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    • 1. 发明专利
    • コネクタ
    • JP2019021460A
    • 2019-02-07
    • JP2017137900
    • 2017-07-14
    • JAPAN AVIATION ELECTRONICS IND LTD
    • ITO YASUKAZUNAKAZAWA KATSUHIKO
    • H01R13/42
    • 【課題】インシュレータから端子を容易に取り外すことができるコネクタを提供すること。【解決手段】コネクタは、端子と、ストッパと、ソケットインシュレータを備えている。ストッパは、端子に夫々取り付けられ、端子とともにソケットインシュレータの収容部に収容される。ストッパには、被ロック部と被ロック部を支持するロックバネ部とが設けられている。ソケットインシュレータには、ロック部と操作部とが形成されている。ロック部は、ストッパが収容部に収容された状態において、被ロック部の後方に位置し、ストッパの後方への移動を規制する。操作部は、前後方向と交差する所定方向において操作可能である。操作部は、操作されると、被ロック部を所定方向に沿って移動させてロック部による被ロック部の規制を解除する。【選択図】図30
    • 2. 发明专利
    • コネクタ
    • JP2019021458A
    • 2019-02-07
    • JP2017137870
    • 2017-07-14
    • JAPAN AVIATION ELECTRONICS IND LTD
    • ITO YASUKAZUNAKAZAWA KATSUHIKO
    • H01R13/44
    • 【課題】コネクタの感電防止機能を維持しつつ、コネクタの組立時において端子を容易に取り換え可能なコネクタを提供すること。【解決手段】コネクタ10は、端子20と、保持孔330を有するベースインシュレータ30と、通過孔430を有するフロントインシュレータ40とを備えている。端子20は、ランス260及びストッパ270が設けられた円筒部22を有している。端子20は、保持孔330に保持されている。保持孔330の内部には、抜止部334が設けられている。抜止部334は、端子20のランス260とストッパ270との間に位置している。保持孔330の内壁332と端子20の円筒部22との間には隙間が形成されている。フロントインシュレータ40は、ベースインシュレータ30に取り付けられており、通過孔430は、保持孔330の前方に位置している。通過孔430は、端子20の円筒部22よりも小さい。【選択図】図5
    • 3. 发明专利
    • Structure of servo accelerometer
    • 伺服加速度计结构
    • JPH11281670A
    • 1999-10-15
    • JP8360098
    • 1998-03-30
    • Japan Aviation Electronics Ind Ltd日本航空電子工業株式会社
    • SHINNO AKIRA
    • G01P15/13G01P15/08
    • PROBLEM TO BE SOLVED: To stabilize the position of a magnet against temperature fluctuation or vibration and to eliminate precise machining for fitting a pole piece bottom and a tubular core.
      SOLUTION: A vertical pot type core 30 for containing a pendulum 6 and a torquer coil 10a comprises a central core 20 and a tubular core (magnet housing) 3. The central core 20 comprises a cylindrical magnet 1, and a disc-like pole piece bottom 5 having coefficient of thermal expansion substantially equal to that of the magnet and boded to the side end face of the tubular core 3 of the magnet. The tubular core 3 is provided, at the closed end thereof, with through holes 3a of significantly smaller diameter than the magnet 1 made along the axis L. The closed end of the tubular core 3 and the pole piece bottom 5 are welded along the inner circumferential edge of through holes 3a touching each other. Continuous welding or spot welding at a plurality of points is employed.
