US20050112014A1 - Fluid compressor - Google Patents
Fluid compressor Download PDFInfo
- Publication number
- US20050112014A1 US20050112014A1 US10/996,585 US99658504A US2005112014A1 US 20050112014 A1 US20050112014 A1 US 20050112014A1 US 99658504 A US99658504 A US 99658504A US 2005112014 A1 US2005112014 A1 US 2005112014A1
- Authority
- US
- United States
- Prior art keywords
- pump chamber
- discharge port
- guide surface
- compressor
- fluid
- 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.)
- Abandoned
Links
- 239000012530 fluid Substances 0.000 title claims abstract description 39
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 56
- 238000007599 discharging Methods 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 64
- 239000001257 hydrogen Substances 0.000 description 56
- 229910052739 hydrogen Inorganic materials 0.000 description 56
- 239000007789 gas Substances 0.000 description 31
- 239000000446 fuel Substances 0.000 description 19
- 238000005192 partition Methods 0.000 description 7
- 230000004913 activation Effects 0.000 description 5
- 239000007800 oxidant agent Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- -1 hydrogen off gas) Chemical compound 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0092—Removing solid or liquid contaminants from the gas under pumping, e.g. by filtering or deposition; Purging; Scrubbing; Cleaning
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2210/00—Fluid
- F04C2210/24—Fluid mixed, e.g. two-phase fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/10—Stators
- F04C2240/102—Stators with means for discharging condensate or liquid separated from the gas pumped
Definitions
- the present invention relates to a compressor, and more particularly, to a compressor for compressing fluid drawn into a pump chamber by rotating a rotor and discharging the fluid out of the pump chamber through a discharge port.
- a compressor that compresses fluid may be used in, for example, a fuel cell system.
- a fuel cell uses hydrogen gas and an oxidizer gas to generate electric power. The fuel cell produces water when generating power. To discharge the water out of the fuel cell, more hydrogen gas and oxidizer gas than the amount of hydrogen gas and oxidizer gas consumed to generate power must be supplied to the fuel cell. Further, the fuel cell discharges hydrogen gas (i.e., hydrogen off gas), which includes hydrogen gas that was not subject to reaction. The discharge of such hydrogen gas lowers fuel efficiency.
- a typical compressor positively circulates the hydrogen off gas and mixes the hydrogen off gas with fresh hydrogen gas to return the hydrogen off gas to the fuel cell.
- FIG. 1 shows an example of such a compressor.
- a fluid compressor 51 has a case 52 , which has the shape of a generally oval cylinder.
- a pump chamber 53 is defined in the case 52 . Hydrogen off gas is drawn into the pump chamber 53 to be compressed.
- Two parallel rotation shafts (drive shaft 54 and driven shaft 55 ) are supported in the pump chamber 53 .
- Two rotors 56 and 57 are respectively fixed to the drive shaft 54 and the driven shaft 55 .
- a driver such as a motor, drives the drive shaft 54 and the driven shaft 55 to rotate the rotors 56 and 57 with a predetermined interval (phase difference) therebetween.
- hydrogen off gas is drawn into the pump chamber 53 through a suction port 58 , which is located at the upper part of the pump chamber, and discharged out of the pump chamber 53 through a discharge port 59 , which is located at the lower part of the pump chamber 53 .
- the wall of the pump chamber 53 is shaped to form two hollow cylindrical portions connected to each other so that the rotors 56 and 57 rotate along the wall. More specifically, the lower middle part of the pump chamber 53 is projected upward as viewed in FIG. 1 .
- the discharge port 59 is formed in the upwardly projecting, lower part of the pump chamber 53 .
- a recess 60 is formed in each side of the discharge port 59 .
- the hydrogen off gas may be supplied to the fluid compressor 51 via a gas-liquid separator. In such a case, however, the humidity of the hydrogen off gas would be high.
- the fluid compressor 51 is in a low temperature atmosphere, the moisture in the hydrogen off gas condenses as the dew point changes and produces water in the pump chamber 53 .
- Such water remains in the recess 60 of the pump chamber 53 . If the fluid compressor 51 is left in such a state under a low temperature for a long period of time, the residual water in the fluid compressor 51 would freeze. Activation of the fuel cell when water is frozen in such a manner would interfere with normal activation of the fuel cell. For example, abnormal current may flow through a motor that drives the fluid compressor 51 .
- Japanese Laid-Open Patent Publication No. 8-109089 describes a root pump (one type of a fluid compressor) that solves the above problem.
- the root pump has a suction port formed in the upper part of a case and a discharge port formed in the lower part of the case.
- the vicinity of the discharge port in the lower part of the case is flat. That is, recesses are not formed in the lower part of the pump chamber. Accordingly, the root pump discharges from the discharge port the water drawn into and the water condensed in the pump chamber so that water does not remain in the pump chamber.
- a root pump is used for various purposes, such as a movable pump or as a pump for use in a vehicle.
- vehicle pumps an automobile is driven (or parked) along sloped roads in addition to level roads.
- the pump would also be inclined depending on the posture of the automobile. If the pump is inclined, water would flow toward the lower position in the inclined state. Accordingly, depending on the posture of the automobile, water may remain in the pump chamber without being discharged through the discharge port.
- the root pump described in Japanese Laid-Open Patent Publication No. 8-109888 the residual water would freeze under a low temperature atmosphere and interfere with normal activation of the pump.
- the present invention provides a fluid compressor that ensures that water drawn into the pump chamber or condensed in the pump chamber is discharged out of the pump chamber through the discharge port.
- the compressor includes a pump chamber for drawing in fluid.
- the pump chamber includes a bottom part at which water in the pump chamber collects due to gravitational force when the compressor is horizontal.
- Two rotatable and parallel rotation shafts are arranged in the pump chamber.
- Two rotors are respectively fixed to the two rotary shafts. The rotors are rotated to compress the fluid in the pump chamber.
- a discharge port discharges the compressed fluid out of the pump chamber.
- the discharge port is located at a lowermost position in the bottom part of the pump chamber when a plane lying along the axes of the two rotary shafts is parallel to a horizontal plane or inclined by a predetermined angle relative to the horizontal plane.
- the pump chamber includes a guide surface for continuously connecting the bottom part partially or entirely to the discharge port.
- the guide surface is sloped downward so that water on the guide surface moves downward to the discharge port due to gravitational force when the discharge port is located at the lowermost portion in the bottom part of the pump chamber.
- a further aspect of the present invention is a compressor for compressing a fluid.
- the compressor includes a pump chamber for drawing in fluid.
- the pump chamber includes a bottom part at which water in the pump chamber collects due to gravitational force.
- the bottom part has a lowermost portion.
- a rotor is arranged in the pump chamber. The rotor is rotated to compress the fluid in the pump chamber.
- a discharge port located in the lowermost portion of the bottom part discharges the compressed fluid out of the pump chamber.
- the pump chamber includes a guide surface for continuously connecting the bottom part partially or entirely to the discharge port. The guide surface is sloped downward so that water on the guide surface moves downward to the discharge port due to gravitational force.
- FIG. 1 is a cross-sectional view showing a pump chamber of a fluid compressor in the prior art
- FIG. 2 is a cross-sectional plan view of a hydrogen compressor according to a preferred embodiment of the present invention
- FIG. 3 is a cross-sectional view taken along lone 3 - 3 in FIG. 2 ;
- FIG. 4 is a partial cross-sectional view taken along line 4 - 4 in FIG. 3 .
