JPS61215856A - Output characteristic variable type load torque reducer - Google Patents

Output characteristic variable type load torque reducer

Info

Publication number
JPS61215856A
JPS61215856A JP5324185A JP5324185A JPS61215856A JP S61215856 A JPS61215856 A JP S61215856A JP 5324185 A JP5324185 A JP 5324185A JP 5324185 A JP5324185 A JP 5324185A JP S61215856 A JPS61215856 A JP S61215856A
Authority
JP
Japan
Prior art keywords
cam
input
output shaft
load torque
output
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
JP5324185A
Other languages
Japanese (ja)
Inventor
Takashi Takaguchi
隆 高口
Yasushi Watabe
渡部 靖
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.)
Japan Steel Works Ltd
Nissan Motor Co Ltd
Technical Research and Development Institute of Japan Defence Agency
Original Assignee
Japan Steel Works Ltd
Nissan Motor Co Ltd
Technical Research and Development Institute of Japan Defence Agency
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 Japan Steel Works Ltd, Nissan Motor Co Ltd, Technical Research and Development Institute of Japan Defence Agency filed Critical Japan Steel Works Ltd
Priority to JP5324185A priority Critical patent/JPS61215856A/en
Publication of JPS61215856A publication Critical patent/JPS61215856A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To set an output characteristic corresponding to a change of the actual load, by arranging the center of a crest in a cam, integrally provided with an input/output shaft, in a neutral phase position and providing cam followers to be arranged in said positions while providing spring means urging the cam followers toward the input/output shaft. CONSTITUTION:A casing 11 contains inside a cam 30, integrally provided with an input/output shaft 15 in its central part, in a bore 12. Circular sectional ball housings 17, penetrating through the casing 11 and reaching the bore 12, mount with a play balls 18 serving as a cam follower. The ball 18 is resiliently pressed by a leaf spring 19 serving as a spring means. Consequently, a load torque reducer, selecting the cam of large degree of freedom in shape selection as a reducing element of a load torque, can set an output characteristic corresponding to the change of an actual load.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は1例えばロケットの操舵翼における゛  よう
な、ばね特性をもった負荷のトルクを軽減する装置、詳
しくは、入・出力軸を中立位相位置から一つの方向に回
動したとき、この入・出力軸が前記の回動力向、したが
って負荷トルクと対抗する方向に付勢されるようにした
重力特性可変型負荷トルク軽減装置に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a device for reducing the torque of a load having spring characteristics, such as a steering blade of a rocket; The present invention relates to a variable gravity characteristic type load torque reducing device in which, when the input/output shaft rotates in one direction from a phase position, the input/output shaft is biased in the direction of the rotational force, and hence in the direction opposite to the load torque.

〔従来の技術〕[Conventional technology]

かかる装置は1例えば米国ERD社(IERD ING
One such device is manufactured by, for example, the American company ERD (IERD ING).
.

−1wasmt*cto* AVE、 FAIRFIE
LD NJ o7ooe−5の社報(BULETIN)
 1/82 ニrENERGY RECOVERY口E
VICES Jとしてその作用が説明されており、該装
置は同社報に記載されているごとく、航空機の翼制御機
構に用いるために開発されたもので、制御用アクチュエ
ータと組合わせるときは□必要人カエネルギを50%ま
で節約することができる。
-1wasmt*cto* AVE, FAIRFIE
LD NJ o7ooe-5 company newsletter (BULETIN)
1/82 ENERGY RECOVERY mouth E
Its function is explained as VICES J, and as stated in the company's bulletin, this device was developed for use in the wing control mechanism of aircraft, and when combined with a control actuator, the required human energy is reduced. You can save up to 50%.

