JPS61168275A - Latch type piezoelectric actuator - Google Patents

Latch type piezoelectric actuator

Info

Publication number
JPS61168275A
JPS61168275A JP60008613A JP861385A JPS61168275A JP S61168275 A JPS61168275 A JP S61168275A JP 60008613 A JP60008613 A JP 60008613A JP 861385 A JP861385 A JP 861385A JP S61168275 A JPS61168275 A JP S61168275A
Authority
JP
Japan
Prior art keywords
movable member
piezoelectric element
contact
movable
piezoelectric
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
JP60008613A
Other languages
Japanese (ja)
Inventor
Tadayasu Uchikawa
内川 忠保
Takashi Oota
孝 太田
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 JP60008613A priority Critical patent/JPS61168275A/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 JPS61168275A publication Critical patent/JPS61168275A/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H57/00Electrostrictive relays; Piezoelectric relays
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H57/00Electrostrictive relays; Piezoelectric relays
    • H01H2057/003Electrostrictive relays; Piezoelectric relays the relay being latched in actuated position by magnet

Landscapes

  • General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)

Abstract

PURPOSE:To eliminate a magnetic interference with a simple structure, small- size, low power and low heating by applying a drive force to an inverting spring mechanism by a piezoelectric element. CONSTITUTION:A movable contact 3 is accelerated as a flying member by the forces generated at the first or second piezoelectric elements 5, 7 at voltage applying time, flown and a movable member is inverted. Thus, the stroke of the contact 3 of the magnitude of the times of several tens to several hundreds of the displacements of the elements 5, 7 can be obtained, and large contacting force is obtained. Further, since the piezoelectric element known as having high energy conversion efficiency is used as the drive source of the contact 3 as the member, magnetic interference is eliminated at low heating.

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ェエータ
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、ラッチ型のアクチェ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〇しかしながら
電磁アクチー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。
(Prior art and its problems) Conventionally, electromagnetic actuators using coils have been used as latch-type actuators. However, electromagnetic actuators generate a magnetic field by energizing the coil and utilize the magnetic force. In order to move the movable members, a large amount of input energy is required, resulting in 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いラッチ
型圧電アクチェエータを提供することにある〇 (発明の構成) 本発明によれば、一端が支持され自由端には飛行部材を
有する可動部材と、その可動部材と一端が接続され他端
を前記可動部材の支持部と距離を隔てて接続され前記可
動部材を傾かせる手段としてのラッチばねと、前記可動
部材の傾斜側に対向して前記飛行部材に力を与える電歪
又は圧電素子とから構成されることを特徴とするラッチ
型圧電アクチェエータが得られる。
(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, and no magnetic interference. Structure) According to the present invention, a movable member is supported at one end and has a flight member at a free end; A latch-type piezoelectric actuator is obtained, characterized in that it is composed of a latch spring as a means for tilting the member, and an electrostrictive or piezoelectric element that faces the tilted side of the movable member and applies force to the flight member. .

(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従来の電磁方式の欠点で
ある銅損、鉄損がなく、エネルギ変換効率の高い電歪ま
たは圧電素子を用いることにょシ低電力、低発熱で磁気
干渉がなくなる。
First, by using an electrostrictive or piezoelectric element with high energy conversion efficiency and without copper loss or iron loss, which are the disadvantages of conventional electromagnetic systems, as a drive source for flight components, low power consumption, low heat generation, and magnetic interference are eliminated.

また、可動部材は一端支持、他端自由の構成によ)片持
梁又はリンクの如き動作が可能でおるが。
Moreover, the movable member can be operated like a cantilever beam or a link (by having one end supported and the other end free).

