JPS60188854A - Wind direction meter - Google Patents

Wind direction meter

Info

Publication number
JPS60188854A
JPS60188854A JP4409184A JP4409184A JPS60188854A JP S60188854 A JPS60188854 A JP S60188854A JP 4409184 A JP4409184 A JP 4409184A JP 4409184 A JP4409184 A JP 4409184A JP S60188854 A JPS60188854 A JP S60188854A
Authority
JP
Japan
Prior art keywords
wind
arrow vane
center
vane
arrow
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
JP4409184A
Other languages
Japanese (ja)
Other versions
JPH032429B2 (en
Inventor
Toshihiko Ota
大田 利彦
Otomi Uyama
宇山 乙巳
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 JP4409184A priority Critical patent/JPS60188854A/en
Publication of JPS60188854A publication Critical patent/JPS60188854A/en
Publication of JPH032429B2 publication Critical patent/JPH032429B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00Indicating or recording presence, absence, or direction, of movement
    • G01P13/02Indicating direction only, e.g. by weather vane

Abstract

PURPOSE:To reduce a time constant of self-vibration, to increase a response speed even in case of a low wind speed, and also to make a titled meter light in weight by installing an arrow vane at a prescribed angle and in a position of the center of gravity of the arrow vane, to two arrow vane installing shafts orthogonal to a rotary cylinder, and bending the upper part and the lower part of the arrow vane by a prescribed angle to the outside. CONSTITUTION:On a rotary cylinder 5, two arrow vane installing shafts 7 orthogonal to said cylinder are provided so as to be opposed to each other on the same straight line, and to both its end parts, an arrow vane 9 is installed so that the front part of the arrow vane is turned to the inside of a wind direction meter at a prescribed angle alpha, respectively, in a position of its center of gravity. The upper part and the lower part of the arrow vane 9 are bent at a prescribed angle beta to the outside so that the width (a) of the vertical surface of the upstream side of an air current becomes smaller than the width (b) of the downstream side. Also, the installing angle alpha of the arrow vane is made large, and said meter is made ligth in weight by omitting a balance weight, therefore, a continuous time of self-vibration is shortened, and it responds exactly and quickly even at the time of a low wind velocity. Also, the center of wind pressure retreats from a position of the center of gravity, and the stability against the horizontal wind is improved.

Description

【発明の詳細な説明】 この発明は、+i向計に係るもので、更に詳しくは、2
枚の矢羽根を回転軸に対して、互に反対位置で、風向計
の中心線に対して対象に設【プた2枚羽根風向泪に関づ
るものCある。
[Detailed Description of the Invention] This invention relates to a +i counter, and more specifically,
There is a design related to a two-blade wind vane, in which two fletching feathers are placed at opposite positions to the axis of rotation and symmetrically to the center line of the wind vane.

従来、風向計は、@造が簡単な1枚の矢羽根を待ったも
のが、一般に使用されてぎた。然し、1枚羽根のj虱向
計は、自己振動の時定数(風向計に直角方向から急に風
が吹いた場合、風向計が動きだしてから振動が停止する
までの時間である。風速1011/SeCの場合5秒以
下とされている。)が大きく、風速が小さい場合には茗
しく大きくなる。これに対し゛(、−Il、)多用され
lこ2枚の矢羽根 ′を持った班11i’jl ;’I
は、自己振動の11.4定数を小さくづることが(・さ
るbの【・あるが、2枚の矢羽根を、従来の1枚矢羽根
の風+n1計と同じJ、うな位ii’? iこ取付けC
いたのC1平衡重鍾が必要であり、また矢羽根の取(q
角(風向G1の中心線ど矢羽根の垂i/j ’l’而と
のなす角)が比較的小さかったのて゛、充分にその長所
を発揮することができ4jかった。まJ: lj;1速
が低い場合、応答速度が遅いという問題があ−)だ。
Traditionally, wind vanes have generally been made from a single arrow blade, which is easy to construct. However, a single-blade fly vane has a self-oscillation time constant (when the wind suddenly blows from a direction perpendicular to the wind vane, it is the time from when the wind vane starts moving until it stops vibrating. Wind speed 1011 /SeC, it is said to be 5 seconds or less.) is large, and when the wind speed is low, it increases considerably. On the other hand, the team 11i'jl with two arrow feathers '(, -Il,) was often used;'I
Is it possible to write the 11.4 constant of self-oscillation small? I installation C
A C1 balanced heavy plow is required, and the fletching (q) is required.
Since the angle (the angle between the center line of the wind direction G1 and the plume's vertical i/j 'l') was relatively small, it was able to fully utilize its advantages. MaJ: lj;If the first gear is low, there is a problem that the response speed is slow.