- the hydrogen compressor 10 is one type of fluid compressor that is used in a fuel cell system.
- the hydrogen compressor 10 includes a motor M and a root pump P.
- the motor M includes a motor housing 11 , which is cylindrical, and a partition wall 12 .
- the motor housing 11 has a closed first end (left end as viewed in FIG. 2 ) and an open second end (right end as viewed in FIG. 2 ).
- the partition wall 12 is coupled to the motor housing 11 so as to close the open second end of the motor housing 11 .
- a motor chamber 13 is defined by the inner surface of the motor housing 11 and the inner surface of the partition wall 12 .
- the pump P includes a pump housing 14 , which has the shape of a generally oval cylinder with a closed end, and a bearing block 16 .
- the pump housing 14 has an open first end (left end as viewed in FIG. 2 ).
- the bearing block 16 is fastened to the pump housing 14 by bolts 15 so as to close the open first end of the pump housing 14 .
- a pump chamber 17 is defined by the inner surface of the pump housing 14 and the inner surface of the bearing block 16 .
- a gear housing 18 which has the shape of a generally oval cylinder and which is smaller than the pump housing 14 , is coupled to the second end (right end as viewed in FIG. 2 ) of the pump housing 14 .
- a gear chamber 19 is defined by the outer surface of the second end of the pump housing 14 and the inner surface of the gear housing 18 .
- a fastener such as a bolt, fastens the partition wall 12 to the bearing block 16 . In other words, the fastener integrally fastens the motor M and the pump P to each other.
- O-rings 20 for ensuring hermetic seal are arranged in the surface joining the motor housing 11 and the partition wall 12 , the surface joining the pump housing 14 and the bearing block 16 , the surface joining the pump housing 14 and the gear housing 18 , and the surface joining the partition wall 12 and the bearing block 16 .
- a bearing 22 is arranged facing towards the motor chamber 13 on the end face 21 of the motor housing 11 in a manner concentric to the motor housing 11 .
- the bearing 22 rotatably supports a first end (left end as viewed in FIG. 2 ) of a drive shaft 23 , which functions as a rotation shaft.
- the drive shaft 23 extends through the partition wall 12 , the bearing block 16 , and the end face 24 of the pump housing 14 and into the gear chamber 19 .
- a bearing 25 is arranged on the end face 24 of the pump housing 14 .
- the bearing 25 rotatably supports a second end of the drive shaft 23 .
- a bearing 26 is arranged in the bearing block 16 .
- the bearing 26 rotatably supports a middle portion of the drive shaft 23 .
- a motor rotor 27 is fixed to the drive shaft 23 .
- a motor stator 28 is fixed to the motor housing 11 around the motor rotor 27 .
- the motor rotor 27 and the motor stator 28 form an electric motor 29 .
- a driven shaft 30 extends parallel to the drive shaft 23 in the pump chamber 17 of the pump P.
- the driven shaft 30 has a first end that is rotatably supported by a bearing 32 , which is arranged in the bearing block 16 .
- a second end of the driven shaft 30 is rotatably supported by a bearing 31 , which is arranged in the end face 24 of the pump housing 14 .
- a drive rotor 33 which is formed by two lobes, is fixed to the drive shaft 23 .
- a driven rotor 34 which is formed by two lobes, is fixed to the driven shaft 30 .
- the driven shaft 30 extends through the end face 24 of the pump housing 14 and into the gear chamber 19 .
- a drive gear 35 which is fixed to the second end of the drive shaft 23 , is meshed with a driven gear 36 , which is fixed to the second end of the driven shaft 30 .
- Seal rings 37 are arranged in the bearing block 16 and the end face 24 of the pump housing 14 at locations contacting the drive shaft 23 and the driven shaft 30 .
- a suction port 38 extends through the top of the pump housing 14 in the pump P. Hydrogen off gas discharged from a fuel cell V is drawn into the pump chamber 17 through the suction port 38 . Further, a discharge port 40 extends through the middle of a bottom part 39 of the pump chamber 17 . The hydrogen off gas compressed in the pump chamber 17 by rotation of the rotors 33 and 34 is discharged through the discharge port 40 . The rotors 33 and 34 are rotated so that their outermost portions define rotation paths R shown in FIG. 3 with a phase difference (90 degrees) between the drive shaft 23 and the driven shaft 30 .
- the rotors 33 and 34 that are rotated in this manner cooperate with the wall of the pump chamber 17 to compress the hydrogen off gas drawn into the pump chamber 17 .
- the wall of the pump chamber 17 includes a cooperation surface formed along the rotation paths R of the rotors 33 and 34 so that a slight clearance exists between the wall of the pump chamber 17 and the rotors 33 and 34 .
- An increase in the area of the cooperation surface improves the efficiency of the compressor.
- the cooperation surface at the upper part of the pump chamber 17 in the vicinity of the suction port 38 is gradually projected inward along the rotation paths R of the of the rotors 33 and 34 .
- the inner surface of the bottom part 39 in the pump chamber 17 is sloped downward toward the discharge port 40 in a generally conical manner, or in a generally funnel-shaped manner.
- the rotors 33 and 34 become closest to the bottom part 39 of the pump chamber 17 at proximal positions r.
- a downwardly sloped conical guide surface 41 is formed from the proximal positions r toward the edge 40 a of the discharge port 40 .
- the guide surface 41 is sloped from the proximal positions r to the discharge port 40 from every direction (radial direction about the discharge port 40 ) including the axial directions of the rotors 33 and 34 (the directions that the drive shaft 23 and the driven shaft 30 extend) and directions perpendicular to the axial directions. Accordingly, the edge 40 a of the discharge port 40 at the center of the conical guide surface 41 is located at the lowermost portion (deepest portion) of the bottom part 39 . More specifically, the bottom part 39 of the pump chamber 17 includes the guide surface 41 , which is sloped outward in the pump housing 14 . In the bottom part 39 , the discharge port 40 is formed at the lowermost portion of the guide surface 41 .
- the guide surface 41 has a cross-section generally shaped in correspondence with part of an ellipse or part of an ellipsoid.
- the discharge port 40 is located at a position where the minor axis of the ellipse and the circumference of the ellipse intersect or at a position located along the direction of the minor axis that extends from the center of the ellipsoid.
- the electric motor 29 is driven to rotate the drive shaft 23 .
- the meshing engagement of the drive gear 35 and the driven gear 36 rotates the driven shaft 30 with the predetermined phase difference from the drive shaft 23 .
- the drive rotor 33 and the driven rotor 34 are synchronously rotated in the pump chamber 17 in the directions indicated by the arrows in FIG. 3 .
- the synchronous rotation of the two rotors 33 and 34 draws the hydrogen off gas discharged from the fuel cell V into the pump chamber 17 .
- the hydrogen off gas is compressed by the rotation of the rotors 33 and 34 and delivered toward the bottom part 39 to be discharged out of the pump chamber 17 from the discharge port 40 , which is located at the lowermost portion of the bottom part 39 .
