JPH057810B2 - - Google Patents

Info

Publication number
JPH057810B2
JPH057810B2 JP60008612A JP861285A JPH057810B2 JP H057810 B2 JPH057810 B2 JP H057810B2 JP 60008612 A JP60008612 A JP 60008612A JP 861285 A JP861285 A JP 861285A JP H057810 B2 JPH057810 B2 JP H057810B2
Authority
JP
Japan
Prior art keywords
piezoelectric element
leaf spring
contact
flying
present
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.)
Expired - Lifetime
Application number
JP60008612A
Other languages
Japanese (ja)
Other versions
JPS61168833A (en
Inventor
Takashi Oota
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
Nippon Electric Co Ltd
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 Nippon Electric Co Ltd filed Critical Nippon Electric Co Ltd
Priority to JP60008612A priority Critical patent/JPS61168833A/en
Priority to EP86300375A priority patent/EP0189302B1/en
Priority to DE8686300375T priority patent/DE3681927D1/en
Priority to CA000499886A priority patent/CA1249620A/en
Priority to US06/820,603 priority patent/US4672257A/en
Publication of JPS61168833A publication Critical patent/JPS61168833A/en
Publication of JPH057810B2 publication Critical patent/JPH057810B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Mechanical Light Control Or Optical Switches (AREA)
  • Electrically Driven Valve-Operating Means (AREA)
  • Displays For Variable Information Using Movable Means (AREA)
  • General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
  • Recording Measured Values (AREA)

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ツチ型のアクチ
ユエータに関する。
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、ラツチ型のアクチユエータとしてはコイ
ルを用いた電磁アクチユエータが使用されてき
た。しかしながら電磁アクチユエータはコイルに
通電することにより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
つた。また、コイルを使うため小型化が難しかつ
た。
(Prior Art and its Problems) Conventionally, an electromagnetic actuator using a coil has been used as a latch-type actuator. 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. Also, since it uses a coil, it is 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
渉のないラツチ型圧電アクチユエータを提供する
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 which has a simple structure, is small in size, has low power consumption, low heat generation, and is free from magnetic interference.

(発明の構成) 本発明のラツチ型圧電アクチユエータは、飛行
部材を有する板ばねと、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、前記圧電素子へ立ち上がりの急峻な電圧を印
加する手段とから構成され、前記圧電素子への前
記急峻な電圧の印加により前記飛行部材が前記圧
電素子から力を受けて飛行し、飛行することによ
り、前記板ばねを反転動作させることを特徴とす
る。
(Structure of the Invention) The latch-type piezoelectric actuator of the present invention includes a leaf spring having a flying member, a support portion that supports the leaf spring in a curved manner, and a support portion that supports the flying member so as to be opposed to a convex surface of the curved leaf spring. and a means for applying a voltage with a steep rise to the piezoelectric element, and the flight member receives a force from the piezoelectric element by applying the steep voltage to the piezoelectric element. It is characterized in that the leaf spring is reversed by flying and flying.

(構成の詳細な説明) 本発明は、上述の構成をとることにより従来技
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-described 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
ことにより低電力、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 flying 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
よりその板ばねは反転ばねとなり、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ツチされ
る。
In addition, by applying an axial force to a leaf spring and bending it, the leaf spring becomes a reversible spring, and when the flight member provided on the leaf spring passes through a straight line connecting both ends of the leaf spring, the leaf spring reverses and latches. be done.

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
素子より力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ツチさ
れ、圧電素子の変位量より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 very quickly, so the flying member receives a force from the piezoelectric element and is accelerated, leaving the piezoelectric element and flying. 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 amount of displacement of the piezoelectric element.

さらに、コイルを用いてないうえ、反転ばねも
板ばねにより構成されているため、構造が単純で
小型となる。
Furthermore, since no coil is used and the reversal spring is also composed of a leaf spring, the structure is simple and compact.

