MAINTENANCE CYCLE FOR AN AIRCRAFT
    2.
    发明申请
    MAINTENANCE CYCLE FOR AN AIRCRAFT 审中-公开
    飞机的维护周期

    公开(公告)号:US20130173480A1

    公开(公告)日:2013-07-04

    申请号:US13690674

    申请日:2012-11-30

    IPC分类号: G06Q10/00

    CPC分类号: G06Q10/20 G06Q10/04 Y02P90/86

    摘要: The invention relates to a maintenance cycle for an aircraft, which comprises the steps a) carrying out a maintenance process for an aircraft after the expiry of a time interval (ΔT) which is less than or equal to a specified maintenance interval (ΔTW); b) collecting findings data for at least one maintenance measure during the maintenance process; c) archiving the findings data from step b) and the time interval ΔT; d) determining at least one classification number using automated statistical evaluation of archived findings data for all maintenance processes occurring within a first observation period and/or using the averaged utilization factor (G) of the maintenance interval for a second observation period, wherein the first observation period and the second observation period can be the same or different and e) producing an action request for checking and/or adaptation of the maintenance interval as long as the at least one classification number from step d) lies outside a specified tolerance range. The invention also relates to a method for assessing and/or monitoring of a maintenance program for aircraft, a method for the comparison of at least two maintenance programs for aircraft, an apparatus for checking and/or adaptation of a maintenance interval for an aircraft and a signal sequence.

    摘要翻译: 本发明涉及飞机的维护周期,其包括以下步骤:a)在小于或等于指定维护间隔(DeltaTW)的时间间隔(DeltaT)期满之后对飞行器进行维护处理; b)在维护过程中收集至少一个维护措施的结果数据; c)归档来自步骤b)和时间间隔DeltaT的发现数据; d)使用在第一观察期间内发生的所有维护过程的归档发现数据的自动统计评估和/或使用第二观察周期的维护间隔的平均利用因子(G))来确定至少一个分类号,其中第一 观察期间和第二观察期间可以相同或不同,e)只要来自步骤d)的至少一个分类号位于指定的公差范围之外,则产生检查和/或调整维护间隔的动作请求。 本发明还涉及一种用于评估和/或监视飞行器维护程序的方法,用于比较飞机的至少两个维护程序的方法,用于检查和/或改装飞机的维护间隔的装置,以及 信号序列。

    Method and apparatus for cleaning a jet engine
    3.
    发明申请
    Method and apparatus for cleaning a jet engine 有权
    用于清洁喷气发动机的方法和装置

    公开(公告)号:US20100000572A1

    公开(公告)日:2010-01-07

    申请号:US12433411

    申请日:2009-04-30

    IPC分类号: B08B7/00

    摘要: An apparatus for cleaning a jet engine includes a supply device configured to make cleaning medium available, a nozzle device configured to introduce the cleaning medium into the jet engine, and a line connection between the supply device and the nozzle device. The cleaning medium can be solid carbon dioxide. A system including a jet engine and the apparatus. A method for cleaning a jet engine using solid carbon dioxide.

    摘要翻译: 一种用于清洁喷气发动机的装置,包括配置成使清洗介质可用的供给装置,被构造成将清洁介质引入喷气发动机中的喷嘴装置,以及供应装置和喷嘴装置之间的管线连接。 清洁介质可以是固体二氧化碳。 一种包括喷气发动机和装置的系统。 一种使用固体二氧化碳清洗喷气发动机的方法。

    Circuit configuration and a method for the testing of storage cells
    4.
    发明授权
    Circuit configuration and a method for the testing of storage cells 失效
    电路配置和存储单元测试方法

    公开(公告)号:US4896322A

    公开(公告)日:1990-01-23

    申请号:US168676

    申请日:1988-03-16

    CPC分类号: G11C29/38 G11C29/36

    摘要: In a circuit configuration and a method for testing storage cells, all of the bit lines lead to one pair of fault lines which is first precharged with mutually-complementary logic levels. All of the storage cells of a word line are always read-out in parallel relative to one another. In the event of "no fault" the pair of fault lines retains its logic states, whereas in the case of a fault one of the fault lines changes its logic state through switching transistors. This is recognized and analyzed by a comparator circuit in the form of an XOR-circuit or an XNOR-circuit.

    摘要翻译: 在用于测试存储单元的电路配置和方法中,所有位线都导致一对故障线,其首先被预充电互补的逻辑电平。 字线的所有存储单元总是相对于彼此并行读出。 在“无故障”的情况下,该对故障线保持其逻辑状态,而在故障的情况下,故障线之一通过开关晶体管改变其逻辑状态。 这是由XOR电路或XNOR电路形式的比较器电路识别和分析的。

    Arrangement for determining the pressure in an undercarriage tyre of an aircraft
    5.
    发明授权
    Arrangement for determining the pressure in an undercarriage tyre of an aircraft 失效
    确定飞机底盘轮胎压力的布置

    公开(公告)号:US08375781B2

    公开(公告)日:2013-02-19

    申请号:US12818027

    申请日:2010-06-17

    IPC分类号: G01P13/00

    CPC分类号: G01L17/005

    摘要: The subject matter of the invention is an arrangement for determining the pressure in an undercarriage tire of an aircraft, which arrangement has a measurement matrix (1) with a plurality of load sensors which are arranged in an area over which the aircraft tire can roll. The invention provides that the arrangement is designed to measure the pressure difference between two or more undercarriage tires.