- the hydrogen off gas drawn into the pump chamber 17 may include water that is produced in the fuel cell V. Accordingly, the hydrogen compressor 10 may draw water into the pump chamber 17 together with the hydrogen off gas. Further, the humidity of the hydrogen off gas may high. In this case, changes in the dew point may condense the water in the hydrogen off gas.
- the hydrogen compressor 10 When the hydrogen compressor 10 is left in a low temperature atmosphere in a state in which water (condensed water) remains in the pump chamber 17 , the residual water may freeze and hinder activation of the hydrogen compressor 10 .
- the first embodiment avoids the occurrence of such a state in a preferable manner.
- the water drawn into the pump chamber 17 collects at the bottom part 39 of the pump chamber 17 due to gravitational force or the rotation of the rotors 33 and 34 .
- the water flows along the downwardly sloped guide surface 41 to the discharge port 40 .
- the discharge port 40 is located at the lowermost portion of the bottom part 39 in the pump chamber 17 .
- the guide surface 41 guides the water collected on the bottom part 39 to the edge 40 a of the discharge port 40 .
- the water that reaches the edge 40 a of the discharge port 40 is discharged out of the pump chamber 17 through the discharge port 40 . Accordingly, water does not remain in the pump chamber 17 .
- the hydrogen compressor 10 may be installed as a compressor for a fuel cell system of an electric automobile.
- the hydrogen compressor 10 may be inclined when, for example, the vehicle is parked on a sloped road.
- the downwardly sloped, conical guide surface 41 extending about the discharge port 40 guides the water collected on the bottom part 39 of the pump chamber 17 to the discharge port 40 . This ensures that the water is discharged out of the pump chamber 17 from the discharge port 40 . Accordingly, the hydrogen compressor 10 prevents water from remaining in the pump chamber 17 .
- the pump chamber 17 into which the hydrogen off gas is drawn in.
- the pump chamber 17 includes the bottom part 39 at which water in the pump chamber 17 collects due to gravitational force.
- the rotors 33 and 34 arranged in the pump chamber 17 are rotated to compress the hydrogen off gas in the pump chamber 17 .
- the discharge port 40 located in the lowermost portion of the bottom part 39 discharges the compressed hydrogen off gas out of the pump chamber 17 .
- the pump chamber 17 includes a guide surface 41 for continuously connecting the bottom part 39 to the discharge port 40 .
- the guide surface 40 is sloped downward so that water on the guide surface 40 moves downward to the discharge port 40 due to gravitational force.
- the hydrogen compressor 10 of the preferred embodiment has the advantages described below.
- the hydrogen compressor 10 In the hydrogen compressor 10 , the water drawn into the pump chamber 17 is guided along the downwardly sloped guide surface 41 toward the discharge port 40 , which is formed at the lowermost portion of the bottom part 39 in the pump chamber 17 . The hydrogen compressor 10 then discharges the water together with compressed hydrogen off gas out of the pump chamber 17 through the discharge port 40 . Accordingly, in the hydrogen compressor 10 , water does not remain in the pump chamber 17 . This prevents residual water from freezing and hindering activation of the hydrogen compressor 10 .
- the guide surface 41 is conical and downwardly sloped toward the discharge port 40 about the discharge port 40 from every direction about the discharge port 40 .
- the guide surface 41 guides water to the discharge port 40 from any direction. Accordingly, the hydrogen compressor 10 discharges water out of the pump chamber 17 through the discharge port 40 even if the hydrogen compressor 10 is inclined when it is installed in a vehicle or when it is movable.
- the discharge port 40 is formed in the middle of the bottom part 39 of the pump chamber 17 .
- the conical guide surface 41 is easily formed.
- the guide surface 41 is downwardly sloped from the proximal positions r toward the edge of the discharge port 40 . That is, the guide surface 41 is downwardly sloped and smoothly connected to the discharge port 40 from the proximal positions r, which are the lowermost positions of the arcuate surface of the pump chamber 17 along the rotation path R of the rotors 33 and 34 . Accordingly, the guide surface 41 smoothly guides the water in the pump chamber 17 to the discharge port 40 .
- the rotors 33 and 34 and the wall of the pump chamber 17 cooperate to start enclosing hydrogen gas at a timing that is earlier than the timing at which the rotors 33 and 34 become vertical in the pump chamber 17 (more specifically, at a timing in which the rotors 33 and 34 pass by the end of the suction port 38 ). Accordingly, the compression efficiency remains the same.
- the hydrogen compressor 10 may be configured as mentioned below.
- the hydrogen compressor 10 (fluid compressor) includes the pump chamber 17 into which hydrogen off gas (fluid) is drawn in.
- the pump chamber 17 includes the bottom part 39 at which water in the pump chamber 17 collects due to gravitational force when the compressor 10 is horizontal.
- the two rotatable and parallel shafts 23 and 30 are arranged in the pump chamber 17 .
- the two rotors 33 and 34 respectively fixed to the two shafts 23 and 30 are rotated to compress the hydrogen off gas in the pump chamber 17 .
- the discharge port 40 discharges the compressed hydrogen off gas out of the pump chamber 17 .
- the discharge port 40 is located at a lowermost position in the bottom part 39 of the pump chamber 17 when a plane lying along the axes of the two shafts 23 and 30 is parallel to a horizontal plane or inclined by a predetermined angle relative to the horizontal plane.
- the pump chamber 17 includes the guide surface 41 for continuously connecting the bottom part 39 to the discharge port 40 .
- the guide surface 41 is sloped downward so that water on the guide surface 41 moves downward to the discharge port 40 due to gravitational force when the discharge port 40 is located at the lowermost portion in the bottom part 39 of the pump chamber 17 .
- the guide surface 41 may be downwardly sloped only in the axial direction of the rotors 33 and 34 (the direction in which the drive shaft 23 and driven shaft 30 extend).
- the hydrogen compressor 10 is installed in an automobile so that the rotation shaft (e.g., drive shaft 23 ) is parallel to the longitudinal direction of the automobile.
- the hydrogen compressor 10 discharges water out of the pump chamber 17 through the discharge port 40 in a satisfactory manner.
- the guide surface 41 may be downwardly sloped only in the direction perpendicular to the axial direction of the rotors 33 and 34 (the direction in which the drive shaft 23 and driven shaft 30 extend).
- the hydrogen compressor 10 is installed in an automobile so that the rotation shaft (e.g., drive shaft 23 ) is parallel to the longitudinal direction of the automobile.
- the hydrogen compressor 10 discharges water out of the pump chamber 17 through the discharge port 40 in a satisfactory manner.
- the guide surface 41 may be downwardly sloped in the axial direction of the rotors 33 and 34 (the direction in which the drive shaft 23 and driven shaft 30 extend) and the direction perpendicular to the axial direction (i.e., only in two directions).
- a groove having a bottom surface, which is downwardly sloped to and connected to the discharge port 40 , may be formed in the bottom part 39 of the pump chamber 17 .
- the bottom surface of the groove functions as the guide surface.
- more than one groove may radially extend from the discharge port 40 .
- the guide surface 41 has a cross-section generally shaped in correspondence with part of an ellipse or part of an ellipsoid.
- the discharge port 40 is located at a position where the minor axis of the ellipse and the circumference of the ellipse intersect or located at a position along the direction of the minor axis that extends from the axis of the ellipsoid.
