Method and device for activating an automatic piloting mode of an aircraft
    1.
    发明授权
    Method and device for activating an automatic piloting mode of an aircraft 有权
    用于激活飞行器的自动驾驶模式的方法和装置

    公开(公告)号:US08478458B2

    公开(公告)日:2013-07-02

    申请号:US12785173

    申请日:2010-05-21

    IPC分类号: G05D1/00

    CPC分类号: G08G5/025 G05D1/0061

    摘要: A method and a device for activating an automatic piloting mode of an aircraft are disclosed. The device can include means for engaging an automatic pilot mode, when (i) the current distance of the aircraft with respect to a reference position on the ground belongs to a determined distance range, and (ii) the current height of the aircraft is at most equal to a reference height associated to the automatic pilot mode.

    摘要翻译: 公开了一种用于激活飞行器的自动驾驶模式的方法和装置。 当(i)飞机相对于地面上的参考位置的当前距离属于确定的距离范围时,该装置可以包括用于接合自动驾驶员模式的装置,以及(ii)飞行器的当前高度在 最相等于与自动导航模式相关的参考高度。

    METHOD AND DEVICE FOR ACTIVATING AN AUTOMATIC PILOTING MODE OF AN AIRCRAFT
    2.
    发明申请
    METHOD AND DEVICE FOR ACTIVATING AN AUTOMATIC PILOTING MODE OF AN AIRCRAFT 有权
    用于激活飞机自动起飞模式的方法和装置

    公开(公告)号:US20100305785A1

    公开(公告)日:2010-12-02

    申请号:US12785173

    申请日:2010-05-21

    IPC分类号: G05D1/04 G01S19/51

    CPC分类号: G08G5/025 G05D1/0061

    摘要: A method and a device for activating an automatic piloting mode of an aircraft are disclosed. The device can include means for engaging an automatic pilot mode, when (i) the current distance of the aircraft with respect to a reference position on the ground belongs to a determined distance range, and (ii) the current height of the aircraft is at most equal to a reference height associated to the automatic pilot mode.

    摘要翻译: 公开了一种用于激活飞行器的自动驾驶模式的方法和装置。 当(i)飞机相对于地面上的参考位置的当前距离属于确定的距离范围时,该装置可以包括用于接合自动驾驶员模式的装置,以及(ii)飞行器的当前高度在 最相等于与自动导航模式相关的参考高度。

    Blasting device
    4.
    发明申请
    Blasting device 失效
    爆破装置

    公开(公告)号:US20080295557A1

    公开(公告)日:2008-12-04

    申请号:US12082434

    申请日:2008-04-11

    IPC分类号: C21D7/06

    CPC分类号: B24C1/10 B24C1/04

    摘要: Disclosed is a blasting device for blasting a part of a turbine blade, which has a blade root, a blade platform and a blade airfoil, with a blasting cubicle, which has an insertion opening, a blasting unit for the discharge of accelerated blasting media into the blasting cubicle, and a mounting for the turbine blade, wherein a seal is provided, which seals a gap between the mounting and the blade airfoil in the region of the insertion opening and so prevents the escape of dust, which is created when blasting, from the blasting cubicle, and wherein the seal seals the gap from the inner side of the cubicle.

    摘要翻译: 公开了一种用于喷射具有叶片根部,叶片平台和叶片翼型的涡轮叶片的一部分的爆破装置,其具有插入开口,用于将加速的爆破介质排出的爆破单元 爆破隔间和用于涡轮叶片的安装件,其中设置有密封件,其在插入开口的区域中密封安装件和叶片翼型件之间的间隙,并且因此防止当喷砂时产生的灰尘逸出, 并且其中所述密封件将所述间隙与所述隔间的内侧密封。

    Cathodic sputtering targets made of aluminum alloy
    5.
    发明授权
    Cathodic sputtering targets made of aluminum alloy 有权
    由铝合金制成的阴极溅射靶

    公开(公告)号:US06264813B1

    公开(公告)日:2001-07-24

    申请号:US09417888

    申请日:1999-10-14

    IPC分类号: C23C1434

    CPC分类号: C23C14/3414 C22C21/00

    摘要: The invention concerns a cathode pulverization target characterized in that its active part, i.e. the volume of the target capable of being removed during the cathode pulverization, consists of a high purity aluminum alloy simultaneously containing copper and iron and having simultaneously a recrystallization temperature well above 20° C. and an electric resistivity less than 2.85 &mgr;&OHgr;.cm at 20° C. The use of the target for making bonding circuits reduces the frequency at which voids and hillocks appear, while maintaining the resistance of the bonding circuits at values comparable to the resistance obtained with a high purity aluminum alloy, while also providing the etching characteristics comparable to those of high purity aluminum alloy.

