JPS62102128A - Method and instrument for measuring partial pressure - Google Patents

Method and instrument for measuring partial pressure

Info

Publication number
JPS62102128A
JPS62102128A JP60241605A JP24160585A JPS62102128A JP S62102128 A JPS62102128 A JP S62102128A JP 60241605 A JP60241605 A JP 60241605A JP 24160585 A JP24160585 A JP 24160585A JP S62102128 A JPS62102128 A JP S62102128A
Authority
JP
Japan
Prior art keywords
component force
detector
output
measuring
vibration
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.)
Granted
Application number
JP60241605A
Other languages
Japanese (ja)
Other versions
JPH065185B2 (en
Inventor
Chinkou Higashijima
鎮▲かく▼ 東島
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP60241605A priority Critical patent/JPH065185B2/en
Publication of JPS62102128A publication Critical patent/JPS62102128A/en
Publication of JPH065185B2 publication Critical patent/JPH065185B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Abstract

PURPOSE:To remove the influence of vibration applied to a fixing part and to reduce a measuring error by measuring component force applied to an object in a required axial direction, measuring acceleration in the same axial direction which is generated by the vibration of the fixing part and executing the arithmetic processing of both the measured values. CONSTITUTION:An air duct testing model 2 is fitted to the surface of a multi- component force detector 1 for detecting 6 component force. The model 2 is arranged in an air duct 3 and air is carried in the white arrow direction. The detector 1 is fixed on a fixed base 4. In the detector 1, the output of a component force detector 31 for detecting component force in a required direction is amplified by an amplifier 32 and the amplified signal is applied to one terminal of an adder 33. The output of an acceleration detector 34 for the component force in the same direction is level-regulated by an amplifier 35 and an output gain-regulated by an output voltage adjuster 36 is supplied to the other terminal of the adder 33. The output of the adder 33 is level-adjusted by an amplifier 37 and outputted to an output terminal 38. Even in a place having large external vibration, multi-component force can be detected without the influence of vibration.

Description

【発明の詳細な説明】 、本発明は、分力検出器を用いた分力計測方法および装
置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a component force measuring method and apparatus using a component force detector.

近年、分力検出器を用いた計測が広く行われるようにな
ってきている。多分力検出器は、X。
In recent years, measurements using component force detectors have become widespread. The multi-force detector is X.

Y、Z三軸それぞれに作用する分力をそれぞれの力およ
びモーメントとして検出し、当該部位に作用する総体的
な力の状態を的確に計測しようとするものである。この
場合、分力検出器の取りつけられている固定台部分が振
動していると、その振動の影響が誤差となって現れるこ
とになり、正しい計測はできない。
The purpose is to detect component forces acting on each of the Y and Z three axes as respective forces and moments, and to accurately measure the overall state of force acting on the relevant region. In this case, if the fixed base part on which the component force detector is attached vibrates, the influence of the vibration will appear as an error, making it impossible to perform accurate measurements.

本発明の目的は、上述のような振動を伴う固定台に取り
つけられた分力検出器による計測における計測誤差を低
減する方法および装置を提供することである。
An object of the present invention is to provide a method and a device for reducing measurement errors in measurements made by a component force detector attached to a fixed base that vibrates as described above.

この目的は、特許請求の範囲に記載の構成を有する分力
計測方法および装置、すなわち、物体に作用す、る所望
軸方向分力を測定し、同時に固定部の振動によって生ず
る同じ軸方向の加速度を測定し、両測定値を演算処理す
ることによって、固定部に作用する振動の影響を除去す
る分力計測方法並びに、物体に作用する所望軸方向分力
を測定する分力測定装置と、固定部の振動によって生ず
る固定部の同じ軸方向の加速度を測定する加速度測定装
置と、そして、両測定装置の出力を演算処理する演算回
路とを有する分力計測装置によって達成される。
The purpose is to provide a force measuring method and device having the structure set forth in the claims, that is, to measure a desired axial component of force acting on an object, and at the same time to measure the acceleration in the same axial direction caused by vibrations of a fixed part. A component force measuring method that removes the influence of vibrations acting on a fixed part by measuring and calculating both measured values, a component force measuring device that measures a desired axial component force acting on an object, and a fixed part This is achieved by a component force measuring device that includes an acceleration measuring device that measures acceleration in the same axial direction of the fixed portion caused by vibration of the fixed portion, and an arithmetic circuit that processes the outputs of both measuring devices.

本発明にかかる分力計測方法および装置によれば、分力
検出器固定台に各種成分の振動が作用する場合において
も、誤差の少ない分力計測が可能となる。
According to the component force measurement method and device according to the present invention, even when vibrations of various components act on the component force detector fixing base, component force measurement with few errors is possible.

