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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- JP
- Japan
- Prior art keywords
- pivot
- pair
- continuously variable
- variable transmission
- oil passage
- 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.)
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- 230000005540 biological transmission Effects 0.000 claims 15
- 230000001808 coupling Effects 0.000 claims 2
- 238000010168 coupling process Methods 0.000 claims 2
- 238000005859 coupling reaction Methods 0.000 claims 2
- 230000002093 peripheral Effects 0.000 claims 2
- 230000000875 corresponding Effects 0.000 claims 1
Claims (10)
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6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.
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.
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)
Publication Number | Publication Date |
---|---|
JP2016166641A JP2016166641A (en) | 2016-09-15 |
JP2016166641A5 true JP2016166641A5 (en) | 2018-04-12 |
JP6554294B2 JP6554294B2 (en) | 2019-07-31 |
Family
ID=56879339
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2015046285A Active JP6554294B2 (en) | 2015-03-09 | 2015-03-09 | Toroidal continuously variable transmission and aircraft drive mechanism integrated power generator |
Country Status (2)
Country | Link |
---|---|
JP (1) | JP6554294B2 (en) |
WO (1) | WO2016143329A1 (en) |
Families Citing this family (1)
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)
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 |
-
2015
- 2015-03-09 JP JP2015046285A patent/JP6554294B2/en active Active
-
2016
- 2016-03-08 WO PCT/JP2016/001255 patent/WO2016143329A1/en active Application Filing
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