(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、板ばね1の中央
部付近に飛行部材として可動接点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,3bにそう入して板ばね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A方向)の一端4
aに第一の固定接点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
固定接点7を接続し、第一の固定接点5と第二の
固定接点7を、可動接点2をはさんで対向して配
置してある。さらに第1図a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固定接
点5に可動接点2がある予圧を持つて接するよう
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。第二の固定接点7は、第一の固
定接点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。
FIG. 1 is a diagram showing an embodiment in which the present invention is applied to a relay. In FIG. 1, a movable contact 2 is provided as a flight member near the center of a leaf spring 1, and both ends of the leaf spring 1 are inserted into grooves 3a and 3b as supporting parts provided in a mounting member 3, and the An axial force is applied to the spring 1, and the leaf spring 1 is curved. Also, one end 4 of the first piezoelectric element 4 in the expansion/contraction direction (direction of arrow A)
The first fixed contact 5 is connected to a, the second fixed contact 7 is connected to one end 6a of the second piezoelectric element 6 in the expansion/contraction direction (arrow B direction), and the first fixed contact 5 and the second The fixed contacts 7 are arranged opposite to each other with the movable contacts 2 interposed therebetween. Furthermore, as shown in FIG. 1a, the first piezoelectric element 4 is connected to the first fixed contact 5 disposed on the curved convex side of the leaf spring 1 so that the movable contact 2 contacts the first fixed contact 5 with a certain preload. The end 4b is fixed to the mounting member 3. The other end 6b of the second piezoelectric element 6 is fixed to the mounting member 3 so that the second fixed contact 7 is in a symmetrical position with respect to the first fixed contact 5 with respect to the straight line connecting both ends of the leaf spring 1. There is.

第1図aに示すような可動接点2が第一の固定
接点5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Aの
方向に微小ながら非常に高速で変位する。する
と、第一の固定接点5に接している飛行部材とし
ての可動接点2は、第一の圧電素子4から力を受
け加速され、第一の固定接点5を離れ飛行し、板
ばね1の両端を結ぶ直線と通過し板ばね1は反転
動作して、第1図bに示すように可動接点2が第
二の固定接点7に接した状態となる。また、第1
図bに示すような可動接点2が第二の固定接点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、可動接点2は第二の圧電素子6から矢
印Bの方向に力を受け加速され第二の固定接点7
を離れ第一の固定接点5の方に飛行し板ばね1は
再び反転動作し、第1図aに示すような可動接点
2が第一の固定接点5に接した状態となる。この
ようにして可動接点2を、第一の固定接点5から
第二の固定接点7へ、あるいは、第二の固定接点
7から第一の固定接点5へ切り替えることができ
る。
When a voltage is applied to the first piezoelectric element 4 in a state where the movable contact 2 is in contact with the first fixed contact 5 as shown in FIG. while displacing at a very high speed. Then, the movable contact 2 as a flying member that is in contact with the first fixed contact 5 is accelerated by receiving the force from the first piezoelectric element 4, flies away from the first fixed contact 5, and touches both ends of the leaf spring 1. The plate spring 1 is reversed and the movable contact 2 is in contact with the second fixed contact 7 as shown in FIG. 1b. Also, the first
The movable contact 2 is the second fixed contact 7 as shown in Figure b.
When a voltage is applied to the second piezoelectric element 6 from a state in which it is in contact with the movable contact 2, the movable contact 2 receives a force from the second piezoelectric element 6 in the direction of arrow B and is accelerated to the second fixed contact 7.
The leaf spring 1 moves in the opposite direction again, leaving the movable contact 2 in contact with the first fixed contact 5 as shown in FIG. 1A. In this way, the movable contact 2 can be switched from the first fixed contact 5 to the second fixed contact 7 or from the second fixed contact 7 to the first fixed contact 5.

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の発生力により
飛行部材としての可動接点2を加速し飛ばし板ば
ね1を反転動作させるため、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
う大きな可動接点2のストロークを得ることがで
き、また、大きな接触力も得られいる。
In the present invention, the movable contact 2 as a flight member is accelerated by the force generated by the first or second piezoelectric elements 4, 6 when a voltage is applied, and the fly leaf spring 1 is reversed. It is possible to obtain a stroke of the movable contact 2 that is several tens to hundreds of times larger than the amount of displacement of the second piezoelectric elements 4 and 6, and also to obtain a large contact force.

さらに、飛行部材としての可動接点2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ているため、低電力、低発熱
で磁気干渉がなくなる。
Furthermore, since a piezoelectric element known for its high energy conversion efficiency is used as a drive source for the movable contact 2 as a flying member, there is no magnetic interference with low power consumption and low heat generation.