その可動部材は、その可動部材の支持部より距離をへた
てて支持されたラッチはねと接合する。このときラッチ
はねには復帰力が作用するように接合し、その2ツチば
ねの復帰力によって可動部材はいづれか一方に傾けられ
る。との構成によシ、可動部材に力を与えて可動部材が
ラッチはねと可動部材の支持部を結ぶ延長線上を通過す
ると、可動部材はラッチはねの力により反転動作を起こ
しラッチされる。また、可動部材には飛行部材が設けら
れ可動部材の傾斜側に対向して飛行部材に力を与える電
歪又は圧電素子が配置されておシ、初期状態においては
いづれか一方の電歪又は圧電素子と飛行部材が接してい
る。そこで、電歪又は圧電素子に電圧を印加すると電歪
又は圧[素子は微少ながら非常に速く変位するため飛行
部材は電歪又は圧電素子よシカを受けて加速され電歪又
は圧電素子を離れ飛行し、これにょシ可動部材は回転動
作をする。その後可動部材がラッチはねと可動部材の支
持部を結ぶ延長線上を通多過ぎると可動部材はラッチば
ねの力にょ夛反転しラッチされる〇このとき飛行部材の
ストロークは電歪又は圧電素子の変位量よシもはるかに
大きい。
The movable member mates with a latch spring supported at a distance from the support of the movable member. At this time, the latch spring is joined so that a restoring force is applied, and the movable member is tilted to one side by the restoring force of the two-way spring. According to the configuration, when a force is applied to the movable member and the movable member passes over an extension line connecting the latch spring and the supporting portion of the movable member, the movable member undergoes a reversal action due to the force of the latch spring and is latched. . Further, the movable member is provided with a flying member, and an electrostrictive or piezoelectric element is arranged opposite to the inclined side of the movable member to apply force to the flying member, and in the initial state, either one of the electrostrictive or piezoelectric elements is disposed. and the flying parts are in contact with each other. Therefore, when a voltage is applied to an electrostrictive or piezoelectric element, the electrostrictive or piezoelectric element displaces very quickly, although slightly, so the flying member is accelerated by the electrostrictive or piezoelectric element, leaves the electrostrictive or piezoelectric element, and flies away. However, the movable member rotates accordingly. After that, when the movable member passes over the extension line connecting the latch spring and the supporting part of the movable member, the movable member is reversed by the force of the latch spring and is latched. At this time, the stroke of the flying member is caused by the electrostrictive or piezoelectric element. The amount of displacement is also much larger.

(実施例) 以下1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) An example of the present invention will be described below in detail with reference to the drawings.

第1(a)図は本発明をリレーに適用した一爽施例を示
す模式的な斜視図であシ、第1(b)図は(a)図の動
作を説明するだめの図である。第1−(a)価)図にお
いて、可動部材1は一端がベース2で回転支持され、他
端が自由の構成をとる。また、可動部材1の自由端部に
は飛行部材としての可動接点3が設けられておル、かつ
、可動部材1には2ツチばね4が設けられている。さら
にラッチばね4は可動部材1の支持部と距離をへだてて
ベース2に接続されている。このとき、可動部材lはラ
ッチばね4の復帰力によ勺いずれか一方に傾けられ、可
動接点3は可動接点3に対応するように設けられた第一
の圧電素子5とその第一の圧電素子5上に接合された第
一の固定接点6に予圧を与えるように支持されている。
FIG. 1(a) is a schematic perspective view showing a refreshing example in which the present invention is applied to a relay, and FIG. 1(b) is a diagram for explaining the operation of FIG. 1(a). . In Figure 1-(a), a movable member 1 has one end rotatably supported by a base 2 and the other end free. Further, a movable contact 3 as a flying member is provided at the free end of the movable member 1, and a two-way spring 4 is provided on the movable member 1. Further, the latch spring 4 is connected to the base 2 at a distance from the support portion of the movable member 1. At this time, the movable member 1 is tilted to either side by the restoring force of the latch spring 4, and the movable contact 3 is connected to the first piezoelectric element 5 provided so as to correspond to the movable contact 3. It is supported so as to apply preload to the first fixed contact 6 bonded on the element 5.