この発明は、従来の2枚羽根の風向口の欠Ji、tを改
善し、時定数が小ざ<、’JII速の低い場合でb、応
答速1文が早く、また軽量な風向h1を提供覆ることを
(」的とづるものである。
This invention improves the deficiency Ji,t of the conventional two-blade wind opening, has a small time constant <,'b at low JII speeds, has a fast response speed, and has a lightweight wind direction h1. It is meant to cover the offer.

一般に、風向口の時定数を小さくするためには、(1)
 自己振動の周期を小さくづ−る。(2)減衰率を大き
くする。(3)(員1イ1モーメン1〜を小さくするこ
とが有効である。本発明省らは、2枚羽根の風向計に+
I3い(、矢羽根の取付角を大ぎくすると、自己振動の
周期が小さくなり、また減衰率が人さくなることを見い
だした。、した、2枚の矢羽根を風向1,10回’l’
z+ ihl+に対しくシ月こ艮対位iii ”C1そ
れぞれの重心位if”jにおい(、矢羽根取イ」軸に取
(=Jけることしこより、1ζ°j性七−メントが著し
く減少し、低風速時の時定数の但1・及び応答速度の向
上に、W;若な効果をあげることができた。
Generally, in order to reduce the time constant of the wind direction, (1)
Decrease the period of self-oscillation. (2) Increase the attenuation rate. (3) It is effective to reduce the value of 1 moment 1.
I3 (I found that if the mounting angle of the fletching was increased, the period of self-oscillation became smaller and the damping rate became weaker.) The two fletchers were rotated 1.10 times in the wind direction. '
z+ ihl+ vs. iii ``C1's respective center of gravity position if'' j odor (, arrow feather removal i'' axis) (=J kerukotoshiko, 1ζ°j sex 7-ment is significantly reduced However, W; a small effect was achieved in improving the time constant and response speed at low wind speeds.

更に、矢羽根の垂直平面の上部及び下部を外方に折り曲
げることにより、水平前方よりの気流が、上手方向へ拡
散Jることを防止づるfJか、斜1hまlこにL−トI
]の気流の水平分力を、イj効に利用で2きることが分
った。また、この折り曲げによって残る垂直平面の幅を
、気流の上流側を、下流側より小さくづることにより、
風圧中心が、重心位置にり後IJに移動し、横風に対し
−Cも安定性がよくなつIこ。この発明は、このような
知見に基づいて行われたものである。
Furthermore, by bending the upper and lower parts of the vertical plane of the fletching outward, the airflow from the horizontal front can be prevented from dispersing upward.
] It was found that the horizontal force of the airflow can be used effectively. In addition, by making the width of the vertical plane left by this bending smaller on the upstream side of the airflow than on the downstream side,
The center of wind pressure moves to IJ after reaching the center of gravity, and -C also becomes more stable against crosswinds. This invention was made based on such knowledge.

即ち、風向i1の回転筒に、これと直交4る2個の失態
板取(’J軸を、Hに反対位置に設置)、前記失態板取
(=I軸の両端部に、矢羽根を所定角度L” 、H−)
、矢羽根の重心位1醒にJ3いて取イζ]す、前記矢羽
根の上部及び1・部を・、外力に所定角度にJJlり曲
げlJことを構成の要旨とJるものである。
That is, on a rotating cylinder in the wind direction i1, there are two blunder plates perpendicular to the rotating cylinder ('J axis is installed at the opposite position to H), and the blunder plates (= arrow feathers are set at both ends of the I axis at a predetermined angle). L", H-)
The gist of the construction is to take the center of gravity of the fletching and bend it at a predetermined angle in response to an external force.

