JP2971235B2 - Balance device - Google Patents

Balance device

Info

Publication number
JP2971235B2
JP2971235B2 JP6398292A JP6398292A JP2971235B2 JP 2971235 B2 JP2971235 B2 JP 2971235B2 JP 6398292 A JP6398292 A JP 6398292A JP 6398292 A JP6398292 A JP 6398292A JP 2971235 B2 JP2971235 B2 JP 2971235B2
Authority
JP
Japan
Prior art keywords
air
specimen
measured
wind tunnel
flow
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.)
Expired - Fee Related
Application number
JP6398292A
Other languages
Japanese (ja)
Other versions
JPH05264396A (en
Inventor
啓三 徳永
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 JP6398292A priority Critical patent/JP2971235B2/en
Publication of JPH05264396A publication Critical patent/JPH05264396A/en
Application granted granted Critical
Publication of JP2971235B2 publication Critical patent/JP2971235B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は、被計測物(以下供試体
という)の表面摩擦抵抗を計測するための天秤装置に関
する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a balance device for measuring the surface frictional resistance of an object to be measured (hereinafter referred to as a "test sample").

【0002】[0002]

【従来の技術】物体の表面は空気等の流れに対し摩擦抵
抗を生じる。このような摩擦抵抗を低減するために物体
の表面にリブレット(小溝)やLEBU(Large
Eddy Break up Device)等を設け
ることがある。これらの効果を計測するために、従来か
ら摩擦抵抗計測用の天秤装置が用いられている。
2. Description of the Related Art The surface of an object generates frictional resistance against the flow of air or the like. In order to reduce such frictional resistance, a riblet (small groove) or LEBU (Large)
Eddy Break up Device) may be provided. In order to measure these effects, a balance device for measuring frictional resistance has conventionally been used.

【0003】図6の(a)(b)(c)は、このような
天秤装置の従来例を示す図である。すなわち、風洞上壁
1に設けられた開口部2には、矩形板状の供試体3が周
辺に若干の間隙をもった状態で嵌込まれている。この供
試体3は、風洞上壁1の上方に位置している天井4から
4本のピアノ線5a〜5dによって、供試体3の表面す
なわち被計測面6が風洞上壁1の下面7と同一平面内に
位置するように吊り下げられている。さらに、矢印Mで
示す気流の上流側の風洞上壁1の上部8にはロードセル
9が設置され、このロードセル9と供試体3の上面とが
ワイヤ10で接続されている。
FIGS. 6A, 6B and 6C are views showing a conventional example of such a balance apparatus. That is, a rectangular plate-shaped specimen 3 is fitted into the opening 2 provided in the upper wall 1 of the wind tunnel with a slight gap around it. The surface of the test piece 3, that is, the surface to be measured 6 is the same as the lower surface 7 of the wind tunnel upper wall 1 by four piano wires 5 a to 5 d from the ceiling 4 located above the wind tunnel upper wall 1. It is suspended so that it is located in a plane. Further, a load cell 9 is installed in the upper portion 8 of the wind tunnel upper wall 1 on the upstream side of the airflow indicated by the arrow M, and the load cell 9 is connected to the upper surface of the specimen 3 by a wire 10.

【0004】かくして、風洞内に図中実線矢印Mで示す
方向に空気等の流体を通流させ、そのときの気流の流れ
に対する供試体3の表面摩擦抵抗を、ワイヤ10を介し
てロードセル9で計測していた。
Thus, a fluid such as air is caused to flow in the wind tunnel in the direction indicated by the solid arrow M in the drawing, and the surface frictional resistance of the specimen 3 against the flow of air at that time is measured by the load cell 9 via the wire 10. I was measuring.

