JP2016166641A5 - - Google Patents

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JP2016166641A5
JP2016166641A5 JP2015046285A JP2015046285A JP2016166641A5 JP 2016166641 A5 JP2016166641 A5 JP 2016166641A5 JP 2015046285 A JP2015046285 A JP 2015046285A JP 2015046285 A JP2015046285 A JP 2015046285A JP 2016166641 A5 JP2016166641 A5 JP 2016166641A5
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Japan
Prior art keywords
pivot
pair
continuously variable
variable transmission
oil passage
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JP2015046285A
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JP2016166641A (en
JP6554294B2 (en
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Priority to JP2015046285A priority Critical patent/JP6554294B2/en
Priority claimed from JP2015046285A external-priority patent/JP6554294B2/en
Priority to PCT/JP2016/001255 priority patent/WO2016143329A1/en
Publication of JP2016166641A publication Critical patent/JP2016166641A/en
Publication of JP2016166641A5 publication Critical patent/JP2016166641A5/ja
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Claims (10)

互いに対向配置される入力ディスク及び出力ディスクと、
前記入力ディスクと前記出力ディスクとの間に傾転可能に挟まれ、前記入力ディスクの回転駆動力を傾転角に応じた変速比で前記出力ディスクに伝達するパワーローラと、
傾転軸線と同軸状に配置された一対の枢軸部、及び、傾転軸線方向において前記一対の枢軸部の間に位置して前記パワーローラが回転自在に取り付けられる本体部を有するトラニオンと、
前記一対の枢軸部に外嵌される軸受と、
前記パワーローラから見て前記本体部と反対側において前記傾転軸線方向に延びて前記トラニオンに連結されるビームと、
前記トラニオン及び前記パワーローラに油を供給する油路と、を備え、
前記一対の枢軸部が、前記本体部から前記傾転軸線方向と垂直な突出方向に突出し、前記油路は、前記一対の枢軸部のうちの一方である第1枢軸部の内部で前記突出方向に延びる第1枢軸油路を有し、
前記ビームが前記一対の枢軸部に挿入される連結具で前記一対の枢軸部と連結され
前記第1枢軸油路および前記連結具が前記軸受の内側に位置する、トロイダル無段変速機。
An input disk and an output disk arranged opposite to each other;
A power roller sandwiched between the input disk and the output disk so as to be tiltable, and transmitting a rotational driving force of the input disk to the output disk at a gear ratio according to a tilt angle;
A pair of pivot portions arranged coaxially with the tilt axis, and a trunnion having a main body portion that is positioned between the pair of pivot portions in the tilt axis direction and to which the power roller is rotatably attached;
Bearings fitted on the pair of pivot parts,
A beam extending in the direction of the tilt axis on the side opposite to the main body as viewed from the power roller and coupled to the trunnion;
An oil passage for supplying oil to the trunnion and the power roller ,
The pair of pivot portions project from the main body portion in a projecting direction perpendicular to the tilt axis direction, and the oil passage is in the projecting direction within the first pivot portion which is one of the pair of pivot portions. A first pivot oil passage extending to
The beam is connected to the pair of pivot parts with a connector inserted into the pair of pivot parts ,
It said first pivot oil path and the connector is you positioned inside the bearing, a toroidal continuously variable transmission.
前記ビームが、前記一対の枢軸部の内面と前記傾転軸線方向に重ねられ、前記連結具が前記傾転軸線方向に挿入される、請求項1に記載のトロイダル無段変速機。   2. The toroidal continuously variable transmission according to claim 1, wherein the beam is overlapped with inner surfaces of the pair of pivot portions in the tilt axis direction, and the connector is inserted in the tilt axis direction. 前記一対の枢軸部は、前記内面の前記突出方向における先端部を前記傾転軸線方向の外側にオフセットすることで形成される一対の段差面を有し、
前記ビームが前記突出方向において前記段差面に重ねられる、請求項2に記載のトロイダル無段変速機。
The pair of pivot portions have a pair of step surfaces formed by offsetting the tip portion of the inner surface in the protruding direction to the outside in the tilt axis direction,
The toroidal continuously variable transmission according to claim 2, wherein the beam is superimposed on the step surface in the protruding direction.
前記連結具は、前記ビームに挿入される非ねじ部を有し、
前記一対の枢軸部の各々が、単一の前記連結具で前記ビームに連結される、請求項3に記載のトロイダル無段変速機。
The connector has a non-threaded portion inserted into the beam,
The toroidal continuously variable transmission according to claim 3, wherein each of the pair of pivot portions is coupled to the beam by a single coupling tool.
前記一対の枢軸部の各々が、1つの前記連結具で、前記ビームに連結され、
前記一対の枢軸部に対応した一対の前記連結具が、前記傾転軸線及び前記突出方向に垂直な前記トラニオンの幅方向における前記枢軸部の中央部で、同軸状に配置される、請求項1乃至4のいずれか1項に記載のトロイダル無段変速機。
Each of the pair of pivot portions is connected to the beam by one connecting tool,
2. The pair of coupling tools corresponding to the pair of pivot portions are arranged coaxially at a central portion of the pivot portion in the width direction of the trunnion perpendicular to the tilt axis and the protruding direction. The toroidal continuously variable transmission of any one of thru | or 4.