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

上述の例では、可動接点2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つても可
動接点2を切り替えることができる。このような
使い方は、従来のラツチ型電磁アクチユエータに
おいてはできなかつた。
In the above example, to switch the movable contact 2,
Although a voltage is applied alternately to the first piezoelectric element 4 and the second piezoelectric element 6, the movable contact 2 can also be applied by simultaneously applying a voltage to the first piezoelectric element 4 and the second piezoelectric element 6. Can be switched. Such usage has not been possible with conventional latch type electromagnetic actuators.

なお圧電素子への電圧の印加はパルス的に破約
立ち上げる必要があるが、パルス幅は短くてもよ
い。例えばパルス幅は0.1ms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
つて発熱もしない。
Note that the voltage applied to the piezoelectric element must be started up 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 even if voltage is continuously applied for a long time, and therefore does not generate heat.

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、取付部材8の形状が前述の実施
例と異なる。なお取付部材の形状にかかわらず本
発明の効果は同様に発揮されることは言うまでも
ない。
FIG. 2 is a perspective view showing another embodiment in which the present invention is applied to a relay, and the shape of the mounting member 8 is different from that of the previous embodiment. It goes without saying that the effects of the present invention can be similarly exhibited regardless of the shape of the mounting member.

第3図は本発明を表示器に適用した一実施例を
示す図である。第3図aにおいて、飛行部材9と
第一の表示板11の接続した板ばね1は、取付部
材3に設けられた支持部としての溝3a,3bに
そう入され軸力を受け湾曲し、飛行部材9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3図bに示すよう
に、板ばね1が反転した場合、飛行部材9が接す
るように取付部材3に接続している。また、第二
の表示板12は、板ばね1が反転した場合、第一
の表示板11が上に重なるような位置に取付部材
3に取り付けられている。さらに、第二の表示板
12の上に窓10が設けられており、外部からは
窓10の所しか見えない。
FIG. 3 is a diagram showing an embodiment in which the present invention is applied to a display device. In FIG. 3a, the leaf spring 1 connected to the flight member 9 and the first display board 11 is inserted into grooves 3a and 3b as supporting parts provided in the mounting member 3, and is bent by receiving an axial force. A flying member 9 is in contact with a first piezoelectric element 4 connected to a mounting member 3. The second piezoelectric element 6 is connected to the mounting member 3 in such a way that the flight member 9 comes into contact with it when the leaf spring 1 is reversed, as shown in FIG. 3b. Further, the second display plate 12 is attached to the mounting member 3 at a position where the first display plate 11 overlaps when the leaf spring 1 is reversed. Furthermore, a window 10 is provided above the second display board 12, and only the window 10 can be seen from the outside.

いま、第3図aに示すように第一の表示板11
に「使用中」、第二の表示板12に「空」という
文字が書かれている場合について説明する。飛行
部材9が、第3図aに示すように、第一の圧電素
子4に接している場合、外部からは窓10を通し
て第二の表示板12上に書かれた「空」という文
字が見える。この状態から第一の圧電素子4に電
圧を印加すると、飛行部材9は第一の圧電素子4
から力を受け加速され、第一の圧電素子4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3図bに示すように飛行部
材9が第二の圧電素子6に接し、第一の表示板1
1が第二の表示板12の上に重なる。したがつて
外部からは窓10を通して第一の表示板11上に
書かれた「使用中」という文字が見えるようにな
る。また第3図bに示すような飛行部材9が第二
の圧電素子6に接している状態から第二の圧電素
子6に電圧を印加すると、板ばね1は再び反転動
作し、第3図aに示すような飛行部材9が第一の
圧電素子4に接した状態に戻り、第二の表示板1
2上に書かれた「空」という文字が見えるように
なる。
Now, as shown in FIG. 3a, the first display board 11
A case will be explained in which the characters "in use" are written on the second display board 12 and the characters "empty" are written on the second display board 12. When the flying member 9 is in contact with the first piezoelectric element 4 as shown in FIG. 3a, the word "sky" written on the second display board 12 can be seen from the outside through the window 10. . When a voltage is applied to the first piezoelectric element 4 from this state, the flight member 9
The flying member 9 flies away from the first piezoelectric element 4 and passes through the straight line connecting both ends of the leaf spring 1, causing the leaf spring 1 to perform a reversal operation and the flying member 9 to move to the second position as shown in FIG. 3b. The first display plate 1 is in contact with the second piezoelectric element 6.
1 overlaps on the second display board 12. Therefore, the words "in use" written on the first display board 11 can be seen from the outside through the window 10. Further, when a voltage is applied to the second piezoelectric element 6 from a state where the flight member 9 is in contact with the second piezoelectric element 6 as shown in FIG. The flying member 9 returns to the state in which it is in contact with the first piezoelectric element 4 as shown in FIG.
2 The word "sky" written above becomes visible.

