JPS61185834A - Latch type piezo-electric actuator - Google Patents

Latch type piezo-electric actuator

Info

Publication number
JPS61185834A
JPS61185834A JP2710085A JP2710085A JPS61185834A JP S61185834 A JPS61185834 A JP S61185834A JP 2710085 A JP2710085 A JP 2710085A JP 2710085 A JP2710085 A JP 2710085A JP S61185834 A JPS61185834 A JP S61185834A
Authority
JP
Japan
Prior art keywords
leaf spring
piezoelectric element
contact
present
flight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2710085A
Other languages
Japanese (ja)
Inventor
孝 太田
内川 忠保
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NEC Corp
Original Assignee
NEC Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by NEC Corp filed Critical NEC Corp
Priority to JP2710085A priority Critical patent/JPS61185834A/en
Priority to DE8686300375T priority patent/DE3681927D1/en
Priority to EP86300375A priority patent/EP0189302B1/en
Priority to CA000499886A priority patent/CA1249620A/en
Priority to US06/820,603 priority patent/US4672257A/en
Publication of JPS61185834A publication Critical patent/JPS61185834A/en
Pending legal-status Critical Current

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、圧電素子を用いたラッチ型のアクチュエータ
に関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a latch-type actuator using a piezoelectric element.

(従来技術とその問題点) 従来、ラッチ型のアクチュエータとしてはコイルを用い
た電磁アクチュエータが使用されてきた。
(Prior Art and its Problems) Conventionally, an electromagnetic actuator using a coil has been used as a latch-type actuator.

しかしながら電磁アクチュエータはコイルに通電するこ
とによシ磁界を発生しその磁力を利用して可動部材を動
かすため、大きな入力エネルギを必要とし発熱および磁
気干渉などの問題点があった。
However, electromagnetic actuators generate a magnetic field by energizing a coil and use the magnetic force to move a movable member, so they require a large amount of input energy and have problems such as heat generation and magnetic interference.

また、コイルを使うため小型化が難しかった。Also, since it uses a coil, it was difficult to miniaturize it.

(発明の目的) 本発明は、このような従来の欠点を除去せしめて、構造
が単純で小型、低電力、低発熱で磁気干渉のなく高信頼
性のラッチ型圧電アクチーエータを提供することにある
(Object of the Invention) An object of the present invention is to eliminate such conventional drawbacks and provide a latch-type piezoelectric actuator with a simple structure, small size, low power consumption, low heat generation, no magnetic interference, and high reliability. .

(発明の構成) 本発明によれば、飛行部材を有する板ばねと、前記板ば
ねから延び作用部材を設けたアーム部と、前記板ばねを
湾曲するように支持する支持部と、前記湾曲した板ばね
の凸面に対向して前記飛行部に力を与える圧電素子とか
ら構成されることを特徴とするラッチ型圧電アクチーエ
ータが得られる。
(Structure of the Invention) According to the present invention, a leaf spring having a flight member, an arm extending from the leaf spring and provided with an action member, a support part supporting the leaf spring in a curved manner, and a A latch-type piezoelectric actuator is obtained, characterized in that it is comprised of a piezoelectric element that faces the convex surface of a leaf spring and applies a force to the flight section.

(構成の詳細な説明) 本発明は、上述の構成をとることによシ従来技術の問題
点を解決した。
(Detailed Description of Configuration) The present invention solves the problems of the prior art by adopting the above-mentioned configuration.

まず、飛行部材の駆動源として、エネルギ変換効率の高
いことで知られている圧電素子を用いることによシ低電
力、低発熱で磁気干渉がなくなる。
First, by using a piezoelectric element, which is known for its high energy conversion efficiency, as the driving source for the flight member, it uses low power, generates little heat, and eliminates magnetic interference.

また、板ばねに軸力を加えて湾曲させることによシその
板ばねは反転ばねとなシ、板ばねに設けられた飛行部材
がその板ばねの両端を結ぶ直線を通過するとその板ばね
は反転動作しラッチされる。
In addition, by applying an axial force to a leaf spring to bend it, the leaf spring becomes a reverse spring.When the flight member provided on the leaf spring passes through a straight line connecting both ends of the leaf spring, the leaf spring It operates in reverse and is latched.

