JP2007225017A - Planetary reduction gear lubricating structure - Google Patents

Planetary reduction gear lubricating structure Download PDF

Info

Publication number
JP2007225017A
JP2007225017A JP2006046586A JP2006046586A JP2007225017A JP 2007225017 A JP2007225017 A JP 2007225017A JP 2006046586 A JP2006046586 A JP 2006046586A JP 2006046586 A JP2006046586 A JP 2006046586A JP 2007225017 A JP2007225017 A JP 2007225017A
Authority
JP
Japan
Prior art keywords
planetary
wheel
shielding plate
grease
reduction gear
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
JP2006046586A
Other languages
Japanese (ja)
Other versions
JP4889318B2 (en
Inventor
Takashi Yamamura
剛史 山村
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 Drive Technology Corp
Original Assignee
Nidec Shimpo Corp
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 Nidec Shimpo Corp filed Critical Nidec Shimpo Corp
Priority to JP2006046586A priority Critical patent/JP4889318B2/en
Publication of JP2007225017A publication Critical patent/JP2007225017A/en
Application granted granted Critical
Publication of JP4889318B2 publication Critical patent/JP4889318B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/04Features relating to lubrication or cooling or heating
    • F16H57/0463Grease lubrication; Drop-feed lubrication
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/04Features relating to lubrication or cooling or heating
    • F16H57/048Type of gearings to be lubricated, cooled or heated
    • F16H57/0482Gearings with gears having orbital motion

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Friction Gearing (AREA)
  • General Details Of Gearings (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a lubricating structure for a planetary reduction gear, capable of circulating grease to a power transmission part to be lubricated without splashing therearound in company with the turn of the power transmission part. <P>SOLUTION: Grease is filled in abutting portions P1, P2, P3 among a sun gear 3, a planetary gear 4, and inner rings 5a, 5b for reducing mutual wear to actualize smooth frictional transmission. A pair of shielding plates 6a, 23 are provided on both axial sides via the abutting portions P1, P2, P3 for covering the abutting portions P1, P2, P3 via gaps. To the other shielding plate 23, a blade portion is attached so that the grease flows toward one shielding plate 6a with the turn. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

本発明は、遊星減速機において、回転部材同士の摩擦伝動部や歯車噛合部などの動力伝達機構を潤滑するための潤滑構造に関する。   The present invention relates to a lubrication structure for lubricating a power transmission mechanism such as a friction transmission portion and a gear meshing portion between rotating members in a planetary reduction gear.

従来、ケーシング内に、駆動源の駆動力を受けて回動する太陽車と、太陽車に空隙を介して同軸状に配置された内リングと、この間隙に配設され太陽車及び内リングに当接する遊星車と、遊星車を回動自在に支持すると共に太陽車と同軸状に回動するキャリアとを備え、太陽車の回動に伴って、太陽車を中心に遊星車を公転させ、この公転運動をキャリアに伝達する遊星減速機が知られている。   Conventionally, a solar wheel that rotates in response to a driving force of a drive source in a casing, an inner ring that is coaxially disposed in the solar wheel via a gap, and a solar wheel and an inner ring that are disposed in the gap. A planetary wheel that abuts, and a carrier that rotatably supports the planetary vehicle and that rotates coaxially with the solar vehicle, and revolves the planetary vehicle around the solar vehicle as the solar vehicle rotates, A planetary speed reducer that transmits this revolution motion to a carrier is known.

また、この遊星減速機では、一般に、太陽車、遊星車、内リングの当接部には、互いのの磨耗を低減し円滑な摩擦伝動を行うためにグリースが充填されている(例えば、特許文献1参照)。
特開2002−78290号公報
In this planetary reduction gear, generally, the contact portions of the sun wheel, the planetary wheel, and the inner ring are filled with grease in order to reduce mutual wear and perform smooth friction transmission (for example, patents) Reference 1).
JP 2002-78290 A

そして、従来の遊星減速機は、摩擦伝動部の周囲にはグリースの飛散を防止するための有効な手段が備えられていないので、太陽車及び遊星車の回動に伴って、グリースが摩擦伝動部の外方に飛散し、飛散した潤滑グリースが摩擦伝動部に循環することができず、動力伝達を損なう虞があった。さらには、グリースの飛散分を補うために、グリースを余分に必要とし、生産性を損なう虞もあった。   Since the conventional planetary speed reducer is not provided with an effective means for preventing the scattering of grease around the friction transmission portion, the grease is frictionally transmitted along with the rotation of the solar wheel and the planetary wheel. As a result, the scattered lubricating grease cannot be circulated to the friction transmission portion, and power transmission may be impaired. Furthermore, in order to compensate for the scattering of grease, extra grease is required, which may impair productivity.

そこで、本発明は、遊星減速機において、動力伝達部を潤滑するグリースが、動力伝達機構の回動に伴って周囲に飛散することなく、動力伝達部に循環し得る潤滑構造を提供することを目的とする。   Therefore, the present invention provides a lubrication structure in a planetary reducer that allows grease that lubricates the power transmission unit to circulate to the power transmission unit without being scattered around as the power transmission mechanism rotates. Objective.