以下、実施例を示す添付図を参照して本発明にかかる分
力計測方法および装置について説明する。
DESCRIPTION OF THE PREFERRED EMBODIMENTS A component force measuring method and device according to the present invention will be described below with reference to the accompanying drawings showing examples.

第1図は多分力検出器によって風胴内の航空機模型に作
用する分力を計測する状態を示すものである。図におい
て6分力を検出するための多分力検出器1の上に風洞試
験用模型2が取りつけられる。模型2は風洞3の中にあ
り、白矢印のような方向に送風される。なお、多分力検
出器1は固定用基礎4の上に取りつけられる。
FIG. 1 shows a state in which a multiforce detector measures component forces acting on an aircraft model within a wind barrel. In the figure, a wind tunnel test model 2 is mounted on a multi-force detector 1 for detecting six component forces. The model 2 is inside a wind tunnel 3, and air is blown in the direction shown by the white arrow. Note that the multi-force detector 1 is mounted on a fixing foundation 4.

多分力検出器1は、歪ゲージ式あるいは圧電素子式等が
広く用いられているが、各分力方向について近似的に1
自由度系の弾性体が組み合わせられていると考えられる
。モーメントの計測についても同様である。なお、多分
力検出器としては、変移を荷重に変更できるものであれ
ば、上述の型式の他にばね式その他のものも使用するこ
とができる。
As the multiforce detector 1, a strain gauge type or a piezoelectric element type is widely used, but approximately 1 in each component force direction.
It is thought that elastic bodies with degrees of freedom are combined. The same applies to moment measurement. In addition to the above-mentioned type, a spring type or other type can be used as the multi-force detector as long as it can convert displacement into a load.

第2図は、X方向の分力検出器の概念図を示すものであ
る0図によれば、ばね定数にの弾性体11によって、質
量Mの計測側物体が固定部3に吊り下げられている。物
体12の静止状態からの運動をXい固定側13の運動を
x2とすると、この場合の運動方程式は、摩擦損を無視
すれば、下記のように二階微分方程式となる。
FIG. 2 shows a conceptual diagram of a component force detector in the X direction. According to FIG. There is. Assuming that the motion of the object 12 from a resting state is X and the motion of the fixed side 13 is x2, the equation of motion in this case becomes a second-order differential equation as shown below, if friction loss is ignored.

固定側の振動x2が、次式であるとすると、x2=Xz
sin  art               (2
)=KX、Sinωt    (3) となり、x2の加速度は以下のようになる。
Assuming that the vibration x2 on the fixed side is the following formula, x2=Xz
sin art (2
)=KX, Sinωt (3), and the acceleration of x2 is as follows.

αxzSin ωt =−X2 ω”5in6Jtこの
(4)式を(3)式に代入すると、この(5)式は、上
記1自由度系の強制力、すな方程式である。(5)式の
解は、次式のようになる。
αxzSin ωt = -X2 ω"5in6Jt Substituting this equation (4) into equation (3), this equation (5) is the forcing force of the above one degree of freedom system, or the equation. Solution of equation (5) is as follows.

−にαxz/ω21 ・Sinωt ω2 1−ω2/ω。′ ここに、ω(1” =Kg/M  である。− to αxz/ω21 ・Sinωt ω2 1−ω2/ω. ′ Here, ω(1″=Kg/M).

固定側の振動によって検出器が計測する誤差力Fは、 g  ωt     1−ω2/ω。′Sinωを 阿 F = −−or B−5inωt(7)となる。この
(7)式は、固定側が振動しているときに検出器に生ず
る誤差力が固定側の加速度に比例することを示している
The error force F measured by the detector due to vibration on the fixed side is g ωt 1−ω2/ω. 'Sinω becomes AF=--or B-5inωt (7). This equation (7) shows that the error force generated in the detector when the fixed side is vibrating is proportional to the acceleration of the fixed side.

したがって、固定側にX方向の加速度計を設置し、その
出力を第3図に示すように荷重検出器の出力と演算する
ことにより、その出力は固足側の振動の影響を受けない
ようにすることができる。図において、多分力検出器に
おける所要方向の分力検出器31の出力を増幅器32に
より増幅した後加算器33の一方の端子に加える。加算
器33の他方の端子には、同一方向分力の加速度検出器
34を適当な増幅器35でレベルを規定しかつ出力電圧
調整器36によってゲイン調整された出力が供給される
Therefore, by installing an accelerometer in the X direction on the fixed side and calculating its output with the output of the load detector as shown in Figure 3, the output can be made unaffected by vibrations on the fixed foot side. can do. In the figure, the output of a component force detector 31 in a desired direction in a multiforce detector is amplified by an amplifier 32 and then applied to one terminal of an adder 33. The other terminal of the adder 33 is supplied with an output whose level is defined by an appropriate amplifier 35 and whose gain is adjusted by an output voltage regulator 36 from an acceleration detector 34 for component forces in the same direction.