- the discharge port 40 may be located in the vicinity of where the minor axis of the ellipse and the circumference of the ellipse intersect or in the vicinity of a position located along the direction of the minor axis that extends from the axis of the ellipsoid.
- the compressor 10 includes the two shafts 23 and 30 and two rotors 33 and 34 .
- the compressor may include more than two shafts and more than two rotors.
- the present invention is embodied in a hydrogen compressor 10 , which forcibly circulates hydrogen off gas in a fuel cell system.
- the present invention may be embodied in an air compressor.
- the present invention may be embodied in a fluid compressor other than one used for a fuel cell system.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
- Fuel Cell (AREA)
Abstract
A fluid compressor that ensures the discharge of water from a discharge port when water is drawn into or condensed in a pump chamber. The compressor includes a pump chamber for drawing in fluid. The pump chamber includes a bottom part located in a lower portion of the pump chamber. Two rotors arranged in the pump chamber are rotated to compress the fluid in the pump chamber. A discharge port located in the bottom part discharges the compressed fluid out of the pump chamber. The bottom part defines a guide surface formed continuously from the discharge port. The guide surface is sloped downward so that water on the guide surface moves downward to the discharge port due to gravitational force.
Description
- The present invention relates to a compressor, and more particularly, to a compressor for compressing fluid drawn into a pump chamber by rotating a rotor and discharging the fluid out of the pump chamber through a discharge port.
- A compressor that compresses fluid, or a fluid compressor, may be used in, for example, a fuel cell system. A fuel cell uses hydrogen gas and an oxidizer gas to generate electric power. The fuel cell produces water when generating power. To discharge the water out of the fuel cell, more hydrogen gas and oxidizer gas than the amount of hydrogen gas and oxidizer gas consumed to generate power must be supplied to the fuel cell. Further, the fuel cell discharges hydrogen gas (i.e., hydrogen off gas), which includes hydrogen gas that was not subject to reaction. The discharge of such hydrogen gas lowers fuel efficiency. To improve fuel efficiency, a typical compressor positively circulates the hydrogen off gas and mixes the hydrogen off gas with fresh hydrogen gas to return the hydrogen off gas to the fuel cell.
FIG. 1 shows an example of such a compressor. - As shown in
FIG. 1 , afluid compressor 51 has acase 52, which has the shape of a generally oval cylinder. Apump chamber 53 is defined in thecase 52. Hydrogen off gas is drawn into thepump chamber 53 to be compressed. Two parallel rotation shafts (drive shaft 54 and driven shaft 55) are supported in thepump chamber 53. Two 56 and 57 are respectively fixed to therotors drive shaft 54 and the drivenshaft 55. A driver, such as a motor, drives thedrive shaft 54 and the drivenshaft 55 to rotate the 56 and 57 with a predetermined interval (phase difference) therebetween. As a result, hydrogen off gas is drawn into therotors pump chamber 53 through asuction port 58, which is located at the upper part of the pump chamber, and discharged out of thepump chamber 53 through adischarge port 59, which is located at the lower part of thepump chamber 53. The wall of thepump chamber 53 is shaped to form two hollow cylindrical portions connected to each other so that the 56 and 57 rotate along the wall. More specifically, the lower middle part of therotors pump chamber 53 is projected upward as viewed inFIG. 1 . Thedischarge port 59 is formed in the upwardly projecting, lower part of thepump chamber 53. Arecess 60 is formed in each side of thedischarge port 59. - As described above, when a fuel cell generates electric power, water is produced and discharged together with hydrogen off gas. Accordingly, water is also drawn into the
pump chamber 53 in addition to hydrogen off gas. The hydrogen off gas may be supplied to thefluid compressor 51 via a gas-liquid separator. In such a case, however, the humidity of the hydrogen off gas would be high. Thus, when thefluid compressor 51 is in a low temperature atmosphere, the moisture in the hydrogen off gas condenses as the dew point changes and produces water in thepump chamber 53. Such water remains in therecess 60 of thepump chamber 53. If thefluid compressor 51 is left in such a state under a low temperature for a long period of time, the residual water in thefluid compressor 51 would freeze. Activation of the fuel cell when water is frozen in such a manner would interfere with normal activation of the fuel cell. For example, abnormal current may flow through a motor that drives thefluid compressor 51. - The above describes only one example of such problem. This problem may occur in any system in which liquid collects in a pump chamber.
- Japanese Laid-Open Patent Publication No. 8-109089 describes a root pump (one type of a fluid compressor) that solves the above problem. The root pump has a suction port formed in the upper part of a case and a discharge port formed in the lower part of the case. The vicinity of the discharge port in the lower part of the case is flat. That is, recesses are not formed in the lower part of the pump chamber. Accordingly, the root pump discharges from the discharge port the water drawn into and the water condensed in the pump chamber so that water does not remain in the pump chamber.
- However, the root pump also has a shortcoming. A root pump is used for various purposes, such as a movable pump or as a pump for use in a vehicle. With regard to vehicle pumps, an automobile is driven (or parked) along sloped roads in addition to level roads. Thus, the pump would also be inclined depending on the posture of the automobile. If the pump is inclined, water would flow toward the lower position in the inclined state. Accordingly, depending on the posture of the automobile, water may remain in the pump chamber without being discharged through the discharge port. As a result, in the root pump described in Japanese Laid-Open Patent Publication No. 8-109888, the residual water would freeze under a low temperature atmosphere and interfere with normal activation of the pump.
- The present invention provides a fluid compressor that ensures that water drawn into the pump chamber or condensed in the pump chamber is discharged out of the pump chamber through the discharge port.
- One aspect of the present invention is a compressor for compressing a fluid. The compressor includes a pump chamber for drawing in fluid. The pump chamber includes a bottom part at which water in the pump chamber collects due to gravitational force when the compressor is horizontal. Two rotatable and parallel rotation shafts are arranged in the pump chamber. Two rotors are respectively fixed to the two rotary shafts. The rotors are rotated to compress the fluid in the pump chamber. A discharge port discharges the compressed fluid out of the pump chamber. The discharge port is located at a lowermost position in the bottom part of the pump chamber when a plane lying along the axes of the two rotary shafts is parallel to a horizontal plane or inclined by a predetermined angle relative to the horizontal plane. The pump chamber includes a guide surface for continuously connecting the bottom part partially or entirely to the discharge port. The guide surface is sloped downward so that water on the guide surface moves downward to the discharge port due to gravitational force when the discharge port is located at the lowermost portion in the bottom part of the pump chamber.
- A further aspect of the present invention is a compressor for compressing a fluid. The compressor includes a pump chamber for drawing in fluid. The pump chamber includes a bottom part at which water in the pump chamber collects due to gravitational force. The bottom part has a lowermost portion. A rotor is arranged in the pump chamber. The rotor is rotated to compress the fluid in the pump chamber. A discharge port located in the lowermost portion of the bottom part discharges the compressed fluid out of the pump chamber. The pump chamber includes a guide surface for continuously connecting the bottom part partially or entirely to the discharge port. The guide surface is sloped downward so that water on the guide surface moves downward to the discharge port due to gravitational force.
- Other aspects and advantages of the present invention will become apparent from the following description, taken in conjunction with the accompanying drawings, illustrating by way of example the principles of the invention.