次にこの発明の実施例につい(、添(J図面IJ J、
って説明Jる。固定1而1の中心部に、回転軸3か回転
1右に設置〕られ、このfin +Ivt ’1lll
ζ3の上部に、回転筒5が猛るされている。回転筒5に
は、これど肖交覆る2木の等長の失態板取(q軸7が、
同−直線十ぐ、回転筒5に夕・]シて71に反λ・j位
U′Yに、−ジ(j))れ、その両端部に矢羽根9がぞ
の重心位1行にJjいで、それぞれ所定角度αで、矢羽
根の前部がBil向h1の内側に向うJ、うに取(’J
 4)られ(−いる1、矢羽根9の上部及び下部は、外
方に所定角度β(この実施例では垂直面と45)哀)で
、気流の上流側の!ti直平面の幅aが、下流側の幅す
より小さくなるJ、うに折り曲げられている。
Next, regarding the embodiments of this invention (, attached (J drawing IJ J,
That's the explanation. Fixed 1 is installed in the center of 1, on the rotation axis 3 or on the right of rotation 1], and this fin +Ivt '1llll
A rotary cylinder 5 is mounted on the upper part of ζ3. On the rotary cylinder 5, there are two wooden boards of equal length that overlap each other (the q-axis 7 is
On the same straight line, the rotary cylinder 5 is placed in a line 71 at an anti-λ·j position U'Y, and the arrow blades 9 are placed in one line at the center of gravity at both ends. At Jj, the front part of the arrow faces toward the inside of Bill direction h1 at a predetermined angle α, J, and sea urchin ('J
4) The upper and lower portions of the fletching 9 are outwardly at a predetermined angle β (45 degrees with respect to the vertical plane in this embodiment) on the upstream side of the airflow! It is bent in a shape J such that the width a of the straight plane is smaller than the width of the downstream side.

次に、この実施例の作用について説明り−る。第4図に
おい゛(、回転軸の中心をO、I!I!l向i1の向心
1を1−1、矢羽根取付軸の長さを12、失態41Nの
取明#llI iμのンγ’ji’(内容に変更なし)
何句をα、その横方向及び縦方向の長さをそれぞれ11
、d、その表面積及び重量をそれぞれS及びW、その重
心位置をG2.Gr、空気の密度をPとし、矢羽根の風
圧の中心は重心位置と一致するものとした。今、速度V
の風が、風向計の中心iHに対して矢羽根の取付角αよ
り小さい角度θで吹いた場合、それぞれの矢羽根に垂直
な風圧の分力PL、 Pr 及びこれらによる回転軸O
の回りのトルクTJ 、 Trばそれぞれ次のようにな
る。
Next, the operation of this embodiment will be explained. In FIG. γ'ji' (no change in content)
How many phrases α, its horizontal and vertical lengths are each 11
, d, its surface area and weight are S and W, respectively, and its center of gravity is G2. Gr, the density of air is P, and the center of the wind pressure of the fletching coincides with the center of gravity. Now the speed V
When the wind blows at an angle θ smaller than the installation angle α of the arrow blades with respect to the center iH of the wind vane, the component forces of wind pressure perpendicular to each arrow blade PL, Pr and the axis of rotation O due to these
The torques around TJ and Tr are as follows, respectively.