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い
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 this embodiment of the present invention, the effects of the present invention such as simple structure, small size, low power consumption, low heat generation, and no magnetic interference are similarly exhibited.

第4図は本発明を光路スイツチに適用した一実
施例を示す図である。第4図aにおいて、飛行部
材9は板ばね1の中央部に設けられており、ミラ
ー13は飛行部材9と板ばね1の固定端3aとの
中間に設けられている。また板ばね1は取付部材
3に設けられた支持部としての溝3a,3bにそ
う入され軸力を受けて湾曲し、飛行部材9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1が反転動作した場合、飛行部材9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 an optical path switch. In FIG. 4a, the flying member 9 is provided at the center of the leaf spring 1, and the mirror 13 is provided intermediate the flying member 9 and the fixed end 3a of the leaf spring 1. Further, the leaf spring 1 is inserted into grooves 3a and 3b as supporting parts provided in the mounting member 3, and is bent by receiving an axial force, and the flight member 9 is connected to the first piezoelectric element 4 connected to the mounting member 3. are in contact with each other. The second piezoelectric element 6 is connected to the mounting member 3 so that the flight member 9 comes into contact with it when the leaf spring 1 reverses, as shown in FIG. 4b.

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9が第一の圧電素子4に接し
ている場合、板ばね1は第一の圧電素子4の方へ
湾曲しているため、矢印Cの方向からの入射光は
ミラー13で反射され矢印Dの方向へ反射光とな
つて出て行く。この状態で第一の圧電素子4に電
圧を印加すると、飛行部材9は第一の圧電素子4
から力を受け加速され、第一の圧電素子4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4図bに示すように飛行部
材9が第二の圧電素子6に接した状態となる。し
たがつて板ばね1は第二の圧電素子6の方に湾曲
しミラー13の入射光に対する角度が変わるた
め、矢印Cの方向からの入射光は矢印Eの方へ反
射光となつて出て行く。また、第4図bに示すよ
うな飛行部材9が第二の圧電素子6に接している
状態から第二の圧電素子6に電圧を印加すると、
板ばね1は再び反転動作し第4図aに示すような
飛行部材9が第一の圧電素子4に接する状態に戻
る。このようにして光路を切り替えることができ
る。
In an embodiment of such a configuration, when the flying member 9 is in contact with the first piezoelectric element 4 as shown in FIG. 4a, the leaf spring 1 is curved toward the first piezoelectric element 4. Therefore, the incident light from the direction of arrow C is reflected by the mirror 13 and goes out in the direction of arrow D as reflected light. When a voltage is applied to the first piezoelectric element 4 in this state, the flight member 9
The flying member 9 flies away from the first piezoelectric element 4 and passes through a straight line connecting both ends of the leaf spring 1, causing the leaf spring 1 to perform a reversal operation, as shown in FIG. 4b. It comes into contact with the second piezoelectric element 6. Therefore, the leaf spring 1 curves toward the second piezoelectric element 6, and the angle of the mirror 13 with respect to the incident light changes, so that the incident light from the direction of the arrow C becomes reflected light in the direction of the arrow E. go. Further, when a voltage is applied to the second piezoelectric element 6 from a state where the flying member 9 is in contact with the second piezoelectric element 6 as shown in FIG. 4b,
The leaf spring 1 reverses again and returns to the state in which the flying member 9 is in contact with the first piezoelectric element 4 as shown in FIG. 4a. In this way, the optical path can be switched.

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い
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 this embodiment of the present invention, the effects of the present invention such as simple structure, small size, low power consumption, low heat generation, and no magnetic interference are similarly exhibited.

