JPS60250260A - Current passage construction of thermoelectric type anemometer - Google Patents

Current passage construction of thermoelectric type anemometer

Info

Publication number
JPS60250260A
JPS60250260A JP10702084A JP10702084A JPS60250260A JP S60250260 A JPS60250260 A JP S60250260A JP 10702084 A JP10702084 A JP 10702084A JP 10702084 A JP10702084 A JP 10702084A JP S60250260 A JPS60250260 A JP S60250260A
Authority
JP
Japan
Prior art keywords
airflow
heating wire
temperature
inlet
current
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
JP10702084A
Other languages
Japanese (ja)
Other versions
JPH0452897B2 (en
Inventor
Seiro Katagiri
片桐 晴郎
Masatoshi Suzuki
正利 鈴木
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.)
Toyota Central R&D Labs Inc
Original Assignee
Toyota Central R&D Labs Inc
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 Toyota Central R&D Labs Inc filed Critical Toyota Central R&D Labs Inc
Priority to JP10702084A priority Critical patent/JPS60250260A/en
Publication of JPS60250260A publication Critical patent/JPS60250260A/en
Publication of JPH0452897B2 publication Critical patent/JPH0452897B2/ja
Granted legal-status Critical Current

Links

Abstract

PURPOSE:To widen the allowable deflection angle of current by making a current passage circle in the section thereof while an introduction port at the inlet side thereof in such a manner as to be larger in the diameter closer to the inlet. CONSTITUTION:An electrically heating wire 5 is applied and a high-temperature contact 10 adapted to be cooled according to the velocity of current to equal the same temperature as the heating wire and a low-temperature contact 12 to become the same temperature as the current are arranged to form thermocouples 6, 7, 9 and 11. A hood 13 is provided to cover the high-temperature contact 10 and the low-temperature contact 12 of the thermocouples 6, 7, 9 and 11 and the heating wire 5 and a current passage 14 is formed running through in the direction of crossing the heating wire 5. Then, a tranpet- or bellmouth-shaped introduction section 16 is formed at the inlet 15 side of the current path 14 in such a manner as to become larger in the diameter closer to the inlet 15.

Description

【発明の詳細な説明】 本発明は、気流中の局所の速度を計測する熱電式風速計
において、電気加熱される電熱線を横断する方向に挿通
した気流通路の構造に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to the structure of an airflow passage inserted in a direction transverse to an electrically heated heating wire in a thermoelectric anemometer that measures local velocity in an airflow.

従来、この種の熱電式風速計は、特開昭5乙−77、!
5g号公報に示されているように、基体の」二に電気加
熱される電熱線を上下方向に張設し、気流の速度に応じ
て冷却される電熱線と同温になる風速測定用高温接点と
、気流と同温になる風温補正用低温接点を基体の」−に
配置した熱電対を設り、基体に熱電対の高温接点と低温
接点及び電熱線を覆う門形のフードを取付けて、’yl
(熱線を横断する前後方向に挿通した長方形断面の気流
通路を形成している。この従来品においては、気流の方
向が気流通路の方向から縦方向又は横方向に偏向してい
るときにも、風速を正確に測定することができるが、測
定誤差が小さい気流の許容偏向角度は、縦方向では35
乃芋グO度0′tであり、横方向では25乃至30度位
であり1才だ充分に広いとは言い難い。
Conventionally, this type of thermoelectric anemometer was published in Japanese Patent Application Laid-Open No. 5-77!
As shown in Publication No. 5g, a heating wire that is electrically heated is stretched vertically on the second part of the base, and the temperature is the same as that of the heating wire that is cooled according to the speed of the airflow. A thermocouple is installed with a contact and a low-temperature contact for correcting the air temperature, which has the same temperature as the airflow, placed on the bottom of the base, and a gate-shaped hood is attached to the base to cover the high-temperature and low-temperature contacts of the thermocouple and the heating wire. Te,'yl
(It forms an air flow passage with a rectangular cross section that extends in the front-rear direction across the hot wire.In this conventional product, even when the direction of the air flow is deviated from the direction of the air flow passage in the vertical or horizontal direction, The permissible deflection angle of the airflow that allows accurate measurement of wind speed but with small measurement error is 35 in the vertical direction.
The angle is 0 degrees, and in the lateral direction it is about 25 to 30 degrees, which is not wide enough for a one year old.