圧電素子に電圧を印加すると、圧電素子は微小ながら非
常に速く変位するため、飛行部材は圧電素子よシカを受
けて加速され圧電素子を離れ飛行する。そして、飛行部
材が板はねの両端を結ぶ直線を通過するとその板ばねは
反転動作しラッチされ、圧電素子の変位量よシもはるか
に長い飛行部材のストロークを得ることができる。
When a voltage is applied to the piezoelectric element, the piezoelectric element is slightly displaced but very quickly, so the flying member is accelerated by the piezoelectric element and flies away from the piezoelectric element. When the flying member passes through a straight line connecting both ends of the leaf spring, the leaf spring is reversed and latched, making it possible to obtain a stroke of the flying member that is much longer than the displacement of the piezoelectric element.

さらに、コイルを用いてないうえ、反転ばねも板ばねに
よシ構成されているだめ、構造が単純で小型となる。
Furthermore, since no coil is used and the reversing spring is also a leaf spring, the structure is simple and compact.

また、板ばねから延びたアーム部に可動接点等の作用部
材を設けることによシ、作用部材の摩耗等の悪影響をア
ーム部で吸引することができ信頼性が高くなる。
Further, by providing an operating member such as a movable contact on the arm extending from the leaf spring, the arm can absorb adverse effects such as wear of the operating member, thereby increasing reliability.

(実施例) 以下、本発明の実施例について図面を参照して詳細に説
明する。
(Example) Hereinafter, an example of the present invention will be described in detail with reference to the drawings.

第1図は本発明をリレーに適用した一実施例を示す図で
ある。第1図において、板はね1に飛行部材2を設け、
この板ばね1の両端を取付部材3に設けられた支持部と
しての溝3a 93bにそう人して板ばね1に軸力を与
え、板ばね1は湾曲している。また、第一の圧電素子4
の伸縮方向(矢印入方向)の一端4aに第一の力伝達部
材5を接続し、第二の圧電素子6の伸縮方向(矢印B方
向)の一端6aに第二の力伝達部材7を接続し、第一の
力伝達部材5ど第二の力伝達部材7を、飛行部材2をは
さんで対向して配置しである。さらに第1図(、)に示
すように、板ばね1の湾曲した凸面側に配置された第一
の力伝達部材5に飛行部材2がある予圧を持りて接する
ように、第一の圧電素子4の他端4bは取付部材3に固
定されている。第二の力伝達部材7は、第一の力伝達部
材5と、板ばね1の両端を結ぶ直線に関して対称な位置
になるように第二の圧電素子6の他端6bが取付部材3
に固定されている。そして板はね1の中央部付近には、
先端に作用部材としての可動接点8の設けられたアーム
9が接続しており、このアーム9は先端部の可動接点8
が取付部材3に接続された第一および第二の固定接点1
0.11に対向するように延びている。
FIG. 1 is a diagram showing an embodiment in which the present invention is applied to a relay. In FIG. 1, a flying member 2 is provided on a plate 1,
Both ends of the leaf spring 1 are inserted into grooves 3a and 93b as supporting parts provided in the mounting member 3 to apply an axial force to the leaf spring 1, so that the leaf spring 1 is curved. Moreover, the first piezoelectric element 4
A first force transmitting member 5 is connected to one end 4a of the second piezoelectric element 6 in the stretching direction (direction of arrow B), and a second force transmitting member 7 is connected to one end 6a of the second piezoelectric element 6 in the stretching direction (direction of arrow B). However, the first force transmitting member 5 and the second force transmitting member 7 are arranged to face each other with the flight member 2 in between. Furthermore, as shown in FIG. The other end 4b of the element 4 is fixed to the mounting member 3. The second force transmitting member 7 is arranged so that the other end 6b of the second piezoelectric element 6 is connected to the mounting member 3 so that the second force transmitting member 7 is in a symmetrical position with respect to the straight line connecting both ends of the leaf spring 1 with respect to the first force transmitting member 5.
is fixed. And near the center of the board 1,
An arm 9 having a movable contact 8 as an operating member is connected to the tip, and this arm 9 has a movable contact 8 at the tip.
first and second fixed contacts 1 connected to a mounting member 3
0.11.