一方、第一の圧電素子5に対向して、可動部材lの支持
部に対称となるように第二の圧電素子7が配置され、ま
た第二の圧電素子7上には第二の固定接点8が接合され
ている。
On the other hand, a second piezoelectric element 7 is disposed opposite to the first piezoelectric element 5 and symmetrically to the supporting part of the movable member l, and a second fixed contact is disposed on the second piezoelectric element 7. 8 are joined.

このような構造において、第一の圧電素子5に電圧が印
加されると、微少ながら高速に変位を生じる。このとき
、第一の固定接点6に接して支持されている可動接点3
は第一の圧電素子5から力を受は加速され、第一の固定
接点6を離れ飛行し、可動接点3がベース2の可動部材
lとラッチばね4の支持部を結ぶ延長線上金超えると可
動部材lはラッチばね4の復帰力によル反転動作し、第
1−(b)図のように可動接点3は第二の固定接点8に
接した状態となる。また次に、第二の圧電素子7に電圧
を印加すると可動接点3は第二の固定接点8を離れ第一
の固定接点6の方向に飛行し、再び反転動作をして第一
の固定接点6に接した状態となる0このようにして、可
動接点3を第一の固定接点6から第二の固定接点8へ、
あるいは第二の固定接点8から第一の固定接点6へ切)
替えることができる。
In such a structure, when a voltage is applied to the first piezoelectric element 5, a small but rapid displacement occurs. At this time, the movable contact 3 supported in contact with the first fixed contact 6
receives a force from the first piezoelectric element 5, is accelerated, flies away from the first fixed contact 6, and when the movable contact 3 crosses the extension line connecting the movable member l of the base 2 and the support part of the latch spring 4, The movable member 1 is reversely operated by the return force of the latch spring 4, and the movable contact 3 is brought into contact with the second fixed contact 8 as shown in FIG. 1-(b). Next, when a voltage is applied to the second piezoelectric element 7, the movable contact 3 leaves the second fixed contact 8 and flies in the direction of the first fixed contact 6, and then reverses again and returns to the first fixed contact. In this way, the movable contact 3 is moved from the first fixed contact 6 to the second fixed contact 8,
or from the second fixed contact 8 to the first fixed contact 6)
It can be changed.

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5,7の発生力にょシ飛行部材として
の可動接点3t−加速し飛ばし可動部材1i反転動作さ
せるため、第一あるいは第二の圧電素子5,7の変位量
の数十倍から数百倍という大きな可動接点3のストロー
クを得ることかでき、また、大きな接触力も得られる。
In the present invention, when a voltage is applied, the force generated by the first or second piezoelectric elements 5, 7 accelerates the movable contact 3t as a flying member, and inverts the movable member 1i. It is possible to obtain a stroke of the movable contact 3 that is several tens to hundreds of times larger than the amount of displacement of the second piezoelectric elements 5 and 7, and also to obtain a large contact force.

さらに、飛行部材としての可動接点3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, as a drive source for the movable contact 3 as a flight member,
Since it uses a piezoelectric element known for its high energy conversion efficiency, it has low power consumption, low heat generation, and eliminates magnetic interference.

そのうえ、コイルがなく、可動部材lとラッチばね4に
よう反転ばねとしてラッチ動作全行わせているため構造
が単純で小型となる。
Moreover, since there is no coil and the movable member 1 and the latch spring 4 perform all the latching operations as reversing springs, the structure is simple and compact.

