    公开(公告)日:2004-03-23

    申请号:US09992365

    申请日:2001-11-19

    IPC分类号: F16J1502

    CPC分类号: B62D25/24 Y10S277/931

    摘要: The present invention is a physical barrier for an orifice in a panel member which includes a plastic carrier and a patch adapted to adhere to said carrier and the panel member. The present invention also includes a method of sealing an orifice in a metal panel member with a plastic carrier. Lastly, the present invention includes a thermoplastic which adheres to both plastic and metal upon the application of heat.

    摘要翻译: 本发明是用于面板构件中的孔的物理屏障,其包括塑料载体和适于粘附到所述载体和面板构件的贴片。 本发明还包括一种用塑料载体密封金属板构件中的孔口的方法。 最后,本发明包括在施加热时粘附于塑料和金属的热塑性塑料。

    Process for cooling and fluidizing
    10.
    发明授权
    Process for cooling and fluidizing 失效
    冷却和流化工艺

    公开(公告)号:US4422302A

    公开(公告)日:1983-12-27

    申请号:US404762

    申请日:1982-08-03

    CPC分类号: B01J8/1836 F17C9/02 F25D3/10

    摘要: In a process for cooling and fluidizing a bed of particles by passing a cryogen through the bed, said bed being first cooled to a desired operating temperature, the improvement comprising:(a) admixing a liquid cryogen and an inert gas, said gas being at ambient temperature, at a point external, but proximate, to the bed to provide a mixture of liquid cryogen and gas at a temperature sufficiently low to maintain the bed at about the desired operating temperature;(b) introducing the mixture from step (a) into at least two heat transfer coils connected in parallel and located in the bed whereby the desired operating temperature is imparted to the bed, and the liquid cryogen in the mixture vaporizes; and(c) removing the mixture of vaporized liquid cryogen and gas formed in step (b) from the coils and introducing the mixture into the bed to fluidize the bed.

    摘要翻译: 在通过使冷冻剂通过床来冷却和流化颗粒床的过程中,所述床首先被冷却到所需的操作温度,改进包括:(a)混合液体冷冻剂和惰性气体,所述气体处于 环境温度,在外部但接近于床处,以在足够低的温度下提供液体冷冻剂和气体的混合物,以将床保持在大约所需的操作温度; (b)将来自步骤(a)的混合物引入平行连接并位于床中的至少两个热传递线圈,由此将所需的操作温度赋予床,混合物中的液体致冷剂蒸发; 和(c)从线圈中除去蒸发的液体冷冻剂和步骤(b)中形成的气体的混合物,并将混合物引入床中以使床流化。