第1図(a)に示すような飛行部材2が第一の力伝達部
材5に接している状態で、すなわち可動接点8が第一の
固定接点10に接している状態で、第一の圧電素子4に
電圧を印加すると、第一の圧電素子4は矢印人の方向に
微小ながら非常に高速で変位する。すると、第一の力伝
達部材5に接している飛行部材2は、第一の圧電素子4
からの力を受は加速され、第一の力伝達部材5を離れ飛
行し、板ばね1の両端を結ぶ直線を通過し板ばね1は反
転動作して、第1図(b)に示すように飛行部材2が第
二の力伝達部材7に接した状態となシ可動接点8が第二
の固定接点11に接する。また、第1図(b)に示すよ
うな、飛行部材2が第二の力伝達部材7に接した状態か
ら、第二の圧電素子6に電圧を印加すると、飛行部材2
は第二の圧電素子6から矢印Bの方向に力を受は加速さ
れ第二の力伝達部材7を離れ第一の力伝達部材5の方に
飛行し板ばね1は再び反転動作し、第1図(a)に示す
ような飛行部材2が第一の力伝達部材5に接した状態と
なシ可動接点8が第一の固定接点10に接する。このよ
うにして可動接点8を、第一の固定接点10から第二の
固定接点11へ、あるいは、第二の固定接点11から第
一の固定接点10へ切シ替えることができる。
When the flying member 2 is in contact with the first force transmitting member 5 as shown in FIG. 1(a), that is, with the movable contact 8 in contact with the first fixed contact 10, When a voltage is applied to the element 4, the first piezoelectric element 4 is slightly displaced at a very high speed in the direction of the arrow. Then, the flight member 2 that is in contact with the first force transmission member 5 transmits the first piezoelectric element 4
The receiving force is accelerated, leaves the first force transmitting member 5, flies, passes through the straight line connecting both ends of the leaf spring 1, and the leaf spring 1 reverses, as shown in FIG. 1(b). When the flying member 2 is in contact with the second force transmitting member 7, the movable contact 8 is in contact with the second fixed contact 11. Further, when a voltage is applied to the second piezoelectric element 6 from a state where the flight member 2 is in contact with the second force transmission member 7 as shown in FIG. 1(b), the flight member 2
receives a force from the second piezoelectric element 6 in the direction of arrow B, is accelerated, leaves the second force transmitting member 7, and flies toward the first force transmitting member 5, and the leaf spring 1 reverses again, When the flying member 2 is in contact with the first force transmitting member 5 as shown in FIG. 1(a), the movable contact 8 is in contact with the first fixed contact 10. In this way, the movable contact 8 can be switched from the first fixed contact 10 to the second fixed contact 11 or from the second fixed contact 11 to the first fixed contact 10.

このような本発明においては、電圧印加時の第一あるい
は第二の圧電素子4.6の発生力によシ飛行部材2を加
速し飛ばし板ばね1を反転動作させるため、板ばね1か
ら延びたアーム9の先端に設けられた可動接点8は、第
一あるいは第二の圧電素子4,6の変位量の数十倍から
数百倍という大きなストロークを得ることができる。
In the present invention, in order to accelerate the flight member 2 and fly the flight member 2 by the force generated by the first or second piezoelectric element 4.6 when a voltage is applied, and cause the leaf spring 1 to perform a reversal operation, a The movable contact 8 provided at the tip of the arm 9 can obtain a stroke as large as several tens to hundreds of times the amount of displacement of the first or second piezoelectric element 4 or 6.

また、可動接点8の摩耗等の悪影響をアーム部の弾性で
吸引することができるため、信頼性が高くlよる。
In addition, since the elasticity of the arm portion can absorb adverse effects such as wear on the movable contact 8, reliability is high.

さらに、飛行部材2の駆動源として、エネルギ変洪効率
の高いことで知られている圧%素子を用いているため、
低″嶋ブハ低発熱で磁気干渉がなくなる。
Furthermore, since a pressure element known for its high energy conversion efficiency is used as the drive source for the flight member 2,
Low heat generation eliminates magnetic interference.

