公开(公告)号：US6102671A

公开(公告)日：2000-08-15

申请号：US131822

申请日：1998-08-10

申请人： Shuichi Yamamoto ,  Kiyoshi Sawai ,  Taise Kohayakawa ,  Shozo Hase ,  Takashi Morimoto ,  Hiromasa Ashitani ,  Hiroyuki Fukuhara

发明人： Shuichi Yamamoto ,  Kiyoshi Sawai ,  Taise Kohayakawa ,  Shozo Hase ,  Takashi Morimoto ,  Hiromasa Ashitani ,  Hiroyuki Fukuhara

IPC分类号： F04C18/02 ,  F04C28/28 ,  F04C29/00 ,  F04B49/00

CPC分类号： F04C28/28 ,  F04C18/0246 ,  F04C18/0269 ,  F04C29/0035

摘要： Base wraps 21a and 31a of a fixed scroll 20 and orbiting scroll 30 both have spiral lengths that satisfy specified compression ratio in low speed drive region. Spiral shaped extension wraps 21b and 31b are provided for at least one of the base wraps 21a and 31a, extended from the spiral end position thereof, and a displacement is effected in the direction in which the thickness of the wraps 21 and 31 becomes thinner, at least at either the inner walls of the extension wraps 21b and 31b or at the outer walls of the wraps 21 and 31 in opposition thereto, making the interrelationship greater.

摘要翻译： 固定涡旋盘20和绕动涡旋盘30的底盘21a和31a均具有在低速驱动区域中满足规定压缩比的螺旋长度。 为从其螺旋端位置延伸的底盖21a和31a中的至少一个提供螺旋形延伸膜21b和31b，并且沿着包层21和31的厚度变薄的方向发生位移， 至少在延伸纸圈21b和31b的内壁处或与纸卷21和31的外壁相反，使得相互关系更大。

公开(公告)号：US06273691B1

公开(公告)日：2001-08-14

申请号：US08895998

申请日：1997-07-17

申请人： Takashi Morimoto ,  Sadayuki Yamada ,  Shuichi Yamamoto ,  Kiyoshi Sawai ,  Taisei Kohayakawa ,  Shozo Hase ,  Hiromasa Ashitani

发明人： Takashi Morimoto ,  Sadayuki Yamada ,  Shuichi Yamamoto ,  Kiyoshi Sawai ,  Taisei Kohayakawa ,  Shozo Hase ,  Hiromasa Ashitani

IPC分类号： F04C1804

CPC分类号： F04C28/16 ,  F04C18/0215 ,  F04C28/26

摘要： It is an object of the present invention to improve the efficiency of a scroll gas compressor by operating a bypass at a proper compression ratio. To achieve the object, the present invention is constituted so that at least one pair of bypass holes whose one ends are opened in a compression chamber currently performing compression nearby a discharge vent and whose other ends communicate with a discharge chamber are asymmetrically arranged on a panel board. This structure makes it possible to improve the efficiency of the compressor by operating the bypass at an optimum compression ratio even if a difference is observed between pressure rises of a pair of symmetric compressed spaces under the compression process.

摘要翻译： 本发明的目的是通过以适当的压缩比操作旁路来提高涡旋式气体压缩机的效率。 为了实现该目的，本发明构成为使得至少一对旁通孔的一端在压缩室中在目前在排气口附近进行压缩并且其另一端与排出室连通的压缩室中打开，不对称地布置在面板 板。 这种结构使得即使在压缩过程中在一对对称压缩空间的压力上升之间观察到差异，也可以通过以最佳压缩比操作旁路来提高压缩机的效率。

公开(公告)号：US5704122A

公开(公告)日：1998-01-06

申请号：US783634

申请日：1997-01-14

申请人： Masahiro Tsubokawa ,  Osamu Aiba ,  Toshiharu Yasu ,  Shuichi Yamamoto ,  Hideo Hirano ,  Taisei Kohayakawa ,  Shozo Hase

发明人： Masahiro Tsubokawa ,  Osamu Aiba ,  Toshiharu Yasu ,  Shuichi Yamamoto ,  Hideo Hirano ,  Taisei Kohayakawa ,  Shozo Hase

IPC分类号： F01C21/10 ,  F04C18/02 ,  B23P15/00

CPC分类号： F04C18/0215 ,  F01C21/102 ,  F04C2230/60 ,  F05C2251/046 ,  Y10T29/4924

摘要： In a sealed-type scroll compressor having a stationary scroll member and an orbiting scroll member, the stationary scroll member is fixed after rotating it in an orbiting direction of the orbiting scroll member by a predetermined angle from a phase angle position where a possible orbiting radius between both scroll members is made maximum at the temperature before driving the scroll compressor.

摘要翻译： 在具有静止涡旋构件和绕动涡旋构件的密封式涡旋压缩机中，固定涡旋构件在绕动涡旋构件的运动方向从相位角位置旋转预定角度后固定，其中可能的轨道半径 两个涡旋构件之间的温度在驱动涡旋压缩机之前的温度最大。

公开(公告)号：US5632610A

公开(公告)日：1997-05-27

申请号：US362679

申请日：1994-12-22

申请人： Masahiro Tsubokawa ,  Osamu Aiba ,  Toshiharu Yasu ,  Shuichi Yamamoto ,  Hideo Hirano ,  Taisei Kohayakawa ,  Shozo Hase

发明人： Masahiro Tsubokawa ,  Osamu Aiba ,  Toshiharu Yasu ,  Shuichi Yamamoto ,  Hideo Hirano ,  Taisei Kohayakawa ,  Shozo Hase

IPC分类号： F01C21/10 ,  F04C18/02 ,  F04C18/04

CPC分类号： F04C18/0215 ,  F01C21/102 ,  F04C2230/60 ,  F05C2251/046 ,  Y10T29/4924

摘要： In a sealed-type scroll compressor having a stationary scroll member and an orbiting scroll member, the stationary scroll member is fixed after rotating it in an orbiting direction of the orbiting scroll member by a predetermined angle from a phase angle position where a possible orbiting radius between both scroll members is made maximum at the temperature before driving the scroll compressor.

摘要翻译： 在具有静止涡旋构件和绕动涡旋构件的密封式涡旋压缩机中，固定涡旋构件在绕动涡旋构件的运动方向从相位角位置旋转预定角度后固定，其中可能的轨道半径 两个涡旋构件之间的温度在驱动涡旋压缩机之前的温度最大。