JPH09211015A - Differential-planetary-type double-speed sensor - Google Patents
Differential-planetary-type double-speed sensorInfo
- Publication number
- JPH09211015A JPH09211015A JP1677796A JP1677796A JPH09211015A JP H09211015 A JPH09211015 A JP H09211015A JP 1677796 A JP1677796 A JP 1677796A JP 1677796 A JP1677796 A JP 1677796A JP H09211015 A JPH09211015 A JP H09211015A
- Authority
- JP
- Japan
- Prior art keywords
- planetary gear
- differential
- output shaft
- input shaft
- differential planetary
- 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
Links
Landscapes
- Retarders (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、差動遊星型複速セ
ンサに関し、特に、差動遊星歯車部とビルトイン型の回
転検出センサを用いて全体構成をコンパクト化し、か
つ、好精度化を計るための新規な改良に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a differential planetary type double speed sensor, and more particularly, it uses a differential planetary gear unit and a built-in type rotation detecting sensor to make the entire structure compact and to improve accuracy. For new improvements for.
【0002】[0002]
【従来の技術】従来、用いられていたこの種の複速多回
転型センサとしては、一般に、1X対2nX(例えば、
1X対32X、1X対64X等)の構成が採用されてい
るが、1X側の粗センサと2nX側の精センサ間の速比
構成としては、複数の平歯車からなる減速機構が採用さ
れている。また、精、粗センサとしてはケースにビルト
イン型として設ける構成ではなく、ケースの外側に装着
する周知のサーボマウント型が採用されていた。2. Description of the Related Art Conventionally, this type of multi-speed / multi-rotation type sensor has been generally used, for example, 1X vs. 2 n X (for example,
1X pair 32X, but construction of 1X pair 64X, etc.) is employed, as the speed ratio configuration between seminal sensor coarse sensor and 2 n X side of 1X side, the speed reduction mechanism is employed comprising a plurality of spur gears ing. Further, as the fine and coarse sensors, a well-known servo mount type which is mounted on the outside of the case is adopted instead of the built-in type structure provided in the case.
【0003】[0003]
【発明が解決しようとする課題】従来の複速多回転型セ
ンサは、以上のように構成されていたため、次のような
課題が存在していた。すなわち、減速機構が複数の平歯
車からなり、その展開構成上、相当の範囲(面積)が必
要で小型化が難しく全体形状の小型化は著しく困難であ
った。また、精、粗センサはケースの外側の同一平面上
に並列に装着されていたため、ケースを小型化したとし
ても全体形状は大型化され、小型化のニーズに対応する
ことは難しかった。Since the conventional double-speed multi-rotation type sensor is constructed as described above, the following problems exist. That is, the reduction gear mechanism is composed of a plurality of spur gears, and due to its expanded configuration, a considerable range (area) is required, which makes it difficult to miniaturize and it is extremely difficult to miniaturize the entire shape. Further, since the fine and coarse sensors are mounted in parallel on the same plane outside the case, even if the case is miniaturized, the overall shape is enlarged and it is difficult to meet the needs for miniaturization.
【0004】本発明は、以上のような課題を解決するた
めになされたもので、特に、差動遊星歯車部とビルトイ
ン型の回転検出センサを用いて全体形状をコンパクト化
し、かつ、好精度化を計るようにした差動遊星型複速セ
ンサを提供することを目的とする。The present invention has been made in order to solve the above problems, and in particular, it uses a differential planetary gear unit and a built-in type rotation detection sensor to reduce the overall shape and improve accuracy. An object of the present invention is to provide a differential planetary type double speed sensor adapted to measure.