      COPYRIGHT: (C)1999,JPO
    • 要解决的问题:为了稳定磁体的位置以抵抗温度波动或振动,并且消除用于安装极靴底部和管状芯的精确加工。 解决方案:用于容纳摆锤6和扭矩线圈10a的垂直盆型芯30包括中心芯20和管状芯(磁体壳体)3。中心芯20包括圆柱形磁体1和盘状极片 底部5的热膨胀系数基本上等于磁体的热膨胀系数,并且连接到磁体的管状芯3的侧端面。 管状芯3在其封闭端设置有直径小于沿着轴线L形成的磁体1的直径的通孔3a。管状芯3和极靴底部5的封闭端沿内部焊接 通孔3a的圆周边缘彼此接触。 采用多点连续焊接或点焊。
    • 4. 发明专利
    • Crimp contact and crimp machine
    • 犯罪联系人和打击机
    • JPH11273760A
    • 1999-10-08
    • JP7920798
    • 1998-03-26
    • Japan Aviation Electronics Ind Ltd日本航空電子工業株式会社
    • TAKAHASHI AKIRAKUWABARA TAKASHI
    • H01R43/00H01R4/18H01R43/048
    • PROBLEM TO BE SOLVED: To provide a crimp contact capable of improving an accuracy in an relative position of two sorts of contacts which are insulated to each other in an axial direction of an electric wire, reducing an installation cost, and reducing a number of processes.
      SOLUTION: Primary contact is composed of fitting part 1, a core barrel 2 for a center conductor of the coaxial cable, and a covered barrel 3 for an internal cover of the coaxial cable. Secondary contact is composed of a core barrel 5 for an external conductor of the coaxial cable and a covered barrel 6 for an external cover of the coaxial cable. Both contacts are connected to an axial direction of the coaxial cable through an intermediate bridge 4. An accuracy in each relative position of the both contacts is secured by a rapping accuracy in a press metal molding. The second contact is connected to a carrier 8 through a bridge 7.
      COPYRIGHT: (C)1999,JPO
    • 要解决的问题:提供一种能够提高电线的轴向彼此绝缘的两种触点的相对位置的精度的压接接触,降低了安装成本,并且减少了多个工艺 。 解决方案:主接触由配合部分1,用于同轴电缆的中心导体的芯筒2和用于同轴电缆的内盖的覆盖筒3组成。 二次接触由用于同轴电缆的外部导体的芯筒5和用于同轴电缆的外部盖的被覆盖的筒6组成。 两个触点通过中间桥4连接到同轴电缆的轴向。两个触点的每个相对位置的精度通过冲压金属模制中的敲击精度来确保。 第二触点通过桥接器7连接到载体8。
    • 5. 发明专利
    • Optical interference angular velocity meter
    • 光学干涉角速度计
    • JPS6147512A
    • 1986-03-08
    • JP16896484
    • 1984-08-13
    • Japan Aviation Electronics Ind Ltd
    • OKADA KENICHIOOUCHI KAZUTANEONO ARITAKA
    • G01C19/00G01C19/64G01C19/72G02F1/11
    • PURPOSE: To simplify a circuit and to dispense with processing for calculating the frequency Δf of difference, by arranging first and second photoelectric converter elements at the position where lefthand light and righthand light are superposed and detecting the polarity and magnitude of input angular velocity.
      CONSTITUTION: When the output 19A of a second comparator 19 comes to H with a delay phase of π/2, the first monostable multivibrator 21 receiving the H- signal at the inable terminal E thereof comes to an inable state and, succeedingly, when the output 18A of a first comparator 18 is fallen to L, the output in the 20D-side of RS flip-flop 20 comes to H. A first monostable multivibrator 22 held under an inable state is triggered by this H-signal to generate a pulse at an output terminal 22Q. Further, when the output 19A of the second comparator 19 comes to L in the delay phase of π/2, the 20D-side output of the RS flip-flop is reversed to be brought to H and sent to the trigger terminal T of the second monostable multivibrator 21. Because the inable terminal E of the second monostable multivibrator 21 is held down by the L-output of the first comparator 18, the second monostable multivibrator 21 is not triggered.
