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    • 1. 发明授权
    • Method for calibrating a piezoelectric actuating drive
    • 用于校准压电致动驱动器的方法
    • US06340858B1
    • 2002-01-22
    • US09490188
    • 2000-01-24
    • Peter Jaenker
    • Peter Jaenker
    • H01L4104
    • H01L41/042H02N2/043H02N2/062
    • A piezoelectric actuating drive is calibrated so that displacements or movements of its actuator output beam (4) become independent of environmental operating conditions and of piezoelectric instabilities. For this purpose an automatic determination and correlating of energizing signal values and respective displacement positions of an actuator beam (4) are performed on the basis of first sensing or measuring striking times (t1, t2) when the actuator beam (4) encounters at least one, preferably two limit stops which limit the beam displacement caused by piezoelectric action. The change of the electric capacitance of a piezostack (3) that displaces the actuator output beam (4) is measured when the beam (4) strikes a limit stop. Instead of measuring a change in the electric capacitance of the piezostack (3), electric charge impulses may be measured at the time (t1, t2) and evaluated for the correlation between the energizing control or input signal and the corresponding output beam displacement. The correlation or calibration is performed automatically by an electronic signal processing circuit when such calibration is desired in response to an operator input or it is performed automatically in response to a control program stored in a memory of the electronic signal processing circuit.
    • 校准压电致动驱动器,使得其致动器输出光束(4)的位移或运动变得与环境操作条件和压电不稳定性无关。 为此,执行器光束(4)的激励信号值和各个位移位置的自动确定和相关是基于执行器光束(4)至少遇到的第一感测或测量打击时间(t1,t2)来执行的 一个,优选两个极限停止,限制由压电作用引起的光束位移。 当光束(4)进行极限停止时,测量位移致动器输出光束(4)的压电堆(3)的电容的变化。 代替测量压电堆(3)的电容的变化,可以在时间(t1,t2)测量电荷脉冲,并评估激励控制或输入信号与相应的输出光束位移之间的相关性。 当需要响应于操作者输入进行这种校准时,由电子信号处理电路自动执行相关或校准,或者响应于存储在电子信号处理电路的存储器中的控制程序而自动执行相关或校准。
    • 2. 发明授权
    • Mechanical resonator having a variable resonance frequency
    • 具有可变谐振频率的机械谐振器
    • US06134964A
    • 2000-10-24
    • US150358
    • 1998-09-09
    • Peter JaenkerHenning Strehlow
    • Peter JaenkerHenning Strehlow
    • B06B1/02F16F7/10F16F7/116F16F15/00G10K11/172G01P15/13H03B5/30
    • F16F7/1005B06B1/0261F16F15/005F16F7/116G10K11/172B06B2201/20B06B2201/30
    • A mechanical resonator has an electronically adjustable resonance frequency and is especially adapted to be used as a tunable vibration absorber. The mechanical resonator includes an inertial mass mounted on a free end of a spring, which is secured at its other end to the structure that is to be vibrationally damped. In order to vary the resonant frequency of the resonator, an electromechanical converter such as a piezoelectric element is connected to the spring and/or the inertial mass, and a displacement and/or acceleration sensor provides a sensor signal that is dependent on the respective displacement and/or acceleration of the spring and/or the inertial mass. An electronic control circuit generates an actuating signal based on the sensor signal. The actuating signal is applied to the electro-mechanical converter, which responsively exerts an adjusting force onto the spring and/or the inertial mass. The control circuit may include one or more variable amplifiers, inverters, and phase shifters, to control the actuating signal such that the adjusting force exerted by the electromechanical converter either counteracts or reinforces the bending force exerted by the inertial mass on the spring. In this manner, the effective total spring constant of the resonator can be increased or decreased relative to the inherent spring constant of the spring, whereby the resonant frequency is adjusted.