第6図および第7図は上記装置の具体例を示すもので、
等角度関係に配置した4木の円柱状のステイ1aないし
ldを介して対向させた1対のフレーム2,2に入・出
力軸3を貫通状態に支承し、この人・出力軸の一方の突
出部を7クチユエータ、例えばサーボモータに連結する
入力軸3aとなし、他方の突出部を負荷1例えばロケッ
トの操舵Hcを接続する出力軸3bとしている。
6 and 7 show specific examples of the above device,
A pair of frames 2, 2 facing each other via four wooden cylindrical stays 1a to ld arranged at equal angles support the input/output shaft 3 in a penetrating state, and one of the input/output shafts One of the protrusions is an input shaft 3a connected to a 7-cut unit, for example a servo motor, and the other protrusion is an output shaft 3b connected to a load 1, for example the steering Hc of a rocket.

4は入・出力軸3の中央部に該軸と一体的に設けた円盤
状のロータで、このロータの出力軸3bがわにビン5a
 、 5bを、また同人力軸3dがわにビン5a’ 、
5b’をそれぞれ軸対称的に植設しである。 8aおよ
び8bは相い対する1対のステイ1aおよび1bに外嵌
した有脚のコイルばねで、それぞれその脚によって6対
のビン5a、5a’および5b、5b’を外方から弾圧
している。
Reference numeral 4 denotes a disk-shaped rotor provided at the center of the input/output shaft 3 and integrally with the shaft, and the output shaft 3b of this rotor is connected to the alligator bin 5a.
, 5b, and the doujinshi axis 3d is also the alligator bottle 5a',
5b' are each implanted axially symmetrically. 8a and 8b are coil springs with legs fitted around a pair of opposing stays 1a and 1b, and the legs press six pairs of bottles 5a, 5a' and 5b, 5b' from the outside. .

以上の構成から、入力軸3aにトルクが生じないときは
、上記の弾圧力によるモーメントが平衡する位置(中立
位相位置)において入・出力軸3が静止する。ここで操
舵5IICに舵角δを付与するべく入力軸3aを矢線R
の方向に駆動すると、ビン5a、5a’および5b、5
b’の位相変化にともなってコイルばね8aおよび8b
の姿勢が2点鎖線示のように変化し、この結果、前記弾
圧力とそのモーメントアームの平衡がくずれて前記回動
力向8回りにトルクが増補される。よって操舵翼Cに作
用する空力弾性力Fによる負荷トルク丁を上記の増補分
だけ減殺することができる。
From the above configuration, when no torque is generated on the input shaft 3a, the input/output shaft 3 stands still at a position (neutral phase position) where the moment due to the above-mentioned elastic force is balanced. Here, in order to give the steering angle δ to the steering wheel 5IIC, the input shaft 3a is moved along the arrow R.
When driven in the direction of , the bins 5a, 5a' and 5b, 5
With the phase change of b', the coil springs 8a and 8b
The posture changes as shown by the two-dot chain line, and as a result, the balance between the elastic force and the moment arm is lost, and the torque is increased around the rotational force direction 8. Therefore, the load torque due to the aeroelastic force F acting on the steering blade C can be reduced by the above-mentioned increase.

操舵gXcに反対の舵角を付与するときも同様である。The same applies when giving the opposite steering angle to the steering gXc.

〔従来技術の問題点〕[Problems with conventional technology]

ところで、かかる従来の装置にあっては、これを例えば
ロケットの操舵系に組入れた場合。
By the way, when such a conventional device is incorporated into a rocket steering system, for example.

操舵翼にかかる負荷トルクの変化と烏該負荷トルク軽減
装置の出力との整合性を得難いという問題があった。
There is a problem in that it is difficult to achieve consistency between changes in the load torque applied to the steering blade and the output of the load torque reduction device.

なぜならば、この従来の装置の出力特性は主として前記
ビンの位相変化にしたがって通常の操舵角範囲ではほぼ
一次関数的に変化するのに対し、操舵翼の負荷トルクは
舵角の高次関数として変化するからである。
This is because the output characteristics of this conventional device change almost linearly in the normal steering angle range mainly in accordance with the phase change of the bin, whereas the load torque of the steering blade changes as a higher-order function of the steering angle. Because it does.

そこで本発明の課題は、負荷トルク軽減装置の出力特性
を実負荷の変化に相応させうるようにすることである。
Therefore, an object of the present invention is to make the output characteristics of a load torque reducing device correspond to changes in the actual load.