かかる目的を達成するためになされた請求項1に記載の発明は、ケーシング内に、駆動源の駆動力を受けて回動する太陽車と、前記太陽車に間隙を介して同軸状に配置された内リングと、前記間隙内に配設され前記太陽車及び前記内リングに当接する遊星車と、前記太陽車と同軸線上に回動自在に配設され、前記遊星車を回動自在に支持するキャリアとを備え、前記太陽車、前記遊星車、前記内リングの当接部には、互いの磨耗を低減し円滑な摩擦伝動を行うためのグリースが充填された遊星減速機の潤滑構造において、前記当接部を介して軸方向の両側に、該当接部を間隙を介して覆う遮蔽板が一対備えられていることを特徴とする。   The invention according to claim 1, which has been made to achieve such an object, is arranged in a casing in a coaxial manner with a sun wheel rotating by receiving a driving force of a driving source, and a space between the sun wheel and a gap. An inner ring, a planetary wheel disposed in the gap and in contact with the sun wheel and the inner ring, and rotatably disposed on a coaxial line with the sun wheel, and rotatably supporting the planetary wheel. A planetary speed reducer lubrication structure in which the abutting portions of the sun wheel, the planetary wheel, and the inner ring are filled with grease for reducing mutual wear and performing smooth friction transmission. A pair of shielding plates are provided on both sides in the axial direction via the abutting portion so as to cover the corresponding contact portion through a gap.

請求項1に記載の遊星減速機の潤滑構造によれば、太陽車、遊星車、内リングの当接部を介して軸方向の両側に、この当接部を間隙を介して覆う遮蔽板が備えられているので、グリースが当接部の遠方に飛散することなく、間隙に沿って循環して当接部の潤滑を良好に維持できる。   According to the lubricating structure of the planetary reduction gear according to claim 1, the shielding plates that cover the abutting portions via the gaps on both sides in the axial direction via the abutting portions of the solar wheel, the planetary wheel, and the inner ring. Since the grease is provided, the grease circulates along the gap without being scattered far away from the contact portion, and the lubrication of the contact portion can be maintained well.

次に、請求項2に記載の発明は、請求項1に記載の遊星減速機の潤滑構造において、前記一対の遮蔽板の内、一方の遮蔽板が前記キャリアと一体に備えられ、他方の遮蔽板が前記太陽車と一体に備えられていることを特徴とする。   Next, according to a second aspect of the present invention, in the planetary speed reducer lubricating structure according to the first aspect, one of the pair of shielding plates is integrally provided with the carrier, and the other shielding member is provided. A plate is provided integrally with the solar wheel.

請求項2に記載の遊星減速機の潤滑構造によれば、一方の遮蔽板がキャリアと一体に備えられ、他方の遮蔽板が太陽車と一体に備えられているので、遊星車の公転と一体になって一方の遮蔽板が回転すると共に、太陽車の回転と共に他方の遮蔽板が回転し、一方の遮蔽板と他方の遮蔽板との間におけるグリースの循環を促進させることができる。また、請求項2に記載の遊星減速機の潤滑構造によれば、軸方向において、一方の遮蔽板及び他方の遮蔽板の位置決めと支持とを容易にできて、生産性を向上できる。   According to the lubricating structure of the planetary reduction gear according to claim 2, since one shielding plate is provided integrally with the carrier and the other shielding plate is provided integrally with the sun wheel, the planetary vehicle revolution is integrated. Thus, one shield plate rotates, and the other shield plate rotates with the rotation of the sun wheel, thereby facilitating the circulation of grease between the one shield plate and the other shield plate. In addition, according to the lubricating structure of the planetary reduction gear according to the second aspect, the positioning and supporting of the one shielding plate and the other shielding plate can be easily performed in the axial direction, and the productivity can be improved.

次に、請求項3に記載の発明は、請求項1又は請求項2に記載の遊星減速機の潤滑構造において、前記他方の遮蔽板には、回動に伴って前記グリースを前記一方の遮蔽板に向けて流動させる羽部が付設されていることを特徴とする。   Next, according to a third aspect of the present invention, there is provided the lubricating structure for a planetary reduction gear according to the first or second aspect, wherein the grease is applied to the other shielding plate as the other shielding plate rotates. It is characterized by a wing part that flows toward the plate.

請求項3に記載の遊星減速機の潤滑構造によれば、他方の遮蔽板には、回動に伴ってグリースを一方の遮蔽板に向けて流動させる羽部が付設されているので、他方の遮蔽板と一方の遮蔽板との間におけるグリースの循環性を向上させることができる。また、この際、羽部が駆動源側に位置する他方の遮蔽板に付設されているので、グリースが駆動源側に流出することがないように抑制できる。   According to the lubricating structure of the planetary reduction gear according to claim 3, the other shielding plate is provided with the wing portion that causes the grease to flow toward the one shielding plate as the other shielding plate is moved. The circulation property of the grease between the shielding plate and one of the shielding plates can be improved. Further, at this time, since the wing portion is attached to the other shielding plate located on the drive source side, it is possible to prevent the grease from flowing out to the drive source side.