第5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5図
aにおいて、ペンホルダ14を接続した板ばね1
は、取付部材3に設けられた支持部としての溝3
a,3bにそう入され軸力を受け第一の圧電素子
4の方へ湾曲している。そして板ばね1に設けら
れた飛行部材9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5図bに示すように、板ばね1が反転した場
合、飛行部材9が接するように取付部材3に接続
している。またペン15はペンホルダ14に支持
されている。
FIG. 5 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. 5a, the leaf spring 1 to which the pen holder 14 is connected
is a groove 3 as a support provided in the mounting member 3.
a, 3b, and is bent toward the first piezoelectric element 4 by receiving an axial force. A flying member 9 provided on the leaf spring 1 is in contact with a first piezoelectric element 4 connected to the mounting member 3. The second piezoelectric element 6 is
As shown in FIG. 5b, when the leaf spring 1 is reversed, it is connected to the mounting member 3 so that the flight member 9 comes into contact with it. Further, the pen 15 is supported by the pen holder 14.

このような構成の実施例において、第5図aに
示すように飛行部材9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9は第一の圧電素子4から力を受
け加速され、第一の圧電素子4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5図bに示すような飛行部材9が第二
の圧電素子6に接した状態となる。したがつてペ
ン15は上から下に降り印字できる。また第5図
bに示すような飛行部材9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1は再び反転動作し第5図aに示すよ
うな飛行部材9が第一の圧電素子4に接した状態
に戻る。このようにしてペン15を昇降させるこ
とができる。
In an embodiment with such a configuration, when a voltage is applied to the first piezoelectric element 4 while the flying member 9 is in contact with the first piezoelectric element 4 as shown in FIG. 5a, the flying member 9 It is accelerated by the force from the first piezoelectric element 4, flies away from the first piezoelectric element 4, passes through a straight line connecting both ends of the leaf spring 1, and the leaf spring 1 performs a reverse operation, as shown in FIG. 5b. The flying member 9 is in contact with the second piezoelectric element 6. Therefore, the pen 15 can descend from the top to the bottom to print. Further, when a voltage is applied to the second piezoelectric element 6 with the flight member 9 in contact with the second piezoelectric element 6 as shown in FIG. 5b, the leaf spring 1 performs the reverse operation again as shown in FIG. 5a The flying member 9 returns to the state in which it is in contact with the first piezoelectric element 4. In this way, the pen 15 can be raised and lowered.

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い
という本発明の効果は同様に発揮されることは原
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, and no magnetic interference can be similarly exhibited.

第6図は本発明を流路の開閉器に適用した一実
施例を示す図である。第6図aにおいて、2個の
飛行部材16,17を設けた板ばね18は、取付
部材19に設けられた支持部としての溝19a,
19bにそう入され軸力を受け湾曲し、飛行部材
16,17は取付部材19に接続された2個の第
一の圧電素子20,21に接している。2個の第
二の圧電素子22,23は第6図bに示すよう
に、板ばね18が反転した場合、2個の飛行部材
16,17が接するように取付部材19に接続し
ている。さらに流路を開閉する弁24は板ばね1
8の中央とリンク25で結ばれている。
FIG. 6 is a diagram showing an embodiment in which the present invention is applied to a flow path switch. In FIG. 6a, the leaf spring 18 provided with the two flight members 16 and 17 has a groove 19a as a support provided in the mounting member 19,
The flying members 16 and 17 are inserted into the piezoelectric member 19b and curved by receiving an axial force, and are in contact with two first piezoelectric elements 20 and 21 connected to the mounting member 19. The two second piezoelectric elements 22, 23 are connected to the mounting member 19 so that when the leaf spring 18 is reversed, the two flying members 16, 17 are in contact with each other, as shown in FIG. 6b. Furthermore, the valve 24 that opens and closes the flow path is a leaf spring 1.
It is connected to the center of 8 by a link 25.