p2 = psl”sin”(α+θ)・・・・・・・
・・・・・・・・・・・・・・・・・・・・(1)Pr
二psV2sin”(α−θ)・・・・・・・・・・・
・・・・・・・・・・・・・・・・(2)’14 ””
 2628M”5inctsin”(α+θ)・・・・
−・・・・・・・・・・(3)Tr==%zSV’si
nαsin’(α−θ)・・・・・・・・・・・・・・
・(4)反時計方向のトルクを正とすれば、風向計に作
用するトルクTは、T1とTrの差で T == pHt Slj’sinαsin 2α5i
n2θ ・・・・・・・・・・−・・−・・・・(5)
明達111四の:’f’:!:(内容に変更なし)とな
る。θが小さい場合には、 T=−(2%tS’L/’sinα5in2α)θ・・
・・・・・・・・・・・・・−+6)となる。即ち、矢
羽根を回すトルクはθに比例する。単位角変位に対する
トルクをKとすれば、K” ” Ply 5fsinα
sin 2α・・・・・・・・・・・・・・・・・・・
・・・・・(7)となる。
p2 = psl"sin" (α+θ)・・・・・・
・・・・・・・・・・・・・・・・・・・・・(1) Pr
2psV2sin” (α−θ)・・・・・・・・・・・・
・・・・・・・・・・・・・・・・・・(2)'14 ””
2628M "5 inctsin" (α+θ)...
−・・・・・・・・・・・・(3) Tr==%zSV'si
nαsin'(α−θ)・・・・・・・・・・・・・・・
・(4) If the counterclockwise torque is positive, the torque T acting on the wind vane is the difference between T1 and Tr: T == pHt Slj'sinαsin 2α5i
n2θ・・・・・・・・・−・・−・・・・(5)
Meida 1114:'f':! : (no change in content). When θ is small, T=-(2%tS'L/'sinα5in2α)θ・・
・・・・・・・・・・・・・−+6). That is, the torque for turning the fletching is proportional to θ. If the torque for unit angular displacement is K, then K""Ply 5fsinα
sin 2α・・・・・・・・・・・・・・・・・・
...(7).

次にこの風向計の回転軸00回りの慣性モーメントを工
とし、矢羽根の取付軸の重量を無視する一般に風向計に
は、角速度の2乗に比例する減衰トルクと、矢羽根の重
量に比例するクーロン摩擦が作用するので、その振動は
、非線形減衰振動となり、減衰率や固有振動数の算出が
複雑になる。
Next, the moment of inertia around the rotation axis 00 of this wind vane is calculated, and the weight of the fletching shaft is ignored.Generally, wind vanes have a damping torque proportional to the square of the angular velocity, and a damping torque proportional to the fletching weight. Since Coulomb friction acts on the vibration, the vibration becomes a nonlinear damped vibration, making calculation of the damping rate and natural frequency complicated.

そこで、以下の説明を簡明にするために、クーロン摩擦
を無視し減衰トルクが角速度に比例するものとして、等
側線形減衰振動について説明する。
Therefore, in order to simplify the following explanation, the isolateral linear damped vibration will be explained assuming that the Coulomb friction is ignored and the damping torque is proportional to the angular velocity.

単位角速度に対する減衰トルクをCとすれば、Cは、矢
羽根の回転方向の面積と、取付軸の長さのほぼ2乗に比
例するので、 明、!:+l13の、γ・2:(内容にiΣ更なし)C
=(472”5sinα ・・・・・・・・・・・・・
−・・・・・・・・・・・・・・・・(9)となる。C
1は比例常数である。
If the damping torque for a unit angular velocity is C, then C is proportional to the area of the arrow blade in the rotational direction and approximately the square of the length of the mounting shaft. :+l13, γ・2: (no iΣ change in content)C
=(472”5sinα ・・・・・・・・・・・・・・・
−・・・・・・・・・・・・・・・(9). C
1 is a constant of proportionality.

前記の単位角変位に対するトルクに1慣性モーメンl−
I、単位角速度に対する減衰トルクCによるこの風向計
の振動は ■θ+Cθ+1(θ=0 ・・・・中・由由・・・・・
・・・・・・・・(IQ)θ: A e−”LCO5(
q を−ψ)・・・・・・・・・・・・・・・・・・・
・・・・・・・・C11+で表わされる。ここでA、ψ
は常数 前記のに、I、Cの値を用いてμ、woを表わとなる。
The torque for the above unit angular displacement is 1 moment of inertia l-
I, the vibration of this wind vane due to damping torque C for unit angular velocity is ■ θ + C θ + 1 (θ = 0...Medium, Yuyu...
・・・・・・・・・(IQ)θ: A e-”LCO5(
q to −ψ)・・・・・・・・・・・・・・・・・・
......Represented by C11+. Here A, ψ
are the constants described above, and express μ and wo using the values of I and C.

