Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS6411840B2 - - Google Patents
[go: Go Back, main page]

JPS6411840B2 - - Google Patents

Info

Publication number
JPS6411840B2
JPS6411840B2 JP2787485A JP2787485A JPS6411840B2 JP S6411840 B2 JPS6411840 B2 JP S6411840B2 JP 2787485 A JP2787485 A JP 2787485A JP 2787485 A JP2787485 A JP 2787485A JP S6411840 B2 JPS6411840 B2 JP S6411840B2
Authority
JP
Japan
Prior art keywords
propeller
mirror
fan motor
finished
motor
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
Application number
JP2787485A
Other languages
Japanese (ja)
Other versions
JPS61187598A (en
Inventor
Kazuo Okazaki
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.)
Nidec Copal Electronics Corp
Original Assignee
Copal Electronics Co 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 Copal Electronics Co Ltd filed Critical Copal Electronics Co Ltd
Priority to JP2787485A priority Critical patent/JPS61187598A/en
Publication of JPS61187598A publication Critical patent/JPS61187598A/en
Publication of JPS6411840B2 publication Critical patent/JPS6411840B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Description

【発明の詳細な説明】 (発明の利用分野) この発明はフアンモータのプロペラに関する。[Detailed description of the invention] (Field of application of the invention) This invention relates to a propeller for a fan motor.

(従来技術) 従来よりプロペラ付フアンモータの回転検出を
行う場合は、近接して設けた光源例えばストロボ
光センサを回転中のプロペラに反射させて実施す
るのが普通であり、光源よりの光線反射用とし
て、マーク若しくはシール等をプロペラの対向上
面に貼着していた。
(Prior art) Conventionally, when detecting the rotation of a fan motor with a propeller, it has been common to use a nearby light source, such as a strobe light sensor, to reflect the light from the rotating propeller. For this purpose, marks or stickers were pasted on the upper surface of the propeller.

又モータのダイナミツクバランスを測定又は修
正を実施する際はプロペラ及びプロペラアセンブ
リ状態で行つていた。
Furthermore, when measuring or correcting the dynamic balance of a motor, the propeller and propeller assembly are used.

(発明の解決しようとする問題点) 回転検出の際、光源反射用としてマーク若しく
はシールを貼着する作業は煩鎖であり又プロペラ
のアセリブリ状態でダイナミツクバランスを測定
しても、最終完成品としてはバランスの狂いが生
じる等の問題点があつた。
(Problems to be Solved by the Invention) When detecting rotation, the work of pasting marks or stickers to reflect the light source is cumbersome, and even if the dynamic balance is measured with the propeller assembled, the final finished product will not work properly. However, there were problems such as imbalance.

(問題解決のための手段) そこで本発明においては、光源反射による回転
検出用マークを金型等を用いてプロペラ自体の面
に一体に仕上げると共にプロペラの内側に、回転
検出用マークを基準として同一ピツチの角度表示
を設け、前記角度表示を用いて、モータの組立完
了後アンバランス位置の修正を容易となした。
(Means for Solving the Problem) Therefore, in the present invention, a rotation detection mark based on light source reflection is finished integrally on the surface of the propeller itself using a mold, etc., and an identical mark is placed on the inside of the propeller using the rotation detection mark as a reference. A pitch angle display is provided, and by using the angle display, the unbalanced position can be easily corrected after the motor is assembled.

(作用) 従つて回転検出用マークを別に貼着することを
不要とし、光源反射による回転検出を容易に実施
でき、同一ピツチの角度表示を用いてプロペラ及
びプロペラアセンブリのダイナミツクバランスの
修正を、モータとして組立完了後に実施できる。
(Function) Therefore, it is not necessary to separately attach a rotation detection mark, rotation can be easily detected by light source reflection, and the dynamic balance of the propeller and propeller assembly can be corrected using the same pitch angle display. This can be done after the motor is assembled.

(実施例) 第1図において、円筒状ボデイ4の外周に羽根
6を装着したプロペラ2の前面板8の一部分10
を、成形金型等を用いて鏡面仕上げとし、その他
の前面板に梨子地仕上げ12を施す。14は前面
板8より後方に突出した回転軸である。尚プロペ
ラ2は通常合成樹脂等よりなる。前記円筒状ボデ
イ4の内側面には、鏡面仕上げ部10を基準とし
て等間隔に角度表線16を施す。従つて、回転検
出の際、光線は鏡面仕上げ部10に反射するが、
梨子地仕上げ部12には反射しない。第2図はモ
ータ回転検出の一例を図示する。プロペラ2は回
転軸14の駆動により回転すると、プロペラ2の
前面板8に近接して設けた光源例えば反射式光セ
ンサ18のビームが前面板8の鏡面仕上げ部10
に反射し、パルスを発生する。発生したパルス波
20は第3図に図示のように、プロペラ1回転毎
に1回順次等間隔に発生するものである。
(Embodiment) In FIG. 1, a portion 10 of a front plate 8 of a propeller 2 having blades 6 attached to the outer periphery of a cylindrical body 4 is shown.
is given a mirror finish using a mold or the like, and the other front plate is given a pear finish 12. Reference numeral 14 denotes a rotating shaft that projects rearward from the front plate 8. The propeller 2 is usually made of synthetic resin or the like. Angular table lines 16 are formed on the inner surface of the cylindrical body 4 at equal intervals with respect to the mirror finished portion 10. Therefore, when detecting rotation, the light beam is reflected by the mirror-finished portion 10, but
It is not reflected on the satin finish portion 12. FIG. 2 illustrates an example of motor rotation detection. When the propeller 2 is rotated by the rotation shaft 14, a beam from a light source, for example, a reflective optical sensor 18 provided close to the front plate 8 of the propeller 2 is emitted onto the mirror-finished portion 10 of the front plate 8.
It reflects and generates a pulse. As shown in FIG. 3, the generated pulse waves 20 are generated once every rotation of the propeller at equal intervals.

次にプロペラ2を組付けたフアンモータ22の
回転中における振動の振巾を測定するために、第
4図に図示のように振動ピツクアツプ24を使用
する。振動ピツクアツプ24により測定した出力
波形26は第5図に図示のようである。この波形
の発生する要因はプロペラ組立時のアンバランス
に起因すると考えられている。
Next, in order to measure the amplitude of vibration during rotation of the fan motor 22 to which the propeller 2 is attached, a vibration pickup 24 is used as shown in FIG. The output waveform 26 measured by the vibration pickup 24 is as shown in FIG. The cause of this waveform is thought to be due to imbalance during propeller assembly.

そこで第3図に図示のパルス波形20を画面上
で六分割調整すると、1分割が60゜となる。これ
を振動波形26と同期させると第6図に図示のよ
うな合成波形が得られる。第6図において、振動
波形26のピーク位置すなわちモータのアンバラ
ンス位置をAとし、パルス波基準設定位置すなわ
ち鏡面仕上げ部12の位置をBとする。今、Aと
Bとの差を画面上で読んだとき1/2分割であると
すれば、前記モータのアンバランス位置とプロペ
ラ鏡面仕上げ部との角度差が30゜となる。勿論第
6図に図示した合成波形は、説明のための一例に
すぎない。各種の事情に応じ、アンバランス位置
が鏡面仕上げ部10より様々な角度の位置に存在
することは勿論である。
Therefore, when the pulse waveform 20 shown in FIG. 3 is adjusted on the screen into six divisions, one division becomes 60 degrees. When this is synchronized with the vibration waveform 26, a composite waveform as shown in FIG. 6 is obtained. In FIG. 6, A is the peak position of the vibration waveform 26, that is, the unbalanced position of the motor, and B is the pulse wave reference setting position, that is, the position of the mirror finish portion 12. Now, if the difference between A and B is read on the screen and is divided into 1/2, the angular difference between the unbalanced position of the motor and the mirror-finished part of the propeller is 30 degrees. Of course, the composite waveform illustrated in FIG. 6 is merely an example for explanation. It goes without saying that the unbalanced position exists at various angles from the mirror finished portion 10 depending on various circumstances.