    • 机械谐振器具有电子调节的共振频率,并且特别适合用作可调节振动吸收器。 机械谐振器包括安装在弹簧的自由端上的惯性质量体,其在另一端被固定在要被振动阻尼的结构上。 为了改变谐振器的谐振频率,诸如压电元件的机电转换器连接到弹簧和/或惯性块,位移和/或加速度传感器提供依赖于相应位移的传感器信号 和/或弹簧和/或惯性质量的加速度。 电子控制电路基于传感器信号产生启动信号。 致动信号被施加到电 - 机械转换器,其响应地对弹簧和/或惯性质量施加调节力。 控制电路可以包括一个或多个可变放大器,反相器和移相器,以控制致动信号,使得由机电转换器施加的调节力抵消或加强由惯性块施加在弹簧上的弯曲力。 以这种方式,可以相对于弹簧的固有弹簧常数增加或减小谐振器的有效总弹簧常数,从而调节谐振频率。
    • 3. 发明授权
    • Piezoelectric actuator
    • 压电执行器
    • US6043587A
    • 2000-03-28
    • US165792
    • 1998-10-02
    • Peter Jaenker
    • Peter Jaenker
    • H01L41/09H02N2/00H02N2/02H01L41/08
    • H01L41/0926H01L41/047H01L41/0475
    • A piezoelectric actuator or sensor includes a solid state body made of a monolithic piezoelectric material, a plurality of actuating electrodes formed as closed-loop electrodes entirely around the perimeter of the solid state body, and a support plate with two contact electrodes respectively having interdigitally intermeshing contact fingers arranged thereon. The intermeshing or alternating contact fingers of the two contact electrodes respectively contact alternating ones of the actuating electrodes, preferably through an adhesive layer having conducting particles dispersed therein. The energized actuating electrodes effectively form virtual piezoelectric layers in the solid state body.
    • 压电致动器或传感器包括由单片压电材料制成的固态主体,多个致动电极,其形成为整体围绕固态主体的周边的闭环电极;以及支撑板,其具有分别具有交叉相互啮合的两个接触电极 布置在其上的接触指状物。 两个接触电极的相互啮合或交替的接触指状物分别接触交替的致动电极,优选地通过其中分散有导电颗粒的粘合剂层。 激励的致动电极在固体中有效地形成虚拟的压电层。
    • 5. 发明授权
    • Reversibly switchable primers
    • 可逆切换引物
    • US06478912B2
    • 2002-11-12
    • US09767213
    • 2001-01-22
    • Hermann GaubAndreas MittelbachPeter JaenkerFelix NitschkeUlrich S. Schubert
    • Hermann GaubAndreas MittelbachPeter JaenkerFelix NitschkeUlrich S. Schubert
    • C09J100
    • C23C22/02C09J5/02C09J2400/163C23F11/149Y10T156/1142Y10T428/31678
    • A ligand layer on a metal surface is capable of being reversibly switched between adhesion and deadhesion. The ligand layer includes substituted pyridine dimers and/or pyridine trimers which are selected from the group consisting of: with R1 through R6 being able to be equal or different and being selected from the group consisting of —R—CH(O)CH2, OH, —O—R, NR2, NHR, NH2, CO2H, CO2R, R and H. R is selected from the group consisting of alkyl and aryl residues with the proviso that not all residues R1 through R6 are hydrogen atoms at the same time. R7 is selected from the group consisting of —R—CH(O)CH2, OH, —O—R, NR2, NHR, NH2, CO2H, CO2R, CONHR, R and H, with R being selected from the group consisting of alkyl and aryl residues. Y is selected from the group consisting of silicon, carbon, nitrogen, phosphorus and oxygen atoms, and X is an oxygen, sulfur or phosphorus atom, and n having the value 0 or 1.