そのうえ、コイルがなく、板ばねに軸力を加えて反転は
ねにしてラッチ動作を行わせるため構造が単純で小型と
なる。
Furthermore, there is no coil, and the structure is simple and compact because an axial force is applied to the leaf spring and the leaf spring is turned into a reverse spring to perform the latching action.

上述の例では、町′6Jh接点8を切り替えるのに、第
一の圧電素子4と第二の圧電素子6に交互に電圧を印加
したが、第一の圧電素子4と第二の圧電素子6に同時に
電圧を印加することによっても可動接点8を切り替える
ことができる。このような使い力は、従来のラッチ凰を
磁アクチュエータにおいてはできなかった。
In the above example, voltage was applied alternately to the first piezoelectric element 4 and the second piezoelectric element 6 to switch the contact 8. The movable contact 8 can also be switched by simultaneously applying a voltage to. Such usage power could not be achieved with conventional latch-type actuators.

なお、圧電素子への電圧の印加はパルス的に速く立ち上
ける必要があるが、パルス幅は短くてもよい。例えばパ
ルス幅は0.1 ms もあれば十分であり、長い分に
はかまわない。圧電素子は電気的にはコンデンサと同じ
であるため、電圧を長時間印加し続けても電力を消費す
ることがなくしたがって発熱もしない。
Note that the voltage applied to the piezoelectric element needs to rise quickly in a pulsed manner, but the pulse width may be short. For example, a pulse width of 0.1 ms is sufficient, and a longer pulse width does not matter. Since a piezoelectric element is electrically the same as a capacitor, it does not consume power and therefore does not generate heat even if a voltage is continuously applied for a long time.

第2図は本発明をリレーに適用した他の実施例を示す斜
視図である。板ばね12とアーム部13は一枚の薄板か
らできている。
FIG. 2 is a perspective view showing another embodiment in which the present invention is applied to a relay. The leaf spring 12 and the arm portion 13 are made of a single thin plate.

なお板ばねとアーム部の形状や接続の仕方にかかわらず
本発明の効果は同様に発揮されることは言うまでもない
It goes without saying that the effects of the present invention can be similarly exhibited regardless of the shape and connection method of the leaf spring and the arm portion.

第3図は本発明をリレーに適用した他の実施例を示す斜
視図である。板ばね14とアーム部15は一枚の薄板か
らできている。第2図に示す実施例のようにアーム部が
板ばねの幅方向に突出していないため、さらに小型にな
っている。
FIG. 3 is a perspective view showing another embodiment in which the present invention is applied to a relay. The leaf spring 14 and the arm portion 15 are made of a single thin plate. Since the arm portion does not protrude in the width direction of the leaf spring as in the embodiment shown in FIG. 2, the size is further reduced.

このような本発明の一実施例においても、本発明の効果
は同様に発揮されることは言うまでもない。
It goes without saying that the effects of the present invention can be similarly exhibited in such an embodiment of the present invention.

第4図は本発明をペンレコーダ等のペンの昇降機構に適
用した一実施例を示す図である。第4図(a)において
、板ばね19は、ペンホルダ20を接続したアーム部2
1が取付けられ、さらに取付部材3に設けられた支持部
としての溝3ay3bにそう人され軸力を受は第一の圧
電素子4の方へ湾曲している。そして板ばね19に設け
られた飛行部材2が取付部材3に接続された第一の圧電
素子4に接している。第二の圧電素子6は、第4図(b
)に示すように、板ば−ね19が反転した場合、飛行部
材2が接するように取付部材3に接続している。
FIG. 4 is a diagram showing an embodiment in which the present invention is applied to a pen lifting mechanism such as a pen recorder. In FIG. 4(a), the leaf spring 19 is connected to the arm portion 2 to which the pen holder 20 is connected.
1 is attached, and further curved toward the first piezoelectric element 4 due to the axial force received by the grooves 3ay 3b provided in the attachment member 3 as a support portion. The flying member 2 provided on the leaf spring 19 is in contact with the first piezoelectric element 4 connected to the mounting member 3. The second piezoelectric element 6 is shown in FIG.
), when the leaf spring 19 is reversed, it is connected to the mounting member 3 so that the flight member 2 comes into contact with it.