本発明の遊星減速機の潤滑構造は、太陽車、遊星車、内リングの当接部を介して軸方向の両側に、この当接部を間隙を介して覆う遮蔽板が備えられているので、グリースが当接部の遠方に飛散することなく、間隙に沿って循環して当接部の潤滑を良好に維持できる。   The planetary reduction gear lubrication structure of the present invention is provided with shielding plates that cover the abutting portions with gaps on both sides in the axial direction via the abutting portions of the sun wheel, the planetary wheel, and the inner ring. The grease circulates along the gap without being scattered far away from the contact portion, and the lubrication of the contact portion can be maintained well.

また、本発明の遊星減速機の潤滑構造は、一方の遮蔽板がキャリアと一体に備えられ、他方の遮蔽板が太陽車と一体に備えられているので、遊星車の公転と一体になって一方の遮蔽板が回転すると共に、他方の遮蔽板が太陽車と一体に回転し、一方の遮蔽板と他方の遮蔽板との間におけるグリースの循環を促進させることができる。また、本発明の遊星減速機の潤滑構造は、軸方向において、一方の遮蔽板及び他方の遮蔽板の位置決めと支持とを容易にできて、生産性を向上できる。   Also, the lubricating structure of the planetary speed reducer according to the present invention has one shielding plate integrated with the carrier and the other shielding plate integrated with the sun wheel, so that it is integrated with the revolution of the planetary vehicle. While one shielding plate rotates, the other shielding plate rotates integrally with the solar wheel, and the circulation of grease between one shielding plate and the other shielding plate can be promoted. Further, the lubricating structure of the planetary reduction gear according to the present invention can easily position and support the one shielding plate and the other shielding plate in the axial direction, thereby improving productivity.

また、本発明の遊星減速機の潤滑構造は、他方の遮蔽板には、回動に伴ってグリースを一方の遮蔽板に向けて流動させる羽部が付設されているので、他方の遮蔽板と一方の遮蔽板との間におけるグリースの循環性を向上させることができる。また、羽部が駆動源側に位置する他方の遮蔽板に付設されているので、グリースが駆動源側に流出することがないように抑制できる。   Further, in the planetary reduction gear lubrication structure of the present invention, the other shielding plate is provided with a wing portion that causes grease to flow toward one shielding plate as the other shielding plate moves. It is possible to improve the circulation of grease between the one shielding plate. Moreover, since the wing part is attached to the other shielding plate located on the drive source side, it is possible to prevent the grease from flowing out to the drive source side.

次に、本発明の一実施例の遊星減速機の潤滑構造を、図面にもとづいて説明する。図1は、本発明の遊星減速機の潤滑構造が適用された遊星減速機の構成を表す断面図、図2は、図1における他方の遮蔽板の構成を表す外観図であって、(a)図が軸方向から視た正面図、(b)図が(a)図におけるBーB断面図、図Cが(a)図におけるC方向から視た平面図である。   Next, a lubricating structure for a planetary reduction gear according to an embodiment of the present invention will be described with reference to the drawings. FIG. 1 is a cross-sectional view showing a configuration of a planetary speed reducer to which a lubricating structure of a planetary speed reducer according to the present invention is applied, and FIG. 2 is an external view showing the configuration of the other shielding plate in FIG. ) Is a front view as viewed from the axial direction, (b) is a cross-sectional view taken along the line BB in FIG. (A), and FIG. C is a plan view as viewed from the C direction in FIG.

図1に表したように、遊星減速機1は、ケーシング21、22内に、駆動モータ(所謂、本発明における駆動源である。)2の駆動力を受けて回動する太陽車3、太陽車3に空隙を介して同軸状に配置された内リング5a、5b、前記間隙内に配設され太陽車3及び内リング5a、5bに当接する遊星車4、太陽車3と同軸線上(図1におけるX−X線上)に配設されて遊星車4を回動自在に支持するキャリア6、キャリア6と一体に回動する出力軸27等を備え、太陽車3、遊星車4、内リング5a、5b等の当接部P1、P2、P3の周囲には、当接部P1、P2、P3の摩擦伝動を潤滑するためのグリースが充填されている。   As shown in FIG. 1, the planetary speed reducer 1 includes a solar wheel 3 that rotates in response to a driving force of a driving motor 2 (so-called driving source in the present invention) 2 in casings 21 and 22. Inner rings 5a and 5b arranged coaxially in the vehicle 3 via a gap, the planetary wheel 4 disposed in the gap and contacting the solar wheel 3 and the inner rings 5a and 5b, on the same axis as the solar wheel 3 (see FIG. 1 on the line XX in FIG. 1, and includes a carrier 6 that rotatably supports the planetary wheel 4, an output shaft 27 that rotates together with the carrier 6, and the like, and includes the solar wheel 3, the planetary wheel 4, and the inner ring. Greases for lubricating the frictional transmission of the contact portions P1, P2, and P3 are filled around the contact portions P1, P2, and P3 such as 5a and 5b.