本発明の目的は、上記のような欠点を有する従来品を改
良し、気流の許容偏向角度が広い熱電式風速計の気流通
路構造を提供することである。
An object of the present invention is to improve the conventional products having the above-mentioned drawbacks, and to provide an airflow passage structure for a thermoelectric anemometer with a wide allowable deflection angle of airflow.

次に1本発明の実施例について説明する。Next, one embodiment of the present invention will be described.

第1実施例(第1図乃至第を図参照) 本例の気流通路構造を備えた熱電式風速計は。First embodiment (see Figure 1 to Figure 1) This example is a thermoelectric anemometer with an air flow passage structure.

第1図に示すように、絶縁体の角棒状基体(1)の先端
面(2)の中央部と風下側端部にそれぞれ燐青銅の直柱
状支柱(3)、逆り形状支柱(4)を突設し、風上側に
突出した逆り形状支柱(4)の先端とこの真下に位置す
る直柱状支柱(3)の先端間にニクロム線の電熱線(5
)を接続して、電気加熱される電熱線(5)を基体の先
端部(2)と直角になる方向に張設し、基体の先端面(
2)の両支柱(3) 、 (4)中間位置と風上側端部
にそねぞれアルメルの第1支柱(6)、第2支柱(7)
を突設し、電熱線(5)の中央に一端(8)を接続した
アルメルの@/熱″6f対線(9)の他端を第1支柱(
6)の先端に接続し、第1熱電対線(9)の電熱線)妾
続端(8)に近接した位置に一端(1OF接続し7たク
ロメルの第2熱電対線01)の他端を第2支柱(7)の
先端に接続している。
As shown in Fig. 1, a phosphor bronze straight pillar (3) and an inverted pillar (4) are located at the center and leeward end of the tip surface (2) of the insulating square bar-shaped base (1). A heating wire (5) of nichrome wire is installed between the tip of the inverted-shaped column (4) protruding to the windward side and the tip of the straight column-shaped column (3) located directly below this column.
), and the electrically heated heating wire (5) is stretched in a direction perpendicular to the tip (2) of the base, and the tip of the base (
2) both pillars (3), (4) Alumel's first pillar (6) and second pillar (7) are threaded at the intermediate position and the windward end.
The other end of the 6f pair wire (9) of Alumel with one end (8) connected to the center of the heating wire (5) is connected to the first support (
6), and the other end of the second thermocouple wire 01 of Chromel connected 1OF at a position close to the heating wire (8) of the first thermocouple wire (9). is connected to the tip of the second support (7).

従って、アルメルの第1熱電対線(9)、第1支柱(6
)。
Therefore, the first thermocouple wire (9) of Alumel, the first column (6
).

第2支柱(7)とクロメルの第2熱電対線01)によっ
て熱電対を構成し、気流の速度に応じて冷却される電熱
線(5)の中央と同n1ユになる第1.第2熱電対線(
9) 、 01)の接続点(1(車を熱電力(6) 、
 (7) 、 (+’)> 、 Ql)の風速測定用高
温接点とし、気流と同温になる第2熱電対線01)と第
2支柱(7)の接続点(1つを熱電対(6) 、 (7
) 。
The second column (7) and the second chromel thermocouple wire (01) constitute a thermocouple, and the first column is the same as the center of the heating wire (5), which is cooled according to the speed of the airflow. Second thermocouple wire (
9), 01) connection point (1(car heat power (6),
(7) , (+')> , Ql) is used as a high temperature contact for wind speed measurement, and the connection point between the second thermocouple wire 01), which has the same temperature as the air flow, and the second pillar (7) (one thermocouple ( 6) , (7
).

(Q) 、 Ql)のIt?lu補正用低温接点として
いる。なお、電熱線用の両支柱(3) 、 (41の末
端間には電熱線(5)を加熱する電源が接続され、熱電
対用の両支柱(6)。
(Q), Ql) It? It is used as a low temperature contact for lu correction. In addition, a power source for heating the heating wire (5) is connected between the ends of the two struts (3) and (41) for the heating wire, and both struts (6) for the thermocouple.

(7)の末端間には熱電対(6) 、 (7) 、 (
9) 、 (11)の熱起電力を測定する風速指示計が
接続される。
There are thermocouples (6), (7), (
9) A wind speed indicator for measuring the thermoelectromotive force of (11) is connected.