上述の例では、可動接点3金切り替えるのに、第一の圧
電索子5と第二の圧電素子7に交互に電圧を印加したが
、第一の圧電素子5と第二の圧電素子7に同時に電圧を
印加することによっても可動接点3f:切り替えること
ができる。このような使い方は、従来のラッチ型電磁ア
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 5 and the second piezoelectric element 7 to switch the movable contact. The movable contact 3f can also be switched by simultaneously applying a voltage. This type of 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速く立ち上げ
る必要があるが、パルス幅は短くてもよい口例えばパル
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
がなくしたがって発熱もしない。、 第2図は本発明’t IJシレー適用した他の実施例を
示す模式的な斜視図である。第2図において、可動部材
9は門型の形状でベースIOに支持され、ラッチはね4
は可動部材9の中央部に配置されている。また可動部材
9には飛行部材としての可動接点3が設けられている。
Note that the voltage applied to the piezoelectric element needs to be raised quickly in the form of a pulse, but the pulse width may be short; for example, a pulse width of 0.1 ms is sufficient, and it does not matter if it is long. 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. FIG. 2 is a schematic perspective view showing another embodiment to which the present invention't IJ relay is applied. In FIG. 2, the movable member 9 has a portal shape and is supported by the base IO, and the latch 4
is arranged at the center of the movable member 9. The movable member 9 is also provided with a movable contact 3 as a flying member.

さらに可動接点3に相対するように第一の圧電素子5と
第二の圧電索子7が配置され、各々の素子上には第一の
固定接点6と第二の固定接点8が接合されている。この
ような構造においても、第一の圧電素子5の励起によシ
可動接点3は第一の固定接点6から第二の固定接点8へ
切シ替わることができ、前述の実施例と同様の効果が得
られる。
Furthermore, a first piezoelectric element 5 and a second piezoelectric cable 7 are arranged so as to face the movable contact 3, and a first fixed contact 6 and a second fixed contact 8 are connected to each element. There is. Even in such a structure, the movable contact 3 can be switched from the first fixed contact 6 to the second fixed contact 8 by excitation of the first piezoelectric element 5, and the same effect as in the previous embodiment is achieved. Effects can be obtained.

第3図は、他の実施例を示す斜視図であり、可動部材1
1は板はね12で支持されている。また、−可動部材1
1には可動接点3、及びラッチはね4が設けられている
。可動部材11はこのような板はね12による支持でも
適用でき本発明では同様の効果が得られる。またラッチ
ばね4はコイルばねの他、引張力が発生するならば板は
ねでも良い。
FIG. 3 is a perspective view showing another embodiment, in which the movable member 1
1 is supported by a plate spring 12. Also, - movable member 1
1 is provided with a movable contact 3 and a latch spring 4. The movable member 11 can be supported by such a plate spring 12, and similar effects can be obtained in the present invention. In addition to the coil spring, the latch spring 4 may be a plate spring if a tensile force is generated.

第4図は本発明を光路スイッ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13は可
動部材14に設けられ、また可動部材14の先端にミラ
ー15が設けられている。また、可動部材14はベース
16によ)支持され、またラッチばね4の力によシ飛行
部材13は第一の圧電素子5に接している。第二の圧電
素子7は第4図(b)に示すように可動部材14が反転
動作したとき飛行部材13と接するように配置されてい
る。
FIG. 4 is a diagram showing an embodiment in which the present invention is applied to an optical path switch. In FIG. 4(a), the flight member 13 is provided on a movable member 14, and a mirror 15 is provided at the tip of the movable member 14. Furthermore, the movable member 14 is supported by the base 16, and the flying member 13 is in contact with the first piezoelectric element 5 due to the force of the latch spring 4. The second piezoelectric element 7 is arranged so as to be in contact with the flight member 13 when the movable member 14 performs a reversal operation, as shown in FIG. 4(b).

このような構成において、第4図(atの状態において
は矢印Cの方向からの入射光はミラー15で反射し矢印
りの方向へ反射光となって出て行く。この状態で第一の
圧電素子5を励起すると飛行部材13は第一の圧電索子
5から力を受は飛行し、それとともに可動部材14は回
転動作し、飛行部材13がベース16上の可動部材14
とラッチばね4の支持部を結ぶ延長線上を超えると可動
部材14はラッチばね4の復帰力によシ反転動作し、第
4図(b)の状態となる。したがってミ2−15の回転
により入射光に対する角度も変わ9.矢印Cの方向から
の入射光は矢印Eの方へ反射光となって出て行く。まだ
、第4図(blに示すような飛行部材13が第二の圧電
索子7に接している状態から第二の圧電素子7に電圧を
印加すると可動部材14は再び反転動作し第4図f、)
に示すような飛行部材13が第一の圧電索子5に接する
状態に戻る。このようにして光路を切シ替えることがで
きる。
In such a configuration, in the state shown in FIG. When the element 5 is excited, the flying member 13 receives a force from the first piezoelectric cable 5 and flies. At the same time, the movable member 14 rotates, and the flying member 13 moves toward the movable member 14 on the base 16.
When the movable member 14 crosses the extension line connecting the support portion of the latch spring 4 and the support portion of the latch spring 4, the movable member 14 reverses itself due to the restoring force of the latch spring 4, and enters the state shown in FIG. 4(b). Therefore, due to the rotation of Mi2-15, the angle to the incident light also changes9. Incident light from the direction of arrow C goes out in the direction of arrow E as reflected light. If a voltage is applied to the second piezoelectric element 7 while the flying member 13 is still in contact with the second piezoelectric cable 7 as shown in FIG. f,)
The flying member 13 returns to the state in which it is in contact with the first piezoelectric cord 5 as shown in FIG. 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〇 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1、)において
、ペンホルダ17を設けた可動部材18はラッチはね4
により第一の圧電素子5の方へ傾けられ、飛行部材13
と第一の圧電素子5とが接している。また第二の圧電素
子7は可動部材18の支持部に関して対称に配置されて
いる。さらにペン19はペンホルダ17に支持されてい
る。
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 are similarly exhibited. FIG. 2 is a diagram showing an example in which the method is applied to a pen lifting mechanism such as a pen recorder. In FIG. 5 1), the movable member 18 provided with the pen holder 17 is attached to the latch spring 4.
is tilted towards the first piezoelectric element 5 by the flying member 13
and the first piezoelectric element 5 are in contact with each other. Further, the second piezoelectric element 7 is arranged symmetrically with respect to the support portion of the movable member 18. Furthermore, the pen 19 is supported by the pen holder 17.

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13が第一の圧電索子5に接している状
態で、第一の圧11を索子5に電圧を印加すると、飛行
部材13は第一の圧電素子5から力を受は加速され、第
一の圧電素子5金離れ飛行し可動部材18とラッチばね
4の支持部金納ぶ直線を通過すると可動部材18は反転
動作して、第5図(b)に示すような飛行部材13が第
二の圧電素子7に接した状態となる。したがってペン1
9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13が第二の圧電素子7に接した状態
で、第二の圧電素子7に電圧を印加すると可動部材18
は再び反転動作し第5図(alに示すような飛行部材1
3が第一の圧電素子5に接した状態に戻る。このように
してベン19を昇降させることができる。
In an embodiment with such a configuration, a voltage is applied to the first pressure 11 to the piezoelectric cable 5 while the flight member 13 is in contact with the first piezoelectric cable 5 as shown in FIG. 5(a). Then, the flying member 13 receives a force from the first piezoelectric element 5 and is accelerated, and when the first piezoelectric element 5 flies away from the movable member 13 and passes through the straight line between the movable member 18 and the support part of the latch spring 4, the movable member 18 The reversing operation brings the flying member 13 into contact with the second piezoelectric element 7 as shown in FIG. 5(b). Therefore pen 1
9 can be printed from top to bottom. Further, when a voltage is applied to the second piezoelectric element 7 with the flying member 13 in contact with the second piezoelectric element 7 as shown in FIG. 5(b), the movable member 18
is reversed again and the flying member 1 as shown in Fig. 5 (a.
3 returns to the state in which it is in contact with the first piezoelectric element 5. In this way, the ben 19 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言うまでもない〇 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(alにおいて、可動部材20はラ
ッチばね4によシ第一の圧電素子5(2)方へ傾けられ
、可動部材20上の飛行部材13と第一の圧電素子5と
が接している。また第二の圧電素子7は可動部材20の
支持部に関して対称に配置されている。一方、可動部材
20と弁21はリンク22によシ接続されている。
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 are similarly exhibited. FIG. 6 shows the present invention. It is a figure which shows one Example which applied this to the switch of a flow path. In FIG. 6 (al), the movable member 20 is tilted toward the first piezoelectric element 5 (2) by the latch spring 4, and the flying member 13 on the movable member 20 and the first piezoelectric element 5 are in contact with each other. Further, the second piezoelectric element 7 is arranged symmetrically with respect to the support portion of the movable member 20. On the other hand, the movable member 20 and the valve 21 are connected by a link 22.