- The invention, together with objects and advantages thereof, may best be understood by reference to the following description of the presently preferred embodiments together with the accompanying drawings in which:
-
FIG. 1 is a cross-sectional view showing a pump chamber of a fluid compressor in the prior art; -
FIG. 2 is a cross-sectional plan view of a hydrogen compressor according to a preferred embodiment of the present invention; -
FIG. 3 is a cross-sectional view taken along lone 3-3 inFIG. 2 ; and -
FIG. 4 is a partial cross-sectional view taken along line 4-4 inFIG. 3 . - A
hydrogen compressor 10 according to a preferred embodiment of the present invention will now be described with reference to FIGS. 2 to 4. Thehydrogen compressor 10 is one type of fluid compressor that is used in a fuel cell system. - Referring to
FIG. 2 , in the preferred embodiment, thehydrogen compressor 10 includes a motor M and a root pump P. The motor M includes amotor housing 11, which is cylindrical, and apartition wall 12. Themotor housing 11 has a closed first end (left end as viewed inFIG. 2 ) and an open second end (right end as viewed inFIG. 2 ). Thepartition wall 12 is coupled to themotor housing 11 so as to close the open second end of themotor housing 11. Amotor chamber 13 is defined by the inner surface of themotor housing 11 and the inner surface of thepartition wall 12. The pump P includes apump housing 14, which has the shape of a generally oval cylinder with a closed end, and abearing block 16. Thepump housing 14 has an open first end (left end as viewed inFIG. 2 ). The bearingblock 16 is fastened to thepump housing 14 by bolts 15 so as to close the open first end of thepump housing 14. Apump chamber 17 is defined by the inner surface of thepump housing 14 and the inner surface of thebearing block 16. - In the pump P, a
gear housing 18, which has the shape of a generally oval cylinder and which is smaller than thepump housing 14, is coupled to the second end (right end as viewed inFIG. 2 ) of thepump housing 14. Agear chamber 19 is defined by the outer surface of the second end of thepump housing 14 and the inner surface of thegear housing 18. A fastener, such as a bolt, fastens thepartition wall 12 to thebearing block 16. In other words, the fastener integrally fastens the motor M and the pump P to each other. O-rings 20 for ensuring hermetic seal are arranged in the surface joining themotor housing 11 and thepartition wall 12, the surface joining thepump housing 14 and thebearing block 16, the surface joining thepump housing 14 and thegear housing 18, and the surface joining thepartition wall 12 and thebearing block 16. - A
bearing 22 is arranged facing towards themotor chamber 13 on theend face 21 of themotor housing 11 in a manner concentric to themotor housing 11. The bearing 22 rotatably supports a first end (left end as viewed inFIG. 2 ) of adrive shaft 23, which functions as a rotation shaft. Thedrive shaft 23 extends through thepartition wall 12, the bearingblock 16, and theend face 24 of thepump housing 14 and into thegear chamber 19. A bearing 25 is arranged on theend face 24 of thepump housing 14. The bearing 25 rotatably supports a second end of thedrive shaft 23. Abearing 26 is arranged in thebearing block 16. The bearing 26 rotatably supports a middle portion of thedrive shaft 23. Amotor rotor 27 is fixed to thedrive shaft 23. Amotor stator 28 is fixed to themotor housing 11 around themotor rotor 27. Themotor rotor 27 and themotor stator 28 form anelectric motor 29. - A driven shaft 30 (rotation shaft) extends parallel to the
drive shaft 23 in thepump chamber 17 of the pump P. The drivenshaft 30 has a first end that is rotatably supported by a bearing 32, which is arranged in thebearing block 16. A second end of the drivenshaft 30 is rotatably supported by abearing 31, which is arranged in theend face 24 of thepump housing 14. Adrive rotor 33, which is formed by two lobes, is fixed to thedrive shaft 23. A drivenrotor 34, which is formed by two lobes, is fixed to the drivenshaft 30. In the same manner as thedrive shaft 23, the drivenshaft 30 extends through theend face 24 of thepump housing 14 and into thegear chamber 19. In thegear chamber 19, adrive gear 35, which is fixed to the second end of thedrive shaft 23, is meshed with a drivengear 36, which is fixed to the second end of the drivenshaft 30. Seal rings 37 are arranged in thebearing block 16 and theend face 24 of thepump housing 14 at locations contacting thedrive shaft 23 and the drivenshaft 30. - The internal structure of the
pump chamber 17 in the pump P will now be described. - As viewed in
FIG. 3 , asuction port 38 extends through the top of thepump housing 14 in the pump P. Hydrogen off gas discharged from a fuel cell V is drawn into thepump chamber 17 through thesuction port 38. Further, adischarge port 40 extends through the middle of abottom part 39 of thepump chamber 17. The hydrogen off gas compressed in thepump chamber 17 by rotation of the 33 and 34 is discharged through therotors discharge port 40. The 33 and 34 are rotated so that their outermost portions define rotation paths R shown inrotors FIG. 3 with a phase difference (90 degrees) between thedrive shaft 23 and the drivenshaft 30. The 33 and 34 that are rotated in this manner cooperate with the wall of therotors pump chamber 17 to compress the hydrogen off gas drawn into thepump chamber 17. The wall of thepump chamber 17 includes a cooperation surface formed along the rotation paths R of the 33 and 34 so that a slight clearance exists between the wall of therotors pump chamber 17 and the 33 and 34. An increase in the area of the cooperation surface improves the efficiency of the compressor. Thus, the cooperation surface at the upper part of therotors pump chamber 17 in the vicinity of thesuction port 38 is gradually projected inward along the rotation paths R of the of the 33 and 34.rotors - The inner surface of the
bottom part 39 in thepump chamber 17 is sloped downward toward thedischarge port 40 in a generally conical manner, or in a generally funnel-shaped manner. Like the drivenrotor 34 shown inFIG. 3 , when each of the 33 and 34 are arranged in a vertical state in therotors pump chamber 17, the 33 and 34 become closest to therotors bottom part 39 of thepump chamber 17 at proximal positions r. A downwardly slopedconical guide surface 41 is formed from the proximal positions r toward theedge 40 a of thedischarge port 40. Theguide surface 41 is sloped from the proximal positions r to thedischarge port 40 from every direction (radial direction about the discharge port 40) including the axial directions of therotors 33 and 34 (the directions that thedrive shaft 23 and the drivenshaft 30 extend) and directions perpendicular to the axial directions. Accordingly, theedge 40 a of thedischarge port 40 at the center of theconical guide surface 41 is located at the lowermost portion (deepest portion) of thebottom part 39. More specifically, thebottom part 39 of thepump chamber 17 includes theguide surface 41, which is sloped outward in thepump housing 14. In thebottom part 39, thedischarge port 40 is formed at the lowermost portion of theguide surface 41. - In other words, the