    • 金属表面上的配体层能够在粘合和粘合之间可逆地切换。 配体层包括取代的吡啶二聚体和/或吡啶三聚体,其选自:R 1至R 6能够相同或不同,并且选自-R-CH(O)CH 2,OH ,-OR,NR 2,NHR,NH 2,CO 2 H,CO 2 R,R和H.选自烷基和芳基残基,条件是不是所有的残基R1至R6都是同时为氢原子。 R 7选自-R-CH(O)CH 2,OH,-OR,NR 2,NHR,NH 2,CO 2 H,CO 2 R,CONHR,R和H,其中R选自烷基和芳基 残留物。 Y选自硅,碳,氮,磷和氧原子,X为氧,硫或磷原子,n为0或1。
    • 6. 发明授权
    • Electrostrictive or piezoelectric actuator device
    • 电致伸缩或压电致动器装置
    • US5986386A
    • 1999-11-16
    • US146266
    • 1998-09-03
    • Peter Jaenker
    • Peter Jaenker
    • H02N2/00H01L41/053H01L41/083H02N2/02H02N2/04H01L41/08
    • H01L41/083H01L41/053H01L41/0533
    • An electrostrictive or piezoelectric actuator device includes a solid state actuator element (4) that is elongated in the lengthwise direction (L) and contracted in the transverse direction (T) upon application of an electric voltage thereto. The actuator element (4) is clampingly held between a housing floor and an actuator output pin (6) in a housing (2). A protective interlayer (12) is respectively arranged between the lengthwise end faces of the actuator element (4) and the housing floor and the actuator pin respectively, to protect the actuator element against transverse stress peaks. The interlayer (12) provides a soft or elastic coupling in the transverse direction and a substantially rigid, force and stroke transmitting coupling in the lengthwise direction. To achieve this, each interlayer (12) is made of a material having an anisotropic modulus of elasticity with a lengthwise stiffness that is considerably higher than that of the solid state material of the actuator element and a transverse stiffness that is less than that of the solid state material of the actuator element.
    • 电致伸缩或压电致动器装置包括固体致动器元件(4),其在长度方向(L)上伸长并且在向其施加电压时沿横向(T)收缩。 致动器元件(4)夹紧地保持在壳体(2)中的壳体底板和致动器输出销(6)之间。 保护性中间层(12)分别布置在致动器元件(4)的纵向端面与壳体底板和致动器销之间,以保护致动器元件抵抗横向应力峰值。 中间层(12)在横向方向上提供软或弹性联接,并且在长度方向上提供基本刚性的力和行程传递联接。 为了实现这一点,每个中间层(12)由具有各向异性弹性模量的材料制成,其长度刚度远高于致动器元件的固态材料的纵向刚度,并且横向刚度小于 致动器元件的固态材料。
    • 8. 发明申请
    • Linear, hydraulic pivot drive
    • 线性,液压枢轴驱动
    • US20050178927A1
    • 2005-08-18
    • US10505678
    • 2003-02-21
    • Ulf BreuerPeter JaenkerThomas Lorkowski
    • Ulf BreuerPeter JaenkerThomas Lorkowski
    • B64C13/40F15B15/06F15B15/08
    • F15B15/068B64C13/40Y10T74/18056
    • The invention relates to a linear, hydraulic pivot drive, especially for the flap control system of aerodynamic structures. Said pivot drive comprises a housing provided with ports for introducing a hydraulic medium, a piston which is arranged inside the housing and can be axially displaced by the effect of the hydraulic medium, and an output shaft which is provided with coarse threads and interacts with the piston in order to cover the axial displacement of the piston into a rotational movement. The invention is characterized in that the output shaft is integrated into the piston, the coarse threads running in the same direction and engaging in the piston, and the cross-section of the piston has a spline profile for effectively preventing a rotational movement of the piston.
    • 本发明涉及一种线性液压枢转驱动装置,特别适用于空气动力结构的挡板控制系统。 所述枢转驱动器包括设置有用于引入液压介质的端口的壳体,布置在壳体内部并且可以通过液压介质的作用而轴向移位的活塞,以及设置有粗螺纹并与其相互作用的输出轴 活塞,以便将活塞的轴向位移覆盖成旋转运动。 本发明的特征在于,输出轴被集成到活塞中,粗螺纹沿相同方向延伸并接合活塞,并且活塞的横截面具有花键轮廓,用于有效地防止活塞的旋转运动 。
    • 9. 发明授权
    • Piezoelectric actuating device for controlling the flaps on the rotor blade of a helicopter
    • 用于控制直升机转子叶片上的襟翼的压电致动装置
    • US06717333B2
    • 2004-04-06
    • US10221814
    • 2002-09-16
    • Frank HermlePeter Jaenker
    • Frank HermlePeter Jaenker
    • H01L4108
    • B64C27/615B64C2027/7283H02N2/043Y02T50/34
    • A piezoelectric actuating device for controlling a flap on a rotor blade of a helicopter includes a piezo element arrangement including at least one piezoelectric stack actuator. A power transmission frame is coupled to the piezo element arrangement, the power transmission frame including an abutment and a driven element and generating a force therebetween from a change in length of the piezo element arrangement upon an excitation thereof, the force acting transversely to a direction of a centrifugal force of the rotor blade. A first holding device is provided including a pair of first flexible straps configured to fix the power transmission frame relative to the rotor blade in the direction of the centrifugal force and to allow the power transmission frame to move relative to the rotor blade transversely to the direction of the centrifugal force within a limited range. A second holding device is provided including a pair of second flexible straps configured to fix the abutment relative to the rotor blade transversely to the direction of the centrifugal force and to allow the abutment to move relative to the rotor blade in the direction of the centrifugal force within a limited range.