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13が第一の圧電素子5に接している状
態では、弁21が流路を閉じていないため流体は矢印F
θ)ように流れることができる。
In an embodiment with such a configuration, when the flying member 13 is in contact with the first piezoelectric element 5 as shown in FIG.
θ).

この状態で第一の圧電素子5に電圧全印加すると、飛行
部材13は第一の圧電素子5から力を受は加速され、第
一の圧電素子5金離れ飛行し可動部材20とラッチばね
4の支持部を結ぶ直線を通過すると可動部材20は反転
動作して、第6図(b)に示すような飛行部材13が第
二の圧電素子7に接した状態となる口すると、弁21は
可動部材20につながれたリンク22によル押されて、
流路を閉じる。また第6図(b)に図すような飛行部材
13が第二の圧電素子7に接している状態で、第二の圧
電素子7に電圧を印加すると可動部材20は再び反転動
作し第6図(、)に示すような飛行部材13が第一の圧
電素子5に接した状態となり、流路を開く。
When the full voltage is applied to the first piezoelectric element 5 in this state, the flying member 13 receives the force from the first piezoelectric element 5 and is accelerated, the first piezoelectric element 5 flies away from the movable member 20 and the latch spring 4. When the movable member 20 passes through the straight line connecting the supporting parts, the movable member 20 reverses and the flying member 13 comes into contact with the second piezoelectric element 7 as shown in FIG. 6(b). Pushed by the link 22 connected to the movable member 20,
Close the channel. Further, when a voltage is applied to the second piezoelectric element 7 while the flight member 13 is in contact with the second piezoelectric element 7 as shown in FIG. The flying member 13 as shown in FIG.

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.

また、本発明の他の実施例として湾曲はねを用いたラッ
チ型リレーの一実施例を第7図(at、 (b)に示す
。第7図(,1は模式的な斜視図を示し、第7図(bl
は(,1の動作を説明するだめの図である。第7図にお
いて、可動部材23は一端支持、他端自由で片持梁又は
リンクの如き回転動作が可能である。
Further, as another embodiment of the present invention, an embodiment of a latch type relay using a curved spring is shown in FIGS. , Figure 7 (bl
(1) is a diagram for explaining the operation of (1). In FIG. 7, the movable member 23 is supported at one end, free at the other end, and can rotate like a cantilever beam or a link.