上述の説明のように、モータのアンバランス位
置の角度差が判明すると、既に説明したボデイ4
の内側に鏡面仕上げ部10を基準として等間隔に
配列した角度表示線16を用いて、前記アンバラ
ンスの鏡面仕上げ部10よりの位置を確認し、ア
ンバランスの修正作業を行うことができる。その
方法としては、(イ)、アンバランスの小さい場合に
はプロペラのその位置(角度差位置)に垂錘等を
付加して修正するか、(ロ)、反対にアンバランスの
大きい場合には、所定角度表示線の角度差に該当
するプロペラの部分を切削等により質量を除去す
ることにより行う。
As explained above, when the angular difference in the unbalanced position of the motor is determined, the body 4
Using the angle display lines 16 arranged at equal intervals on the inside of the mirror-finished part 10, the unbalanced position relative to the mirror-finished part 10 can be confirmed, and the unbalance can be corrected. The methods are (a) if the unbalance is small, correct it by adding a plumb or the like to that position of the propeller (angular difference position); or (b) if the unbalance is large, correct it. , by removing the mass of the portion of the propeller corresponding to the angle difference between the predetermined angle display lines by cutting or the like.

(効果) 本発明においては、プロペラボデイの前面板に
光線反射用鏡面仕上げ部を設けて、シール等の別
の反射部材の貼着を不要とし、更にプロペラボデ
イ内側面に鏡面仕上げ部を基準として等間隔の角
度表示線を配設し、光線反射によるパルス波と振
動による振動波との画面上の角度差によりモータ
のアンバランス位置を実際に角度表示線上に割り
出すことにより、プロペラ組付完了後のモータの
アンバランス修正を容易とする。
(Effects) In the present invention, a mirror-finished part for reflecting light is provided on the front plate of the propeller body, making it unnecessary to attach another reflective member such as a sticker, and furthermore, the mirror-finished part on the inner surface of the propeller body is used as a reference. By arranging angle display lines at equal intervals and actually determining the unbalanced position of the motor on the angle display lines based on the angle difference on the screen between the pulse wave caused by light reflection and the vibration wave caused by vibration, it is possible to easily determine the unbalanced position of the motor on the angle display line after propeller assembly is completed. This makes it easy to correct motor imbalance.

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

第1図aは本発明に係るプロペラの前面より見
た斜視図。同bは後面より見た斜視図。第2図は
光センサを配設した側面略線図。第3図は光反射
によるパルスの略線図。第4図は振動波形を示す
図。第5図は振動ピツクアツプを装着したフアン
モータの一部断面図。第6図はパルス波と振動波
との角度差を示す合成波形図。 2……プロペラ、4……ボデイ、8……前面
板、10……鏡面仕上げ部、12……梨子地仕上
げ部、16……角度表示線、18……光センサ、
20……パルス波、22……フアンモータ、26
……振動波形。
FIG. 1a is a perspective view of a propeller according to the present invention, seen from the front. Figure b is a perspective view seen from the rear. FIG. 2 is a schematic side view of the arrangement of optical sensors. FIG. 3 is a schematic diagram of pulses due to light reflection. FIG. 4 is a diagram showing vibration waveforms. Figure 5 is a partial sectional view of a fan motor equipped with a vibrating pickup. FIG. 6 is a composite waveform diagram showing the angular difference between a pulse wave and a vibration wave. 2...Propeller, 4...Body, 8...Front plate, 10...Mirror finish section, 12...Pearl finish section, 16...Angle display line, 18...Photo sensor,
20...Pulse wave, 22...Fan motor, 26
...Vibration waveform.