またペン22はペンホルダ20に支持されている。Further, the pen 22 is supported by the pen holder 20.

このような構成の実施例において、第4図(a)に示す
ように飛行部材2が第一の圧電素子4に接している状態
で、第一の圧電素子4に電圧を印加すると、飛行部材2
は第一の圧電素子4から力を受は加速され、第一の圧電
素子4を離れ飛行し板はね190両端を結ぶ直線を通過
し板ばね19は反転動作して、第4図(b)に示すよう
な飛行部材2が第二の圧電素子6に接した状態となる。
In an embodiment with such a configuration, when a voltage is applied to the first piezoelectric element 4 while the flying member 2 is in contact with the first piezoelectric element 4 as shown in FIG. 4(a), the flying member 2
is accelerated by the force from the first piezoelectric element 4, flies away from the first piezoelectric element 4, passes through the straight line connecting both ends of the plate spring 190, and the plate spring 19 reverses its action, as shown in Fig. 4(b). ), the flying member 2 is in contact with the second piezoelectric element 6.

したがってペン22は上から下に降り印字できる。また
第4図(b)に示すような飛行部材2が第二の圧電素子
6に接した状態で、第二の圧電素子6に電圧を印加する
と板ばね19は再び反転動作し第4図(a)に示すよう
な飛行部材2が第一の圧電素子4に接した状態に戻る。
Therefore, the pen 22 can descend from the top to the bottom and print. Further, when a voltage is applied to the second piezoelectric element 6 in a state where the flight member 2 is in contact with the second piezoelectric element 6 as shown in FIG. The flying member 2 returns to the state in which it is in contact with the first piezoelectric element 4 as shown in a).

仁のようにしてペン22を昇降させることができる。The pen 22 can be raised and lowered in a vertical manner.

このような本発明の一実施例においても、構造が単純で
小型、低電力、低発熱で磁気干渉のなく高信頼性という
本発明の効果は同様に発揮されることは言うまでもない
It goes without saying that even in such an embodiment of the present invention, the effects of the present invention such as simple structure, small size, low power consumption, low heat generation, no magnetic interference, and high reliability are similarly exhibited.

なお、本発明は上述の実施例のみならず、さまざまなラ
ッチ型アクチーエータに適用でき同様の効果を発揮する
。本発明の効果は、飛行部材を有する板ばねと、板ばね
から延び作用部材を設けたアーム部と、板ばねを湾曲す
るようにして支持する支持部と、湾曲した板はねの凸面
に対向して飛行部材に力を与える圧電素子とから構成す
ることによって発揮されるものである。
It should be noted that the present invention can be applied not only to the embodiments described above but also to various latch-type actuators and achieve similar effects. The effects of the present invention include: a leaf spring having a flight member; an arm extending from the leaf spring and provided with an action member; a supporting member supporting the leaf spring in a curved manner; This is accomplished by comprising a piezoelectric element that applies force to the flying member.

さらに上述の実施例においては、板はねの湾曲した凸面
側と反対側の凹面側の両方にそれぞれ圧電素子を配置し
た例を示したが、板ばねの反転復帰手段を用いれば湾曲
した板ばねの凸面側にのみ圧電素子を配置しても本発明
の効果は同様に発揮される。
Furthermore, in the above embodiment, piezoelectric elements were arranged on both the curved convex side and the opposite concave side of the leaf spring, but if the leaf spring inversion return means is used, the curved leaf spring Even if the piezoelectric element is placed only on the convex surface side, the effects of the present invention can be similarly exhibited.

また本発明においては縦効果や横効果のある単板の圧電
素子のほか、積層型の圧電素子さらには電歪素子によっ
ても同様の効果が得られる。
Further, in the present invention, in addition to a single-plate piezoelectric element having a longitudinal effect or a transverse effect, similar effects can be obtained by using a laminated piezoelectric element or even an electrostrictive element.