guide surface 41 has a cross-section generally shaped in correspondence with part of an ellipse or part of an ellipsoid. Thedischarge port 40 is located at a position where the minor axis of the ellipse and the circumference of the ellipse intersect or at a position located along the direction of the minor axis that extends from the center of the ellipsoid. - The operation of the hydrogen compressor 10 (fluid compressor) when water flows out of the
pump chamber 17 from thedischarge port 40 will now be discussed. - First, the
electric motor 29 is driven to rotate thedrive shaft 23. As a result, the meshing engagement of thedrive gear 35 and the drivengear 36 rotates the drivenshaft 30 with the predetermined phase difference from thedrive shaft 23. Accordingly, thedrive rotor 33 and the drivenrotor 34 are synchronously rotated in thepump chamber 17 in the directions indicated by the arrows in FIG. 3. The synchronous rotation of the two 33 and 34 draws the hydrogen off gas discharged from the fuel cell V into therotors pump chamber 17. Further, the hydrogen off gas is compressed by the rotation of the 33 and 34 and delivered toward therotors bottom part 39 to be discharged out of thepump chamber 17 from thedischarge port 40, which is located at the lowermost portion of thebottom part 39. - As described above, the hydrogen off gas drawn into the
pump chamber 17 may include water that is produced in the fuel cell V. Accordingly, thehydrogen compressor 10 may draw water into thepump chamber 17 together with the hydrogen off gas. Further, the humidity of the hydrogen off gas may high. In this case, changes in the dew point may condense the water in the hydrogen off gas. When thehydrogen compressor 10 is left in a low temperature atmosphere in a state in which water (condensed water) remains in thepump chamber 17, the residual water may freeze and hinder activation of thehydrogen compressor 10. However, the first embodiment avoids the occurrence of such a state in a preferable manner. - The water drawn into the
pump chamber 17 collects at thebottom part 39 of thepump chamber 17 due to gravitational force or the rotation of the 33 and 34. At therotors bottom part 39, the water flows along the downwardly slopedguide surface 41 to thedischarge port 40. Thedischarge port 40 is located at the lowermost portion of thebottom part 39 in thepump chamber 17. Thus, theguide surface 41 guides the water collected on thebottom part 39 to theedge 40 a of thedischarge port 40. Then, the water that reaches theedge 40 a of thedischarge port 40 is discharged out of thepump chamber 17 through thedischarge port 40. Accordingly, water does not remain in thepump chamber 17. - The
hydrogen compressor 10 may be installed as a compressor for a fuel cell system of an electric automobile. In such a case, thehydrogen compressor 10 may be inclined when, for example, the vehicle is parked on a sloped road. However, with thehydrogen compressor 10, the downwardly sloped,conical guide surface 41 extending about thedischarge port 40 guides the water collected on thebottom part 39 of thepump chamber 17 to thedischarge port 40. This ensures that the water is discharged out of thepump chamber 17 from thedischarge port 40. Accordingly, thehydrogen compressor 10 prevents water from remaining in thepump chamber 17. - As mentioned above, in the
hydrogen compressor 10, thepump chamber 17 into which the hydrogen off gas is drawn in. Thepump chamber 17 includes thebottom part 39 at which water in thepump chamber 17 collects due to gravitational force. The 33 and 34 arranged in therotors pump chamber 17 are rotated to compress the hydrogen off gas in thepump chamber 17. Thedischarge port 40 located in the lowermost portion of thebottom part 39 discharges the compressed hydrogen off gas out of thepump chamber 17. Thepump chamber 17 includes aguide surface 41 for continuously connecting thebottom part 39 to thedischarge port 40. Theguide surface 40 is sloped downward so that water on theguide surface 40 moves downward to thedischarge port 40 due to gravitational force. Thus, when the water in thepump chamber 17 collects at thebottom part 39 due to gravitational force, the water is guided in the downward sloping direction of theguide surface 41, which is continuous with thedischarge port 40, to thedischarge port 40, which is located at the lowermost portion of thebottom part 39. This ensures that the water flows out of thepump chamber 17 from thedischarge port 40. Accordingly, there is no residual water in thepump chamber 17. - The
hydrogen compressor 10 of the preferred embodiment has the advantages described below. - (1) In the
hydrogen compressor 10, the water drawn into thepump chamber 17 is guided along the downwardly slopedguide surface 41 toward thedischarge port 40, which is formed at the lowermost portion of thebottom part 39 in thepump chamber 17. Thehydrogen compressor 10 then discharges the water together with compressed hydrogen off gas out of thepump chamber 17 through thedischarge port 40. Accordingly, in thehydrogen compressor 10, water does not remain in thepump chamber 17. This prevents residual water from freezing and hindering activation of thehydrogen compressor 10. - (2) The
guide surface 41 is conical and downwardly sloped toward thedischarge port 40 about thedischarge port 40 from every direction about thedischarge port 40. Thus, even if thehydrogen compressor 10 is inclined, theguide surface 41 guides water to thedischarge port 40 from any direction. Accordingly, thehydrogen compressor 10 discharges water out of thepump chamber 17 through thedischarge port 40 even if thehydrogen compressor 10 is inclined when it is installed in a vehicle or when it is movable. - (3) The
discharge port 40 is formed in the middle of thebottom part 39 of thepump chamber 17. Thus, theconical guide surface 41 is easily formed. - (4) The
guide surface 41 is downwardly sloped from the proximal positions r toward the edge of thedischarge port 40. That is, theguide surface 41 is downwardly sloped and smoothly connected to thedischarge port 40 from the proximal positions r, which are the lowermost positions of the arcuate surface of thepump chamber 17 along the rotation path R of the 33 and 34. Accordingly, therotors guide surface 41 smoothly guides the water in thepump chamber 17 to thedischarge port 40. Further, the 33 and 34 and the wall of therotors pump chamber 17 cooperate to start enclosing hydrogen gas at a timing that is earlier than the timing at which the 33 and 34 become vertical in the pump chamber 17 (more specifically, at a timing in which therotors 33 and 34 pass by the end of the suction port 38). Accordingly, the compression efficiency remains the same.rotors - It should be apparent to those skilled in the art that the present invention may be embodied in many other specific forms without departing from the spirit or scope of the invention. Particularly, it should be understood that the present invention may be embodied in the following forms.