      COPYRIGHT: (C)1986,JPO&Japio
    • 目的:为了简化电路,省略用于计算差分频率DELTAf的处理,通过将第一和第二光电转换元件放置在左右光和右手光叠加的位置处,并检测输入角速度的极性和大小。 构成:当第二比较器19的输出端19A以π/ 2的延迟相位达到H时,在其可终端E处接收H信号的第一单稳态多谐振荡器21变为可启动状态,接着,当 第一比较器18的输出18A下降到L,RS触发器20的20D侧的输出变为H.由H信号触发保持在可能状态的第一单稳态多谐振荡器22以产生脉冲 在输出端22Q。 此外,当第二比较器19的输出端19A在pi / 2的延迟相位中变为L时,RS触发器的20D侧输出反转为H并发送到触发端子T 第二单稳态多谐振荡器21.由于第二单稳态多谐振荡器21的不可用端子E被第一比较器18的L输出压低,所以第二单稳态多谐振荡器21不被触发。
    • 6. 发明专利
    • Light interfering angular velocity meter
    • 光干扰角速度计
    • JPS59214773A
    • 1984-12-04
    • JP8951683
    • 1983-05-20
    • Japan Aviation Electronics Ind Ltd
    • OKADA KENICHI
    • H01S3/083G01C19/64G01C19/72G01P3/36G01P9/00
    • G01C19/72
    • PURPOSE:To make a double refracting crystal plate hard to be affected by changes in the double refractive index due to an ambient temperature by applying an alternating magnetic field to first and second magnetooptic elements of a directional phase shifter to invert the phase difference of light passing through the phase shifter in the opposite direction to each other. CONSTITUTION:Light incident from the left and right of a double refracting crystal plate 23 passing through a crystal plate to generate a phase difference as given by psi=(nx-ny).k.l, where nx and ny represent refractive indexes of index of the double refracting crysal plate 23, l the thickness thereof and k the propagation constant thereof. An alternating magnetic field H applied to magnetooptic elements 22 and 24 are inverted in the direction, the phase difference turns to psi2=-(nx-ny).k.l. 1PSI1=1psi21=pi/2 is selected. Here, the phase difference between lights 16 and 17 is biased by DELTApsi, namely an angular velocity OMEGA and changes by pi/2 and -pi/2 centered on the value. An output light 18 of a light distributive connection means 12 is detected synchronously about the frequency of the alternating magnetic field with a signal processor 31 through a photoelectric signal converter 19 and the amplitude of the signal obtained at a terminal 35 is proportional to DELTApsi to obtain an output with a high sensitivity.
    • 目的:通过向定向移相器的第一和第二磁光元件施加交变磁场,使双折射晶体板难以受到环境温度下双折射率变化的影响,以反转光通过的相位差 通过移相器在彼此相反的方向。 构成:通过晶体板的双折射晶体板23的左侧和右侧入射的光,以产生由psi =(nx-ny)·k1给出的相位差,其中nx和ny表示折射率 双折射冷板23,其厚度和k的传播常数。 施加到磁光元件22和24的交变磁场H在方向上反转,相位差变为psi2 = - (nx-ny).k.l。 1PSI1 = 1psi21 = pi / 2被选择。 这里,光16和17之间的相位差由DELTApsi偏置,即角速度OMEGA,以该值为中心以pi / 2和-pi / 2改变。 光分配连接装置12的输出光18通过光电信号转换器19与信号处理器31同步地检测交变磁场的频率,并且在端子35处获得的信号的振幅与DELTApsi成比例,以获得 具有高灵敏度的输出。
    • 7. 发明专利
    • Optical shape measuring instrument
    • 光学形状测量仪器
    • JPS59203909A
    • 1984-11-19
    • JP7857683
    • 1983-05-02
    • Japan Aviation Electronics Ind Ltd
    • ITOU SHIGENORI
    • G01B11/24G01B11/245
    • G01B11/245
    • PURPOSE:To decide on a shape with high precision by irradiating a body to be measured with the parallel irradiation light of a unit optical path formation part successively and adding the output signal of a corresponding photodetecting element. CONSTITUTION:Plural unit optical path formation parts are composed of photodetecting elements 14-1-14-4 facing light sources 11-1-11-4, and the body 13 to be measured is arranged in the measurement space 16. A driving means 17 select the unit optical path formation parts in the space 16 successively to drive the light sources, and obtain output signals of corresponding photodetecting element successively. Then, decision processing means 19 and 20 process the output signal of the means 17 to decide on the shape of the body 13 to be measured.