また、遊星減速機1は、駆動モータ2がブラケット2a及びボルト25を介してケーシング21に固定され、リング5aとブラケット2aとの間に、リング5aの回転を係止する係止リング7と、リング5aをリング5b側に付勢するコイルスプリング11とを備えている。   The planetary speed reducer 1 includes a locking ring 7 in which the drive motor 2 is fixed to the casing 21 via a bracket 2a and a bolt 25, and the rotation of the ring 5a is locked between the ring 5a and the bracket 2a. And a coil spring 11 that urges the ring 5a toward the ring 5b.

出力軸27は、駆動モータ2側に位置する一端がキャリア6に圧入されて固定されると共にベアリング18を介してケーシング21に回動自在に支持され、他端がベアリング19を介してケーシング22に回動自在に支持されている。また、ベアリング19は、一端側において、出力軸27に係合した止め輪20に内輪が当接し、他端側において、軸方向に弾性を有するウェーブワッシャ13に外輪が当接し、軸方向に支持されている。   One end of the output shaft 27 located on the drive motor 2 side is press-fitted and fixed to the carrier 6 and is rotatably supported on the casing 21 via the bearing 18, and the other end is attached to the casing 22 via the bearing 19. It is supported rotatably. The bearing 19 has an inner ring abutting against a retaining ring 20 engaged with the output shaft 27 at one end side, and an outer ring abutting against a wave washer 13 having elasticity in the axial direction at the other end side. Has been.

内リング5a、5bは、遊星車4を挟むように対向して設けられ、それぞれ係止リング7に備えられた突起部7a、ケーシング21に備えられた突起部21aに係合して、ケーシング21に対して回転不能に装着されいる。また。内リング5aは、軸方向にスライド自在に装着され、コイルスプリング11により、内リング5bに向かって付勢されている。   The inner rings 5a and 5b are provided to face each other so as to sandwich the planetary wheel 4, and engage with the protrusion 7a provided on the locking ring 7 and the protrusion 21a provided on the casing 21, respectively. It is mounted so that it cannot rotate. Also. The inner ring 5a is slidably mounted in the axial direction, and is biased toward the inner ring 5b by the coil spring 11.

遊星車4は、キャリアピン12によりキャリア6に対して片持ちで回転自在に支持されており、大径ローラ部4aと、小径ローラ部4bとから構成されている。大径ローラ部4aの外周面は太陽車3の外周面に当接している。小径ローラ部4bは、大径ローラ部4aの両側面中央部から大径ローラ部4aと同心でかつ円錐台状に突出して形成されていおり、この小径ローラ部4bのテーパ面に、内リング5a及び内リング5bの内周面に形成されたテーパ面が当接している。また、遊星車4は、ベアリング10を介してキャリアピン12に回動自在に支持されている。   The planetary wheel 4 is supported by a carrier pin 12 so as to be cantilevered and rotatable with respect to the carrier 6 and is composed of a large diameter roller portion 4a and a small diameter roller portion 4b. The outer peripheral surface of the large diameter roller portion 4 a is in contact with the outer peripheral surface of the solar wheel 3. The small-diameter roller portion 4b is formed so as to protrude from the center of both side surfaces of the large-diameter roller portion 4a concentrically with the large-diameter roller portion 4a and in a truncated cone shape, and an inner ring 5a is formed on the tapered surface of the small-diameter roller portion 4b. And the taper surface formed in the internal peripheral surface of the inner ring 5b is contact | abutting. Further, the planetary wheel 4 is rotatably supported by the carrier pin 12 via a bearing 10.

また、遊星減速機1は、内リング5a、5bを遊星車4の小径ローラ部4bに圧接するための複数のコイルスプリング11を備えている。複数のコイルスプリング11は、係止リング7に形成された貫通孔に収納され、一端がブラケット2aに支持されて他端がリング5aに当接し、内リング5aを内リング5b側に付勢している。   Further, the planetary reduction gear 1 includes a plurality of coil springs 11 for press-contacting the inner rings 5 a and 5 b to the small diameter roller portion 4 b of the planetary wheel 4. The plurality of coil springs 11 are housed in through holes formed in the locking ring 7, one end is supported by the bracket 2a, the other end abuts on the ring 5a, and urges the inner ring 5a toward the inner ring 5b. ing.