- The
hydrogen compressor 10 may be configured as mentioned below. The hydrogen compressor 10 (fluid compressor) includes thepump chamber 17 into which hydrogen off gas (fluid) is drawn in. Thepump chamber 17 includes thebottom part 39 at which water in thepump chamber 17 collects due to gravitational force when thecompressor 10 is horizontal. The two rotatable and 23 and 30 are arranged in theparallel shafts pump chamber 17. The two 33 and 34 respectively fixed to the tworotors 23 and 30 are rotated to compress the hydrogen off gas in theshafts pump chamber 17. Thedischarge port 40 discharges the compressed hydrogen off gas out of thepump chamber 17. Thedischarge port 40 is located at a lowermost position in thebottom part 39 of thepump chamber 17 when a plane lying along the axes of the two 23 and 30 is parallel to a horizontal plane or inclined by a predetermined angle relative to the horizontal plane. Theshafts pump chamber 17 includes theguide surface 41 for continuously connecting thebottom part 39 to thedischarge port 40. Theguide surface 41 is sloped downward so that water on theguide surface 41 moves downward to thedischarge port 40 due to gravitational force when thedischarge port 40 is located at the lowermost portion in thebottom part 39 of thepump chamber 17. - The
guide surface 41 may be downwardly sloped only in the axial direction of therotors 33 and 34 (the direction in which thedrive shaft 23 and drivenshaft 30 extend). In such a case, for example, thehydrogen compressor 10 is installed in an automobile so that the rotation shaft (e.g., drive shaft 23) is parallel to the longitudinal direction of the automobile. Thus, when the automobile is driven or stopped (parked) on a sloped road, thehydrogen compressor 10 discharges water out of thepump chamber 17 through thedischarge port 40 in a satisfactory manner. - The
guide surface 41 may be downwardly sloped only in the direction perpendicular to the axial direction of therotors 33 and 34 (the direction in which thedrive shaft 23 and drivenshaft 30 extend). In such a case, for example, thehydrogen compressor 10 is installed in an automobile so that the rotation shaft (e.g., drive shaft 23) is parallel to the longitudinal direction of the automobile. Thus, when the automobile sways sideward when driven, thehydrogen compressor 10 discharges water out of thepump chamber 17 through thedischarge port 40 in a satisfactory manner. - The
guide surface 41 may be downwardly sloped in the axial direction of therotors 33 and 34 (the direction in which thedrive shaft 23 and drivenshaft 30 extend) and the direction perpendicular to the axial direction (i.e., only in two directions). - A groove having a bottom surface, which is downwardly sloped to and connected to the
discharge port 40, may be formed in thebottom part 39 of thepump chamber 17. In this case, the bottom surface of the groove functions as the guide surface. Further, more than one groove may radially extend from thedischarge port 40. - In the preferred embodiment, the
guide surface 41 has a cross-section generally shaped in correspondence with part of an ellipse or part of an ellipsoid. Further, thedischarge port 40 is located at a position where the minor axis of the ellipse and the circumference of the ellipse intersect or located at a position along the direction of the minor axis that extends from the axis of the ellipsoid. Instead, thedischarge port 40 may be located in the vicinity of where the minor axis of the ellipse and the circumference of the ellipse intersect or in the vicinity of a position located along the direction of the minor axis that extends from the axis of the ellipsoid. - In the preferred embodiment, the
compressor 10 includes the two 23 and 30 and twoshafts 33 and 34. Alternatively, the compressor may include more than two shafts and more than two rotors.rotors - In the preferred embodiment, the present invention is embodied in a
hydrogen compressor 10, which forcibly circulates hydrogen off gas in a fuel cell system. Instead, the present invention may be embodied in an air compressor. Alternatively, the present invention may be embodied in a fluid compressor other than one used for a fuel cell system. - The present examples and embodiments are to be considered as illustrative and not restrictive, and the invention is not to be limited to the details given herein, but may be modified within the scope and equivalence of the appended claims.
Claims (10)
1. A compressor for compressing a fluid, the compressor comprising:
a pump chamber for drawing in fluid, the pump chamber including a bottom part located in a lower portion of the pump chamber with respect to the gravitational direction in a normal installation state of the compressor;
two parallel rotation shafts arranged in the pump chamber;
two rotors respectively fixed to the two rotary shafts, the rotors being rotated to compress the fluid in the pump chamber; and
a discharge port for discharging the compressed fluid out of the pump chamber, the discharge port located at a lowermost position in the pump chamber when a plane including the axes of the two rotary shafts is substantially lies along a horizontal plane or is inclined by a predetermined angle relative to the horizontal plane;
wherein the bottom part partially or entirely defines a guide surface formed continuously from the discharge port, the guide surface being sloped downward so that water on the guide surface moves downward to the discharge port due to gravitational force when the discharge port is located at the lowermost portion in the bottom part of the pump chamber.
2. The compressor according to claim 1 , wherein the guide surface is generally funnel-shaped so that the discharge port is located at the bottom of the guide surface.
3. The compressor according to claim 1 , wherein the rotors rotate along a rotation path, and the guide surface is shaped differently from the rotation path.
4. The compressor according to claim 1 , wherein the guide surface has a cross-section generally shaped in correspondence with part of an ellipse, and the discharge port is located at a position where the minor axis and circumference of the ellipse intersect or in the vicinity of the position where the minor axis and circumference of the ellipse intersect.
5. The compressor according to claim 1 , wherein the guide surface has a cross-section generally shaped in correspondence with part of an ellipsoid, and the discharge port is located at a position along the direction of the minor axis that extends from the center of the ellipsoid or in the vicinity of the position along the direction of the minor axis that extends from the center of the ellipsoid.
6. A compressor for compressing a fluid, the compressor comprising:
a pump chamber for drawing in fluid, the pump chamber including a bottom part located in a lower portion of the pump chamber;
a rotor arranged in the pump chamber, the rotor being rotated to compress the fluid in the pump chamber; and
a discharge port, located in the bottom part, for discharging the compressed fluid out of the pump chamber;
wherein the bottom part partially or entirely defines a guide surface formed continuously from the discharge port, the guide surface being sloped downward so that water on the guide surface moves downward to the discharge port due to gravitational force.
7. The compressor according to claim 6 , wherein the guide surface is generally funnel-shaped so that the discharge port is located at the bottom of the guide surface.
8. The compressor according to claim 6 , wherein the rotors rotate along a rotation path, and the guide surface is shaped differently from the rotation path.
9. The compressor according to claim 6 , wherein the guide surface has a cross-section generally shaped in correspondence with part of an ellipse, and the discharge port is located at a position where the minor axis and circumference of the ellipse intersect or in the vicinity of the position where the minor axis and circumference of the ellipse intersect.
