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    • 1. 发明公开
    • MULTIVOLTAGE WELDING APPARATUS
    • 多电极焊接设备
    • EP3219004A1
    • 2017-09-20
    • EP15798569.8
    • 2015-11-05
    • Esab AB
    • ADMUTHE, Vaijnath BhimraoGERDIN, LarsVILAS, Pimple VinayUTTAM, Pisal KiranBHANUSHANKER, Dave Homeshkumar
    • H02M7/217B23K9/10
    • B23K9/1043B23K9/124H01F27/006H01F27/306H02M3/33592H02M3/3376H02M7/217H02M2001/007H02M2001/008
    • An apparatus may include an input circuit to receive an AC input voltage having a first magnitude within a range of AC input voltages, and generate a first DC voltage; a boost converter to receive the first DC voltage and output a second DC voltage having a fixed magnitude that is not dependent upon the first magnitude of the AC input voltage; an output circuit to receive the second DC voltage and convert the second DC voltage into welding type power; a control DC-DC converter to receive the first DC voltage and output a control power signal as a third DC voltage; a boost converter control component to receive the control power signal and generate a control signal to control operation of the boost converter; and an auxiliary AC power source to receive the second DC voltage output by the boost converter and to generate an AC auxiliary output voltage.
    • 一种装置可以包括:输入电路,用于接收具有在AC输入电压的范围内的第一量值的AC输入电压,并且生成第一DC电压; 升压转换器,用于接收第一DC电压并且输出具有不依赖于AC输入电压的第一量值的固定量值的第二DC电压; 输出电路,用于接收第二DC电压并将第二DC电压转换成焊接型电力; 控制DC-DC转换器,接收第一DC电压并输出控制功率信号作为第三DC电压; 升压转换器控制部件,用于接收控制功率信号并产生控制信号以控制升压转换器的操作; 以及辅助交流电源,用于接收升压转换器输出的第二直流电压并产生交流辅助输出电压。
    • 4. 发明公开
    • WRIST DEVICE FOR A PROSTHETIC LIMB
    • 用于假肢肢体的手腕装置
    • EP3200730A1
    • 2017-08-09
    • EP15774669.4
    • 2015-09-24
    • Touch Bionics Limited
    • GILL, Hugh
    • A61F2/58A61F2/50B25J17/02
    • A61F2/585A61F2/588A61F2/68A61F2/76A61F2002/5003A61F2002/6854
    • A wrist device for a prosthetic limb is provided. The device (1) comprises a base member (3) connectable to the wearer of the device, and a support member (13) connectable to the limb. The support member (13) is pivotably connected to the base member (3) such that the support member can pivot about a pivot axis (A) relative to the base member. A damping mechanism is located between the base (3) member and the support member (5). The damping mechanism comprises a pinion (47) connected to the support member (5) and rotatable about the pivot axis (A) relative to the base member (3). A rack (35) is engaged with the pinion (47) such that rotational motion of the pinion causes a linear motion of the rack, and at least one biasing member (41) extends between the base member (3) and the rack. The biasing member (41) biases the rack (35) and support member (13) into a neutral position. A prosthetic limb incorporating the wrist device is also provided.