そして、コイルスプリング11によって、内リング5a及び内リング5bの内周テーパ面が遊星車4の小径ローラ部4bのテーパ面に圧接され、その圧接力のうちの中心部に向かう成分によって遊星車4の大径ローラ部4aの外周面が太陽車3の外周面に圧接されている。したがって、各当接部P1、P2、P3はトラクション方式によってトルクが伝達され、遊星車4が太陽車3の周りを公転しながら自転するように構成されている。   The inner peripheral tapered surfaces of the inner ring 5a and the inner ring 5b are pressed against the tapered surface of the small-diameter roller portion 4b of the planetary wheel 4 by the coil spring 11, and the planetary wheel 4 is generated by a component of the pressing force toward the center. The outer peripheral surface of the large-diameter roller portion 4 a is pressed against the outer peripheral surface of the sun wheel 3. Therefore, each contact portion P1, P2, P3 is configured such that torque is transmitted by a traction method, and the planetary wheel 4 rotates while revolving around the solar wheel 3.

キャリア6は、リング状の部材であり、中心部の孔には出力軸27が挿入されて互いに相対回転不能に固定されている。なお、キャリア6と出力軸27とは、一体に形成してもよい。   The carrier 6 is a ring-shaped member, and an output shaft 27 is inserted into a hole in the center portion and fixed so as not to rotate relative to each other. Note that the carrier 6 and the output shaft 27 may be integrally formed.

そして、遊星減速機1は、駆動モータ2が駆動すると、その回転速度が、太陽車3、遊星車4の大径ローラ部4a、小径ローラ部4b及び内リング5a、5bのそれぞれの外径、内径によって決まる減速比によって減速され、キャリア6及び出力軸27を介して、その回転力が出力される。   When the drive motor 2 is driven, the planetary speed reducer 1 has the rotational speeds of the outer diameters of the sun wheel 3, the large diameter roller part 4a, the small diameter roller part 4b, and the inner rings 5a and 5b of the planetary car 4, The speed is reduced by a reduction ratio determined by the inner diameter, and the rotational force is output via the carrier 6 and the output shaft 27.

また、遊星減速機1は、出力軸27の回転速度を検出し、図示しない制御機器に出力するロータリエンコーダ8を備えている。詳しくは、ロータリエンコーダ8は、周方向に複数の識別符号を有する回転板8aと、回転板8aの回転に伴ってこの識別符号を順次検知し回転速度に応じたパルス信号を出力するセンサ部8bとによって構成されている。また、回転板8aは、ブッシュ9を介して出力軸27に固定されている。そして、このパルス信号が図示しない制御機器に入力され、制御機器が、検出されたパルスと基準パルスとの位相差を検出して、この位相差がなくなるように駆動モータ2の回転速度を制御する。   Further, the planetary reduction gear 1 includes a rotary encoder 8 that detects the rotational speed of the output shaft 27 and outputs it to a control device (not shown). Specifically, the rotary encoder 8 includes a rotating plate 8a having a plurality of identification codes in the circumferential direction, and a sensor unit 8b that sequentially detects the identification codes as the rotating plate 8a rotates and outputs a pulse signal corresponding to the rotation speed. And is composed of. The rotating plate 8 a is fixed to the output shaft 27 via the bush 9. Then, this pulse signal is input to a control device (not shown), and the control device detects the phase difference between the detected pulse and the reference pulse, and controls the rotational speed of the drive motor 2 so as to eliminate this phase difference. .

次に、遊星減速機1の潤滑構造は、摩擦伝動部(図中の当接部P1、P2、P3)を潤滑するグリースが、摩擦伝動部の回動に伴って周囲に飛散することないように、当接部P1、P2、P3を介して軸方向の両側に、当接部P1、P2、P3を間隙を介して覆う一対の遮蔽板6a、23を備え、一方の遮蔽板6aがキャリア6と一体に形成され、他方の遮蔽板23が太陽車3に固定されている。   Next, the lubricating structure of the planetary reduction gear 1 is such that the grease that lubricates the friction transmission parts (contact parts P1, P2, and P3 in the figure) does not scatter around the rotation of the friction transmission parts. In addition, a pair of shielding plates 6a and 23 are provided on both sides in the axial direction via the contact portions P1, P2, and P3 so as to cover the contact portions P1, P2, and P3 with a gap therebetween. 6 and the other shielding plate 23 is fixed to the solar wheel 3.

一方の遮蔽板6aは、太陽車3の軸方向の端部及び遊星車4の軸方向の端部に沿って形成され、これらの端部に対して略一様な間隙を有するように構成されている。   One shielding plate 6 a is formed along the axial end of the solar wheel 3 and the axial end of the planetary wheel 4, and is configured to have a substantially uniform gap with respect to these ends. ing.

他方の遮蔽板23は、図2に表したように、太陽車3が挿通する貫通孔23aと、太陽車3に対して固定するボルトのねじ込み孔23fと、回動に伴ってグリースを一方の遮蔽板6aに向けて流動させる三枚の羽部23bが形成されている。   As shown in FIG. 2, the other shielding plate 23 includes a through hole 23 a through which the solar wheel 3 is inserted, a screw-in hole 23 f for a bolt that is fixed to the solar wheel 3, and grease that is supplied with the rotation of the other one. Three wings 23b are formed to flow toward the shielding plate 6a.

