21 |
SCROLL COMPRESSOR WITH CAPTURED THRUST WASHER |
EP13764551.1 |
2013-03-21 |
EP2839158A1 |
2015-02-25 |
HEUSLER, Kenneth, D.; DUPPERT, Ronald, J. |
A load transmittal apparatus transfers an axial load to a thrust surface during operation of a scroll compressor. |
22 |
PRESS-FIT BEARING HOUSING WITH LARGE GAS PASSAGES |
EP13763461 |
2013-03-13 |
EP2839162A4 |
2016-08-24 |
DUPPERT RONALD J; WANG XIANGHONG; BESSEL KURT WILLIAM ROBERT; BUSH JAMES W |
A scroll compressor that includes a housing and scroll compressor bodies disposed in the housing. A motor is disposed within the housing and operably connected to a drive shaft for driving one of the scroll compressor bodies. The drive shaft is rotationally supported at one end by a crankcase which includes a bearing housing and a bearing. The crankcase includes a plurality of openings or gas passages passing through the crankcase, as well as a plurality of generally cylindrical sections positioned respectively between adjacent openings. The cylindrical sections define contact regions which can engage an inner periphery of the housing when the crankcase is mounted therein. |
23 |
AN INTERNAL COMBUSTION ROTARY ENGINE |
EP08776210.0 |
2008-07-16 |
EP2171213A2 |
2010-04-07 |
McDonald, Kenneth |
An engine comprising a first section having a first face and a second section having a second face, the first and second faces being opposed to one another and arranged for relative rotation, the first face comprising at least one chamber, the second face comprising a plurality of discrete regions each being associated with a discrete stage of a combustion cycle, wherein the first and second faces are arranged such that relative rotation thereof causes the at least one chamber of the first face to be exposed to the discrete regions of the second face. |
24 |
전동 압축기 |
KR1019830000229 |
1983-01-21 |
KR1019840003334A |
1984-08-20 |
후지와라타까요시-1 |
내용없음 |
25 |
AN INTERNAL COMBUSTION ROTARY ENGINE |
PCT/GB2008050575 |
2008-07-16 |
WO2009010796A3 |
2009-11-26 |
MCDONALD KENNETH |
An engine comprising a first section having a first face and a second section having a second face, the first and second faces being opposed to one another and arranged for relative rotation, the first face comprising at least one chamber, the second face comprising a plurality of discrete regions each being associated with a discrete stage of a combustion cycle, wherein the first and second faces are arranged such that relative rotation thereof causes the at least one chamber of the first face to be exposed to the discrete regions of the second face. |