【0005】[0005]
【課題を解決するための手段】本発明による差動遊星型
複速センサは、ケースに設けられた入力軸を複数回転さ
せ減速部を介して出力軸を1回転させるようにした複速
センサにおいて、前記減速部をなす差動遊星歯車部と、
前記入力軸に同軸配置されビルトイン型の入力軸用精回
転検出センサと、前記出力軸に同軸配置されビルトイン
型の出力軸用粗回転検出センサとを備え、前記ケースの
各端部位置に前記各回転検出センサが各軸と同一軸線位
置に配設されている構成である。A differential planetary type double speed sensor according to the present invention is a double speed sensor in which an input shaft provided in a case is rotated a plurality of times and an output shaft is rotated once through a reduction unit. A differential planetary gear unit forming the reduction unit,
The input shaft includes a built-in type precise rotation detection sensor for a built-in type input shaft, and a built-in type coarse rotation detection sensor for a built-in type disposed coaxially with the output shaft, each of which is provided at each end position of the case. The rotation detection sensor is arranged at the same axial line position as each axis.
【0006】さらに詳細には、前記差動遊星歯車部は、
1個の遊星ギヤを有する構成である。More specifically, the differential planetary gear unit comprises:
This is a configuration having one planetary gear.
【0007】さらに詳細には、前記差動遊星歯車部は、
1対の遊星ギヤを有する構成である。More specifically, the differential planetary gear unit comprises:
This is a configuration having a pair of planet gears.
【0008】本発明による差動遊星型複速センサにおい
ては、入力軸と出力軸間に設けられた減速部がコンパク
トな差動遊星歯車部で構成されているため、全体機構を
従来よりも小型化することができ、かつ、入力軸用精回
転検出センサが入力軸にビルトイン型で同軸配置され、
出力軸用粗回転検出センサが出力軸にビルトイン型で同
軸配置されていることにより各センサがケースと一体状
となり、全体形状を極めて小さくかつ高精度に構成する
ことができる。In the differential planetary type double speed sensor according to the present invention, the reduction mechanism provided between the input shaft and the output shaft is composed of a compact differential planetary gear unit, so that the entire mechanism is smaller than the conventional one. And the fine rotation detection sensor for the input shaft is coaxially arranged with a built-in type on the input shaft,
Since the coarse rotation detection sensor for the output shaft is coaxially arranged on the output shaft in a built-in type, each sensor is integrated with the case, and the overall shape can be made extremely small and highly accurate.
【0009】[0009]
【発明の実施の形態】以下、図面と共に本発明による差
動遊星型複速センサの好適な実施例について詳細に説明
する。図1において符号1で示されるものは全体形状が
ほぼ箱形をなすケースであり、このケースの入力側1a
に設けられた第1軸受2には入力軸3が回転自在に設け
られ、この入力軸3の外周位置には取付ねじ4で固定さ
れたビルトイン型(ケース1の内部に一体状に設けられ
ている)の入力軸用精回転検出センサ5が入力軸3と同
軸状に設けられている。この入力軸用精回転検出センサ
5は、周知の巻線型のシンクロ又はレゾルバよりなり、
ケース1の端面の凹部1b内に配設されている。BEST MODE FOR CARRYING OUT THE INVENTION Preferred embodiments of a differential planetary type double speed sensor according to the present invention will be described in detail below with reference to the drawings. In FIG. 1, reference numeral 1 indicates a case whose overall shape is substantially box-shaped, and the input side 1a of this case is
An input shaft 3 is rotatably provided on a first bearing 2 provided at the built-in type (which is integrally provided inside the case 1 and fixed at an outer peripheral position of the input shaft 3 by a mounting screw 4). The input shaft precision rotation detection sensor 5 is provided coaxially with the input shaft 3. The fine rotation detection sensor 5 for the input shaft is composed of a well-known winding type synchronizer or resolver,
It is arranged in the recess 1 b on the end surface of the case 1.
【0010】前記ケース1の出力側1cには、1対の第
2軸受6を介して出力軸7が回転自在に設けられ、この
出力軸7は前記ケース1から外部に突出し、この出力軸
7の突出部7aの外周位置には、この出力軸7と同軸配
置の輪状をなす周知の巻線型のシンクロ又はレゾルバよ
りなる出力軸用粗回転検出センサ8が取付ねじ9によっ
てビルトイン型(ケース1の端面に一体接合)として一
体状に設けられている。An output shaft 7 is rotatably provided on the output side 1c of the case 1 through a pair of second bearings 6. The output shaft 7 projects from the case 1 to the outside, and the output shaft 7 At the outer peripheral position of the projecting portion 7a, a coarse rotation detection sensor 8 for the output shaft, which is a well-known winding type synchro or resolver that is coaxially arranged with the output shaft 7, is attached by a mounting screw 9 to a built-in type (of the case 1). It is integrally provided as an end face).