(発明の効果) 本発明によれば、構造が単純で小型、低電力、低発熱で
磁気干渉のなく高信頼性のラッチ型圧電アクチーエータ
が得られる。
(Effects of the Invention) According to the present invention, a latch-type piezoelectric actuator with a simple structure, small size, low power consumption, low heat generation, and high reliability without magnetic interference can be obtained.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明をリレーに適用した一実施例を示す図、
第2図は本発明をリレーに適用した他の実施例を示す図
、第3図は本発明をリレーに適用した他の実施例を示す
図、第4図は本発明をペンレコーダ等のペンの昇降機構
に適用した一実施例を示す図である。 図において 1.12,14,19・・・板ばね、2・・・飛行部材
、3・・・取付部材、4・・・第一の圧電素子、5・・
・第一の力伝達部材、6・・・第二の圧電素子、7・・
・第二〇力伝達部材、8・・・可動接点、9・13,1
5ν21・・・アーム部、10・・・第一の固定接点、
11・・・第二の固定接点、20・・・ペンホンダ、2
2・・・ペンをそれぞれ示す。
FIG. 1 is a diagram showing an embodiment in which the present invention is applied to a relay,
FIG. 2 is a diagram showing another embodiment in which the present invention is applied to a relay, FIG. 3 is a diagram showing another embodiment in which the present invention is applied to a relay, and FIG. 4 is a diagram showing another embodiment in which the present invention is applied to a pen recorder etc. It is a figure which shows one Example applied to the elevating mechanism of. In the figure, 1. 12, 14, 19... leaf spring, 2... flight member, 3... mounting member, 4... first piezoelectric element, 5...
- First force transmission member, 6... Second piezoelectric element, 7...
・No. 20 Force transmission member, 8... Movable contact, 9.13, 1
5ν21... Arm part, 10... First fixed contact,
11...Second fixed contact, 20...Pen Honda, 2
2... Each pen is shown.

Claims (1)

【特許請求の範囲】[Claims] 飛行部材を有する板ばねと、前記板ばねから延び作用部
材を設けたアーム部と、前記板ばねを湾曲するように支
持する支持部と、前記湾曲した板ばねの凸面に対向して
前記飛行部材に力を与える圧電素子とから構成されるこ
とを特徴とするラッチ型圧電アクチュエータ。
a leaf spring having a flight member; an arm portion extending from the leaf spring and provided with an action member; a support portion supporting the leaf spring in a curved manner; and the flight member facing the curved convex surface of the leaf spring. A latch-type piezoelectric actuator is characterized in that it is comprised of a piezoelectric element that applies force to a piezoelectric actuator.
JP2710085A 1983-03-20 1985-02-14 Latch type piezo-electric actuator Pending JPS61185834A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2710085A JPS61185834A (en) 1985-02-14 1985-02-14 Latch type piezo-electric actuator
DE8686300375T DE3681927D1 (en) 1985-01-21 1986-01-20 PIEZOELECTRIC BISTABLE ACTUATOR WITH A PROJECTILE THAT RECEIVES A SHOCK.
EP86300375A EP0189302B1 (en) 1985-01-21 1986-01-20 Piezoelectric latching actuator having an impact receiving projectile
CA000499886A CA1249620A (en) 1985-01-21 1986-01-20 Piezoelectric latching actuator having an impact receiving projectile
US06/820,603 US4672257A (en) 1983-03-20 1986-01-21 Piezoelectric latching actuator having an impact receiving projectile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2710085A JPS61185834A (en) 1985-02-14 1985-02-14 Latch type piezo-electric actuator

Publications (1)

Publication Number Publication Date
JPS61185834A true JPS61185834A (en) 1986-08-19

Family

ID=12211661

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2710085A Pending JPS61185834A (en) 1983-03-20 1985-02-14 Latch type piezo-electric actuator

Country Status (1)

Country Link
JP (1) JPS61185834A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6366817A (en) * 1986-09-05 1988-03-25 日本電気株式会社 Latch type relay

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6366817A (en) * 1986-09-05 1988-03-25 日本電気株式会社 Latch type relay

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