基体(1)の先端部に84 、第1図と第、! 1mに
示すように、基体の先端面(2)上の各支柱(31、(
41、(6)、 (7)と電熱線(5)及び各P電対線
(g) 、 (11)を覆う円筒状のフード03をや付
けて、電熱線(5)と直交する方向に挿通した円形断面
の気流通路(1優を形成し、気流通路(1→の入口側に
、入口05)に近づくに従って大径になる朝顔形ないし
ベルマウス形の導入部0ゆを形成している。
84 at the tip of the base (1), Figures 1 and ! 1m, each strut (31, (
41, (6), (7), the heating wire (5), and each P couple wire (g), (11). The air flow passage (1) with a circular cross section is formed through the air flow passage (1 →), and a morning glory-shaped or bell mouth-shaped introduction part 0 is formed which becomes larger in diameter as it approaches the air flow passage (1 → inlet side, inlet 05). .

なお、各部の寸法は、気流通路04)の長さが/15朋
で、その径が6 rtrmであり、導入部Oeの長さが
55m1で、入口09の径が/!;IIIITあり、電
熱線用の逆り形状支柱(4)の高さが3 MMであり、
電熱線(5)の奥行が入口(慢から97MIMである。
The dimensions of each part are as follows: The length of the air flow passage 04) is /15 mm, its diameter is 6 rtrm, the length of the introduction part Oe is 55 m1, and the diameter of the inlet 09 is /! ; with IIIT, the height of the inverted-shaped support (4) for the heating wire is 3 MM,
The depth of the heating wire (5) is 97 MIM from the entrance.

気流の許容偏向角度の実験 本例の熱電式風速計と前記した長方形断面の気流通路材
の従来の熱電式風速計をそれぞれ用い、/ Om / 
sea位の一定速度に維持した気流の方向を、各支柱(
3) 、 (41、(61、(7)と電熱線(5)を含
む平面と平行に保持し、気流通路04に入る前の気流の
方向が電熱線(5)と直交する気流通路0IOの方向か
ら電熱線に沿った縦方向にずれる偏向角度θを6値に設
定して、その6値についてそれぞれ気流の速度を測定し
た。第3図は、この測定結果を示し、縦軸にρ11定風
速■を、横軸に上記の偏向角度θをそれぞれ採り、本例
の風速計の測定結果を黒丸付実線で、従来のそれを白丸
付破線でそれぞれ示す。
Experiment on the permissible deflection angle of airflow The thermoelectric anemometer of this example and the conventional thermoelectric anemometer with the rectangular cross-section airflow passage material described above were used, respectively. / Om /
The direction of the airflow maintained at a constant speed at the sea level is
3) , (41, (61, (7)) of the airflow passage 0IO held parallel to the plane containing the heating wire (5), and the direction of the airflow before entering the airflow passage 04 is perpendicular to the heating wire (5). The deflection angle θ that deviates from the direction along the heating wire in the vertical direction was set to six values, and the airflow velocity was measured for each of the six values.Figure 3 shows the measurement results, and the vertical axis shows the ρ11 constant. The wind speed (■) is plotted on the horizontal axis, and the deflection angle θ is plotted on the horizontal axis, and the measurement results of the anemometer of this example are shown by a solid line with a black circle, and those of the conventional one are shown by a broken line with a white circle.

第3図の線図から明らかなように、測定誤差が小さい気
流の縦方向への許容偏向角度は、従来品においては35
乃至llO度位であるのに対し、発明品においては70
度位であり、発明品の方が広い。
As is clear from the diagram in Figure 3, the permissible deflection angle in the vertical direction of the airflow with small measurement error is 35 for the conventional product.
Invented products have a temperature of 70 to 10 degrees.
It is a degree, and inventions are broader.

また、/ Q mrx / Sea位の一定速度に維持
した気流の方向を!熱線(5)と直交する平面と平行に
保持し、気流通路04)に入る前の気流の方向が気流通
路 5− 04)の方向から電熱線(5)と直交する横方向にずれ
る偏向角度αを6値に設定して、その6値についてそれ
ぞれ気流の速度を測定した。第を図は、この測定結果を
第3図と同様にして示す。
Also, the direction of the airflow maintained at a constant speed of / Q mrx / Sea! The deflection angle α is such that the direction of the airflow before entering the airflow passage 04) is held parallel to a plane perpendicular to the heating wire (5) and deviates from the direction of the airflow passage 5-04) in a lateral direction perpendicular to the heating wire (5). was set to six values, and the airflow velocity was measured for each of the six values. Figure 3 shows the results of this measurement in the same manner as in Figure 3.