10. The compressor according to claim 6 , wherein the guide surface has a cross-section generally shaped in correspondence with part of an ellipsoid, and the discharge port is located at a position along the direction of the minor axis that extends from the center of the ellipsoid or in the vicinity of the position along the direction of the minor axis that extends from the center of the ellipsoid.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2003394414 | 2003-11-25 | ||
| JP2003-394414 | 2003-11-25 | ||
| JP2004333357A JP2005180421A (en) | 2003-11-25 | 2004-11-17 | Fluid compressor |
| JP2004-333357 | 2004-11-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20050112014A1 true US20050112014A1 (en) | 2005-05-26 |
Family
ID=34594001
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/996,585 Abandoned US20050112014A1 (en) | 2003-11-25 | 2004-11-24 | Fluid compressor |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20050112014A1 (en) |
| JP (1) | JP2005180421A (en) |
| DE (1) | DE102004056744A1 (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070217939A1 (en) * | 2006-03-20 | 2007-09-20 | Kazuho Sato | Gas-compression module for a fuel cell |
| US20080304981A1 (en) * | 2007-06-08 | 2008-12-11 | Jaguar Precision Industry Co., Ltd. | Motor direct drive air pump and related applications thereof |
| WO2009112178A1 (en) | 2008-03-11 | 2009-09-17 | Daimler Ag | Method and device for operating a fuel cell system with a recirculation blower arranged in a fuel circuit of the fuel cell system |
| WO2010143031A3 (en) * | 2009-06-10 | 2011-05-12 | Toyota Jidosha Kabushiki Kaisha | Fluid compressor and fuel cell vehicle |
| US20110236232A1 (en) * | 2009-04-20 | 2011-09-29 | Yi-Lin Chu | Air compression device |
| CN103375404A (en) * | 2012-04-30 | 2013-10-30 | 伊顿公司 | Positive displacement pump assembly with movable end plate for rotor face clearance control |
| US20180301722A1 (en) * | 2017-04-18 | 2018-10-18 | Toyota Jidosha Kabushiki Kaisha | Fuel cell system |
| CN111022323A (en) * | 2019-12-26 | 2020-04-17 | 烟台菱辰能源有限公司 | A hydrogen circulation pump with an anti-icing structure |
| USD941360S1 (en) | 2019-01-31 | 2022-01-18 | Elliott Company | Oval steam turbine casing |
| US20230258179A1 (en) * | 2020-09-02 | 2023-08-17 | Eaton Intelligent Power Limited | Rear drive egr pump |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4677892B2 (en) | 2005-12-07 | 2011-04-27 | トヨタ自動車株式会社 | Roots type pump and fuel cell system |
| JP4893072B2 (en) * | 2006-04-05 | 2012-03-07 | トヨタ自動車株式会社 | pump |
| KR101292410B1 (en) | 2007-05-31 | 2013-08-01 | 한라비스테온공조 주식회사 | Air compressor and expander |
| DE102021105044A1 (en) | 2021-03-03 | 2022-09-08 | Audi Aktiengesellschaft | ejector |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US905967A (en) * | 1907-04-16 | 1908-12-08 | Connersville Blower Co | Rotary blower or gas-pump. |
| US1644401A (en) * | 1924-10-06 | 1927-10-04 | Elton F Ross | Pump |
| US2531726A (en) * | 1946-01-26 | 1950-11-28 | Roper Corp Geo D | Positive displacement rotary pump |
| US5253618A (en) * | 1991-11-16 | 1993-10-19 | Sanshin Kogyo Kabbushiki Kaisha | Marine engine |
-
2004
- 2004-11-17 JP JP2004333357A patent/JP2005180421A/en active Pending
- 2004-11-24 DE DE102004056744A patent/DE102004056744A1/en not_active Ceased
- 2004-11-24 US US10/996,585 patent/US20050112014A1/en not_active Abandoned
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US905967A (en) * | 1907-04-16 | 1908-12-08 | Connersville Blower Co | Rotary blower or gas-pump. |
| US1644401A (en) * | 1924-10-06 | 1927-10-04 | Elton F Ross | Pump |
| US2531726A (en) * | 1946-01-26 | 1950-11-28 | Roper Corp Geo D | Positive displacement rotary pump |
| US5253618A (en) * | 1991-11-16 | 1993-10-19 | Sanshin Kogyo Kabbushiki Kaisha | Marine engine |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070217939A1 (en) * | 2006-03-20 | 2007-09-20 | Kazuho Sato | Gas-compression module for a fuel cell |
| US20080304981A1 (en) * | 2007-06-08 | 2008-12-11 | Jaguar Precision Industry Co., Ltd. | Motor direct drive air pump and related applications thereof |
| US8748047B2 (en) | 2008-03-11 | 2014-06-10 | Daimler Ag | Method for operating a fuel cell system with a recirculation blower arranged in a fuel circuit thereof |
| WO2009112178A1 (en) | 2008-03-11 | 2009-09-17 | Daimler Ag | Method and device for operating a fuel cell system with a recirculation blower arranged in a fuel circuit of the fuel cell system |
| US20110053013A1 (en) * | 2008-03-11 | 2011-03-03 | Daimler Ag | Method for Operating a Fuel Cell System with a Recirculation Blower Arranged in a Fuel Circuit Thereof |
| US20110236232A1 (en) * | 2009-04-20 | 2011-09-29 | Yi-Lin Chu | Air compression device |
| WO2010143031A3 (en) * | 2009-06-10 | 2011-05-12 | Toyota Jidosha Kabushiki Kaisha | Fluid compressor and fuel cell vehicle |
| CN102459908A (en) * | 2009-06-10 | 2012-05-16 | 丰田自动车株式会社 | Fluid compressor and fuel cell vehicle |
| EP2806167A1 (en) * | 2009-06-10 | 2014-11-26 | Toyota Jidosha Kabushiki Kaisha | Fuel cell vehicle with fluid compressor |
| US9905865B2 (en) | 2009-06-10 | 2018-02-27 | Toyota Jidosha Kabushiki Kaisha | Fluid compressor and fuel cell vehicle |
| US8801402B2 (en) * | 2010-04-20 | 2014-08-12 | Cycle Arrow Technology Co. Ltd. | Air compression device |
| CN103375404A (en) * | 2012-04-30 | 2013-10-30 | 伊顿公司 | Positive displacement pump assembly with movable end plate for rotor face clearance control |
| US20180301722A1 (en) * | 2017-04-18 | 2018-10-18 | Toyota Jidosha Kabushiki Kaisha | Fuel cell system |
| US10811707B2 (en) * | 2017-04-18 | 2020-10-20 | Toyota Jidosha Kabushiki Kaisha | Fuel cell system |
| USD941360S1 (en) | 2019-01-31 | 2022-01-18 | Elliott Company | Oval steam turbine casing |
| CN111022323A (en) * | 2019-12-26 | 2020-04-17 | 烟台菱辰能源有限公司 | A hydrogen circulation pump with an anti-icing structure |
| US20230258179A1 (en) * | 2020-09-02 | 2023-08-17 | Eaton Intelligent Power Limited | Rear drive egr pump |
| US12338817B2 (en) * | 2020-09-02 | 2025-06-24 | Eaton Intelligent Power Limited | Rear drive EGR pump |
| US20250297609A1 (en) * | 2020-09-02 | 2025-09-25 | Eaton Intelligent Power Limited | Rear drive egr pump |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2005180421A (en) | 2005-07-07 |
| DE102004056744A1 (en) | 2005-08-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP5828863B2 (en) | Gas compressor | |
| US20080044305A1 (en) | Sealed-type rotary compressor and refrigerating cycle device | |
| US7281910B2 (en) | Motor driven compressor | |
| EP2479436B1 (en) | Multistage compressor | |
| CN1016259B (en) | Scroll compressor | |
| JP2005180421A (en) | Fluid compressor | |
| KR101447039B1 (en) | Scroll compressor | |
| JP5150564B2 (en) | Horizontal hermetic compressor | |
| CN1757927A (en) | Orbiting vane compressor | |
| KR101533251B1 (en) | Scroll compressor | |
| JP4052404B2 (en) | Hermetic scroll compressor | |
| KR100230999B1 (en) | Liquid refrigerant separating device of accumulator built-in rotary compressor | |
| JP2005180297A (en) | Scroll compressor | |
| KR200239620Y1 (en) | Rotary compressor | |
| KR100270871B1 (en) | Rotary compressor | |
| KR20210080889A (en) | Inverter-Integrated Electric Compressor | |
| JP3564903B2 (en) | Scroll compressor | |
| CN2615385Y (en) | Turbocompressor | |
| KR20000046855A (en) | Oil supply structure of crank shaft of hermetic rotation compressor | |
| KR19990012574A (en) | Refrigerant suction pipe connection structure of accumulator built-in rotary compressor | |
| KR0130248Y1 (en) | Horizontal type scroll compressor | |
| JP2706516B2 (en) | Compressor | |
| KR100286550B1 (en) | Airtight yype rotary compressor | |
| KR101391227B1 (en) | Scroll Compressor | |
| KR101130472B1 (en) | Outlet valve retainer apparatus for rotary compressor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: KABUSHIKI KAISHA TOYOTA JIDOSHOKKI, JAPAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SHIROMARU, KATSUTOSHI;KAWAMURA, KOJI;KATO, HIROAKI;AND OTHERS;REEL/FRAME:016211/0848 Effective date: 20041209 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |