JPS61215064A - Printing hammer - Google Patents

Printing hammer

Info

Publication number
JPS61215064A
JPS61215064A JP5733285A JP5733285A JPS61215064A JP S61215064 A JPS61215064 A JP S61215064A JP 5733285 A JP5733285 A JP 5733285A JP 5733285 A JP5733285 A JP 5733285A JP S61215064 A JPS61215064 A JP S61215064A
Authority
JP
Japan
Prior art keywords
hammer
flight
printing
permanent magnet
flight hammer
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
JP5733285A
Other languages
Japanese (ja)
Inventor
Takashi Oota
孝 太田
Tadayasu Uchikawa
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 JP5733285A priority Critical patent/JPS61215064A/en
Publication of JPS61215064A publication Critical patent/JPS61215064A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B41PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41JTYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
    • B41J2/00Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
    • B41J2/22Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by selective application of impact or pressure on a printing material or impression-transfer material
    • B41J2/23Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by selective application of impact or pressure on a printing material or impression-transfer material using print wires
    • B41J2/27Actuators for print wires
    • B41J2/295Actuators for print wires using piezoelectric elements

Landscapes

  • Impact Printers (AREA)

Abstract

PURPOSE:To attain to enhance a printing speed by effectively and rapidly suppressing rebound, by attracting the flight hammer driven by a piezoelectric element by a permanent magnet. CONSTITUTION:In a printing hammer for a dot impact type printer, when a flight hammer 13 is contacted with the force transmitting member 15 connected to the leading end of a piezoelectric element 11, the magnetic flux generated from a permanent magnet 18 passes through a first yoke 16, the flight hammer 13 and a second yoke 17 to be returned to the permanent magnet 18 as shown by an arrow B. Therefore, attraction force acts on the flight hammer 13. Because the flight hammer 13 flies out forwardly during printing operation, the magnetic flux generated from the permanent magnet 18 reaches the second yoke 17 through the first yoke 16 and does not pass through the flight hammer 13 and, therefore, almost no attraction force 13 acts on the flight hammer 13. Because large attraction force acts only when the flight hammer 13 is contacted with the force transmitting member 15 as mentioned above, rebound can be rapidly suppressed without almost exerting adverse effect on printing operation.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、圧電素子を用いたドツトインパクト型プリン
タ用の印字ハンマに関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a printing hammer for a dot impact printer using a piezoelectric element.

(従来技術とその問題点) 従来ドツトインパクト型プリンタ用の印字ハンマとして
は、コイルを用いた電磁型の印字ハンマが広く用いられ
てきた。しかしながら電磁型の印字ハンマは、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
駆動するため、太きな入力エネルギを必要とし発熱及び
磁気干渉などの問題点があった。そこで近年、電気0機
械エネルギ変換効率がよく低電力、低発熱で磁気干渉の
ないEIE電素子を用いた第5図に示すような印字ハン
マが報告されている(電気通信学会機構部品研究会資料
BMC84−49)。
(Prior Art and its Problems) Conventionally, electromagnetic printing hammers using coils have been widely used as printing hammers for dot impact printers. However, electromagnetic printing hammers generate a magnetic field by energizing a coil and are driven using the magnetic force, so they require a large amount of input energy and have problems such as heat generation and magnetic interference. Therefore, in recent years, a printing hammer as shown in Figure 5 has been reported, which uses an EIE electronic element that has good electrical and mechanical energy conversion efficiency, low power consumption, low heat generation, and no magnetic interference. BMC84-49).

これは、圧電素子51の変位方向(矢印入方向)前方に
板ばね52で支持されたフライトハンマ53が配置され
た構造となっている。なおフライトハンマ53には、ド
ツトを印字するための印字ワイヤヌが設けである。
This has a structure in which a flight hammer 53 supported by a leaf spring 52 is disposed in front of the piezoelectric element 51 in the direction of displacement (in the direction of the arrow). Note that the flight hammer 53 is provided with a printing wire for printing dots.