第7図の線図から明らかなように、気流の横方向への許
容偏向角度は、従来品においては25乃至30度位であ
るのに対し、発明品においては乙0乃至go度位であり
、発明品の方が広い。
As is clear from the diagram in Figure 7, the allowable horizontal deflection angle of the airflow is about 25 to 30 degrees in the conventional product, whereas it is about 0 to 0 degrees in the invented product. , inventions are broader.

また、本例の熱電式風速計においては、気流通路04)
の断面形状が円形であるので、長方形である従来品にお
けるのとは異なり、気流が縦方向と横方向の中間の斜方
向に偏向しているときにも、風速を正確に測定すること
ができ、気流の斜方向への許容偏向角度は広いものと推
定される。
In addition, in the thermoelectric anemometer of this example, the airflow passage 04)
Since the cross-sectional shape of the is circular, unlike conventional products which are rectangular, it is possible to accurately measure wind speed even when the airflow is deflected in an oblique direction between the vertical and horizontal directions. , the allowable angle of deflection of the airflow in the oblique direction is estimated to be wide.

第2実施例(第5図と第3図、第q図参照)本例の気流
通路構造を備えた熱電式風速計は、第5図に示すように
、気流通路0荀の入口09側に設けた導入部OQを開き
角が乙O度の円錐筒形状ないしテーバ孔形杖に形成した
ものである。その他の点は、前例におけるのと同様であ
るので、第S図 6− に同一符号を付して説明を省略する。
Second Embodiment (See Figures 5, 3, and q) The thermoelectric anemometer with the airflow passage structure of this example has a The provided introduction part OQ is formed into a conical cylinder shape or a Taber hole shape with an opening angle of O degrees. Other points are the same as those in the previous example, so the same reference numerals are given to FIG. S6- and the explanation thereof will be omitted.

本例の熱電式風速計について前例におけるのと同様に気
流の許容偏向角度の実験を行い、第3図と第4図に半黒
丸付鎖線で示す測定結果を得た。
For the thermoelectric anemometer of this example, experiments were conducted on the allowable deflection angle of the airflow in the same manner as in the previous example, and the measurement results shown in FIGS. 3 and 4 by the dashed line with half-black circles were obtained.

第3図と第り図の線図から明らかなように、本例の熱電
式風速計における気流の縦方向又は横方向への許容偏向
角度は、前例におけるのと同様に広い。
As is clear from the diagrams in FIGS. 3 and 3, the permissible vertical or lateral deflection angle of the air flow in the thermoelectric anemometer of this example is as wide as in the previous example.

上記の各実施例の熱電式風速計において、気流通路の出
口に格子や網のよつな気流抵抗体を取付けると、気流通
路の出口に近接した位置に気流を乱す物体が存在する場
合、その気流の乱わが気流通路内に波及せず、風速を正
確に測定することができる。
In the thermoelectric anemometers of the above embodiments, if an airflow resistor such as a grid or a mesh is installed at the outlet of the airflow passage, if there is an object that disturbs the airflow near the outlet of the airflow passage, Airflow turbulence does not spread into the airflow path, allowing accurate measurement of wind speed.

本発明は、電気加熱される電熱線を張設し、気流の速度
に応じて冷却される電熱線と同温になる高温接点と、気
流と同温になる低温接点を設けたpP、電対を構成し、
熱電対の高温接点と低温接点及び電熱線を覆うフードを
設けて、電熱線P横断する方向に挿通した気流通路を形
成した熱電式風速計において、気流通1洛の断面形状を
円形に形成し、気流通路の入口側に、入口に近づくに従
って大径になる導入部な形成したことを特徴とする熱電
式風速計の気流通路構造である。
The present invention provides a pP, electric couple, in which a heating wire that is electrically heated is stretched, and a high-temperature contact that has the same temperature as the heating wire that is cooled according to the speed of the airflow, and a low-temperature contact that has the same temperature as the airflow. constitutes,
In a thermoelectric anemometer in which a hood is provided to cover the high-temperature and low-temperature contacts of the thermocouple and the heating wire, and an airflow passage is formed that extends in the direction across the heating wire P, the cross-sectional shape of the airflow is circular. This is an air flow passage structure of a thermoelectric anemometer, characterized in that an introduction part is formed on the inlet side of the air flow passage, the diameter of which increases as it approaches the inlet.

この気流通路構造においては、測定誤差が小さい気流の
許容偏向角度が広い。
This airflow passage structure has a wide allowable deflection angle for airflow with small measurement errors.