出力端子38には、増幅器37によって適当なレベルに
調整された加算器33の出力が得られる。
An output terminal 38 receives the output of the adder 33 adjusted to an appropriate level by an amplifier 37.

このように、本発明にかかる方法および装置によれば、
外部振動の激しい場所においても、振動の影響を受ける
ことなしに多分力検出が可能となる。したがって、従来
不可能とされた振動を伴う部位での正確な多分力検出が
でき、当該計測技術分野において新たな一面が展開され
ることになる。
Thus, according to the method and apparatus according to the present invention,
Even in locations with severe external vibrations, multi-force detection is possible without being affected by vibrations. Therefore, it is possible to accurately detect multiple forces in areas with vibration, which was previously considered impossible, and a new aspect will be developed in the field of measurement technology.

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

第1図は、分力検出器によって風胴内の航空機模型に作
用する分力を計測する状態を示すものである。 第2図は、X方向分力検出器の概念図を示すものである
。 第3図は、本発明にかかる方法を実施するための演算回
路の例を示すブロック図である。 図中の主な参照符号の対応は以下の通り。 11−弾性体   12:物体 13:固定側
FIG. 1 shows a state in which a component force detector is used to measure component forces acting on an aircraft model within a wind barrel. FIG. 2 shows a conceptual diagram of the X-direction component force detector. FIG. 3 is a block diagram showing an example of an arithmetic circuit for implementing the method according to the invention. The correspondence of the main reference symbols in the figure is as follows. 11-Elastic body 12: Object 13: Fixed side

Claims (1)

【特許請求の範囲】 1、固定部に弾性的に支持された物体に作用する分力を
測定するための方法において、 物体に作用する所望軸方向分力を測定し、同時に固定部
の振動によって生ずる同じ軸方向の加速度を測定し、両
測定値を演算処理することによって、固定部に作用する
振動の影響を除去することを特徴とする分力計測方法。 2、固定部に弾性的に支持された物体に作用する分力を
測定するための装置において、 物体に作用する所望軸方向分力を測定する分力測定装置
と、固定部の振動によって生ずる固定部の同じ軸方向の
加速度を測定する加速度測定装置と、そして、両測定装
置の出力を演算処理する演算回路とを有し、該演算出力
によって固定部に作用する振動の影響を除去することを
特徴とする分力計測装置。
[Claims] 1. A method for measuring a component force acting on an object elastically supported by a fixed part, which measures a desired axial component force acting on the object and at the same time A component force measurement method characterized in that the influence of vibration acting on a fixed part is removed by measuring the acceleration in the same axial direction that occurs and calculating and processing both measured values. 2. In a device for measuring the component force acting on an object elastically supported by a fixed part, there is a component force measuring device that measures the desired axial component force acting on the object, and a component force measuring device that measures the component force acting on the object in the desired axial direction, and It has an acceleration measuring device that measures the acceleration in the same axial direction of the fixed portion, and an arithmetic circuit that processes the outputs of both measuring devices, and uses the calculated output to remove the influence of vibrations acting on the fixed portion. Features component force measuring device.
JP60241605A 1985-10-30 1985-10-30 Component force measuring method and device Expired - Lifetime JPH065185B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60241605A JPH065185B2 (en) 1985-10-30 1985-10-30 Component force measuring method and device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60241605A JPH065185B2 (en) 1985-10-30 1985-10-30 Component force measuring method and device

Publications (2)

Publication Number Publication Date
JPS62102128A true JPS62102128A (en) 1987-05-12
JPH065185B2 JPH065185B2 (en) 1994-01-19

Family

ID=17076801

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60241605A Expired - Lifetime JPH065185B2 (en) 1985-10-30 1985-10-30 Component force measuring method and device

Country Status (1)

Country Link
JP (1) JPH065185B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02269918A (en) * 1989-04-11 1990-11-05 Kubota Corp Freight calculator
JP2004516452A (en) * 2000-06-08 2004-06-03 ブリヂストン/フアイヤーストーン・ノース・アメリカン・タイヤ・エルエルシー Dynamic force measurement system for tire testing station
JP2008164495A (en) * 2006-12-28 2008-07-17 Japan Aerospace Exploration Agency Method for measuring multi-component force, and device thereof

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02269918A (en) * 1989-04-11 1990-11-05 Kubota Corp Freight calculator
JP2004516452A (en) * 2000-06-08 2004-06-03 ブリヂストン/フアイヤーストーン・ノース・アメリカン・タイヤ・エルエルシー Dynamic force measurement system for tire testing station
JP2008164495A (en) * 2006-12-28 2008-07-17 Japan Aerospace Exploration Agency Method for measuring multi-component force, and device thereof

Also Published As

Publication number Publication date
JPH065185B2 (en) 1994-01-19

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