【0011】前記各回転検出センサ5,8間に配設され
た減速部としての周知の差動遊星歯車部10は、前記入
力軸3に設けられた第1回転体11と、この第1回転体
11の周縁に軸受13を介して回転自在に設けられた第
1遊星ギヤ14と、前記第1回転体11の周縁に位置し
前記第1遊星ギヤ14に対してカウンタとなるバランス
ウエイト11aと、前記出力軸7に設けられ第1遊星ギ
ヤ14と噛合する出力ギヤ15と、前記ケース1の出力
側1cに一体に形成され第1遊星ギヤ14と噛合するケ
ース側ギヤ16とから構成されている。この図1で示す
構成は、その機能のみを概略的に示すと図2及び図3で
示す通りであり、出力ギヤ15の歯数をZ=63とし、
ケース側ギヤ16の歯数をZ=64とすると、この差動
遊星歯車部10は、ギヤ比=64−63/64=1/6
4となり、精側の入力軸3を64Xとすると粗側の出力
軸7は1Xとなる。従って、1X対64Xの複速構成で
あるにも拘わらず、前記差動遊星歯車部10が従来の平
ギヤ構成よりもコンパクトで、かつ、各回転検出センサ
5,8がビルトイン型で各軸3,7と同一軸線位置でか
つ同軸配置であるため、複速センサ自体の形状が従来よ
りもコンパクト、高精度(ギヤの噛合個所が少ないた
め)、高寿命を達成することができる。A well-known differential planetary gear unit 10 as a speed reducing unit disposed between the rotation detecting sensors 5 and 8 includes a first rotating body 11 provided on the input shaft 3 and the first rotating body. A first planetary gear 14 rotatably provided on the peripheral edge of the body 11 via a bearing 13, and a balance weight 11a located on the peripheral edge of the first rotary body 11 and serving as a counter for the first planetary gear 14. , An output gear 15 provided on the output shaft 7 and meshing with the first planetary gear 14, and a case side gear 16 integrally formed on the output side 1c of the case 1 and meshing with the first planetary gear 14. There is. The configuration shown in FIG. 1 is as schematically shown in FIGS. 2 and 3 only in its function, and the number of teeth of the output gear 15 is Z = 63,
When the number of teeth of the case side gear 16 is Z = 64, the differential planetary gear unit 10 has a gear ratio of 64-63 / 64 = 1/6.
4 and the input shaft 3 on the fine side is 64X, the output shaft 7 on the rough side is 1X. Therefore, the differential planetary gear unit 10 is more compact than the conventional spur gear structure, and the rotation detection sensors 5 and 8 are built-in type shafts in spite of the 1X to 64X double speed structure. , 7 and the same axial line position and coaxial arrangement, the shape of the multi-speed sensor itself is more compact than before, high accuracy (because there are few gear meshing points), and long life can be achieved.
【0012】また、図4から図6で示す構成は図1の他
の実施例であり、図1と同一部分には同一符号を付し、
図1と異なる部分のみについて述べる。すなわち、図1
におけるバランスウエイト11aが第2遊星ギヤ14A
となり、この第2遊星ギヤ14Aに出力ギヤ15とケー
ス側ギヤ16が噛合し、図5で示すように、各ギヤ1
5,16の歯数をZ=62、Z=64とし、遊星ギヤ1
4,14Aの歯数をZ=32とすると、ギヤ比=64−
62/64=2/64=1/32となり、精側が32
X、粗側が1Xとなる。なお、この複速の比はこの比に
限られるものではなく、任意に設定できるものである。The structure shown in FIGS. 4 to 6 is another embodiment of FIG. 1, and the same parts as those in FIG.
Only the parts different from FIG. 1 will be described. That is, FIG.
Balance weight 11a in the second planetary gear 14A
Then, the output gear 15 and the case side gear 16 mesh with the second planetary gear 14A, and as shown in FIG.
