JPH09257635A - Apparatus for measuring load if moving body - Google Patents

Apparatus for measuring load if moving body

Info

Publication number
JPH09257635A
JPH09257635A JP6434296A JP6434296A JPH09257635A JP H09257635 A JPH09257635 A JP H09257635A JP 6434296 A JP6434296 A JP 6434296A JP 6434296 A JP6434296 A JP 6434296A JP H09257635 A JPH09257635 A JP H09257635A
Authority
JP
Japan
Prior art keywords
model
force
moving
output
movement control
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.)
Withdrawn
Application number
JP6434296A
Other languages
Japanese (ja)
Inventor
Ryoji Nonaka
亮二 野中
Yumiko Inoue
裕美子 井上
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP6434296A priority Critical patent/JPH09257635A/en
Publication of JPH09257635A publication Critical patent/JPH09257635A/en
Withdrawn legal-status Critical Current

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  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

PROBLEM TO BE SOLVED: To perform securely and automatically the wind-tunnel experiment forming the second model neat the first model safely, and to make it possible to decrease the man-hours by a large extent without the occurrence of the contact breakdown of the model. SOLUTION: The parts performing the functions as follow are provided. A first model 1 is fixed to the upper part of a wind tunnel 15. A triaxial moving means is arranged at the lower part of the win tunnel 15 and has an attaching arm. A movement control means 4 control the moving means. A second model 2 is attached to the attaching arm 16 of the moving means 4. A force detecting means detects the force applied on the second model 2. A load operating means 8 receiver the output of the detecting means through an amplifier and an A/D converter 7, computes the above described force and sends the stopping signal to the movement control means 4 when the second model 2 comes into contact and the reaction force is larger than the preset value.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は衝突による破損防止
を図った移動物体荷重計測装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a moving object load measuring device for preventing damage due to collision.

【0002】[0002]

【従来の技術】風洞実験で、例えば投下模型の空力荷重
を計測する場合、母機模型近くでの計測が非常に重要で
ある。
2. Description of the Related Art In a wind tunnel experiment, for example, when measuring the aerodynamic load of a dropping model, it is very important to measure near the mother model.

【0003】従来技術における計測物体を取付けた移動
装置を有する移動物体荷重計測装置では計測物体の衝突
による破損を防止するため、運転員が、計測物体を目視
によって監視し、衝突すると判断すると手動で移動装置
を非常停止させていた。
In a moving object load measuring device having a moving device to which a measuring object is attached in the prior art, in order to prevent damage due to collision of the measuring object, an operator visually monitors the measuring object, and manually judges that the collision occurs. The moving device was in an emergency stop.

【0004】[0004]

【発明が解決しようとする課題】上記従来技術は次のよ
うな問題点があった。
The above-mentioned prior art has the following problems.

【0005】(1)移動装置運転員の衝突判定から、計
測物体が停止するまでの時間遅れによる衝突・損傷。
(1) Collision / damage due to a time delay from the collision judgment of the moving device operator to the stop of the measuring object.

【0006】(2)目視による衝突判定時の移動装置運
転員による個人差の発生。及びそれによる衝突回避が確
実に行えないこと。
(2) Occurrence of individual differences among operators of moving devices when visually determining collision. And that collision avoidance cannot be performed reliably.

【0007】[0007]

【課題を解決するための手段】本発明は上記課題を解決
するため次の手段を講ずる。
The present invention employs the following means to solve the above-mentioned problems.

【0008】すなわち、移動物体荷重計測装置として、
風洞上部に固定された第1の模型と、同風洞下部に配置
され取付けアームを持つ3軸移動式の移動手段と、同移
動手段を制御する移動制御手段と、上記移動手段の取付
けアームに取付けられた第2の模型と、同第2の模型に
加わる力を検出する力検出手段と、同力検出手段の出力
を受ける増幅器と、同増幅器の出力を受けるA/D変換
器と、同A/D変換器の出力を受け上記力を算出すると
ともに上記第2の模型がが接触しその反力が予め定めら
れた設定値以上のとき停止信号を上記移動制御手段へ送
る荷重演算手段とを設ける。
That is, as a moving object load measuring device,
A first model fixed to the upper part of the wind tunnel, a three-axis moving means having a mounting arm arranged at the lower part of the wind tunnel, a movement control means for controlling the moving means, and a mounting arm for the moving means. The second model, the force detecting means for detecting the force applied to the second model, the amplifier receiving the output of the force detecting means, the A / D converter receiving the output of the amplifier, and the A And a load calculation means for receiving the output of the D / D converter, calculating the force, and sending a stop signal to the movement control means when the reaction force of the second model contacts and the reaction force is equal to or more than a predetermined set value. Set up.

【0009】以上において、例えば第2の模型は第1の
模型から投下される投下物模型とする。
In the above, for example, the second model is a dropped object model dropped from the first model.

【0010】移動制御手段は第2の模型を投下飛しょう
経路に対応する各位置に移動する制御信号を移動手段に
送る。移動手段はこの信号に応じて移動し、第2の模型
を投下飛しょう経路に沿い移動する。力検出手段は第2
の模型に加わる力を検出し、その信号を増幅器、A/D
変換器を経て荷重演算手段へ送る。荷重演算手段は入力
信号から第2の模型に加わる空力荷重を各位置に対応し
て演算出力する。
The movement control means sends to the movement means a control signal for moving the second model to each position corresponding to the dropping flight path. The moving means moves according to this signal, and moves along the flight path on which the second model is dropped. The force detection means is the second
Of the force applied to the model of the car, the signal is amplified, A / D
It is sent to the load calculation means via the converter. The load calculation means calculates and outputs the aerodynamic load applied to the second model from the input signal corresponding to each position.

【0011】万一、移動手段の移動により第2の模型が
第1の模型に接触した場合、その反力は上記と同様に作
用して荷重演算手段で算出される。荷重演算手段はこの
反力が所定の設定値以上になったとき、停止信号を移動
制御手段へ送る。移動制御手段はこの信号を受けて移動
手段を停止させる。
In the unlikely event that the second model comes into contact with the first model due to the movement of the moving means, the reaction force acts in the same manner as described above and is calculated by the load calculating means. The load calculation means sends a stop signal to the movement control means when the reaction force exceeds a predetermined set value. The movement control means receives this signal and stops the movement means.

【0012】上記の設定値を模型の接触によって模型が
破損しない範囲内に設定しておく。
The above set values are set within a range in which the model is not damaged by contact with the model.

【0013】以上のようにして、模型を接触破損するこ
となく、各種の経路にわたる空力荷重の計測が安全、確
実に行えるようになる。
As described above, the aerodynamic load can be measured safely and reliably over various routes without damaging the model by contact.

【0014】[0014]

【発明の実施の形態】本発明の実施の一形態を図1と図
2により説明する。
BEST MODE FOR CARRYING OUT THE INVENTION An embodiment of the present invention will be described with reference to FIGS.

【0015】図1にて、風洞15の上部には第1の模型
1(母機模型)が配置されている。その下方には移動装
置4が配置されている。
In FIG. 1, a first model 1 (mother machine model) is arranged above the wind tunnel 15. The moving device 4 is arranged below it.

【0016】移動装置4は車輪装置10を持つ台車11
の上に、左右移動装置12を持つ柱14が設けられてい
る。また柱14に沿って移動する上下移動装置13が設
けられている。また上下移動装置13の前端には取付ア
ーム16が前方に取付けられ、その先端に第2の模型
(例えば投下物体の模型)2が取付けられている。
The moving device 4 is a dolly 11 having a wheel device 10.
A pillar 14 having a left-right moving device 12 is provided on the upper part. Further, a vertical movement device 13 that moves along the pillar 14 is provided. A mounting arm 16 is attached to the front end of the vertical movement device 13, and a second model (for example, a model of a dropped object) 2 is attached to its tip.

【0017】第2の模型2内には6分力天秤3が搭載さ
れていて、その出力は増幅器6,A/D変換器7を順次
経て荷重計測用計算器8へ送られる。
A 6-component force balance 3 is mounted in the second model 2, and its output is sent to a load measuring calculator 8 via an amplifier 6 and an A / D converter 7 in sequence.

【0018】移動装置制御用計算機5の出力は車輪装置
10,左右移動装置12,上下移動装置13へ送られて
いる。また荷重計測用計算器8の出力は移動装置制御用
計算機5へ送られている。
The output of the moving device control computer 5 is sent to the wheel device 10, the lateral moving device 12, and the vertical moving device 13. The output of the load measuring calculator 8 is sent to the moving device controlling calculator 5.

【0019】以上において、第2の模型2の風洞実験を
する場合、移動装置制御用計算機5は第2の模型2を投
下飛しょう経路に対応する各位置に移動する制御信号を
移動装置4に送る。移動装置4はこの制御信号に応じて
移動し、第2の模型2を投下飛しょう経路に沿い移動す
る。
In the above, when performing the wind tunnel experiment of the second model 2, the moving device control computer 5 sends to the moving device 4 a control signal for moving the second model 2 to each position corresponding to the flight path. send. The moving device 4 moves according to this control signal, and moves the second model 2 along the drop flight path.

【0020】6分力天秤3は第2の模型2に加わる力を
検出し、その信号を増幅器6,A/D変換器7を経て荷
重計測用計算機8へ送る。荷重計測用計算機8は入力信
号から第2の模型2に加わる空力荷重を各位置に対応し
て演算出力する。
The 6-component force balance 3 detects the force applied to the second model 2 and sends the signal to the load measuring computer 8 via the amplifier 6 and the A / D converter 7. The load measurement computer 8 calculates and outputs the aerodynamic load applied to the second model 2 from the input signal corresponding to each position.

【0021】万一、移動装置4の移動により第2の模型
2が第1の模型1に接触した場合、その反力は上記と同
様に作用して荷重計測用計算機8で算出される。荷重計
測用計算機8はこの反力が所定の設定値以上になったと
き、停止信号(非常停止信号)を移動装置制御用計算機
5へ送る。移動装置制御用計算機5はこの停止信号を受
けて各移動装置10,12,13を非常停止させる。
If the second model 2 comes into contact with the first model 1 due to the movement of the moving device 4, the reaction force thereof acts in the same manner as described above and is calculated by the load measuring computer 8. The load measurement computer 8 sends a stop signal (emergency stop signal) to the mobile device control computer 5 when the reaction force exceeds a predetermined set value. The mobile device control computer 5 receives the stop signal and causes the mobile devices 10, 12, and 13 to make an emergency stop.

【0022】上記の設定値を模型1,2の接触によって
模型が破損しない範囲内に設定しておく。移動装置制御
用計算機5は反力の上昇率とともにその大きさを計算
し、上記設定値以上になったとき停止信号を出力する。
処理フロー図を図2に示す。
The above set values are set within a range in which the models are not damaged by the contact between the models 1 and 2. The moving device control computer 5 calculates the magnitude of the reaction force together with the rate of increase, and outputs a stop signal when the value exceeds the set value.
A processing flow chart is shown in FIG.

【0023】以上のようにして、模型2が模型1に接触
破損することなく、各種の経路にわたる空力荷重の計測
が安全、確実に行えるようになる。
As described above, the aerodynamic load can be measured safely and reliably over various routes without the model 2 coming into contact with and damaging the model 1.

【0024】[0024]

【発明の効果】以上に説明したように本発明によれば次
の効果を奏する。
As described above, the present invention has the following effects.

【0025】(1)第1の模型の近くで第2の模型を移
動する風洞実験が、安全,確実に自動的に行える。
(1) A wind tunnel experiment in which the second model is moved near the first model can be automatically performed safely and reliably.

【0026】(2)模型の接触破損が発生せず、大幅な
工数低減が図れる。
(2) Contact damage to the model does not occur, and the number of steps can be greatly reduced.

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

【図1】本発明の実施の一形態の構成系統図である。FIG. 1 is a configuration system diagram of an embodiment of the present invention.

【図2】同一形態の処理フロー図である。FIG. 2 is a processing flow chart of the same form.

【符号の説明】[Explanation of symbols]

1 母機模型(第1の模型) 2 力計測用模型(第2の模型) 3 6分力天秤 4 移動装置 5 移動装置制御用計算機 6 アンプ 7 A/D変換器 8 荷重計測用計算機 10 車輪装置 11 台車 12 左右移動装置 13 上下移動装置 14 柱 15 風洞 16 取付アーム 1 mother machine model (first model) 2 force measurement model (second model) 3 6 component balance 4 moving device 5 moving device control computer 6 amplifier 7 A / D converter 8 load measuring computer 10 wheel device 11 Cart 12 Horizontal movement device 13 Vertical movement device 14 Pillar 15 Wind tunnel 16 Mounting arm

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 風洞上部に固定された第1の模型と、同
風洞下部に配置され取付けアームを持つ3軸移動式の移
動手段と、同移動手段を制御する移動制御手段と、上記
移動手段の取付けアームに取付けられた第2の模型と、
同第2の模型に加わる力を検出する力検出手段と、同検
出手段の出力を受ける増幅器と、同増幅器の出力を受け
るA/D変換器と、同A/D変換器の出力を受け上記力
を算出するとともに上記第2の模型が接触しその反力が
予め定められた設定値以上のとき停止信号を上記移動制
御手段へ送る荷重演算手段とを備えてなることを特徴と
する移動物体荷重計測装置。
1. A first model fixed to the upper part of the wind tunnel, a three-axis moving type moving means having a mounting arm arranged at the lower part of the wind tunnel, a movement control means for controlling the moving means, and the moving means. A second model attached to the mounting arm of
The force detecting means for detecting the force applied to the second model, the amplifier receiving the output of the detecting means, the A / D converter receiving the output of the amplifier, and the output of the A / D converter are described above. A moving object comprising: a force calculation means for calculating a force and sending a stop signal to the movement control means when the reaction force of the second model comes into contact with the second model and is equal to or more than a predetermined set value. Load measuring device.
JP6434296A 1996-03-21 1996-03-21 Apparatus for measuring load if moving body Withdrawn JPH09257635A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6434296A JPH09257635A (en) 1996-03-21 1996-03-21 Apparatus for measuring load if moving body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6434296A JPH09257635A (en) 1996-03-21 1996-03-21 Apparatus for measuring load if moving body

Publications (1)

Publication Number Publication Date
JPH09257635A true JPH09257635A (en) 1997-10-03

Family

ID=13255481

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6434296A Withdrawn JPH09257635A (en) 1996-03-21 1996-03-21 Apparatus for measuring load if moving body

Country Status (1)

Country Link
JP (1) JPH09257635A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002340734A (en) * 2001-05-15 2002-11-27 Fuji Heavy Ind Ltd Method and apparatus for testing motion simulation of test model
JP2003279439A (en) * 2003-02-10 2003-10-02 Tech Res & Dev Inst Of Japan Def Agency Dynamic wind tunnel testing device and method
CN102539107A (en) * 2012-02-17 2012-07-04 中国空气动力研究与发展中心高速空气动力研究所 Method for accurately synchronizing test signals of wind tunnel
CN108151996A (en) * 2017-12-26 2018-06-12 中国空气动力研究与发展中心高速空气动力研究所 The appraisal procedure and system of Flight Safety in a kind of tip vortex region
CN113029505A (en) * 2021-03-12 2021-06-25 中国空气动力研究与发展中心高速空气动力研究所 Wind tunnel flow field mobile measuring device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002340734A (en) * 2001-05-15 2002-11-27 Fuji Heavy Ind Ltd Method and apparatus for testing motion simulation of test model
JP2003279439A (en) * 2003-02-10 2003-10-02 Tech Res & Dev Inst Of Japan Def Agency Dynamic wind tunnel testing device and method
CN102539107A (en) * 2012-02-17 2012-07-04 中国空气动力研究与发展中心高速空气动力研究所 Method for accurately synchronizing test signals of wind tunnel
CN108151996A (en) * 2017-12-26 2018-06-12 中国空气动力研究与发展中心高速空气动力研究所 The appraisal procedure and system of Flight Safety in a kind of tip vortex region
CN113029505A (en) * 2021-03-12 2021-06-25 中国空气动力研究与发展中心高速空气动力研究所 Wind tunnel flow field mobile measuring device
CN113029505B (en) * 2021-03-12 2023-07-04 中国空气动力研究与发展中心高速空气动力研究所 Wind tunnel flow field mobile measurement device

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Effective date: 20030603