この印字ハンマにおいて圧電素子51に電圧を印加する
と、フライトハンマ53はEEt素子51から力を受は
加速され圧電素子51を離れ飛行する。そして印字ワイ
ヤ54が、前方にあるインクリボン5話紙団を介してプ
ラテン57に衝突しドツトを印材る。その後フライトハ
ンマ53はプラテン57からの反発力と板ばね52の後
帰力により圧電素子51の所へもどる。しかしながらこ
の時、フライトハンマ53は圧電素子51と衝突するた
め反発されリバウンドが生じる。そのフライトハンマ5
3の変位波形を第6図に示す。印字動作を開始してがら
りバウンドが静定するまでに約2msかかっており、高
速化のネックとなっていた。
When a voltage is applied to the piezoelectric element 51 in this printing hammer, the flight hammer 53 receives a force from the EEt element 51, is accelerated, leaves the piezoelectric element 51, and flies. Then, the printing wire 54 collides with the platen 57 via the ink ribbon 5 paper group in front to form dots on the printing material. Thereafter, the flight hammer 53 returns to the piezoelectric element 51 due to the repulsive force from the platen 57 and the return force of the leaf spring 52. However, at this time, the flight hammer 53 collides with the piezoelectric element 51 and is repelled, causing rebound. The flight hammer 5
The displacement waveform of No. 3 is shown in FIG. It took about 2 ms for the bounce to stabilize after the printing operation started, which was a bottleneck in increasing the speed.

(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、低電
力、低発熱で磁気干渉がなく高速な印字ハンマを提供す
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 high-speed printing hammer with low power consumption, low heat generation, and no magnetic interference.

(発明の構成) 本発明によれば、フライトハンマと、前記フライトハン
マを吸引する吸引機構と、前記フライトハンマに力を与
える圧電素子とから構成されることを特徴とする印字ハ
ンマが得られる。
(Structure of the Invention) According to the present invention, there is obtained a printing hammer characterized in that it is composed of a flight hammer, a suction mechanism that attracts the flight hammer, and a piezoelectric element that applies force to the flight hammer.

(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、フライトハンマの駆動源として、電気。First, electricity is used as the driving source for the flight hammer.

機械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。また、フライトハンマが圧電素子に接している時
に、フライトハンマに大きな吸引力が働くような永久磁
石を利用した吸引機構を用いることにより、リバウンド
を効果的に速く静定させることができ、高速化できる。
By using a piezoelectric element known for its high mechanical energy conversion efficiency, it uses less power, generates less heat, and eliminates magnetic interference. In addition, by using a suction mechanism using a permanent magnet that applies a large suction force to the flight hammer when it is in contact with the piezoelectric element, the rebound can be effectively and quickly stabilized, increasing speed. can.

(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図は本発明の一実施例を示す図である。第1図にお
いて、圧電素子11の変位方向(矢印入方向)前方に、
板ばね12で支持された磁性体フライトハンマ13が配
置された構造となっている。なおフライトハンマ13に
は、ドツトを印字するための印字ワイヤ14が設けてあ
り、圧電素子11の先端には力伝達部材15が接続して
いる。また、フライトハンマ13の両側には、空隙をお
いて磁性体の第一および第二のヨーク16.17の一端
が対向し、他端は永久磁石18にG多気的に接続してお
り、これらはフライトハンマ13を、吸引するための吸
引機構となっている。
FIG. 1 is a diagram showing an embodiment of the present invention. In FIG. 1, forward in the displacement direction (arrow direction) of the piezoelectric element 11,
The structure includes a magnetic flight hammer 13 supported by a leaf spring 12. The flight hammer 13 is provided with a printing wire 14 for printing dots, and a force transmitting member 15 is connected to the tip of the piezoelectric element 11. Further, on both sides of the flight hammer 13, one ends of first and second yokes 16 and 17 made of magnetic material face each other with a gap in between, and the other ends are connected to the permanent magnet 18 in a G polygonal manner. serves as a suction mechanism for suctioning the flight hammer 13.