    • 目的:通过依次对单位光路形成部的平行照射光照射被测体,并对相应的光检测元件的输出信号进行相加,来决定高精度的形状。 构成:多个单位光路形成部由与光源11-1-11-4对置的受光元件14-1-14-4构成,被测定体13配置在测量空间16内。驱动机构17 依次选择空间16中的单位光路形成部,驱动光源,依次取得对应的受光元件的输出信号。 然后,判定处理装置19和20处理装置17的输出信号以决定要测量的主体13的形状。
    • 8. 发明专利
    • Manufacture of ferrule for photoconnector
    • 光电子器件的制造
    • JPS59154412A
    • 1984-09-03
    • JP2816283
    • 1983-02-22
    • Japan Aviation Electronics Ind Ltd
    • NAKAMURA HIDEJI
    • G02B6/24G02B6/38
    • G02B6/3833
    • PURPOSE:To form a highly accurate and low cost ferrule for a high performance photoconnector by drawing a ferrule having a core wire inserted in the hole. CONSTITUTION:A rigid core wire 10 having diameter nearly equal to that of an optical fiber is inserted in the small hole 21 of a ferrule 20, and the cylindrical part 26 is held by the chuck of a lathe etc. A pair of drawing tools 30a, 30b are fixed with semi-circular inner diameter of the drawing holes 31a, 31b brought into close contact with outer periphery of finished diameter 24 of the ferrule 20. After giving lubricating oil to the outer diameter part 23 of the ferrule 20, the ferrule is rotated around its center axis. At the same time, drawing tools 30a, 30b are moved in the direction of B until drawing holes 31a, 31b come out from an end of the ferrule 20, and the outer diameter part 23 of the ferrule 20 is drawn to cylindrical shape which has equal diameter with finished diameter part of drawing and coaxial with the small hole 21. At this time, inner diameter of the small hole 21 is reduced until its inner peripheral face comes into close contact with outer peripheral face of the core wire 10. When the core wire 10 is pulled out, a ferrule having a small hole 27 that fits accurately to the optical fiber is formed.
    • 目的:通过绘制插入孔中的芯线的套圈,为高性能光电连接器形成高精度和低成本的套圈。 构成:将直径几乎等于光纤直径的刚性芯线10插入到套圈20的小孔21中,并且圆柱形部分26由车床等夹持。一对拉拔工具30a 30b被固定成具有与套圈20的精加工直径24的外周紧密接触的拉拔孔31a,31b的半圆形内径。在将套筒20的外径部23赋予润滑油之后, 围绕其中心轴旋转。 同时,拉拔工具30a,30b沿着B方向移动,直到拉出孔31a,31b从套圈20的一端出来,套圈20的外径部分23被拉成圆柱形, 其直径与成品直径部分相同,与小孔21同轴。此时,小孔21的内径减小直到其内周面与芯线10的外周面紧密接触。当 芯线10被拉出,形成具有与光纤精确配合的小孔27的套圈。
    • 9. 发明专利
    • Formation of conductive and corrosion resistant aluminum oxide film
    • 形成导电和耐腐蚀氧化铝薄膜
    • JPS59118886A
    • 1984-07-09
    • JP23425382
    • 1982-12-24
    • Japan Aviation Electronics Ind Ltd
    • KATAOKA IZUMIKAWAHARA YUKIOYAMADA ICHIROU
    • C23C22/00
    • PURPOSE: To form superposedly a dense and chemically strong film and a thick and mechanically strong film by impressing and discharging successively a negative voltage and positive voltage on an object to be formed thereon with an aluminum oxide film in a gaseous oxygen atmosphere in a vacuum vessel.