μは減衰定数で、式(12)から明らかなように矢羽根
の取付角αを大きく、その面積Sを大きく、風向計の重
i:Wを小さくすれば、共に大きくなる。即ち振動が早
く停止する。この発明18開F38GO−188854
(3)はこれらの条件に沿ったものである。tl)oは
減衰のない場合の固有角振動数(rad /sec )
で、この風向81の固有角振動数t7.− (rad 
/sea )は、woを人ぎくずれば、大ぎくなる。即
ら周期が小さくなる。(JJoは式(13)から明らか
なように風向計の重量Wを小さくし、矢羽根の取(=l
角αを大きく、面積を大ぎく、長さを短かく、即ち組方
風向51にθの角度で風が吹いた場合、Jll向J1が
風の方向に追従する応答速度は、風向itの固有振動角
速度例に比例づ−るので、hoを大きくり−れば、例が
大きくなり、応答速度が大きくなる。また式(13)か
ら明らかなように(SoはI!ill 3W Fに比例
覆るので、低風速時の風向h1の応答速度は小さくなる
が、この発明においては、前記のように失態411!の
取イ]角αを人さく、重量を小さくしたので、従来の風
向計に比較し低風速時の応答速度を著しく人さくするこ
とができた。
μ is the attenuation constant, and as is clear from equation (12), if the mounting angle α of the fletching blade is increased, the area S thereof is increased, and the weight i:W of the wind vane is decreased, both of them increase. That is, the vibration stops quickly. This invention 18 open F38GO-188854
(3) is in line with these conditions. tl)o is the natural angular frequency (rad/sec) without damping
Then, the natural angular frequency t7 of this wind direction 81. - (rad
/sea) becomes a big deal if you make wo awkward. That is, the period becomes smaller. (As is clear from Equation (13), JJo reduces the weight W of the wind vane, and the length of the arrow blade (=l
When the angle α is increased, the area is increased, and the length is shortened, that is, when the wind blows at an angle θ in the wind direction 51, the response speed at which the Jll direction J1 follows the wind direction is determined by the characteristic of the wind direction it. Since it is proportional to the vibration angular velocity, if ho is increased, the velocity becomes larger and the response speed increases. Furthermore, as is clear from equation (13) (because So is proportional to I!ill 3W F, the response speed of wind direction h1 at low wind speed becomes small, but in this invention, as mentioned above, the response speed of wind direction h1 is small) By reducing the angle α and reducing the weight, we were able to significantly reduce the response speed at low wind speeds compared to conventional wind vanes.

・、i6’1ll−4iの21曇、jシ(内容に変更な
し)この発明の風向計で矢羽根の取付角αを、30度に
したものの風洞実験によると、1虱速10m/Secに
おける時定数は、3.5 secであり、1.5 m 
/secの低風速時の時定数は7.5 secであった
。風向計の風速I Q m/SQCでの時定数t、。か
ら、任意の風速”Ll’n時の時定数knをめる実験式
として、次のものがある。
・, i6'1ll-4i's 21 cloudy, jshi (no change in content) According to wind tunnel experiments of the wind vane of this invention in which the installation angle α of the fletching blade was set to 30 degrees, at a speed of 10 m/Sec. The time constant is 3.5 sec and 1.5 m
The time constant at low wind speed of /sec was 7.5 sec. Wind vane wind speed I Q m/time constant t at SQC. From this, the following is an empirical formula for calculating the time constant kn at an arbitrary wind speed "Ll'n.