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

第7図は本発明の第1実施例の熱電式風速計の気流通路
構造の一部縦断側面図であり、第2[グは同気流通路構
造の正面図である。 第3図は発明品と従来品における測定風速Vと気流の縦
方向への偏向角度θの関係を示す線図であり、第1図は
発明品と従来品における測定風速Vと気流の横方向への
偏向角度αの関係を示す線図である。 第5図は本発明の第2実施例の熱電式風速計の気流通路
構造の一部縦断側面図である。 5:電熱線 6,7,9,11 :熱電対10:高温接
点 12:低温接点 13:フード 14:気流通路 15:入 口 16:導入部  9−
FIG. 7 is a partially longitudinal sectional side view of the air flow passage structure of the thermoelectric anemometer according to the first embodiment of the present invention, and FIG. 7 is a front view of the air flow passage structure. Figure 3 is a diagram showing the relationship between the measured wind speed V and the deflection angle θ in the vertical direction of the airflow in the invention and the conventional product, and Figure 1 is a diagram showing the relationship between the measured wind speed V and the horizontal direction of the airflow in the invention and the conventional product. FIG. 3 is a diagram showing the relationship of the deflection angle α to FIG. 5 is a partially vertical side view of the airflow passage structure of the thermoelectric anemometer according to the second embodiment of the present invention. 5: Heating wire 6, 7, 9, 11: Thermocouple 10: High temperature contact 12: Low temperature contact 13: Hood 14: Airflow passage 15: Inlet 16: Introduction part 9-

Claims (1)

【特許請求の範囲】[Claims] 電気加熱される電熱線を張設し、気流の速度に応じて冷
却される’KW線と同温になる高温接点と、気流と同温
になる低温接点を設けた熱電対を構成し、熱電対の高温
接点と低温接点及び電熱線を覆うフードを設けて、電熱
線を横断する方向に挿通した気流通路を形成した熱電式
風速計において、気流通路の断面形状を円形に形成し、
気流通路の入口側に、入口に近づくに従って大径になる
導入部を形成したことを特徴とする熱電式風速計の気流
通路構造。
A thermocouple is constructed by installing a heating wire that is electrically heated, and has a high-temperature contact that has the same temperature as the KW wire that is cooled according to the speed of the airflow, and a low-temperature contact that has the same temperature as the airflow. In a thermoelectric anemometer in which a hood covering a pair of high-temperature and low-temperature contacts and a heating wire is provided to form an airflow passage extending in a direction transverse to the heating wire, the airflow passage has a circular cross-sectional shape,
An air flow passage structure for a thermoelectric anemometer, characterized in that an introduction part is formed on the inlet side of the air flow passage, the diameter of which increases as it approaches the inlet.
JP10702084A 1984-05-25 1984-05-25 Current passage construction of thermoelectric type anemometer Granted JPS60250260A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10702084A JPS60250260A (en) 1984-05-25 1984-05-25 Current passage construction of thermoelectric type anemometer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10702084A JPS60250260A (en) 1984-05-25 1984-05-25 Current passage construction of thermoelectric type anemometer

Publications (2)

Publication Number Publication Date
JPS60250260A true JPS60250260A (en) 1985-12-10
JPH0452897B2 JPH0452897B2 (en) 1992-08-25

Family

ID=14448474

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10702084A Granted JPS60250260A (en) 1984-05-25 1984-05-25 Current passage construction of thermoelectric type anemometer

Country Status (1)

Country Link
JP (1) JPS60250260A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CZ304794B6 (en) * 2013-09-03 2014-10-22 České vysoké učení technické v Praze, Fakulta strojní, Ústav mechaniky tekutin a termodynamiky Flow meter

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5437333U (en) * 1977-08-12 1979-03-12
JPS5439749A (en) * 1977-07-07 1979-03-27 Greene Jerome Flexible joint
JPS5679258A (en) * 1979-11-30 1981-06-29 Toyota Central Res & Dev Lab Inc Detecting body for thermoelectric and air-temperature anemometer

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5439749A (en) * 1977-07-07 1979-03-27 Greene Jerome Flexible joint
JPS5437333U (en) * 1977-08-12 1979-03-12
JPS5679258A (en) * 1979-11-30 1981-06-29 Toyota Central Res & Dev Lab Inc Detecting body for thermoelectric and air-temperature anemometer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CZ304794B6 (en) * 2013-09-03 2014-10-22 České vysoké učení technické v Praze, Fakulta strojní, Ústav mechaniky tekutin a termodynamiky Flow meter

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