The number of teeth 5 and 16 is set to Z = 62 and Z = 64, and the planetary gear 1
If the number of teeth of 4, 14A is Z = 32, gear ratio = 64−
62/64 = 2/64 = 1/32, 32 on the fine side
X, 1X on the rough side. The ratio of the multiple speeds is not limited to this ratio and can be set arbitrarily.
【0013】[0013]
【発明の効果】本発明による差動遊星型複速センサは、
以上のように構成されているため、次のような効果を得
ることができる。すなわち、入力軸及び出力軸にセンサ
としてのビルトイン型の精回転検出センサ及び粗回転検
出センサが軸に対して同軸状に設けられていると共に、
減速部がギヤ数の少ないコンパクトな差動遊星歯車部で
構成されているため、複速センサ全体形状の小型化、構
造の簡素化、高精度化(各センサが各軸に直結されてい
ることによる)を達成することができる。The differential planetary type double speed sensor according to the present invention comprises:
With the above configuration, the following effects can be obtained. That is, a built-in type fine rotation detection sensor and a coarse rotation detection sensor as sensors are provided on the input shaft and the output shaft coaxially with the shaft,
Since the reduction unit is composed of a compact differential planetary gear unit with a small number of gears, the overall shape of the compound speed sensor is downsized, the structure is simplified, and the accuracy is improved (each sensor is directly connected to each axis. Can be achieved.
【図1】本発明による差動遊星型複速センサを示す断面
図である。FIG. 1 is a sectional view showing a differential planetary type double speed sensor according to the present invention.
【図2】図1の概略機能構成図である。FIG. 2 is a schematic functional configuration diagram of FIG.
【図3】図1の概略機能構成図である。FIG. 3 is a schematic functional configuration diagram of FIG. 1.
【図4】図1の他の実施例を示す断面図である。FIG. 4 is a sectional view showing another embodiment of FIG.
【図5】図4の概略機能構成図である。5 is a schematic functional configuration diagram of FIG. 4. FIG.
【図6】図4の概略機能構成図である。FIG. 6 is a schematic functional configuration diagram of FIG. 4.
1 ケース 3 入力軸 5 入力軸用精回転検出センサ 7 出力軸 8 出力軸用粗回転検出センサ 10 差動遊星歯車部 14,14A 遊星ギヤ 1 Case 3 Input shaft 5 Precision rotation detection sensor for input shaft 7 Output shaft 8 Coarse rotation detection sensor for output shaft 10 Differential planetary gear unit 14, 14A Planetary gear
Claims (3)
回転させ減速部を介して出力軸(7)を1回転させるよう
にした複速センサにおいて、前記減速部をなす差動遊星
歯車部(10)と、前記入力軸(3)に同軸配置されビルトイ
ン型の入力軸用精回転検出センサ(5)と、前記出力軸(7)
に同軸配置されビルトイン型の出力軸用粗回転検出セン
サ(8)と、を備え、前記ケース(1)の各端部位置に前記各
回転検出センサ(5,8)が前記各軸(3,7)と同一軸線位置に
配設されていることを特徴とする差動遊星型複速セン
サ。1. A multi-speed sensor in which a plurality of input shafts (3) provided on a case (1) are rotated a plurality of times to rotate an output shaft (7) once through a speed reducing unit, and a difference between the speed reducing units is formed. A moving planetary gear unit (10), a built-in type fine rotation detection sensor for input shaft (5) coaxially arranged on the input shaft (3), and the output shaft (7)
A coarse rotation detection sensor for built-in type output shaft coaxially arranged (8), and each rotation detection sensor (5, 8) at each end position of the case (1) each shaft (3, A differential planetary type double speed sensor, which is arranged at the same axial position as 7).
ギヤ(14)を有することを特徴とする請求項1記載の差動
遊星型複速センサ。2. The differential planetary type double speed sensor according to claim 1, wherein the differential planetary gear unit (10) has one planetary gear (14).
ギヤ(14,14A)を有することを特徴とする請求項1記載の
差動遊星型複速センサ。3. The differential planetary type double speed sensor according to claim 1, wherein the differential planetary gear unit (10) has a pair of planetary gears (14, 14A).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP01677796A JP4046297B2 (en) | 1996-02-01 | 1996-02-01 | Differential planetary double speed sensor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP01677796A JP4046297B2 (en) | 1996-02-01 | 1996-02-01 | Differential planetary double speed sensor |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH09211015A true JPH09211015A (en) | 1997-08-15 |
JP4046297B2 JP4046297B2 (en) | 2008-02-13 |
Family
ID=11925637
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP01677796A Expired - Fee Related JP4046297B2 (en) | 1996-02-01 | 1996-02-01 | Differential planetary double speed sensor |
Country Status (1)
Country | Link |
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JP (1) | JP4046297B2 (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002250408A (en) * | 2001-02-23 | 2002-09-06 | Asmo Co Ltd | Motor actuator |
US20110230305A1 (en) * | 2010-03-18 | 2011-09-22 | Ricoh Company, Limited | Driving device and image forming apparatus |
US8068766B2 (en) * | 2007-07-12 | 2011-11-29 | Ricoh Company, Ltd. | Rotary drive device and image forming apparatus |
WO2014002144A1 (en) * | 2012-06-29 | 2014-01-03 | 株式会社ハーモニック・ドライブ・システムズ | Planetary differential speed reducer |
WO2017216897A1 (en) * | 2016-06-15 | 2017-12-21 | 三菱重工コンプレッサ株式会社 | Variable speed accelerator |
US10663039B2 (en) | 2016-06-15 | 2020-05-26 | Mitsubishi Heavy Industries Compressor Corporation | Variable speed accelerator and method for controlling variable speed accelerator |
US10738858B2 (en) | 2016-07-20 | 2020-08-11 | Mitsubishi Heavy Industries Compressor Corporation | Variable-speed speed increaser, variable-speed speed increaser control device, and variable-speed speed increaser control method |
-
1996
- 1996-02-01 JP JP01677796A patent/JP4046297B2/en not_active Expired - Fee Related
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002250408A (en) * | 2001-02-23 | 2002-09-06 | Asmo Co Ltd | Motor actuator |
US8068766B2 (en) * | 2007-07-12 | 2011-11-29 | Ricoh Company, Ltd. | Rotary drive device and image forming apparatus |
US20110230305A1 (en) * | 2010-03-18 | 2011-09-22 | Ricoh Company, Limited | Driving device and image forming apparatus |
US8585537B2 (en) * | 2010-03-18 | 2013-11-19 | Ricoh Company, Limited | Driving device and image forming apparatus |
US8864617B2 (en) | 2012-06-29 | 2014-10-21 | Harmonic Drive Systems, Inc. | Planetary differential reduction device |
JP5450889B1 (en) * | 2012-06-29 | 2014-03-26 | 株式会社ハーモニック・ドライブ・システムズ | Planetary differential reducer |
WO2014002144A1 (en) * | 2012-06-29 | 2014-01-03 | 株式会社ハーモニック・ドライブ・システムズ | Planetary differential speed reducer |
TWI565891B (en) * | 2012-06-29 | 2017-01-11 | Harmonic Drive Systems | Planetary differential deceleration device |
WO2017216897A1 (en) * | 2016-06-15 | 2017-12-21 | 三菱重工コンプレッサ株式会社 | Variable speed accelerator |
JPWO2017216897A1 (en) * | 2016-06-15 | 2019-03-07 | 三菱重工コンプレッサ株式会社 | Variable speed gearbox |
US10663039B2 (en) | 2016-06-15 | 2020-05-26 | Mitsubishi Heavy Industries Compressor Corporation | Variable speed accelerator and method for controlling variable speed accelerator |
US11025180B2 (en) | 2016-06-15 | 2021-06-01 | Mitsubishi Heavy Industries Compressor Corporation | Variable speed accelerator |
US10738858B2 (en) | 2016-07-20 | 2020-08-11 | Mitsubishi Heavy Industries Compressor Corporation | Variable-speed speed increaser, variable-speed speed increaser control device, and variable-speed speed increaser control method |
Also Published As
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