このような構成の実施例において、第6図aに
示すような飛行部材16,17が第一の圧電素子
20,21に接している状態では、弁24が流路
を閉じていないため流体は矢印Fのように流れる
ことができる。この状態で第一の圧電素子20,
21に電圧を印加すると、飛行部材16,17は
第一の圧電素子20,21から力を受け加速さ
れ、第一の圧電素子20,21を離れ飛行し板ば
ね18の両端を結ぶ直線を通過し板ばね18は反
転動作して第6図bに示すような飛行部材16,
17が第二の圧電素子22,23に接した状態と
なる。すると、弁24は板ばね18につながれた
リンク25により押されて、流路を閉じる。また
第6図bに示すような飛行部材16,17が第二
の圧電素子22,23に接している状態で、第二
の圧電素子22,23に電圧を印加すると板ばね
18は再び反転動作し第6図aに示すような飛行
部材16,17が第一の圧電素子20,21に接
した状態となり、流路を開く。
In an embodiment with such a configuration, when the flying members 16, 17 are in contact with the first piezoelectric elements 20, 21 as shown in FIG. 6a, the fluid does not flow because the valve 24 does not close the flow path. It can flow like arrow F. In this state, the first piezoelectric element 20,
When voltage is applied to 21, the flying members 16 and 17 are accelerated by the force from the first piezoelectric elements 20 and 21, fly away from the first piezoelectric elements 20 and 21, and pass through a straight line connecting both ends of the leaf spring 18. The leaf spring 18 reverses and moves the flying member 16 as shown in FIG. 6b.
17 is in contact with the second piezoelectric elements 22 and 23. The valve 24 is then pushed by the link 25 connected to the leaf spring 18, closing the flow path. Further, when a voltage is applied to the second piezoelectric elements 22, 23 with the flying members 16, 17 in contact with the second piezoelectric elements 22, 23 as shown in FIG. Then, the flying members 16 and 17 as shown in FIG. 6a come into contact with the first piezoelectric elements 20 and 21, opening a flow path.

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い
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 this embodiment of the present invention, the effects of the present invention such as simple structure, small size, low power consumption, low heat generation, and no magnetic interference are similarly exhibited.

なお、本発明は上述の実施例のみならず、さま
ざまなラツチ型アクチユ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、飛行部材を設
けた板ばねに軸力を加え湾曲させて、飛行部材を
飛ばす圧電素子を配置した構造にすることによつ
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 above-mentioned embodiments but also to various latch-type actuators with similar effects. The effects of the present invention are achieved by applying an axial force to a leaf spring provided with a flying member to curve it, and creating a structure in which a piezoelectric element is arranged to fly the flying member.

さらに上述の実施例においては、板ばねの湾曲
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 return means is used, the curved convex side of the leaf spring Even if the piezoelectric element is arranged only on the 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
電歪素子によつても同様の効果が得られる。
Further, in the present invention, similar effects can be obtained not only by a single-plate piezoelectric element having a longitudinal effect or a lateral effect, but also by a laminated piezoelectric element or 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いラツチ型圧電アクチユエ
ータが得られる。
(Effects of the Invention) According to the present invention, the structure is simple, small, low power,
A latch-type piezoelectric actuator with low heat generation and no magnetic interference can be obtained.

【図面の簡単な説明】[Brief explanation of 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、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図は本発明を表示器に適用
した一実施例を示す図、第4図は本発明を光路ス
イツチに適用した一実施例を示す図、第5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、第6図は本発明を流路の開
閉器に適用した一実施例を示す図である。 図において、1,18……板ばね、2……可動
接点、3,8,19……取付部材、4,20,2
1……第一の圧電素子、5……第一の固定接点、
6,22,23……第二の圧電素子、7……第二
の固定接点、9,16,17……飛行部材、10
……窓、11……第一の表示板、12……第二の
表示板、13……ミラー、14……ペンホルダ、
15……ペン、24……弁、25……リンク、を
それぞれ示す。
Fig. 1 is a diagram showing one 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, and Fig. 3 is a diagram showing an embodiment in which the present invention is applied to a display. FIG. 4 is a diagram showing an embodiment in which the present invention is applied to an optical path switch; FIG. 5 is a diagram showing an embodiment in which the present invention is applied to a pen lifting mechanism such as a pen recorder; FIG. 6 is a diagram showing an embodiment in which the present invention is applied to a flow path switch. In the figure, 1, 18...plate spring, 2...movable contact, 3, 8, 19...mounting member, 4, 20, 2
1... First piezoelectric element, 5... First fixed contact,
6, 22, 23... Second piezoelectric element, 7... Second fixed contact, 9, 16, 17... Flight member, 10
... window, 11 ... first display board, 12 ... second display board, 13 ... mirror, 14 ... pen holder,
15...Pen, 24...Valve, and 25...Link are shown, respectively.

