公开(公告)号：US06413391B1

公开(公告)日：2002-07-02

申请号：US09700784

申请日：2000-11-20

申请人： Stephen A Wilson ,  John A Billington ,  Peter May

发明人： Stephen A Wilson ,  John A Billington ,  Peter May

IPC分类号： C25D1704

CPC分类号： C25D17/08 ,  C25D5/02

摘要： Apparatus for metal plating an article comprising a frame having a plurality of sealing members positioned thereon, the frame being capable of conducting an electrical current between sealing members, each sealing member being adapted to be in close contact with part of an article to be located thereon, and to thereby substantially prevent fluid from touching that part of the article or entering into a bore or recess of the article, each sealing member further being adapted to conduct current between the frame and the article.

摘要翻译： 一种用于金属电镀物品的设备，包括具有定位在其上的多个密封构件的框架，所述框架能够在密封构件之间传导电流，每个密封构件适于与要位于其上的制品的一部分紧密接触 并且由此基本上防止流体接触制品的该部分或进入制品的孔或凹部，每个密封构件还适于在框架和制品之间传导电流。

公开(公告)号：US08170052B2

公开(公告)日：2012-05-01

申请号：US11577815

申请日：2005-10-25

申请人： Georgios Orfanos ,  Francesc Dalmases ,  Joerg Habetha ,  Begonya Otal ,  Peter May

发明人： Georgios Orfanos ,  Francesc Dalmases ,  Joerg Habetha ,  Begonya Otal ,  Peter May

IPC分类号： H04L12/43

CPC分类号： H04W72/02 ,  H04W74/0816

摘要： A method of operating a network node of a network, a network node, a network system, a computer-readable medium, and a program element A method (300) of operating a network node (101-104) of a network system (100), comprising the steps of generating (305) a signal to be transmitted, selecting (310) one of a plurality of communication channels (105-108) of the network system (100) for transmitting the signal, and, in case that the selected channel (105-108) is not ready for transmitting the signal, selecting (345) another one of the plurality of communication channels (105-108) for transmitting the signal.

摘要翻译： 一种操作网络的网络节点的方法，网络节点，网络系统，计算机可读介质和节目元素操作网络系统（100）的网络节点（101-104）的方法（300） ），包括以下步骤：产生（305）要发送的信号，选择（310）所述网络系统（100）的多个通信信道（105-108）中的一个用于发送所述信号，并且在 选择信道（105-108）未准备好发送信号，选择（345）多个通信信道（105-108）中的另一个用于发送信号。

公开(公告)号：US20070006645A1

公开(公告)日：2007-01-11

申请号：US11316151

申请日：2005-12-22

申请人： Detlev Schwetzler ,  Peter May

发明人： Detlev Schwetzler ,  Peter May

IPC分类号： G01P13/00

CPC分类号： G01M9/06 ,  G01M9/062

摘要： The present invention relates to a method for improving the precision of wind tunnel measurements, particularly to correct the influence of a suspension device, wherein a model, particularly an aircraft model, being introduced into a wind tunnel on the suspension device, which has multiple suspension wires, and at least one sleeve being attached to each suspension wire, having the following steps: performing at least two measurements with identical model configuration with at least one effective diameter and/or with the suspension wire diameter in each case to ascertain at least two raw measured values and ascertaining a corrected final measured value for the model from at least two measured values. According to a first embodiment variation of the method according to the present invention, for example, in the course of detecting raw measured values of the air resistance coefficient of the model, the effective diameter of the suspension wires is reduced in at least three steps by removing sleeves which have been pushed on. A final measured value of the air resistance coefficient, which has been corrected for the influence of the suspension device and the interference between model and suspension device, may be ascertained from the raw measured values through interpolation. According to a further variation, the correction is performed through difference calculation of only two raw measured values, one of the raw measured values being ascertained with the suspension wire diameter without sleeves pushed on. The method is suitable for correcting all aerodynamic characteristic variables measurable in the wind tunnel. Furthermore, the present invention relates to a device for performing the method.