前記油路は、前記本体部の内部で前記傾転軸線方向に延びる本体油路を有し、前記軸受の一部が前記本体油路に対して前記突出方向において外側に位置する、請求項1乃至5のいずれか1項に記載のトロイダル無段変速機。 The oil passage has a main body oil passage extending in the tilt axis direction inside the main body portion, and a part of the bearing is located outside in the projecting direction with respect to the main body oil passage. The toroidal continuously variable transmission of any one of thru | or 5. 前記トラニオンは、前記本体部の内面に開口する取付孔を有し、前記パワーローラは、前記取付孔に回転可能に挿入される取付軸を介して前記本体部に取り付けられ、
前記取付孔及び前記第1枢軸油路は、前記傾転軸線から前記傾転軸線方向及び前記突出方向に垂直な前記トラニオンの幅方向の一方側に偏在し、
前記油路は、前記本体部の内部で前記傾転軸線方向に延び、前記第1枢軸油路の前記突出方向における基端部を前記取付孔に連通させる本体油路を含む、請求項1乃至のいずれか1項に記載のトロイダル無段変速機。
The trunnion has an attachment hole that opens to the inner surface of the main body, and the power roller is attached to the main body via an attachment shaft that is rotatably inserted into the attachment hole.
The mounting hole and the first pivot oil passage are unevenly distributed from the tilt axis to one side in the width direction of the trunnion perpendicular to the tilt axis direction and the protruding direction,
The oil passage extends to the tilting axis direction within said body portion includes a body oil passage communicating the base end portion in the protruding direction of the first pivot oil passage in the mounting hole, to claim 1 The toroidal continuously variable transmission of any one of 6.
前記油路は、前記第1枢軸油路の前記突出方向における先端部と連通し、前記第1枢軸部の内面に開口して前記パワーローラの周面と対向する第1ノズルと、前記一対の枢軸部のうちの他方である第2枢軸部の内面に開口して前記パワーローラの周面と対向する第2ノズルと、前記第1枢軸油路の前記突出方向における基端部から前記本体部及び前記第2枢軸部の内部を通って前記第2ノズルに接続される分配油路と、を含む、請求項5乃至7のいずれか1項に記載のトロイダル無段変速機。   The oil passage communicates with a distal end portion of the first pivot oil passage in the protruding direction, opens to an inner surface of the first pivot portion, and faces a peripheral surface of the power roller, and the pair of A second nozzle that opens on the inner surface of the second pivot portion that is the other of the pivot portions and faces the peripheral surface of the power roller; and a base end portion in the protruding direction of the first pivot oil passage from the main body portion The toroidal continuously variable transmission according to any one of claims 5 to 7, further comprising: a distribution oil passage connected to the second nozzle through the inside of the second pivot portion. 請求項1乃至8のいずれか1項に記載のトロイダル無段変速機と、
航空機のエンジン回転軸から取り出される回転動力を前記トロイダル無段変速機に入力する入力機構と、
前記トロイダル無段変速機の出力で駆動される発電機と、を備える、航空機用駆動機構一体型発電装置。
A toroidal continuously variable transmission according to any one of claims 1 to 8,
An input mechanism for inputting rotational power extracted from an engine rotation shaft of an aircraft to the toroidal continuously variable transmission;
And a generator driven by an output of the toroidal continuously variable transmission.
前記入力機構が、前記エンジン回転軸から取り出された回転動力が入力される装置入力軸と、前記装置入力軸の回転を前記トロイダル無段変速機に伝達するギヤ対とを備え、
前記装置入力軸が、前記トロイダル無段変速機の軸方向と平行であり、
前記トロイダル無段変速機の前記傾転軸線が、前記装置入力軸と前記トロイダル無段変速機における回転軸とを結ぶ直線の延在方向と非垂直である、請求項9に記載の航空機用駆動機構一体型発電装置。
The input mechanism includes a device input shaft to which rotational power extracted from the engine rotation shaft is input, and a gear pair that transmits rotation of the device input shaft to the toroidal continuously variable transmission;
The device input shaft is parallel to the axial direction of the toroidal continuously variable transmission;
10. The aircraft drive according to claim 9, wherein the tilt axis of the toroidal continuously variable transmission is non-perpendicular to an extending direction of a straight line connecting the device input shaft and a rotating shaft in the toroidal continuously variable transmission. Mechanism-integrated power generator.
JP2015046285A 2015-03-09 2015-03-09 Toroidal continuously variable transmission and aircraft drive mechanism integrated power generator Active JP6554294B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP2015046285A JP6554294B2 (en) 2015-03-09 2015-03-09 Toroidal continuously variable transmission and aircraft drive mechanism integrated power generator
PCT/JP2016/001255 WO2016143329A1 (en) 2015-03-09 2016-03-08 Toroidal continuously variable transmission, and drive-mechanism-integrated power generating device for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2015046285A JP6554294B2 (en) 2015-03-09 2015-03-09 Toroidal continuously variable transmission and aircraft drive mechanism integrated power generator