式(14)によって、この風向計の] Om/secの
時定数3.5秒から1.5 m / secにおける時
定数をめると tn : 13,2 sec になる。
According to equation (14), subtracting the time constant at 1.5 m/sec from the time constant of 3.5 seconds of Om/sec of this wind vane results in tn: 13.2 sec.

この値が従来の風向計の平均的な時′iJl数である。This value is the average hour'iJl number of a conventional wind vane.

これに比較し、この発明の風向計は、前記のように時定
数が7.5秒であり、低風速の場合でも、振動が速やか
に停止する。
In comparison, the wind vane of the present invention has a time constant of 7.5 seconds as described above, and vibrations quickly stop even at low wind speeds.

この風向計は、矢羽根の上部及び下部を外方に曲げであ
るので、気流が整流され、上下斜方向の気流の場合でも
、水平分力を有効に利用することができ、風向i1の性
能が向上した。更に垂直平面部の幅を、11ら部を後部
より小さクシ−(あるのぐ、Jili+圧中心が車中心
置より後退し、横風に対゛りる安定性が向上した。
In this wind vane, the upper and lower parts of the fletching blades are bent outward, so the airflow is rectified, and even in the case of vertical and oblique airflow, the horizontal force can be effectively used, and the performance in wind direction i1 is improved. improved. Furthermore, the width of the vertical plane part has been made smaller than the rear part (11), and the center of pressure is set back from the center of the vehicle, improving stability against crosswinds.

115図に、線中形風向h111の小心位置”に、この
発明の風向h1を取りイリリた他の実施例を示しCある
Figure 115 shows another embodiment of the present invention in which the wind direction h1 of the present invention is taken at the small center position of the medium wind direction h111.

以上の説明から理解されるにうに、このブト明は待バ〕
請求の範囲に記載の構成を備えているのC゛、下記のよ
うなJぐれた効果を′秦するものCある。
As can be understood from the above explanation, this Buto Ming is a waiting bar]
There are C's which are equipped with the structure described in the claims, and C's which have the following superior effects.

(1) 自己振動の継続時間が知い。(1) Know the duration of self-oscillation.

(2) 低風速11、iにも、正確に、迅速に応答りる
(2) Responds accurately and quickly even to low wind speeds 11,i.

(3) 平衡Φ錘が不要であるので1.′frijであ
る。
(3) Since no equilibrium Φ weight is required, 1. 'frij.

jメ上の結果、広い範囲の1虱速に対して、正確に且つ
迅速に出向を指示覆ることができるもの(・ある。
As a result of the above, there are some systems that can accurately and quickly change the dispatch direction for a wide range of speeds.

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

第1図、第2図及び第3図は、この発明の実施例のそれ
ぞれ、正面図、平面図及び側面図である。 第4図はこの発明の実施例の作用説明図、第5図は他の
実施例を示づ立体図である。 (図面中に表わされた主要な符号の説明)3・・・回転
軸 5・・・回転筒 7・・・矢羽根取付軸第4図 q 第5図 手続ネii正書吻へ) 昭和59年2月2z日 特許庁長官 良 賀 学 殿 3、補正をする者 乙、代理人 住 所 〒105東京都港区虎ノ門1丁目2%3号虎ノ
門第−どル5階 く発送日 昭和J7年r月2Z日) 1、 Ji’正の村も 旧[]月−ft’la I471L明==l j4紳’
J tL明−’+@−7、、nFH’正ηロブ隈 山 叶1イlll−1/71 ネ3−喧 1竿1反 、
芋鍾 及び羊7Q茫71r民的り名・す、−出1すう。 (Ikl!隈1:友動fJ L 、 ) δ 添/1専′並n目録 (1) 四嶺IJン 、71 竿■ 、羊/q 2 ?
^7夏 及び 矛γ状。
1, 2, and 3 are a front view, a top view, and a side view, respectively, of an embodiment of the present invention. FIG. 4 is an explanatory diagram of the operation of an embodiment of the present invention, and FIG. 5 is a three-dimensional diagram showing another embodiment. (Explanation of the main symbols shown in the drawings) 3...Rotating shaft 5...Rotating tube 7...Fetching shaft (Fig. 4q) Fig. 5 Procedure (ii) To the orthographic proboscis) Showa era February 2, 1959 Manabu Yoshiga, Commissioner of the Patent Office3, Person making the amendment, Agent address: 5th floor, Toranomon Doll, 1-2% 3, Toranomon, Minato-ku, Tokyo 105 Date of shipment: Showa J7 2Z day of r month) 1, Ji'sei's village is also old [] month-ft'la I471L light==l j4 gentleman'
J tL light-'+@-7,, nFH' positive η Rob Kumayama Kano 1ll-1/71 Ne3-Ken 1 rod 1 anti,
Imo zhong and sheep 7Q 茫 71r folk name, - out 1 s. (Ikl! Kuma 1: Yudo fJ L, ) δ attachment/1 special' parallel n catalog (1) Shirei IJn, 71 rod■, sheep/q 2?
^7 Summer and cylindrical shape.

Claims (1)

【特許請求の範囲】[Claims] 回転11)5に、これと直交りる2個の矢羽恨取イ]ク
ツ117を、Hに反対位置に設り、前記矢羽根取付軸7
の両端部に、矢羽根9を所定角度αで且つ、矢羽根の重
心位置において取(=Jす、前記矢羽根9の一1育tl
i及び1・部を、外力に所定角度βで折り曲げたことを
特徴とづるj虱向h1゜
Two fletching grippers 117 perpendicular to the rotation 11) 5 are provided at opposite positions to H, and the fletching attachment shaft 7
At both ends of the fletching, the fletching 9 is taken at a predetermined angle α and at the center of gravity of the fletching.
It is characterized by bending the i and 1 parts at a predetermined angle β due to external force.
JP4409184A 1984-03-09 1984-03-09 Wind direction meter Granted JPS60188854A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4409184A JPS60188854A (en) 1984-03-09 1984-03-09 Wind direction meter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4409184A JPS60188854A (en) 1984-03-09 1984-03-09 Wind direction meter

Publications (2)

Publication Number Publication Date
JPS60188854A true JPS60188854A (en) 1985-09-26
JPH032429B2 JPH032429B2 (en) 1991-01-16

Family

ID=12681947

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4409184A Granted JPS60188854A (en) 1984-03-09 1984-03-09 Wind direction meter

Country Status (1)

Country Link
JP (1) JPS60188854A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011139869A1 (en) 2010-04-29 2011-11-10 American Power Conversion Corporation Airflow detector and method of measuring airflow
US8534119B2 (en) 2010-12-30 2013-09-17 Schneider Electric It Corporation System and method for air containment zone air leakage detection
CN113658353A (en) * 2021-07-07 2021-11-16 中国人民解放军海军航空大学青岛校区 Airborne comprehensive collector

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011139869A1 (en) 2010-04-29 2011-11-10 American Power Conversion Corporation Airflow detector and method of measuring airflow
CN102322900A (en) * 2010-04-29 2012-01-18 美国能量变换公司 The method of pneumatic detector and measurement air-flow
US8407004B2 (en) 2010-04-29 2013-03-26 Schneider Electric It Corporation Airflow detector and method of measuring airflow
CN102322900B (en) * 2010-04-29 2015-03-25 美国能量变换公司 Airflow detector and method of measuring airflow
US8534119B2 (en) 2010-12-30 2013-09-17 Schneider Electric It Corporation System and method for air containment zone air leakage detection
US9274019B2 (en) 2010-12-30 2016-03-01 Schneider Electric It Corporation System and method for air containment zone air leakage detection
CN113658353A (en) * 2021-07-07 2021-11-16 中国人民解放军海军航空大学青岛校区 Airborne comprehensive collector
CN113658353B (en) * 2021-07-07 2023-05-16 中国人民解放军海军航空大学青岛校区 Airborne comprehensive collector

Also Published As

Publication number Publication date
JPH032429B2 (en) 1991-01-16

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