To provide a link geometry of a multi-link engine which does not cause deformation of a cylinder liner even if the rigidity of a cylinder liner becomes weak due to formation of a defect part in the lower end of the cylinder liner.
The link geometry of the multi-link engine includes: an upper link 11 connected to a piston 32; a lower link 12 which is fitted to a crank pin 33b of a crank shaft 33 freely rotatably and is connected to the upper link 11; and a control link 13 which is connected to the lower link 12 and rocks around a rocking center shaft 24. The crank pin 33b is arranged on a line connecting an upper pin 22 to a control pin 23, and an angle formed by a traverse axis passing the axis center of a crank journal 33a and crossing at a right angle to the cylinder axial line and a line connecting the control pin 23 to the upper pin 22 is nearly the same in the top dead center and in the bottom dead center of the piston.
TOMITA MASAYUKI
USHIJIMA KENJI
HIRATANI KOJI
TSUCHIDA HIROBUMI
AOYAMA SHUNICHI
| JP2003013764A | 2003-01-15 | |||
| JP2003278567A | 2003-10-02 | |||
| JP2006144615A | 2006-06-08 | |||
| JP2006052667A | 2006-02-23 | |||
| JP2006200375A | 2006-08-03 | |||
| JPS57186638U | 1982-11-26 | |||
| JPS5932147U | 1984-02-28 |
Masahiro Fujii
Masaaki Iida
Yasunari Mita
Next Patent: AEROSOL SEPARATOR, AND METHOD