〔発明の手段〕[Means of invention]

上記1!Jimを解決した本発明の手段は、入・出力軸
にカムを一体的に設けてこのカムにおけるカム山の中心
を中立位相位置に配し、この中立位相位置にカムホロワ
を配設するとともに該カムホロワを入・出力軸の方へ付
勢するばね手段を設けたものである。
Above 1! The means of the present invention that solves Jim's problem is to integrally provide a cam on the input and output shafts, arrange the center of the cam ridge in the cam at a neutral phase position, arrange a cam follower at this neutral phase position, and dispose the cam follower at the neutral phase position. A spring means is provided to bias the input/output shaft toward the input/output shaft.

〔作用〕[Effect]

上記手段によれば、入・出力軸が中立位相位置にあると
き、カムホロワがカム山の中心において入・出力軸の方
へ付勢されているので該軸にはトルクが生じない、ここ
で入・出力軸を一つの方向に回動すると、カムホロワが
その回動後位の傾斜カム面に当接してばね手段により弾
圧される結果、このカム面には回動前位、すなわち回動
方向へ向う分力が生じてトルクが増補される。そしてこ
の分力はばね手段のばね特性とカムプロフィルとによっ
て決定されるので、これら両者を適宜に選定することに
より出力トルクの特性を所望のように設定することがで
きる。
According to the above means, when the input/output shaft is in the neutral phase position, the cam follower is biased toward the input/output shaft at the center of the cam mount, so no torque is generated on the shaft. - When the output shaft is rotated in one direction, the cam follower comes into contact with the inclined cam surface at the rear of the rotation and is compressed by the spring means. A force is generated in the opposite direction and the torque is augmented. Since this component force is determined by the spring characteristics of the spring means and the cam profile, by appropriately selecting both of these, the characteristics of the output torque can be set as desired.

〔実施例〕〔Example〕

第1図および第2図において1口は主体部外形が正四角
形のケーシングでその中央に円形のポア12を有し、1
3.13はこのケーシングの両側面の各々4木のビス1
4を用いて取付けたカバー、 15はこれらのカバーに
ベアリング18.18を介して支承した入・出力軸、1
5aおよび15bはそれぞれ該軸における入力軸および
出力軸である。
In FIGS. 1 and 2, one mouth is a casing whose main part has a square outer shape and has a circular pore 12 in the center.
3.13 is the 4 wooden screws 1 on each side of this casing.
4, 15 is the input/output shaft supported on these covers via bearings 18 and 18, 1
5a and 15b are the input shaft and output shaft of the shaft, respectively.

30は入・出力軸15の中央部に該軸と一体的に設けた
カムでポア12の中に収容され1図示の姿勢は中立位相
位置にある場合を示している。カム30は4つの対称形
カム山31を等角度関係にそなえ、前記の中立姿勢にお
いて各カム山の中心線0−Aが前記四角形の各辺の中央
に向う。
Reference numeral 30 denotes a cam provided integrally with the central part of the input/output shaft 15, and is accommodated in the pore 12, and the posture shown in FIG. 1 shows the case where the cam is in a neutral phase position. The cam 30 has four symmetrical cam ridges 31 arranged in equiangular relation, and in the neutral position, the center line 0-A of each cam ridge is directed toward the center of each side of the quadrangle.

17はケーシング11を貫通してポア12に至る断面円
形のポールハウジングで上記中心線0−Aと同心に設け
られ、1日はこのポールハウジングに遊装したカムホロ
ワとしてのポールである。
Reference numeral 17 denotes a pole housing having a circular cross section that passes through the casing 11 and reaches the pore 12, and is provided concentrically with the center line 0-A, and 17 is a pole as a cam follower that is loosely attached to this pole housing.

19はばね手段としての板ばねで、その一端部をボルト
20を用いてケーシング11に固定し、他端部によりポ
ール18を弾圧している。よってポール18はこの中立
位相位置においてカム山31の頂部に当接し、ポールハ
ウジング17によって動きを規制されつつ入・出力軸1
5の方へ付勢される。
Reference numeral 19 denotes a leaf spring as a spring means, one end of which is fixed to the casing 11 using a bolt 20, and the other end of which presses against the pole 18. Therefore, the pawl 18 comes into contact with the top of the cam ridge 31 in this neutral phase position, and the movement of the pawl 18 is regulated by the pawl housing 17 while the input/output shaft 1
It is biased towards 5.

実施例は以上の如くであって、図示の中立位相位置にお
いては各ポール18が対称形のカム山31の頂部に弾接
しているのでいずれの方向へもトルクが生じない、ここ
で前記舵角δを与えるべく入力軸15aを矢MRの方向
へ回動させるとポール18が板ばね19により押し込め
られて回動後位の傾斜カム面32に弾接する。
The embodiment is as described above, and since each pole 18 is in elastic contact with the top of the symmetrical cam ridge 31 in the illustrated neutral phase position, no torque is generated in any direction. When the input shaft 15a is rotated in the direction of arrow MR to give δ, the pawl 18 is pushed in by the leaf spring 19 and comes into elastic contact with the inclined cam surface 32 at the rear of the rotation.

第3図(A)の2点鎖線はこの場合におけるカム30の
姿勢を示し、33はカム面32とポール18との接点、
rtはこのときの板ばね19の弾圧力。
The two-dot chain line in FIG. 3(A) shows the attitude of the cam 30 in this case, and 33 is the contact point between the cam surface 32 and the pole 18;
rt is the elastic force of the leaf spring 19 at this time.

fはカム30の接線方向分力、見はそのモーメントアー
ムで、便宜上摩擦トルクを無視すれば、該負荷トルク軽
減装置の出力トルクTOはTO=Ta+4f11!;L となる、但し、Taは入力軸15aに入力されるアクチ
ュエータのトルクである。そしてこの増補されるトルク
f−1は上記弾圧力fl (ベクトル)の関数となるか
ら結局板ばね19のばね特性とカム面32のプロフィル
によって決定される。
f is the tangential force of the cam 30, and is its moment arm.If friction torque is ignored for convenience, the output torque TO of the load torque reduction device is TO=Ta+4f11! ;L, where Ta is the actuator torque input to the input shaft 15a. Since this augmented torque f-1 is a function of the elastic force fl (vector), it is ultimately determined by the spring characteristics of the leaf spring 19 and the profile of the cam surface 32.

よってこれらの要素を適宜に選択することによって、同
図(B)に示すごとく、出力特性(カーブX)を負荷特
性 (カーブY)に対応させることができ、る。
Therefore, by appropriately selecting these elements, it is possible to make the output characteristics (curve X) correspond to the load characteristics (curve Y), as shown in FIG.

第4図(A)はカムの別の実施例を示すもので、該カム
30’のカム山頂部に入・出力軸15と同心の円弧面3
4を形成して、同図(B)に示すごとく、不感帯aをも
つ出力特性X°としたもので、これによって入・出力軸
15を中立位相位置に安定して保持しうる。
FIG. 4(A) shows another embodiment of the cam, in which a circular arc surface 3 concentric with the input/output shaft 15 at the top of the cam 30'
4 to provide an output characteristic of X° with a dead zone a as shown in FIG.

第5図(A)は更に別の実施例を示し、同図(B)にY
oで示す如く、中立位相位置の近傍において負荷トルク
Tに変動があるとき出力特性x°° をこれに対応させ
るべく、該カム30°°のカム山頂部に副カム山35.
35を対称的に形成したものである。
FIG. 5(A) shows yet another embodiment, and FIG. 5(B) shows Y
As shown by o, when there is a variation in the load torque T in the vicinity of the neutral phase position, in order to adjust the output characteristic x° to correspond to this, an auxiliary cam ridge 35.
35 is formed symmetrically.

〔効果〕〔effect〕

以上説明したように、本発明は負荷トルクの軽減要素と
して形状選定の自由度が大きいカムを採択したので、実
負荷の変化に相応した出力特性を設定することができ、
これによって操舵サーボ系などの制御精度を高め、また
アクチュエータの歩容量化を図りうるちのである。
As explained above, the present invention adopts a cam with a large degree of freedom in shape selection as a load torque reducing element, so it is possible to set output characteristics that correspond to changes in actual load.
This increases the control precision of the steering servo system, etc., and increases the walking capacity of the actuator.

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

第1図は本発明の1実施例を示す断面図、第2図は第1
図の■−■視断面断面図3図は第1図の実施例の作用説
明図、第4図および第5図はそれぞれ別の実施例の要部
およびその作用説明図、第8図は従来の装置を示す側面
図、第7図は第6図の■−■視断面断面図る。 3.15・・・入・出力軸 3a、15a・・・入力軸 3b、15b・・・出力軸 18・・・カムホロワ (ポール) 19・・・ばね手段(板ばね) 30・・・カム 31・・・カム山 0−A・・・カム山の中心線 R・・・一つの回動方向 T・・・負荷トルク TO・・・出力トルク 特許出願人 防衛庁技術研究本部長 大森幸衛同出願人
 日産自動車株式会社 壺に JS   忙       \ −り。 (コ 第3図 Δ (B) 第4図 1日 (8)   、 D
FIG. 1 is a sectional view showing one embodiment of the present invention, and FIG. 2 is a cross-sectional view showing one embodiment of the present invention.
Figure 3 is an explanatory diagram of the operation of the embodiment shown in Figure 1, Figures 4 and 5 are illustrations of the main parts of different embodiments and their operation, and Figure 8 is a conventional FIG. 7 is a side view showing the device of FIG. 3.15... Input/output shaft 3a, 15a... Input shaft 3b, 15b... Output shaft 18... Cam follower (pole) 19... Spring means (plate spring) 30... Cam 31 ...Cam mount 0-A...Cam mount center line R...One rotation direction T...Load torque TO...Output torque Patent applicant Yukie Omori, Director of Technology Research Headquarters, Agency of Defense People Nissan Motor Co., Ltd. JS Busy \ -ri. (Figure 3 Δ (B) Figure 4 1st (8), D

Claims (1)

【特許請求の範囲】[Claims] 入・出力軸を中立位相位置から一つの方向に回動したと
きこの入・出力軸が前記の回動方向に付勢されるように
して該軸の出力側に接続した負荷のトルクを軽減する装
置において、入・出力軸にカムを一体的に設けてこのカ
ムにおけるカム山の中心を中立位相位置に配し、この中
立位相位置にカムホロワを配設するとともに該カムホロ
ワを入・出力軸の方へ付勢するばね手段を設けた出力特
性可変型負荷トルク軽減装置。
When the input/output shaft is rotated in one direction from the neutral phase position, the input/output shaft is biased in the direction of rotation, thereby reducing the torque of the load connected to the output side of the shaft. In the device, a cam is integrally provided on the input and output shafts, the center of the cam ridge on this cam is placed at a neutral phase position, and a cam follower is placed at this neutral phase position, and the cam follower is placed in the direction of the input and output shafts. A load torque reducing device with variable output characteristics equipped with a spring means for biasing the load.
JP5324185A 1985-03-19 1985-03-19 Output characteristic variable type load torque reducer Pending JPS61215856A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5324185A JPS61215856A (en) 1985-03-19 1985-03-19 Output characteristic variable type load torque reducer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5324185A JPS61215856A (en) 1985-03-19 1985-03-19 Output characteristic variable type load torque reducer

Publications (1)

Publication Number Publication Date
JPS61215856A true JPS61215856A (en) 1986-09-25

Family

ID=12937295

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5324185A Pending JPS61215856A (en) 1985-03-19 1985-03-19 Output characteristic variable type load torque reducer

Country Status (1)

Country Link
JP (1) JPS61215856A (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5560753A (en) * 1978-10-25 1980-05-08 Tetra Pak Int Compensating method for inertia force in indexing movent of machine element and attaining device therefor

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5560753A (en) * 1978-10-25 1980-05-08 Tetra Pak Int Compensating method for inertia force in indexing movent of machine element and attaining device therefor

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