一方、その可動部材23の支持部から離れた支持部と可
動部材23の自由端部とで挾むようにし、またなおかつ
湾曲するようにラッチばね24を支持する。このラッチ
ばね24は圧縮ばねと同様の作用をして可動部材23に
力を与え、いづれか一方に傾けられる。またこの構成に
おいて可動部材に力を与え傾きを減少する方向に戻すと
きラッチばね24と可動部材23の支持部を結ぶ延長線
を通過すると可動部材23にはラッチばね24の作設け
られておシ、可動部材23の傾斜側に対向して可動接点
3に力會与える電歪又は圧電素子5゜7が配置され、定
常時にはいづれか一方の電歪又・ は圧電素子5,7上
の固定接点6,8と可動接点3とが接している。そこで
、電歪又は圧電素子5゜7に電圧を印加すると電歪又は
圧電素子5,7は衆知のように微少ながら非常に速く変
位を生じるため可動接点3は電歪又は圧電素子5.7よ
シカを受けて加速され電歪又は圧電素子5,7を離れ飛
行するとともに可動部材23も回転動作を起こす。その
後回動部材23がラッチばね24と可動部材23の支持
部を結ぶ延長線上を通過すると可動部材23はラッチば
ね24の圧縮力により今までの位置と反射側に反転しラ
ッチされる。このときの可動接点3又は可動部材23の
ストロークは電歪又は圧電素子の生じる変位量よシも極
めて大きい量が得られる。このようにラッチはね24の
ように板ばねを湾曲してその復帰力を用いたものにも適
用できる。
On the other hand, the latch spring 24 is supported so as to be sandwiched between the free end portion of the movable member 23 and a support portion remote from the support portion of the movable member 23, and to be curved. This latch spring 24 acts similar to a compression spring to apply force to the movable member 23 so that it can be tilted to either side. In addition, in this configuration, when a force is applied to the movable member to return it in the direction of decreasing the inclination, when the extension line connecting the latch spring 24 and the support portion of the movable member 23 is passed, the movable member 23 is provided with the latch spring 24 and the movable member 23 is provided with the latch spring 24. , an electrostrictive or piezoelectric element 5゜7 that applies force to the movable contact 3 is arranged facing the inclined side of the movable member 23, and in a steady state, a fixed contact 6 on one of the electrostrictive or piezoelectric elements 5, 7 , 8 and the movable contact 3 are in contact with each other. Therefore, when a voltage is applied to the electrostrictive or piezoelectric elements 5 and 7, the electrostrictive or piezoelectric elements 5 and 7 produce a slight but very fast displacement as is well known, so the movable contact 3 The movable member 23 is accelerated by the deer, leaves the electrostrictive or piezoelectric elements 5 and 7, and flies, and the movable member 23 also rotates. Thereafter, when the rotating member 23 passes over the extension line connecting the latch spring 24 and the support portion of the movable member 23, the movable member 23 is reversed from its previous position to the reflection side by the compressive force of the latch spring 24 and is latched. At this time, the stroke of the movable contact 3 or the movable member 23 is extremely large compared to the amount of displacement generated by the electrostrictive or piezoelectric element. In this way, the present invention can also be applied to a latch spring 24 in which a leaf spring is bent and its return force is used.

また第8図、第9図のようにラッチばね24と可動部材
23を一体にしたリレーも本発明は可能であり、同様の
効果が得られる。
Further, the present invention can be applied to a relay in which the latch spring 24 and the movable member 23 are integrated as shown in FIGS. 8 and 9, and similar effects can be obtained.

なお、本発明は上述の実施のみならず、さまざまなラッ
チ型アクチュエータに適用でき同様の効果が得られる。
Note that the present invention can be applied not only to the above implementation but also to various latch type actuators and similar effects can be obtained.

本発明の効果は、飛行部材を設けた可動部材に支持端を
異にした2ツチばねを接続し、飛行部材を飛ばす圧電素
子を配置した構造によって発揮されるものである。また
本発明にお(八ては縦効果や横効果のある単板の圧電素
子の他。
The effects of the present invention are achieved by a structure in which two springs with different support ends are connected to a movable member provided with a flying member, and a piezoelectric element for making the flying member fly is arranged. The present invention also includes a single-plate piezoelectric element having a vertical effect or a horizontal effect.

積層型の圧電素子、さらには電歪素子によっても同様の
効果が得られ適用が可能である。
Similar effects can be obtained and applied to laminated piezoelectric elements and even electrostrictive elements.

また本発明においては、可動部材の両側に2個の圧電素
子全配置しているが、復帰手段を用いることによk)1
個の圧電素子でも可能である。
In addition, in the present invention, two piezoelectric elements are all arranged on both sides of the movable member, but by using a return means k)1
It is also possible to use a single piezoelectric element.