      CONSTITUTION: The inside of a vacuum vessel 1 is evacuated through an evacuation pipe 6 and a variable leak valve 7 is operated to introduce gaseous oxygen in the vessel 1. When a contact C is connected to by operating a switch 11, a negative voltage is impressed on an object 4 attached to the 1st electrode 5 and a positive electrode is impressed through a grounding circuit on the 2nd electrode 9. Discharge is executed between the object and the 2nd electrode and a dense aluminum oxide film is formed on the surface of the object 4. When the contact C of the switch 11 is changed over to B, a positive voltage is impressed on the 1st electrode 5 and a negative voltage on the 2nd electrode 9, by which discharge is executed and the porous aluminum oxide film is superposedly formed.
      COPYRIGHT: (C)1984,JPO&Japio
    • 目的:通过在真空容器中的气态氧气氛中用氧化铝膜在其上形成的物体上连续施加负电压和正电压来叠加形成致密和化学强的薄膜和厚而机械强的薄膜 。 构成:真空容器1的内部通过排气管6排出,并且可操作的可变泄漏阀7被操作以在容器1中引入气态氧。当通过操作开关11连接触点C时,负电压为 施加在附接到第一电极5的物体4上,并且通过第二电极9上的接地电路施加正电极。在物体和第二电极之间执行放电,并且在物体和表面上形成致密的氧化铝膜 对象4.当开关11的触点C转换为B时,在第一电极5上施加正电压,在第二电极9上施加正电压,通过放电进行多孔氧化铝膜的叠加 形成。
    • 10. 发明专利
    • Angular velocity detector
    • 角速度检测器
    • JPS5947787A
    • 1984-03-17
    • JP15869182
    • 1982-09-10
    • Japan Aviation Electronics Ind Ltd
    • INUI KATSUAKI
    • G01C19/66H01S3/083
    • G01C19/66
    • PURPOSE:To enable to make a piece of mirror block having a ring form groove sufficient by a method wherein only one mirror of a plurality of mirrors which compose a photo closed loop is formed in a structure wherein the alternations of advance-retreat direction and angles can be performed. CONSTITUTION:When the mirror block 3b is decided as a just plane mirror, and the ring form groove 14 is formed in the mirror block 3c, the detector is so constructed that the length of an optical path is controlled by moving a mirror surface 3c' of the mirror block 3c wherein the ring form groove 14 is formed in advance-retreat direction by a means 11 of controlling the length of the optical path, and that the angle of the mirror surface 3c' is controlled by a lock-in control means adhered at a thin part formed in the mirror block 3c. For example, the case of construction by sticking ring form piezoelectric elements 16a and 16b on the back surface of a member 17 mounted on the back surface side of the mirror block 3c is shown. When the outside piezoelectric element 16b is so deformed as to expand by shrinking the inside piezoelectric element 16a, the member 17 deforms and thus makes the mirror surfaces 3c' project toward the inside the block.
    • 目的:为了能够通过一种方法制造具有环形凹槽足够的镜片块,其中仅构成组成光闭环的多个反射镜的一个反射镜形成为其中前进后退方向和角度的改变 可以执行。 构成:当镜面块3b被确定为正平面镜,并且环形凹槽14形成在反射镜块3c中时,检测器被构造成通过移动镜面3c'来控制光路的长度, 其中通过控制光路长度的装置11在前后方向上形成环形槽14,并且镜面3c'的角度由锁定控制装置 粘附在形成在镜块3c中的薄部分。 例如,示出了在安装在镜块3c的背面侧的构件17的背面上通过粘结环构造压电元件16a和16b的情况。 当外部压电元件16b通过收缩内部压电元件16a而变形而变形时,构件17变形,从而使镜面3c'朝向块的内侧突出。