また、羽部23bは、図2(c)に表したように、一方の遮蔽板6a側に位置する端面が勾配23c、23dを成して形成され、回動に伴って、グリースの流動を促進できるように構成されている。   In addition, as shown in FIG. 2C, the wing portion 23b is formed such that the end surface located on the one shielding plate 6a side forms a gradient 23c, 23d, and the grease flows as it rotates. It is configured to promote.

以下に、前記実施例の遊星減速機1の潤滑構造の作用効果を記載する。   Below, the effect of the lubrication structure of the planetary reduction gear 1 of the said Example is described.

本実施例の遊星減速機1の潤滑構造によれば、太陽車3、遊星車4、内リング5a、5bの当接部P1、P2、P3を介して軸方向の両側に、この当接部P1、P2、P3を間隙を介して覆う遮蔽板6a、23が備えられているので、グリースが当接部P1、P2、P3の遠方に飛散することなく、間隙に沿って循環して当接部P1、P2、P3の潤滑を良好に維持できる。   According to the lubrication structure of the planetary reduction gear 1 of the present embodiment, the contact portions are provided on both sides in the axial direction via the contact portions P1, P2, and P3 of the sun wheel 3, the planetary wheel 4, and the inner rings 5a and 5b. Since the shielding plates 6a and 23 that cover P1, P2, and P3 through the gaps are provided, the grease circulates along the gaps without contacting the contact parts P1, P2, and P3. The lubrication of the parts P1, P2, and P3 can be maintained well.

また、本実施例の遊星減速機1の潤滑構造によれば、一方の遮蔽板6aがキャリア6と一体に備えられ、他方の遮蔽板23が太陽車3に固定されているので、遊星車4の公転と一体になって一方の遮蔽板6aが回転すると共に、他方の遮蔽板23が太陽車3と共に回転し、一方の遮蔽板6aと他方の遮蔽板23との間におけるグリースの循環を促進させることができ、且つ、軸方向において、一方の遮蔽板6a及び他方の遮蔽板23の位置決めと支持を容易にできて、生産性を向上できる。   Further, according to the lubricating structure of the planetary speed reducer 1 of the present embodiment, one of the shielding plates 6 a is provided integrally with the carrier 6, and the other shielding plate 23 is fixed to the solar wheel 3. One shield plate 6a rotates together with the revolution of the other, and the other shield plate 23 rotates with the sun wheel 3 to promote the circulation of grease between the one shield plate 6a and the other shield plate 23. In addition, it is possible to easily position and support the one shielding plate 6a and the other shielding plate 23 in the axial direction, thereby improving productivity.

本実施例の遊星減速機1の潤滑構造によれば、他方の遮蔽板23には、回動に伴ってグリースを一方の遮蔽板6aに向けて流動させる羽部23bが付設されているので、他方の遮蔽板23と一方の遮蔽板6aとの間におけるグリースの循環性を向上させることができる。また、この際、羽部23bが駆動源側に位置する他方の遮蔽板23に付設されているので、グリースが駆動モータ2側に流出することがないように抑制できる。   According to the lubricating structure of the planetary reduction gear 1 of the present embodiment, the other shielding plate 23 is provided with the wing portion 23b that causes the grease to flow toward the one shielding plate 6a as it rotates. It is possible to improve the circulation of grease between the other shielding plate 23 and the one shielding plate 6a. At this time, since the wing 23b is attached to the other shielding plate 23 located on the drive source side, it is possible to prevent the grease from flowing out to the drive motor 2 side.

以上、本発明の一実施例について説明したが、本発明は、前記実施例に限定されるものではない。   As mentioned above, although one Example of this invention was described, this invention is not limited to the said Example.

例えば、本実施例例の遊星減速機の潤滑構造は、太陽車3、遊星車4、内リング5a、5b等が互いに当接して回転力が摩擦伝動するトラクション式に用いたが、トラクション式に代えて、太陽車3、遊星車4、内リング5a、5b等が歯車によって噛合する歯車伝動式に用いてもよい。   For example, the lubricating structure of the planetary speed reducer according to the present embodiment was used for the traction type in which the solar wheel 3, the planetary wheel 4, the inner rings 5a, 5b, etc. are in contact with each other and the rotational force is frictionally transmitted. Instead, the sun wheel 3, the planetary wheel 4, the inner rings 5a, 5b and the like may be used in a gear transmission type in which the gears mesh with each other.

また、本実施例例の遊星減速機1の潤滑構造は、一方の遮蔽板6aをキャリア6と一体に形成したが、これらを別々に形成し、固定したり着脱できるように構成してもよい。また、他方の遮蔽板23を太陽車3と一体に形成してもよい。   Moreover, although the lubricating structure of the planetary reduction gear 1 of the present embodiment is formed with the one shielding plate 6a integrally with the carrier 6, these may be formed separately and fixed or detachable. . The other shielding plate 23 may be formed integrally with the solar wheel 3.

また、本実施例の遊星減速機1の潤滑構造は、一方の遮蔽板6aが、太陽車3の軸方向の端部及び遊星車4の軸方向の端部に沿って形成され、これらの端部に対して略一様な間隙を有するように構成したが、当接部P1、P2、P3の近傍にグリースが溜り易いように、当接部P1、P2、P3に対する一方の遮蔽板6aの間隙を他の部分よりも広くしたり、一方の遮蔽板6aに当接部P1、P2、P3と対向する凹部を形成したりしてもよい。また、他方の遮蔽板23も、遊星車4と対向する端面を、遊星車4の軸方向の端部に沿って形成してもよい。   Further, in the lubrication structure of the planetary reduction gear 1 of the present embodiment, one shielding plate 6a is formed along the axial end of the solar wheel 3 and the axial end of the planetary wheel 4, and these ends Although it is configured so as to have a substantially uniform gap with respect to the portion, one of the shielding plates 6a with respect to the contact portions P1, P2, and P3 is arranged so that the grease easily collects in the vicinity of the contact portions P1, P2, and P3. The gap may be made wider than the other part, or a recess facing the contact parts P1, P2, P3 may be formed on one shielding plate 6a. Further, the other shielding plate 23 may also be formed with an end face facing the planetary car 4 along the end of the planetary car 4 in the axial direction.

本発明の遊星減速機の潤滑構造が適用された遊星減速機の構成を表す断面図である。It is sectional drawing showing the structure of the planetary reduction gear to which the lubrication structure of the planetary reduction gear of this invention was applied. 図1における他方の遮蔽板の構成を表す外観図であって、(a)図が軸方向から視た正面図、(b)図が(a)図におけるBーB断面図、図Cが(a)図におけるC方向から視た平面図である。同実施例における故障検出部の回路図である。It is an external view showing the structure of the other shielding board in FIG. 1, (a) The figure is a front view seen from the axial direction, (b) is a BB cross-sectional view in FIG. a) It is the top view seen from the C direction in a figure. It is a circuit diagram of the failure detection part in the same Example.

符号の説明Explanation of symbols

1…遊星減速機、2…駆動モータ、2a…ブラケット、3…太陽車、4…遊星車、4a…大径ローラ部、4b…小径ローラ部、5a,5b…内リング、6…キャリア、6a,23遮蔽板、7…係止リング、7a,21a…突起部、8…ロータリエンコーダ、8a…回転板、8b…センサ部、9…ブッシュ、10,18,19…ベアリング、11…コイルスプリング、12…キャリアピン、13…ウェーブワッシャ、20…止め輪、21,22…ケーシング、23a…貫通孔、23b…羽部、23c,23d…勾配、23f…ねじ込み孔、25,26…ボルト、27…出力軸。   DESCRIPTION OF SYMBOLS 1 ... Planetary reducer, 2 ... Drive motor, 2a ... Bracket, 3 ... Sun wheel, 4 ... Planetary wheel, 4a ... Large diameter roller part, 4b ... Small diameter roller part, 5a, 5b ... Inner ring, 6 ... Carrier, 6a , 23 shielding plate, 7 ... locking ring, 7a, 21a ... projection, 8 ... rotary encoder, 8a ... rotating plate, 8b ... sensor part, 9 ... bushing, 10, 18, 19 ... bearing, 11 ... coil spring, DESCRIPTION OF SYMBOLS 12 ... Carrier pin, 13 ... Wave washer, 20 ... Retaining ring, 21, 22 ... Casing, 23a ... Through-hole, 23b ... Wing part, 23c, 23d ... Gradient, 23f ... Screw-in hole, 25, 26 ... Bolt, 27 ... Output shaft.

Claims (3)