    • 提供用于假肢的腕部装置。 装置(1)包括可连接到装置佩戴者的基座构件(3)和可连接到肢体的支撑构件(13)。 支撑构件(13)可枢转地连接到基座构件(3),使得支撑构件可相对于基座构件绕枢转轴线(A)枢转。 阻尼机构位于基部(3)构件和支撑构件(5)之间。 阻尼机构包括连接到支撑构件(5)并可相对于基座构件(3)绕枢转轴线(A)旋转的小齿轮(47)。 齿条(35)与小齿轮(47)接合,使得小齿轮的旋转运动引起齿条的线性运动,并且至少一个偏置构件(41)在基座构件(3)和齿条之间延伸。 偏置构件41将齿条35和支撑构件13偏置到中立位置。 还提供了包含手腕装置的假肢。
    • 5. 发明公开
    • A HELICOPTER ENGINE MOUNTING SYSTEM AND METHODS
    • 直升机发动机安装系统和方法
    • EP3184433A1
    • 2017-06-28
    • EP16203044.9
    • 2011-06-14
    • LORD Corporation
    • ZAMEROSKI, Daniel
    • B64D27/26F16F13/26
    • B64D27/26B64C27/001B64C2027/005B64D2027/262B64D2027/266B64F5/10F16F13/26Y10T29/49826
    • A helicopter engine mounting system is provided for mounting an engine (50) to an aircraft body (54). The aircraft body (54) is supported in flight by a rotary wing system (56) rotating with an operational rotating frequency (P) with a plurality of (N) rotating blades (58), said aircraft body having a persistent in flight operational rotating frequency vibration from said rotating blades. The engine mounting system includes a top fluid chamber fluid engine mount (60t) and a bottom fluid chamber fluid engine mount (60b). The top fluid chamber fluid engine mount (60t) has a bottom end (62) for grounding to said aircraft body (54), and said bottom fluid chamber fluid engine mount (60b) has a bottom end (62) for grounding to said aircraft body. The top fluid chamber fluid engine mount (60t) has a top fluid chamber (64t) distal from said top fluid chamber fluid engine mount bottom end (62). The bottom fluid chamber fluid engine mount (60b) has a bottom fluid chamber (64b) proximate said bottom fluid chamber fluid engine mount bottom end (62). The system also includes an intermediate cradle (65) with a lateral link (4), said lateral link having a first end (68a) for grounding to said aircraft body (54) and a second distal end (68c). The second distal end (68c) is distal from said first end (68a) and is linked to said intermediate cradle (65). The top fluid chamber fluid engine mount bottom end (62) and said bottom fluid chamber fluid engine mount bottom end (62) are each grounded to said aircraft body (54), with said intermediate cradle (65) disposed between said top fluid chamber fluid engine mount (60t) and said bottom fluid chamber fluid engine mount (60b) and said engine (50). A fluid conduit (70) connects said top fluid chamber fluid engine mount top fluid chamber (64t) with said bottom fluid chamber fluid engine mount bottom fluid chamber (64b) wherein a transfer of said persistent in flight operational rotating frequency vibration from said aircraft body (54) to said engine (50) is inhibited.
    • 提供了用于将发动机(50)安装到飞机主体(54)的直升机发动机安装系统。 飞行器主体(54)由旋转机翼系统(56)在飞行中支撑,所述旋转机翼系统利用多个(N)旋转叶片(58)以可操作旋转频率(P)旋转,所述飞行器主体具有持续飞行操作旋转 来自所述旋转叶片的高频振动。 发动机安装系统包括顶部流体腔室流体发动机支架(60t)和底部流体腔室流体发动机支架(60b)。 所述顶部流体腔室流体发动机支架(60t)具有用于接地所述飞机主体(54)的底端(62),并且所述底部流体腔室流体发动机支架(60b)具有用于接地所述飞机的底端(62) 身体。 顶部流体腔室流体发动机支架(60t)具有远离所述顶部流体腔室流体发动机支架底端(62)的顶部流体腔室(64t)。 底部流体腔室流体发动机支架(60b)具有靠近所述底部流体腔室流体发动机支架底端(62)的底部流体腔室(64b)。 该系统还包括具有横向连杆(4)的中间支架(65),所述横向连杆具有用于接地至所述飞机主体(54)的第一端(68a)和第二远端(68c)。 第二远端(68c)远离所述第一端(68a)并连接到所述中间支架(65)。 所述中间支架(65)布置在所述顶部流体腔室流体(54)之间,所述顶部流体腔室流体发动机支架底端(62)和所述底部流体腔室流体发动机支架底端(62)各自接地到所述飞机主体 发动机支架(60t)和所述底部流体腔室流体发动机支架(60b)和所述发动机(50)。 流体导管(70)将所述顶部流体腔室流体发动机支架顶部流体腔室(64t)与所述底部流体腔室流体发动机支架底部流体腔室(64b)连接,其中从所述飞行器主体 (54)到所述发动机(50)的操作被禁止。