摘要翻译： 本发明涉及一种用于提高风洞测量精度的方法，特别是用于校正悬挂装置的影响的方法，其中将模型，特别是飞行器模型引入到具有多个悬架的悬挂装置上的风洞中 线和至少一个套筒连接到每个悬挂线，具有以下步骤：在具有至少一个有效直径和/或每种情况下的悬挂线直径的情况下执行具有相同模型构造的至少两个测量以确定至少两个 原始测量值，并从至少两个测量值确定模型的校正最终测量值。 根据本发明的方法的第一实施方式的变形例，例如，在检测模型的空气阻力系数的原始测量值的过程中，悬挂线的有效直径在至少三个步骤中通过 去除被推上的袖子。 可以从原始测量值通过插值确定已经针对悬挂装置的影响进行校正的空气阻力系数的最终测量值和模型和悬挂装置之间的干扰。 根据进一步的变化，通过仅计算两个原始测量值的差分计算来执行校正，其中一个原始测量值用悬挂线直径确定，而没有套筒被推开。 该方法适用于校正风洞中可测量的所有空气动力学特征变量。 此外，本发明涉及一种用于执行该方法的装置。

公开(公告)号：US07070148B2

公开(公告)日：2006-07-04

申请号：US10713161

申请日：2003-11-17

申请人： Susanne Wyrembek ,  Peter May ,  Klaus Muthreich

发明人： Susanne Wyrembek ,  Peter May ,  Klaus Muthreich

IPC分类号： B64C9/32

CPC分类号： B64C9/32 ,  B64C9/323 ,  B64C23/076 ,  Y02T50/164

摘要： An aerodynamic including a main body and a control member. The main body is configured to be connected to a wing of an aircraft. The control member is connected to the main body, the control member including a fixed member secured to the main body and a pivotable member configured to increase a drag of the aircraft without substantially changing a lift of the aircraft.

摘要翻译： 包括主体和控制构件的空气动力学。 主体被配置为连接到飞机的翼。 控制构件连接到主体，控制构件包括固定到主体的固定构件和可枢转构件，其构造成增加飞行器的阻力，而基本上不改变飞行器的升力。

公开(公告)号：US06364254B1

公开(公告)日：2002-04-02

申请号：US09523421

申请日：2000-03-10

申请人： Peter May

发明人： Peter May

IPC分类号： B64C922

CPC分类号： B64C9/24 ,  B64C7/00 ,  B64C9/36

摘要： An arrangement of an airfoil, such as a main wing of an aircraft, includes a close-mounted engine on a short pylon connected to the airfoil, an inboard slat arranged inboard from the engine pylon along the leading edge of the airfoil, and an auxiliary high lift device. An open cut-out space is formed between the outboard edge of the inboard slat, the engine pylon, and the leading edge of the airfoil when the inboard slat is extended. The auxiliary high lift device is configured and arranged to be extendable into an extended position in which it aerodynamically covers or closes the cut-out space. The auxiliary high lift device is a movable high lift component that can be retracted into a retracted position in which it is recessed and integrated into the outer contour of the engine nacelle and/or the pylon. Thereby, the structural arrangement and mechanisms necessary for extending and retracting the auxiliary high lift device are simplified, and the weight and costs are reduced.

摘要翻译： 诸如飞机的主翼的机翼的布置包括连接到翼型件的短塔上的紧密搭载的发动机，沿着翼型的前缘从发动机塔架排列的内侧板条，以及辅助 高升降装置。 当内侧板条延伸时，在内侧板条的外侧边缘，发动机塔架和翼型的前缘之间形成开放的切割空间。 辅助高升降装置被构造和布置成可延伸到延伸位置，空间动力学地覆盖或关闭切除空间。 辅助高升力装置是可移动的高升力部件，其可以缩回到缩回位置，在该缩回位置中它被凹入并且集成到发动机舱和/或塔架的外轮廓中。 因此，简化了辅助高升降装置的伸缩所需的结构布置和机构，并且减轻了重量和成本。