ケーシング内に、
駆動源の駆動力を受けて回動する太陽車と、
前記太陽車に間隙を介して同軸状に配置された内リングと、
前記間隙内に配設され前記太陽車及び前記内リングに当接する遊星車と、
前記太陽車と同軸線上に回動自在に配設され、前記遊星車を回動自在に支持するキャリアとを備え、
前記太陽車、前記遊星車、前記内リングの当接部には、互いの磨耗を低減し円滑な摩擦伝動を行うためのグリースが充填され、
前記当接部を介して軸方向の両側に、該当接部を間隙を介して覆う遮蔽板が一対備えられている、
ことを特徴とする遊星減速機の潤滑構造。
In the casing,
A sun wheel that rotates in response to the driving force of the driving source;
An inner ring coaxially arranged in the solar wheel with a gap therebetween;
A planetary wheel disposed in the gap and in contact with the solar wheel and the inner ring;
A carrier rotatably disposed on a coaxial line with the sun wheel, and a carrier for rotatably supporting the planetary wheel;
The sun wheel, the planetary wheel, and the contact portion of the inner ring are filled with grease for reducing wear and smooth friction transmission,
A pair of shielding plates are provided on both sides in the axial direction via the abutting part, covering the corresponding part with a gap,
A lubrication structure for a planetary speed reducer.
前記一対の遮蔽板の内、一方の遮蔽板が前記キャリアと一体に備えられ、他方の遮蔽板が前記太陽車と一体に備えられている、
ことを特徴とする請求項1に記載の遊星減速機の潤滑構造。
Of the pair of shielding plates, one shielding plate is provided integrally with the carrier, and the other shielding plate is provided integrally with the solar wheel.
The lubrication structure of the planetary reduction gear according to claim 1, wherein:
前記他方の遮蔽板には、回動に伴って前記グリースを前記一方の遮蔽板に向けて流動させる羽部が付設されている、
ことを特徴とする請求項1又は請求項2に記載の遊星減速機の潤滑構造。
The other shielding plate is provided with a wing portion that causes the grease to flow toward the one shielding plate with rotation,
The lubricating structure for a planetary speed reducer according to claim 1 or 2, wherein the lubricating structure is a planetary speed reducer.
JP2006046586A 2006-02-23 2006-02-23 Lubricating structure of planetary reducer Expired - Fee Related JP4889318B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2006046586A JP4889318B2 (en) 2006-02-23 2006-02-23 Lubricating structure of planetary reducer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2006046586A JP4889318B2 (en) 2006-02-23 2006-02-23 Lubricating structure of planetary reducer

Publications (2)

Publication Number Publication Date
JP2007225017A true JP2007225017A (en) 2007-09-06
JP4889318B2 JP4889318B2 (en) 2012-03-07

Family

ID=38547016

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006046586A Expired - Fee Related JP4889318B2 (en) 2006-02-23 2006-02-23 Lubricating structure of planetary reducer

Country Status (1)

Country Link
JP (1) JP4889318B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011214415A (en) * 2010-03-31 2011-10-27 Toyota Industries Corp Compressor with transmission
JP2012062978A (en) * 2010-09-16 2012-03-29 Ricoh Co Ltd Mechanism for supplying grease into epicycle reduction gear, epicycle reduction gear and image forming apparatus
JP2015511691A (en) * 2012-03-23 2015-04-20 浙江超級電気科技有限公司 Automatic pressing friction transmission speed reducer

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06117508A (en) * 1992-10-08 1994-04-26 Nippondenso Co Ltd Planetary roller type power transmission
JPH09112642A (en) * 1995-10-23 1997-05-02 Mitsubishi Heavy Ind Ltd Planet roller type power transmission device

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06117508A (en) * 1992-10-08 1994-04-26 Nippondenso Co Ltd Planetary roller type power transmission
JPH09112642A (en) * 1995-10-23 1997-05-02 Mitsubishi Heavy Ind Ltd Planet roller type power transmission device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011214415A (en) * 2010-03-31 2011-10-27 Toyota Industries Corp Compressor with transmission
JP2012062978A (en) * 2010-09-16 2012-03-29 Ricoh Co Ltd Mechanism for supplying grease into epicycle reduction gear, epicycle reduction gear and image forming apparatus
JP2015511691A (en) * 2012-03-23 2015-04-20 浙江超級電気科技有限公司 Automatic pressing friction transmission speed reducer

Also Published As

Publication number Publication date
JP4889318B2 (en) 2012-03-07

Similar Documents

Publication Publication Date Title
JP7188849B2 (en) Reducer and Actuator
US8932170B2 (en) Planetary gear device
JP5822817B2 (en) Wheel drive device
JP2008502850A (en) Drive device and brake assembly
JP2006307910A (en) Rotary support structure of carrier in planetary gear reduction gear
JP2006307909A (en) Rotary support structure of carrier in planetary gear reduction gear
JP6699313B2 (en) Driving force transmission device and four-wheel drive vehicle
US9017206B2 (en) Gear device
KR20150079607A (en) Eccentric oscillation-type gear device
JP4889318B2 (en) Lubricating structure of planetary reducer
JP2007138975A (en) Lubrication mechanism of planetary gear device
US20140260743A1 (en) Wheel driving apparatus
JP2005282593A (en) Gear transmission
JP2012137113A (en) Shaft device
KR101505414B1 (en) End-cover for reducer
JP4646831B2 (en) Decelerator
JP2005076810A (en) Retainer for needle bearing and needle bearing
JP2016156389A (en) Final speed reduction device
JP2006258270A (en) Supporting structure of turning member in planetary gear reducer
JP2010210073A (en) Drive unit
JP5228533B2 (en) Support structure for rotating shaft member
JP2010043679A (en) Reduction gear and method for fixing planetary gear for the same
JP6247519B2 (en) Interrupting device
JP2011089583A (en) Lubricating structure for vehicular continuously variable transmission
JP2008051163A (en) Epicyclic gear reducer

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20080909

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20110329

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20110330

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20110527

RD03 Notification of appointment of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7423

Effective date: 20110527

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20111115

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20111213

R150 Certificate of patent or registration of utility model

Ref document number: 4889318

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20141222

Year of fee payment: 3

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees