Fuel supply system
    5.
    发明授权
    Fuel supply system 失效
    燃油供应系统

    公开(公告)号:US5660358A

    公开(公告)日:1997-08-26

    申请号:US395677

    申请日:1995-02-28

    摘要: Fuel supply system for multijet airplanes using cryogenic fuel with one tank or one tank group for each engine or for all engines on one side of the longitudinal central plane of the airplane, and, if desired, with an additional, common tank or an additional, common tank group for all engines. A transfer line with shut-off valve leads from each tank/tank group associated with a defined engine or with the engines of one side of the airplane to at least one other tank/tank group and/or, if desired, to the tank/tank group common to all engines. If desired, at least one transfer line leads from the common tank/tank group to at least one other tank/tank group.

    摘要翻译: 用于使用低温燃料的多喷气机的燃料供应系统,每个发动机具有一个罐或一个罐组,或者用于在飞机的纵向中心平面的一侧上的所有发动机,并且如果需要,使用附加的公共罐或附加的, 所有发动机的普通坦克组。 具有截止阀的传输线从与定义的发动机相关联的每个罐/罐组引导,或与飞机的一侧的发动机连接至至少另一个罐/罐组,和/或如果需要, 坦克组通用于所有发动机。 如果需要,至少一条输送管线从公共罐/罐组引导到至少另一个罐/罐组。

    Method for Producing an Organic Electronic Component, and Organic Electronic Component
    6.
    发明申请
    Method for Producing an Organic Electronic Component, and Organic Electronic Component 审中-公开
    有机电子元件的制造方法和有机电子元件

    公开(公告)号:US20110070456A1

    公开(公告)日:2011-03-24

    申请号:US12922833

    申请日:2009-06-17

    IPC分类号: B32B37/14 B32B27/32

    摘要: A method for producing an organic electronic component comprises, in particular, the following steps: A) producing at least one functional layer stack (10) with the following substeps: A1) providing a flexible first substrate (1), A2) applying at least one organic layer (2) in large-area fashion on the first substrate (1) by means of a coil coating plant (90), and A3) singulating the first substrate (1) with the at least one organic layer (2) into a plurality of functional layer stacks (10); B) providing a second substrate (5), which has a lower flexibility and a higher impermeability with respect to moisture and oxygen than the first substrate (1); and C) applying the at least one of the plurality of the functional layer stacks (10) with a surface (11) of the first substrate (1) remote from the organic layer (2) on the second substrate (5).

    摘要翻译: 一种制造有机电子部件的方法特别包括以下步骤:A)产生具有以下子步骤的至少一个功能层堆叠(10):A1)提供柔性第一基板(1),A2)至少施加 一个有机层(2)以大面积方式通过线圈涂覆设备(90)在第一基底(1)上,以及A3)将具有至少一个有机层(2)的第一基底(1)分成 多个功能层堆叠(10); B)提供第二衬底(5),其具有比第一衬底(1)更低的柔性和相对于水分和氧气的更高的不渗透性; 以及C)将所述多个所述功能层堆叠(10)中的所述至少一个与所述第一基板(1)的远离所述有机层(2)的表面(11)施加在所述第二基板(5)上。

    Method and device for the continuous polycondensation of polyester material in the solid phase
    7.
    发明授权
    Method and device for the continuous polycondensation of polyester material in the solid phase 有权
    聚酯材料在固相中连续缩聚的方法和装置

    公开(公告)号:US07884177B2

    公开(公告)日:2011-02-08

    申请号:US10470988

    申请日:2001-02-26

    IPC分类号: C08G63/80 C08G63/88 C08F6/26

    摘要: The invention relates to a method and device for the continuous polycondensation of polyester material in the solid phase, in particular in the form of partially crystalline granulate. The aim of the invention is to achieve a high product throughput on recrystallising and recondensation of polyester material with a low initial IV. Said aim is achieved, whereby on recrystallisation, a low residence time of 1-10 minutes is achieved, by means of a rapid heating of a thin product layer, followed by an SSP treatment.

    摘要翻译: 本发明涉及一种在固相中聚酯材料的连续缩聚,特别是部分结晶颗粒形式的方法和装置。 本发明的目的是在初始IV低的聚酯材料的重结晶和再缩合中实现高产品生产量。 实现所述目的,由此在再结晶时,通过快速加热薄的产物层,随后进行SSP处理,实现1-10分钟的低停留时间。

    SYSTEM AND METHOD FOR MODELING OF TURBO-CHARGED ENGINES AND INDIRECT MEASUREMENT OF TURBINE AND WASTE-GATE FLOW AND TURBINE EFFICIENCY
    8.
    发明申请
    SYSTEM AND METHOD FOR MODELING OF TURBO-CHARGED ENGINES AND INDIRECT MEASUREMENT OF TURBINE AND WASTE-GATE FLOW AND TURBINE EFFICIENCY 失效
    涡轮增压发动机的建模系统和方法以及涡轮机和废气流量和涡轮机效率的间接测量

    公开(公告)号:US20090094009A1

    公开(公告)日:2009-04-09

    申请号:US11867422

    申请日:2007-10-04

    申请人: Martin Muller

    发明人: Martin Muller

    IPC分类号: G06G7/48

    摘要: A real-time system for modeling a turbo-charged engine includes a model configured to estimate various exhaust states such as turbine inlet pressure, turbine outlet pressure, turbine outlet temperature, turbine mass flow rate and waste-gate valve mass flow rate. The model is dependent only on the availability of normal operating values available in a conventionally-configured automotive controller and one or more measured intake side parameters such as ambient pressure, boost pressure, ambient temperature and compressor mass flow rate. The model is constructed to reflect a high-level application of energy conservation between the turbine (generated power) and compressor (absorbed power). A method for the indirect measurement of turbine and waste-gate flow uses turbine inlet and outlet pressure, inlet temperature and engine mass air flow rate measurements. A method for the indirect measurement of turbine efficiency avoids the need for manufacturer's turbine data.

    摘要翻译: 用于对涡轮增压发动机进行建模的实时系统包括被配置为估计各种排气状态的模型,例如涡轮进口压力,涡轮出口压力,涡轮出口温度,涡轮质量流量和废气门阀质量流量。 该模型仅取决于常规配置的汽车控制器中可用的正常工作值的可用性以及一个或多个测量的进气侧参数,例如环境压力,增压压力,环境温度和压缩机质量流量。 该模型被构造为反映在涡轮(发电)和压缩机(吸收功率)之间的节能的高水平应用。 用于间接测量涡轮机和废气门流量的方法使用涡轮机入口和出口压力,入口温度和发动机质量空气流量测量。 用于间接测量涡轮机效率的方法避免了制造商的涡轮数据的需要。