(発明の効果) 本発明によれば、構造が簡単で小型、低電力。(Effect of the invention) According to the present invention, the structure is simple, small, and low power.

低発熱で磁気干渉のないラッチ型圧電アクチーエータが
得られる。
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ta+は本発明をリレーに適用した一実施例を示
す図、第1図(b)は(a)の動作を説明するだめの図
、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図は本発明の他の実施例を示す図、第4図は本
発明を光路スイッ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、第7図、第8図、第9図は
本発明をリレーに適用した他の実施例を示す図である。 図中各記号はそれぞれ次の内容を示す。 1+  9t  11+  14+  18t  20
t  23・・・可動部材s L  10t  16・
・・ベース、3・・・可動接点、4.24・・・ラッチ
ばね、5・・・第一の圧電素子、6・・・第一の固定接
点、7・・・第二の圧電素子、8・・・第二の固定接点
、12・・・板ばね、13・・・飛行部材、15・・・
ミ7−,17・・・ペンホルダ、19・・・ペン、21
・・・弁、22・・・リンク。 ;11′t  図 (a) (b) オ 5 図 (a) (b) 21−6  図 (a) 7第二の圧電素子 (b) 諏 78図 79図 □ 一23可動部材
Fig. 1 (ta+) is a diagram showing an embodiment in which the present invention is applied to a relay, Fig. 1 (b) is a diagram for explaining the operation of (a), and Fig. 2 is a diagram showing an embodiment in which the present invention is applied to a relay. FIG. 3 is a diagram showing another embodiment of the present invention. FIG. 4 is a diagram showing an embodiment in which the present invention is applied to an optical path switch.
The figures show an embodiment in which the present invention is applied to a pen lifting mechanism such as a pen recorder, FIG. 6 shows an embodiment in which the present invention is applied to a flow path switch, and FIGS. 8 and 9 are diagrams showing other embodiments in which the present invention is applied to a relay. Each symbol in the figure indicates the following content. 1+ 9t 11+ 14+ 18t 20
t 23...Movable member s L 10t 16.
... Base, 3... Movable contact, 4.24... Latch spring, 5... First piezoelectric element, 6... First fixed contact, 7... Second piezoelectric element, 8... Second fixed contact, 12... Leaf spring, 13... Flight member, 15...
Mi7-, 17... Pen holder, 19... Pen, 21
... Valve, 22... Link. ;11't Figure (a) (b) O 5 Figure (a) (b) 21-6 Figure (a) 7 Second piezoelectric element (b) 78 Figure 79 Figure □ - 23 Movable member

Claims (1)

【特許請求の範囲】[Claims] 一端が支持され自由端には飛行部材を有する可動部材と
、その可動部材と一端が接続され、他端を前記可動部材
の支持部と距離を隔てて接続され、前記可動部材を傾か
せる手段としてのラッチばねと、前記可動部材の傾斜側
に対向して前記飛行部材に力を与える電歪又は圧電素子
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 movable member having one end supported and a free end having a flight member, one end connected to the movable member, and the other end connected at a distance to a supporting portion of the movable member, and a means for tilting the movable member. A latch type piezoelectric actuator comprising: a latch spring; and an electrostrictive or piezoelectric element that faces the inclined side of the movable member and applies force to the flight member.
JP60008613A 1983-03-20 1985-01-21 Latch type piezoelectric actuator Pending JPS61168275A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP60008613A JPS61168275A (en) 1985-01-21 1985-01-21 Latch type piezoelectric 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
JP60008613A JPS61168275A (en) 1985-01-21 1985-01-21 Latch type piezoelectric actuator

Publications (1)

Publication Number Publication Date
JPS61168275A true JPS61168275A (en) 1986-07-29

Family

ID=11697799

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60008613A Pending JPS61168275A (en) 1983-03-20 1985-01-21 Latch type piezoelectric actuator

Country Status (1)

Country Link
JP (1) JPS61168275A (en)

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