    摘要翻译: 本发明涉及一种阴极粉碎目标,其特征在于其活性部分即在阴极粉碎期间能够除去的靶的体积由同时含有铜和铁的高纯度铝合金组成,同时重结晶温度远高于20℃ °C,电阻率在20°C时小于2.85μOMEGA.cm。使用制造接合电路的目标降低了出现空隙和小丘的频率,同时保持接合电路的电阻值与 由高纯度铝合金获得的电阻,同时还提供与高纯度铝合金相当的蚀刻特性。

    Cathode sputtering targets with a low level of particle emission,
precursors of these targets, and processes for obtaining them
    6.
    发明授权
    Cathode sputtering targets with a low level of particle emission, precursors of these targets, and processes for obtaining them 失效
    具有低水平颗粒排放的阴极溅射靶,这些靶的前体,以及获得它们的方法

    公开(公告)号:US5887481A

    公开(公告)日:1999-03-30

    申请号:US762415

    申请日:1996-12-09

    摘要: A process is provided for ultrasonic testing the internal soundness of cathode sputtering targets including an active part made of very pure aluminum or of very pure aluminum alloy. In particular, this process, after the choice of an ultrasound sensor functioning at an operating frequency greater than 5 MHZ, and preferably between 10 and 50 MHZ, and adjustment of the appropriate measurement sequence, using a target immersed in a liquid and having certain artificial defects simulating the decohesions in the target, consists of taking a count in terms of size and number of the internal decohesions per unit volume and of selecting the targets with a decohesion density of .ltoreq.0.1 decohesion larger than 0.1 mm per cm.sup.3 of active metal of the targets, and preferably less than 0.1 decohesion larger than 0.04 mm per cm.sup.3 of active metal. The process also pertains to selecting precursors of the cathode sputtering targets, containing less than 0.1 internal decohesion larger than 0.04 mm per cm.sup.3.

    摘要翻译: 提供了一种用于超声波测试阴极溅射靶的内部健全性的方法,包括由非常纯的铝或非常纯的铝合金制成的活性部分。 特别地,该过程在超声波传感器选择工作频率大于5MHZ,优选10-50MZZ之间,并且调整适当的测量顺序之后,使用浸没在液体中并具有某些人造 模拟目标中的解吸的缺陷包括对每单位体积的内部解吸量的大小和数量进行计数,并且选择具有大于0.1mm / cm 3活性金属的解吸密度

    Automatic method and device for aiding the piloting of an airplane
    7.
    发明授权
    Automatic method and device for aiding the piloting of an airplane 有权
    用于辅助飞机驾驶的自动方法和装置

    公开(公告)号:US08695921B2

    公开(公告)日:2014-04-15

    申请号:US13113632

    申请日:2011-05-23

    IPC分类号: B64C13/18 G05D1/04

    CPC分类号: G05D1/0077

    摘要: A method of aiding the piloting of an airplane ensures the availability of an automatic pilot and a thrust regulation system on board the airplane. To this end, the method includes determining first information by measuring the actual airspeed of the airplane, and this first information is used to control the automatic pilot and the thrust regulation system in a primary mode during normal operations of the airplane. When the first information is lost by becoming unavailable or unreliable, the automatic pilot and the thrust regulation system are each controlled in a secondary mode by control parameters determined using additional flight data independent from the actual airspeed of the airplane and the first information. Consequently, an alternative or redundant control is supplied for ensuring the continued operation of an automatic pilot without necessary intervention from crew members on board the airplane.

    摘要翻译: 协助飞机驾驶的方法确保飞机上的自动飞行员和推力调节系统的可用性。 为此,该方法包括通过测量飞机的实际空速来确定第一信息,并且该第一信息用于在飞机的正常操作期间以主模式控制自动驾驶员和推力调节系统。 当第一信息由于变得不可用或不可靠而丢失时,通过与独立于飞机的实际空速和第一信息的附加飞行数据确定的控制参数,自动驾驶和推力调节系统各自被控制在次级模式。 因此,提供替代或冗余控制以确保自动飞行员的持续操作,而不需要飞机上的乘务员进行必要的干预。

    Method and device for driving an aircraft during the ground run thereof
    8.
    发明授权
    Method and device for driving an aircraft during the ground run thereof 有权
    在地面运行中驾驶飞行器的方法和装置

    公开(公告)号:US07967247B2

    公开(公告)日:2011-06-28

    申请号:US11917304

    申请日:2006-06-12

    IPC分类号: B64C25/42 G05D1/02

    CPC分类号: B64C13/02 B64C25/48

    摘要: The method of the invention includes forming a difference between left and right braking commands, by converting the difference into an additional control command for rudder and for a steerable nose gear, and applying the additional control command to the rudder and steerable nose gear according to both of the following conditions: the difference is greater than a first threshold and the combined control command transmitted to the rudder and steerable nose gear by a rudder bar is less than a second threshold.

    摘要翻译: 本发明的方法包括:通过将差值转换为方向舵和可转向前档的附加控制指令,形成左右制动指令之间的差异,并将附加控制指令应用于舵和可转向前档 的差异大于第一阈值,并且通过舵杆传送到舵和可转向前档的组合控制命令小于第二阈值。

    Method and Device for Driving an Aircraft During the Ground Run Thereof
    9.
    发明申请
    Method and Device for Driving an Aircraft During the Ground Run Thereof 有权
    在地面运行期间驾驶飞机的方法和装置

    公开(公告)号:US20080197239A1

    公开(公告)日:2008-08-21

    申请号:US11917304

    申请日:2006-06-12

    IPC分类号: B64C13/02 G05D1/00

    CPC分类号: B64C13/02 B64C25/48

    摘要: The inventive method consists in forming a difference (D1) between left and right braking commands (FG, FD), in converting said difference (D1) into an additional control command (D2) for rudder (16) and for a steerable nose gear (4) and in applying said additional control command (D2) to said rudder (16) and steerable nose gear (4) according to both following conditions: the difference (D1) is greater than a first threshold and the combined control command transmitted to the rudder and steerable nose gear (4) by a rudder bar is less than a second threshold.

    摘要翻译: 本发明的方法包括在左和右制动指令(FG,FD)之间形成差值(D 1),将所述差值(D 1)转换成方向舵(16)的附加控制命令(D 2) 前置档(4),并根据以下两个条件将所述附加控制命令(D 2)应用于所述舵(16)和可转向前档(4):差值(D 1)大于第一阈值,并且组合 通过舵杆传递到舵和可转向前档(4)的控制命令小于第二阈值。

    Method and device for multimode and multifunction communication between
an operator and one or more processors
    10.
    发明授权
    Method and device for multimode and multifunction communication between an operator and one or more processors 失效
    用于操作员和一个或多个处理器之间的多模和多功能通信的方法和装置

    公开(公告)号:US6072473A

    公开(公告)日:2000-06-06

    申请号:US249079

    申请日:1994-05-25

    摘要: The system embodying the invention involves a communications instrument comprising a sensitive surface coupled to a processor ensuring management of a plurality of display elements, the dialogue between said instrument and said processor taking place according to a sequence comprising a first operational mode in which the sensitive surface is virtually divided into a plurality of zones corresponding isomorphically with the geometrical disposition of the display elements, and a second operational mode in which a variable displayed on a visualisation element is modified subsequent to displacement of the operator's finger on the sensitive surface. This system is notably suitable in the case of management of a large number of display elements and is highly ergonomic.

    摘要翻译: 体现本发明的系统涉及一种通信工具,其包括耦合到处理器的敏感表面,确保管理多个显示元件,根据包括第一操作模式的序列发生所述仪器和所述处理器之间的对话,其中敏感表面 实际上分为与显示元件的几何配置同构地对应的多个区域,以及第二操作模式,其中在操作者的手指在敏感表面上移位之后,显示在可视化元件上的变量被修改。 该系统特别适用于管理大量显示元件并具有高度人机工程学特性。