    • 用于控制直升机的转子叶片上的翼片的压电致动装置包括包括至少一个压电叠层致动器的压电元件装置。 动力传递框架联接到压电元件装置,动力传递框架包括邻接件和从动元件,并且在压电元件装置的激励时由压电元件装置的长度的变化产生其间的力,横向于方向 的转子叶片的离心力。 提供了一种第一保持装置,包括:一对第一柔性带,其构造成在离心力方向上相对于转子叶片固定动力传递框架,并允许动力传递框架相对于转子叶片横向移动 的离心力在有限的范围内。 提供了第二保持装置,其包括一对第二柔性带,其构造成相对于转子叶片横向于离心力的方向固定支座,并允许邻接件相对于转子叶片在离心力方向上移动 在有限的范围内。
    • 10. 发明授权
    • Aerodynamic component with a leading edge flap
    • 具有前缘皮瓣的气动元件
    • US06371415B1
    • 2002-04-16
    • US09658905
    • 2000-09-11
    • Thomas LorkowskiFrank HermlePeter Jaenker
    • Thomas LorkowskiFrank HermlePeter Jaenker
    • B64C1324
    • B64C27/001B64C27/615B64C2027/7283Y02T50/34
    • An aerodynamic component such as a helicopter rotor blade has an aerodynamic flow profile, a free end and a mounting end forming a blade root for attachment to a rotor mast. A blade section between the root and the free end has a leading edge and a trailing edge as viewed in the flow or chord direction. The blade is enclosed on its suction side and its pressure side with a respective skin. A nose flap or leading edge flap is secured to the leading edge by a bearing or hinge. The blade tilting angle is adjustable by piezo-drive elements arranged in at least one pair forming an actuator for each nose flap. The piezo-elements of a pair are arranged in the chord direction one behind the other and the pair is secured to the body of the blade by a fixed point positioned between the elements of a pair. The expansion and contraction from the piezo-element closer to the trailing edge is transmitted to the flap by a push rod. The expansion and contraction of the piezo-element closer to the leading edge is transmitted to the flap by a pronged pull-fork. The push rod and the pull-fork drive a free end of a lever secured to the flap, whereby a displacement of the push rod or of the pull fork causes the tilting adjustment of the flap by a push-pull action.
    • 诸如直升机转子叶片的空气动力学部件具有空气动力学流动分布,自由端和形成用于附接到转子桅杆的叶片根部的安装端。 根部和自由端之间的叶片部分具有从流动或弦向方向观察的前缘和后缘。 叶片在其吸力侧和其压力侧被封闭,并具有相应的皮肤。 鼻翼或前缘皮瓣通过轴承或铰链固定到前缘。 刀片倾斜角度可以通过布置在至少一对中的压电驱动元件来调节,形成每个鼻翼的致动器。 一对的压电元件沿着弦方向一个在另一个之上布置,并且该对被固定在一对位置的元件之间的固定点。 来自压电元件的靠近后缘的膨胀和收缩通过推杆传递到翼片。 靠近前缘的压电元件的膨胀和收缩通过叉形叉子传递到翼片。 推杆和拉叉驱动固定到翼片的杠杆的自由端,由此推杆或拉叉的位移通过推拉动作导致翼片的倾斜调节。