Claims (1)

【特許請求の範囲】[Claims] 1 飛行部材を有する板ばねと、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、前記圧電素子へ立ち上がりの急峻な
電圧を印加する手段とから構成され、前記圧電素
子への前記急峻な電圧の印加により前記飛行部材
が前記圧電素子から力を受けて飛行し、飛行する
ことにより、前記板ばねを反転動作させることを
特徴とするラツチ型圧電アクチユエータ。
1 A leaf spring having a flight member, a support portion that supports the leaf spring in a curved manner, a piezoelectric element that applies force to the flight member in opposition to a convex surface of the curved leaf spring, and a piezoelectric element that applies a force to the flight member, and a and a means for applying a steep voltage to the piezoelectric element, and by applying the steep voltage to the piezoelectric element, the flying member receives a force from the piezoelectric element and flies, and by flying, the leaf spring is reversed. A latch-type piezoelectric actuator that operates.
JP60008612A 1983-03-20 1985-01-21 Latch type piezo-electric actuator Granted JPS61168833A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP60008612A JPS61168833A (en) 1985-01-21 1985-01-21 Latch type piezo-electric actuator
EP86300375A EP0189302B1 (en) 1985-01-21 1986-01-20 Piezoelectric latching actuator having an impact receiving projectile
DE8686300375T DE3681927D1 (en) 1985-01-21 1986-01-20 PIEZOELECTRIC BISTABLE ACTUATOR WITH A PROJECTILE THAT RECEIVES A SHOCK.
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
JP60008612A JPS61168833A (en) 1985-01-21 1985-01-21 Latch type piezo-electric actuator

Publications (2)

Publication Number Publication Date
JPS61168833A JPS61168833A (en) 1986-07-30
JPH057810B2 true JPH057810B2 (en) 1993-01-29

Family

ID=11697773

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60008612A Granted JPS61168833A (en) 1983-03-20 1985-01-21 Latch type piezo-electric actuator

Country Status (1)

Country Link
JP (1) JPS61168833A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4554054B2 (en) * 2000-09-21 2010-09-29 Necトーキン株式会社 Piezoelectric actuator
JP5533173B2 (en) * 2010-04-13 2014-06-25 いすゞ自動車株式会社 Fuel supply device
GB2532270B (en) * 2014-11-14 2017-05-10 Ge Aviat Systems Ltd An aircraft assembly with load and position indicator

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59175532A (en) * 1983-03-25 1984-10-04 日本電気株式会社 Piezoelectric relay

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59175532A (en) * 1983-03-25 1984-10-04 日本電気株式会社 Piezoelectric relay

Also Published As

Publication number Publication date
JPS61168833A (en) 1986-07-30

Similar Documents

Publication Publication Date Title
JP4238132B2 (en) Switching device especially for optical applications
US4303302A (en) Piezoelectric optical switch
US6465929B1 (en) Microelectromechanical system actuator for extended linear motion
US4736131A (en) Linear motor driving device
US6810163B2 (en) Optical switch and optical waveguide apparatus
KR100312432B1 (en) Optical Switch using Micro Structures
US20020113281A1 (en) MEMS device having an actuator with curved electrodes
JP2004538507A (en) Micro system switch
JPH057810B2 (en)
JPS61176176A (en) Latch-type piezoelectric actuator
JPS61176175A (en) Latch-type piezoelectric actuator
US6278223B1 (en) Differential type piezoelectric actuator
JPS61185834A (en) Latch type piezo-electric actuator
JP2006343482A (en) Optical scanner
JPS61187284A (en) Latch type piezoelectric actuator
JPS61218038A (en) Latch type piezo-electric actuator
JPS61218039A (en) Latch type piezo-electric actuator
JPS61168275A (en) Latch type piezoelectric actuator
JPS61218040A (en) Latch type piezo-electric actuator
JPS61216217A (en) Latch type piezo-electric actuator
JPS61216218A (en) Latch type piezo-electric actuator
JPH04368484A (en) Driver for moving body
JPS6010220A (en) Optical switch
JP4491064B2 (en) Optical path changing device, optical switch, and optical head
JPS61216219A (en) Latch type piezo-electric actuator

Legal Events

Date Code Title Description
EXPY Cancellation because of completion of term