このような構成の印字ハンマにおいて、フライトハンマ
13が圧電素子11の先端に接続された力伝達部材15
に接している時は、永久磁石18の発する磁石は矢印B
のように第一のヨーク16、フライトハンマ13、第二
のヨーク17を通って永久磁石18に戻る。したがって
フライトハンマ13には吸引力が働く。また、印字動作
中は、フライトハンマ13は前方に飛び出すため、永久
磁石18の発する磁束は第一のヨーク16を通って第二
のヨーク17に至り、フライトハンマ13を通らないた
めフライトハンマ13には吸引力はほとんど働かない。
In the printing hammer having such a configuration, the flight hammer 13 has a force transmitting member 15 connected to the tip of the piezoelectric element 11.
When in contact with , the magnet emitted by the permanent magnet 18 is
It passes through the first yoke 16, the flight hammer 13, and the second yoke 17 and returns to the permanent magnet 18 as shown in FIG. Therefore, a suction force acts on the flight hammer 13. Also, during the printing operation, the flight hammer 13 jumps forward, so the magnetic flux generated by the permanent magnet 18 passes through the first yoke 16 and reaches the second yoke 17, and does not pass through the flight hammer 13, so it is directed to the flight hammer 13. has almost no suction power.

そのため、フライトハンマ13が力伝達部材15に接し
ている時はフライトハンマ13に大きな吸引力が働き、
印字動作中すなわちフライトハンマ13が力伝達部材1
5から離れている時はフライトハンマ13には吸引力が
ほとんど働かない構造となる。そのため印字動作にはほ
とんど悪影響をおよぼすことなくリバウンドを速く静定
させることができる。
Therefore, when the flight hammer 13 is in contact with the force transmission member 15, a large suction force acts on the flight hammer 13,
During the printing operation, that is, the flight hammer 13 is
5, the flight hammer 13 has a structure in which almost no suction force acts on it. Therefore, the rebound can be quickly stabilized without having almost any adverse effect on the printing operation.

第2図に、圧電素子11に電圧を印加して駆動した場合
のフライトハンマ13の変位波形を示す。印字動作を開
始してからリバウンドが静定するまで約1m8で済み、
従来の場合(第6図)と比較して約2倍高速な印字ハン
マを得ることができた。
FIG. 2 shows a displacement waveform of the flight hammer 13 when the piezoelectric element 11 is driven by applying a voltage. It only takes about 1 m8 from the start of printing operation until the rebound stabilizes.
It was possible to obtain a printing hammer that is approximately twice as fast as the conventional case (FIG. 6).

第3図に本発明の他の実施例を示す。第3図において、
圧電素子31の変位方向(矢印A方向)前方に、板はね
32で支持された磁性体のフライトハンマ33が配置さ
れた構造となっている。なお板ばね32の先端部には、
ドツトを印字するための印字ビン34が設けてあり、圧
電素子31の先端には力伝達部材35が接続している。
FIG. 3 shows another embodiment of the invention. In Figure 3,
The structure is such that a flight hammer 33 made of a magnetic material and supported by a plate spring 32 is arranged in front of the piezoelectric element 31 in the displacement direction (direction of arrow A). In addition, at the tip of the leaf spring 32,
A printing bin 34 for printing dots is provided, and a force transmitting member 35 is connected to the tip of the piezoelectric element 31.

またフライトハンマ33と空隙において永久磁石38を
配置してあり、これはフライトハンマ33を吸引するた
めの吸引機構となっている。
Further, a permanent magnet 38 is arranged in the air gap between the flight hammer 33 and the permanent magnet 38, which serves as a suction mechanism for attracting the flight hammer 33.

このような構成の印字ハンマにおいては、永久磁石38
の発する磁束は矢印Cのように流れ、フライトハンマ3
3が永久磁石38に非常に接近している時はフライトハ
ンマ33に大きな吸引力が働くが、フライトハンマ33
と永久磁石38の距離が少し大きくなると永久磁石38
の吸引力は急激に減小してほとんど働くなる。そのため
印字動作にはほとんど悪影響をおよぼすことなくリバウ
ンドを速く静定させることができ、前述の実施例と同桶
の幼芽を発揮する。
In the printing hammer having such a configuration, the permanent magnet 38
The magnetic flux emitted by the flight hammer 3 flows as shown by arrow C.
3 is very close to the permanent magnet 38, a large attractive force acts on the flight hammer 33, but the flight hammer 33
When the distance between the permanent magnet 38 and the permanent magnet 38 becomes a little larger, the permanent magnet 38
The suction power decreases rapidly and becomes almost useless. Therefore, the rebound can be quickly stabilized without having almost any adverse effect on the printing operation, and the same buds as in the above-mentioned embodiments are exhibited.

第4図に本発明の他の実施1例を示す。第4図において
EEm素子41の変位方向(矢印入方向)前方ニ、印字
ワイヤ44を設けたフライトハンマ43が配置され、印
字ワイヤ44はガイド49により支持されている。なお
フライトハンマ43はコイルばね42により圧電素子4
1の先端に接続された力伝達部材45に押王されている
。また、フライトハンマ43の両(ill!には空隙を
おいて砕性体の第一および第二のヨーク46.47の一
端が対向し、他端は永久磁石48に接続しており、これ
らはフライトハンマ43を吸引するための吸引機構とな
っている。
FIG. 4 shows another embodiment of the present invention. In FIG. 4, a flight hammer 43 provided with a printing wire 44 is disposed in front of the EEm element 41 in the direction of displacement (arrow direction), and the printing wire 44 is supported by a guide 49. The flight hammer 43 is connected to the piezoelectric element 4 by the coil spring 42.
It is pressed by a force transmitting member 45 connected to the tip of 1. Further, one ends of the first and second yokes 46 and 47 of the crushable body are opposed to each other (ill!) of the flight hammer 43 with a gap in between, and the other end is connected to the permanent magnet 48. It serves as a suction mechanism for suctioning the flight hammer 43.

このような構成の印字ハンマにおいて、フライトハンマ
43が圧電素子41の先端に接続された力伝達部材45
に接し、ている時は、永久磁石48の発する磁束りのよ
うに第一のヨーク46、フライトハンマ43、第二のヨ
ーク47を通って永久磁石48に戻り、フライトハンマ
43には吸引力が働く。
In the printing hammer having such a configuration, the flight hammer 43 has a force transmitting member 45 connected to the tip of the piezoelectric element 41.
When the magnetic flux generated by the permanent magnet 48 passes through the first yoke 46, the flight hammer 43, and the second yoke 47 and returns to the permanent magnet 48, the flight hammer 43 has an attractive force. work.

また、印字動作中は、フライトハンマ43はTTI方に
飛び出すため、フライトハンマ43にハ吸引力はほとん
ど−1かない。そのため印字M)作にはほとんど悲影腎
をおよ(テすことなくリバウンドを沖く静定させること
ができ、前述の実施例と同様の効果を発揮する。
Further, during the printing operation, the flight hammer 43 flies out in the TTI direction, so the flight hammer 43 has almost no -1 suction force. Therefore, the rebound can be stabilized without causing any negative effects on the printing (M), and the same effect as in the above-mentioned embodiment is achieved.

また本発明においては縦効果や横ダ1果のある重板の圧
電素子あるいは積層捜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, similar effects can be obtained by using a multi-plate piezoelectric element having a vertical effect or a horizontal effect, a laminated piezoelectric element, or an electrostrictive element.

前述の実施例においては、印字後フライトハンマを力伝
達部材の所に復帰させるために板ばねやコイルはわを用
いた例を示したが、第4図の実施例のように印字ワイヤ
の接続したフライトハンマをガイドなどによって支持ず
れは、コイルばねを用いなくてもかまわない。印字向の
プラテンの反発力と少しではあるが吸引機構の吸引力に
より力伝達部材の所にもどるこ七ができる。
In the above-mentioned embodiment, an example was shown in which a leaf spring or coil flap was used to return the flight hammer to the force transmitting member after printing, but as in the embodiment shown in FIG. It is not necessary to use a coil spring to prevent the flight hammer from being supported by a guide or the like. It is possible to return to the force transmitting member by the repulsive force of the platen in the printing direction and a small amount of suction force of the suction mechanism.

(発明の効果) 本発明によれば、低電力、低発熱で信・気干渉がなく高
速な印字ハンマが糊られる。
(Effects of the Invention) According to the present invention, a high-speed printing hammer can be applied with low power consumption, low heat generation, and no signal/air interference.

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

第1図は本発明の一実施例を示す図、第2図は本発明の
一実施例の場合のフライトハンマの変位波形を示す図、
第3図は本発明の他の実施例を示す図、第4図は本発明
の他の実施例を示す図1第5図は従来の一実施例を示す
図、第6図は従来の一実施例の場合のフライトハンマの
変位波形を示す図である。 図において、 1131、41.51・・・圧電素子、12.32.5
2・・・板ばね、42・・・コイルばわ、13.33.
43.53・・・フライトハンマ、 14.44.54
・・・印字ワイヤ、34・・・印字ビン、15、35.
45・・・力伝達部材、16.46・・・第一のヨーク
、17.47・・・第二のヨーク、18.38.48・
・・永久磁石、55・・・インクリボン、56・・・紙
、57・・・プラテン、49・・・ガイド をそれぞれ示す。 第1図 Δ 18永久磁石 第2図 時間(ms ) 第3図 第4図 第5図 bン 板はね
FIG. 1 is a diagram showing an embodiment of the present invention, FIG. 2 is a diagram showing a displacement waveform of a flight hammer in the case of an embodiment of the present invention,
Fig. 3 is a diagram showing another embodiment of the present invention, Fig. 4 is a diagram showing another embodiment of the present invention, Fig. 5 is a diagram showing a conventional embodiment, and Fig. 6 is a diagram showing a conventional embodiment. It is a figure which shows the displacement waveform of the flight hammer in the case of an Example. In the figure, 1131, 41.51...piezoelectric element, 12.32.5
2... Leaf spring, 42... Coil spring, 13.33.
43.53...Flight hammer, 14.44.54
...Print wire, 34...Print bottle, 15, 35.
45... Force transmission member, 16.46... First yoke, 17.47... Second yoke, 18.38.48.
...Permanent magnet, 55... Ink ribbon, 56... Paper, 57... Platen, 49... Guide, respectively. Fig. 1 Δ 18 permanent magnet Fig. 2 Time (ms) Fig. 3 Fig. 4 Fig. 5 b

Claims (1)

【特許請求の範囲】[Claims] フライトハンマと、前記フライトハンマを吸引する吸引
機構と、前記フライトハンマ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印字ハンマ。
A printing hammer comprising a flight hammer, a suction mechanism that attracts the flight hammer, and a piezoelectric element that applies force to the flight hammer.
JP5733285A 1985-03-20 1985-03-20 Printing hammer Pending JPS61215064A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5733285A JPS61215064A (en) 1985-03-20 1985-03-20 Printing hammer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5733285A JPS61215064A (en) 1985-03-20 1985-03-20 Printing hammer

Publications (1)

Publication Number Publication Date
JPS61215064A true JPS61215064A (en) 1986-09-24

Family

ID=13052613

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5733285A Pending JPS61215064A (en) 1985-03-20 1985-03-20 Printing hammer

Country Status (1)

Country Link
JP (1) JPS61215064A (en)

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