    摘要翻译: 本发明的主题是用于确定飞机的底盘轮胎中的压力的​​装置,该装置具有测量矩阵(1),该测量矩阵具有布置在飞机轮胎能够滚动的区域中的多个负载传感器。 本发明提供了该装置被设计成测量两个或多个起落架轮胎之间的压力差。

    Method and apparatus for cleaning a jet engine
    6.
    发明授权
    Method and apparatus for cleaning a jet engine 有权
    用于清洁喷气发动机的方法和装置

    公开(公告)号:US08109807B2

    公开(公告)日:2012-02-07

    申请号:US12433411

    申请日:2009-04-30

    IPC分类号: B24B41/00

    摘要: An apparatus for cleaning a jet engine includes a supply device configured to make cleaning medium available, a nozzle device configured to introduce the cleaning medium into the jet engine, and a line connection between the supply device and the nozzle device. The cleaning medium can be solid carbon dioxide. A system including a jet engine and the apparatus. A method for cleaning a jet engine using solid carbon dioxide.

    摘要翻译: 一种用于清洁喷气发动机的装置,包括配置成使清洗介质可用的供给装置,被构造成将清洁介质引入喷气发动机中的喷嘴装置,以及供应装置和喷嘴装置之间的管线连接。 清洁介质可以是固体二氧化碳。 一种包括喷气发动机和装置的系统。 一种使用固体二氧化碳清洗喷气发动机的方法。

    Process for the model-supported simulation of the coolant temperature in
the case of a vehicle based on initially measured conditions
    7.
    发明授权
    Process for the model-supported simulation of the coolant temperature in the case of a vehicle based on initially measured conditions 失效
    基于初始测量条件,在车辆情况下对模型支持的模拟冷却液温度的过程

    公开(公告)号:US6086248A

    公开(公告)日:2000-07-11

    申请号:US884670

    申请日:1997-06-27

    CPC分类号: G01K7/42 F01P11/16

    摘要: A process for the model-supported simulation of the coolant temperature in the case of a vehicle is provided. Conventionally, two temperature sensors are used for determining the coolant temperature, in which case one exists only for determining the temperature when an engine is switched off. Such an additional sensor is cost-intensive and should be avoided. The process avoids using an additional sensor by detecting the coolant temperature at the point in time of the switching-off of the driving engine. A current coolant temperature is continuously calculated while including vehicle-specific data using a temperature model. As an alternative, the current coolant temperature is not continuously calculated, but rather is calculated from a point in time as of which a theoretically determined coolant temperature falls below a specific value.

    摘要翻译: 提供了在车辆的情况下用于模型支持的模拟冷却剂温度的过程。 通常,使用两个温度传感器来确定冷却剂温度,在这种情况下仅存在用于确定发动机关闭时的温度。 这种额外的传感器是成本密集型的​​,应该避免。 该过程通过检测在驱动发动机关闭的时间点处的冷却剂温度来避免使用额外的传感器。 在使用温度模型包括车辆特定数据的同时连续地计算当前的冷却剂温度。 作为替代,目前的冷却剂温度不是连续计算的,而是从理论上确定的冷却剂温度低于特定值的时间点计算。

    ARRANGEMENT FOR DETERMINING THE PRESSURE IN AN UNDERCARRIAGE TYRE OF AN AIRCRAFT
    10.
    发明申请
    ARRANGEMENT FOR DETERMINING THE PRESSURE IN AN UNDERCARRIAGE TYRE OF AN AIRCRAFT 失效
    确定航空器承包轮胎压力的安排

    公开(公告)号:US20110185802A1

    公开(公告)日:2011-08-04

    申请号:US12818027

    申请日:2010-06-17

    IPC分类号: B60C23/02

    CPC分类号: G01L17/005

    摘要: The subject matter of the invention is an arrangement for determining the pressure in an undercarriage tyre of an aircraft, which arrangement has a measurement matrix (1) with a plurality of load sensors which are arranged in an area over which the aircraft tyre can roll. The invention provides that the arrangement is designed to measure the pressure difference between two or more undercarriage tyres.

    摘要翻译: 本发明的主题是用于确定飞机的底盘轮胎中的压力的​​装置,该装置具有测量矩阵(1),该测量矩阵具有布置在飞机轮胎能够滚动的区域中的多个负载传感器。 本发明提供了该装置被设计成测量两个或多个起落架轮胎之间的压力差。