Publications (3)

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JP2016166641A JP2016166641A (en) 2016-09-15
JP2016166641A5 true JP2016166641A5 (en) 2018-04-12
JP6554294B2 JP6554294B2 (en) 2019-07-31

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JP (1) JP6554294B2 (en)
WO (1) WO2016143329A1 (en)

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Publication number Priority date Publication date Assignee Title
JP7449088B2 (en) 2019-12-25 2024-03-13 川崎重工業株式会社 toroidal continuously variable transmission

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002106667A (en) * 2000-10-04 2002-04-10 Honda Motor Co Ltd Toroidal continuously variable transmission
JP4003119B2 (en) * 2001-11-02 2007-11-07 日本精工株式会社 Toroidal continuously variable transmission
JP4461349B2 (en) * 2001-08-27 2010-05-12 日本精工株式会社 Toroidal continuously variable transmission
JP3991703B2 (en) * 2002-02-14 2007-10-17 日本精工株式会社 Toroidal continuously variable transmission
JP4474908B2 (en) * 2003-07-23 2010-06-09 日本精工株式会社 Toroidal continuously variable transmission
JP4836047B2 (en) * 2005-08-17 2011-12-14 日本精工株式会社 Toroidal continuously variable transmission
JP2007240004A (en) * 2007-05-07 2007-09-20 Nsk Ltd Power roller unit for toroidal continuously variable transmission
JP5755689B2 (en) * 2013-06-26 2015-07-29 川崎重工業株式会社 Toroidal continuously variable transmission

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