【0005】[0005]

【発明が解決しようとする課題】上記した従来の天秤装
置では、ピアノ線5a〜5dの長さが比較的長く、しか
も単に供試体3を吊り下げたものとなっているので、供
試体3は水平面内で気流の通流方向に沿った動きの外、
気流の流れに直交する左右方向、すなわち図3の(c)
の実線矢印Nの方向にも自由に移動する。このため、供
試体3に加わる気流の流通方向成分以外の力がロードセ
ル9で計測されたり、供試体3の両側端が開口部2の端
面11,12に当たるなどして、正確な計測ができない
という問題があった。そこで本発明は、供試体に加わる
空気等の流体の流れに沿った方向の力成分のみを正確に
計測できる天秤装置を提供することを目的としている。
In the above-mentioned conventional balance apparatus, the length of the piano wires 5a to 5d is relatively long, and the test piece 3 is simply suspended. Outside the movement along the direction of air flow in the horizontal plane,
The horizontal direction orthogonal to the flow of the air flow, that is, FIG.
In the direction of the solid arrow N. Therefore, a force other than the flow direction component of the airflow applied to the specimen 3 is measured by the load cell 9, and both ends of the specimen 3 hit the end surfaces 11 and 12 of the opening 2, so that accurate measurement cannot be performed. There was a problem. Therefore, an object of the present invention is to provide a balance device that can accurately measure only a force component in a direction along a flow of a fluid such as air applied to a specimen.

【0006】[0006]

【課題を解決するための手段】上記課題を解決し目的を
達成するために、本発明では、次のような手段を講じ
た。すなわち、風洞の内壁面の一部に設けられた開口部
に上記内壁面と被計測物の表面とが同一平面内に位置す
るように上記被計測物を支持する支持機構と、前記被計
測物に働く風洞内流体の流れに沿った方向の力を測定す
る測定手段とを備えた天秤装置であって、前記支持機構
を、前記被計測物を前記流体の通流方向に沿ってのみス
ライド可能な如く支持するエアスライダを備えたものと
した。
Means for Solving the Problems In order to solve the above problems and achieve the object, the present invention takes the following measures. That is, a support mechanism for supporting the object to be measured such that the inner wall surface and the surface of the object to be measured are located in the same plane at an opening provided in a part of the inner wall surface of the wind tunnel; A measuring means for measuring a force in a direction along a flow of a fluid in a wind tunnel acting on the support mechanism, wherein the support mechanism can slide the object to be measured only along a flow direction of the fluid. The air slider was provided with such a support.

【0007】[0007]

【作用】上記手段を講じた結果、次のような作用が生じ
る。供試体を支持するエアスライダは軸方向のみに移動
可能で、軸方向に対して直角方向には移動しないので、
このエアスライダにより被計測物を流体通流方向にのみ
スライド可能な如く支持することができ、供試体に加わ
る流体通流方向の力成分のみを正確に計測することが可
能となる。
The following effects are obtained as a result of taking the above measures. The air slider supporting the specimen can move only in the axial direction, and does not move in the direction perpendicular to the axial direction.
The object to be measured can be supported by the air slider so as to be slidable only in the fluid flow direction, and only the force component applied to the specimen in the fluid flow direction can be accurately measured.

【0008】[0008]

【実施例】図1および図2の(a)(b)は本発明の第
1実施例に係る天秤装置を示す図である。なお、これら
の図において、図6にて示した部分と同一部分には同一
符号を付し、重複する部分の説明は省略する。
1 and 2 (a) and (b) show a balance apparatus according to a first embodiment of the present invention. In these figures, the same parts as those shown in FIG. 6 are denoted by the same reference numerals, and description of overlapping parts will be omitted.

【0009】この第1の実施例に係る天秤装置が従来の
天秤装置と異なる主な点は、供試体3を支持する構成に
ある。すなわちこの実施例では、供試体3の支持にエア
スライダ20a〜20d、すなわち空気軸受を用いてい
る。このエアスライダ20a〜20dは風洞上壁1に設
けられた長方形の開口部2の周囲に配置されている。こ
れらのエアスライダ20a〜20dのうち、エアスライ
ダ20aを代表としてその構造を示すと、図3の(a)
(b)に示すように構成されている。
The main difference between the balance apparatus according to the first embodiment and the conventional balance apparatus lies in the structure for supporting the specimen 3. That is, in this embodiment, the air sliders 20a to 20d, that is, the air bearings are used to support the specimen 3. The air sliders 20 a to 20 d are arranged around a rectangular opening 2 provided in the upper wall 1 of the wind tunnel. Of these air sliders 20a to 20d, the structure of the air slider 20a is shown as a representative.
It is configured as shown in FIG.

【0010】同図において21は固定体を示している。
この固定体21は、枠体22と、この枠体22の内部に
設けられた空気案内板23と、この空気案内板23のほ
ぼ中心部を貫通するように設けられた柱状空洞部24と
で構成されている。そして、柱状空洞部24内には、柱
状に形成された可動体25が柱状空洞部24の軸心線方
向に沿って移動自在に配置されている。
In FIG. 1, reference numeral 21 denotes a fixed body.
The fixed body 21 includes a frame 22, an air guide plate 23 provided inside the frame 22, and a columnar cavity 24 provided so as to penetrate substantially the center of the air guide plate 23. It is configured. In the columnar cavity 24, a movable body 25 formed in a columnar shape is movably arranged along the axial direction of the columnar cavity 24.

【0011】このように構成されたエアスライダ20a
には、高圧空気が図1に示されている高圧空気供給装置
26からエアホース27aを通して供給される。かくし
て空気案内板23と可動体25との間隙に高圧空気を満
たすことにより、可動体25を浮上させている。このと
き空気案内板23と可動体25との間隙は一定間隔に保
たれるため、可動体25は図中実線矢印X方向およびY
方向、すなわち軸方向と直角な方向には動くことができ
ない。したがって、可動体25aは図中実線矢印Z方
向、すなわち軸方向のみ自由に移動可能である。
The air slider 20a constructed as described above
, High-pressure air is supplied from a high-pressure air supply device 26 shown in FIG. 1 through an air hose 27a. Thus, the movable body 25 is levitated by filling the gap between the air guide plate 23 and the movable body 25 with high-pressure air. At this time, since the gap between the air guide plate 23 and the movable body 25 is kept at a fixed interval, the movable body 25 is
It cannot move in the direction, that is, the direction perpendicular to the axial direction. Therefore, the movable body 25a can freely move only in the direction of the solid arrow Z in the drawing, that is, only in the axial direction.

【0012】図1,図2の(a)(b)に説明を戻す。
エアスライダ20aと20bとは開口部2の上流側に配
置され、エアスライダ20cと20dとは開口部2の下
流側に配置されている。ここで、スライダ20a〜20
dは各可動体25a〜25dの軸方向が全て平行になる
ような向きに配置されており、各可動体25a〜25d
の先端に供試体3が固定されている。28はワイヤ、2
9は力計測センサである。
Returning to FIGS. 1 and 2 (a) and (b).
The air sliders 20a and 20b are arranged on the upstream side of the opening 2, and the air sliders 20c and 20d are arranged on the downstream side of the opening 2. Here, sliders 20a-20
d is arranged in such a direction that the axial directions of the movable bodies 25a to 25d are all parallel, and the movable bodies 25a to 25d
Specimen 3 is fixed to the tip of. 28 is a wire, 2
9 is a force measurement sensor.

【0013】このように構成された本実施例において
は、エアスライダ20a〜20dに高圧空気供給装置2
6から高圧空気を供給すると、可動体25a〜25dは
浮上し、供試体3が所定の位置、すなわち供試体3の下
面6が風洞上壁1の内壁面7と同一平面内に位置するよ
うに支持される。続いて風洞内に図中実線矢印Mで示す
方向に空気を通流させ、空気との摩擦抵抗によって供試
体3に作用する力をワイヤ28を介して力計測センサ2
9によって計測する。
In the embodiment constructed as described above, the high-pressure air supply device 2 is connected to the air sliders 20a to 20d.
When the high-pressure air is supplied from 6, the movable bodies 25a to 25d float, and the specimen 3 is positioned at a predetermined position, that is, the lower surface 6 of the specimen 3 is located on the same plane as the inner wall surface 7 of the wind tunnel upper wall 1. Supported. Subsequently, air is allowed to flow through the wind tunnel in the direction indicated by the solid arrow M in the figure, and the force acting on the specimen 3 due to frictional resistance with the air is transmitted through the wire 28 to the force measurement sensor 2.
Measured by 9.

【0014】このように本実施例では、供試体3が一方
向のみ、すなわち空気の通流方向のみに変位するように
規制されるので、供試体3に加わる気流の通流方向のみ
の力成分が高精度に計測されることになる。
As described above, in the present embodiment, since the specimen 3 is regulated so as to be displaced only in one direction, that is, only in the direction of air flow, the force component of the air flow applied to the specimen 3 only in the direction of air flow. Is measured with high accuracy.

【0015】図4および図5の(a)(b)は本発明の
第2実施例に係る天秤装置を示す図である。なお、これ
らの図において、図1および図2の(a)(b)にて示
した部分と同一部分には同一符号を付し、重複する部分
の説明は省略する。
FIGS. 4 and 5A and 5B show a balance apparatus according to a second embodiment of the present invention. In these figures, the same parts as those shown in FIGS. 1 and 2A and 2B are denoted by the same reference numerals, and the description of the overlapping parts will be omitted.

【0016】第2実施例が前記第1実施例と異なる点
は、供試体33が表面に所定の曲率を有する円板である
点である。すなわち、球殻の一部を形成する形状の供試
体33が、この供試体33と同じ曲率を有する風洞上壁
31に設けられた開口部32に対し、周辺に若干の間隙
をもった状態で嵌込まれている。この供試体33は、第
1実施例と同様に開口部32の周囲に配置されたエアス
ライダ20a〜20dによって支持されている。この実
施例においても、スライダ20a〜20dは可動体25
a〜25dの軸方向が全て平行になるような向きに配置
されており、各可動体25a〜25dの先端には供試体
33が固定されている。
The second embodiment differs from the first embodiment in that the specimen 33 is a disk having a predetermined curvature on its surface. That is, the specimen 33 having a shape that forms a part of a spherical shell has a slight gap around the opening 32 provided in the wind tunnel upper wall 31 having the same curvature as the specimen 33. It is embedded. The specimen 33 is supported by air sliders 20a to 20d arranged around the opening 32, as in the first embodiment. Also in this embodiment, the sliders 20a to 20d
The specimens 33 are fixed to the ends of the movable bodies 25a to 25d so that the axial directions of a to 25d are all parallel.

【0017】このように構成された本実施例において
は、エアスライダ20a〜20dに高圧空気供給装置2
6から高圧空気を供給すると、可動体25a〜25dは
浮上し、供試体33が所定の位置、すなわち供試体33
の下面36が風洞上壁31の内壁面37と同一曲面内に
位置するように支持される。
In the embodiment constructed as described above, the high-pressure air supply device 2 is provided to the air sliders 20a to 20d.
When the high-pressure air is supplied from 6, the movable bodies 25a to 25d float, and the specimen 33 is moved to a predetermined position, that is, the specimen 33
Is supported such that the lower surface 36 is located within the same curved surface as the inner wall surface 37 of the wind tunnel upper wall 31.

【0018】このように本実施例においても、第1実施
例と同様に供試体33が一方向のみ、すなわち空気の通
流方向のみに変位するように規制されるので、供試体3
3に加わる気流の通流方向のみの力成分が高精度に計測
されることになる。なお、本発明は前記各実施例に限定
されるものではなく本発明の要旨を逸脱しない範囲で種
々変形実施可能であるのは勿論である。
As described above, also in this embodiment, the specimen 33 is restricted so as to be displaced in only one direction, that is, only in the direction of air flow, as in the first embodiment.
The force component only in the direction of flow of the airflow applied to 3 is measured with high accuracy. It should be noted that the present invention is not limited to the above-described embodiments, and it goes without saying that various modifications can be made without departing from the spirit of the present invention.

【0019】[0019]

【発明の効果】本発明によれば、供試体の変位方向が流
体の通流方向にのみ変位するように規制されるので、供
試体に加わる流体の通流方向のみの力成分を高精度に計
測することができる。
According to the present invention, since the displacement direction of the specimen is regulated so as to be displaced only in the direction of flow of the fluid, the force component applied only to the direction of flow of the fluid applied to the specimen can be accurately detected. Can be measured.

【0020】また、エアスライダの軸方向に直角な方向
には移動しないので、供試体が風洞の開口部内に入り込
み、流体が供試体の端面にあたり、力計測センサに余分
な力が加わるようなことが避けられ、測定値の精度を一
層向上させ得る。
In addition, since the specimen does not move in the direction perpendicular to the axial direction of the air slider, the specimen enters the opening of the wind tunnel, and the fluid hits the end face of the specimen and an extra force is applied to the force measuring sensor. Can be avoided, and the accuracy of the measured value can be further improved.

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

【図1】本発明の第1実施例に係る天秤装置の構成を示
す平面図。
FIG. 1 is a plan view showing the configuration of a balance device according to a first embodiment of the present invention.

【図2】同実施例の要部を図1における2A−2A線お
よび2B−2B線に沿ってそれぞれ切断し矢印方向に見
た断面図。
FIG. 2 is a sectional view of a main part of the embodiment taken along lines 2A-2A and 2B-2B in FIG. 1 and viewed in the direction of the arrows;

【図3】同実施例のエアスライダの構成を示す斜視図お
よび断面図。
FIG. 3 is a perspective view and a cross-sectional view showing a configuration of the air slider of the embodiment.

【図4】本発明の第2実施例に係る天秤装置の構成を示
す平面図。
FIG. 4 is a plan view showing a configuration of a balance device according to a second embodiment of the present invention.

【図5】同実施例の要部を図4における5A−5A線お
よび5B−5B線に沿ってそれぞれ切断し矢印方向に見
た断面図。
FIG. 5 is a cross-sectional view taken along the line 5A-5A and the line 5B-5B of FIG.

【図6】従来の天秤装置の要部の平面図と断面図。FIG. 6 is a plan view and a cross-sectional view of a main part of a conventional balance device.

【符号の説明】[Explanation of symbols]

1、31…風洞、 2,32…開口
部、3、33…供試体、 20a〜20
d…エアスライダ、21…固定体、
25a〜25d…可動体、26…高圧空気供給装置、
27a〜27d…エアホース。
1, 31: wind tunnel, 2, 32: opening, 3, 33: specimen, 20a-20
d: air slider, 21: fixed body,
25a to 25d: movable body, 26: high-pressure air supply device,
27a-27d ... air hose.

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】流体が被計測物の表面に作用する力(表面
摩擦抵抗)を計測するための天秤装置であって、 風洞の内壁面の一部に設けられた開口部と、この開口部
内にその表面が前記風洞の内壁面と同一平面内に位置す
るように前記被計測物を支持する支持機構と、この支持
機構により支持された前記被計測物に働く風洞内流体の
流れに沿った方向の力を測定する測定手段とを備え、 前記支持機構は、前記被計測物を前記流体の通流方向に
沿ってのみスライド可能な如く支持するエアスライダを
備えてなることを特徴とする天秤装置。
1. A balance device for measuring a force (surface friction resistance) of a fluid acting on a surface of an object to be measured, comprising: an opening provided in a part of an inner wall surface of a wind tunnel; A support mechanism for supporting the object to be measured so that its surface is located in the same plane as the inner wall surface of the wind tunnel, and a flow of fluid in the wind tunnel acting on the object to be measured supported by the support mechanism. Measuring means for measuring a force in a direction, wherein the support mechanism includes an air slider which supports the object to be measured so as to be slidable only along a flow direction of the fluid. apparatus.
JP6398292A 1992-03-19 1992-03-19 Balance device Expired - Fee Related JP2971235B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6398292A JP2971235B2 (en) 1992-03-19 1992-03-19 Balance device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6398292A JP2971235B2 (en) 1992-03-19 1992-03-19 Balance device

Publications (2)

Publication Number Publication Date
JPH05264396A JPH05264396A (en) 1993-10-12
JP2971235B2 true JP2971235B2 (en) 1999-11-02

Family

ID=13245004

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6398292A Expired - Fee Related JP2971235B2 (en) 1992-03-19 1992-03-19 Balance device

Country Status (1)

Country Link
JP (1) JP2971235B2 (en)

Also Published As

Publication number Publication date
JPH05264396A (en) 1993-10-12

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