Claims (1)

【特許請求の範囲】 1 プロペラ前面部のビームに反射する部分を鏡
面仕上げ部に、その他は反射しない部分に形成
し、ボデイ内側に鏡面仕上げ部を基準とした同一
間隔の角度表示を設けたことを特徴とするフアン
モータのプロペラ。 2 合成樹脂よりなるプロペラを有する特許請求
の範囲第1項に記載のフアンモータのプロペラ。 3 パルス波と振動波との角度差にもとづきモー
タのアンバランス位置を確認することを可能とす
る角度表示を具えた特許請求の範囲第1項に記載
のフアンモータのプロペラ。 4 鏡面仕上げ部以外を梨子地仕上げとなした前
面部を有する特許請求の範囲第1項に記載のフア
ンモータのプロペラ。
[Claims] 1. The part of the front surface of the propeller that reflects the beam is formed into a mirror-finished part, and the other part is formed into a non-reflective part, and angle indicators are provided at the same intervals on the inside of the body with reference to the mirror-finished part. A fan motor propeller featuring: 2. A propeller for a fan motor according to claim 1, which has a propeller made of synthetic resin. 3. A propeller for a fan motor according to claim 1, which is provided with an angle display that makes it possible to confirm an unbalanced position of the motor based on the angular difference between the pulse wave and the vibration wave. 4. A propeller for a fan motor according to claim 1, which has a front portion having a satin finish except for the mirror finished portion.
JP2787485A 1985-02-15 1985-02-15 Propeller of fan motor Granted JPS61187598A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2787485A JPS61187598A (en) 1985-02-15 1985-02-15 Propeller of fan motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2787485A JPS61187598A (en) 1985-02-15 1985-02-15 Propeller of fan motor

Publications (2)

Publication Number Publication Date
JPS61187598A JPS61187598A (en) 1986-08-21
JPS6411840B2 true JPS6411840B2 (en) 1989-02-27

Family

ID=12233040

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2787485A Granted JPS61187598A (en) 1985-02-15 1985-02-15 Propeller of fan motor

Country Status (1)

Country Link
JP (1) JPS61187598A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4629197B2 (en) * 2000-07-28 2011-02-09 株式会社岡村製作所 Cushion body retractor and cushion body support structure
JP5182554B2 (en) * 2007-12-26 2013-04-17 日本電産株式会社 Fan motor and rotational speed measurement method
JP7318566B2 (en) * 2019-05-23 2023-08-01 株式会社デンソー Fan Device Manufacturing Apparatus and Fan Device Manufacturing Method
WO2026063265A1 (en) * 2024-09-18 2026-03-26 パナソニックIpマネジメント株式会社 Fan rotational balance adjustment method, and fan

Also Published As

Publication number Publication date
JPS61187598A (en) 1986-08-21

Similar Documents

Publication Publication Date Title
CA1120590A (en) Apparatus for measuring contour configuration of articles
CA1119055A (en) Indicator gauge with illuminated pointer
JPS6239890B2 (en)
JPS6388409A (en) Laser vibrometer
JPS6411840B2 (en)
JP3531290B2 (en) Blade shape measurement device
SU1442824A1 (en) Method of checking photoelectric autocollimators
JPH0120641Y2 (en)
SU646199A1 (en) Method of measuring oscillation of turbo-compressor hinged blades
JPH0247449Y2 (en)
JPS59135304A (en) Method for measuring the position of a moving object using a light beam
JPS57179628A (en) Torsional vibration measuring apparatus for rotating shaft
JPH045142B2 (en)
JPH01174908A (en) How to measure the torsion angle of a rotating shaft
SU1280336A1 (en) Compensation vibration meter
JPH03255927A (en) Deformation measuring method for polygon mirror
JPS6017431U (en) shaft horsepower meter
JPH0338647Y2 (en)
JPS62255807A (en) Measuring instrument for thickness of film
RU93008987A (en) METHOD FOR DETERMINING THE DISCONTANCE ANGLE POINT WITHIN THE BALANCING
SU43189A1 (en) Mirror tool for checking the indicator "Pioneer"
JPH0213953Y2 (en)
RU1584539C (en) Measuring unit for balancing machine
JPH0419455Y2 (en)
JPS60111906A (en) Angle measuring method