GB2155108A - Gerotor hydraulic device with fluid control passageways through the rotor - Google Patents
Gerotor hydraulic device with fluid control passageways through the rotor Download PDFInfo
- Publication number
- GB2155108A GB2155108A GB08506824A GB8506824A GB2155108A GB 2155108 A GB2155108 A GB 2155108A GB 08506824 A GB08506824 A GB 08506824A GB 8506824 A GB8506824 A GB 8506824A GB 2155108 A GB2155108 A GB 2155108A
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- rotor
- pair
- fluid
- gerotor
- passageways
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Classifications
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- 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
- F04C2/00—Rotary-piston machines or pumps
- F04C2/08—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C2/10—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member
- F04C2/103—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member one member having simultaneously a rotational movement about its own axis and an orbital movement
- F04C2/104—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member one member having simultaneously a rotational movement about its own axis and an orbital movement having an articulated driving shaft
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
- Hydraulic Motors (AREA)
- Details And Applications Of Rotary Liquid Pumps (AREA)
Abstract
The device may be a pump or a motor, e.g. for power steering, and is provided with a number of fluid passageways 35, 37, 37a in the rotor 27. The rotor passageways are in communication with the inlet 30 and outlet 31 of the device via passages in a stator plate 21 and are in selective communication with the working chambers (29, Fig. 4) of the device via passages in a stator plate 23. In alternative embodiments the inlet and outlet are on opposite sides of the rotor. <IMAGE>
Description
1 GB 2 155 108 A 1
SPECIFICATION
Rotary Gerotor Hydraulic Device with Fluid Control Passageways through the Rotor An object of this invention is to provide a rotary fluid pressure device including a gerotor having a fixed stator inside of which is an orbiting and rotating rotor. The rotation of the orbiting rotor member provides the output or input at the shaft member. This rotor has a continuous ring valve on one side and both of the supplies of intake and exhaust pressure fluid are on the opposite side. A star-pointed annulus increases commutation fluid flow. The second embodiment shows again a fixed stator with an orbiting rotor with the rotating component of the rotor used at the output shaft; but in this embodiment the intake is on the internal diameter of one side of the rotor member with balanced area grooves in communication with the first named intake and exhaust grooves on the opposite side of the rotor so as to provide a hydraulically balanced rotor.
An added object of this invention is to provide a 85 pressure loaded commutator ring urged with a wave spring for initial contact, together with a drive pin connected between the rotor and the commutator ring.
Another object of the invention is to provide a pressure loading plate in the end cover of the housing so as to cause a pressure balance providing ahead force towards the manifold and gerotor set.
The present invention reduces the number of manufacturing operations necessary to make hydraulic pressure devices. The devices made in accord with this invention are simple, reliable and efficient.
Another object of this invention is to provide a 100 hydraulically balanced rotor.
Still another object is to reduce the wear of and cool the wobble stick drive connections.
Another object of the invention is to increase the commutation fluid flow.
Other objects and advantages of the present invention will be apparent from the accompanying drawings and the description.The essential features will beset forth in the appended claims.
Brief Description of the Drawings
Figure 1 is a central sectional viewthrough a first embodiment of this invention; Figure 2 is a sectional view taken along the line 2-2ofFigurel; Figure 3 is a sectional view taken along the line 3-3 of Figure 1; Figure 4 is a sectional viewtaken along the line 4-4 of Figure 1; Figure 5 is a sectional view taken along the line 5-5 of Figure 1; Figure 5A is a fragmental sectional view taken along the line 5A-5A of Figure 5; Figure 6 is a sectional view taken along the line 6-6ofFigurel; Figure 7 is a sectional view taken along the line 7-7 of Figure 1; Figure 8 is a central sectional view through the second embodiment of this invention; Figures, 9, 10 and 11 are, respectively, sectional views taken along the lines 9--9, 10-10 and 11-11 of Figure 8; Figure 12 is a fragmental sectional view taken at the righthand end of Figure 1 and showing a pressure loaded commutator ring; while Figure 13 is a fragmental sectional viewtaken at the right hand end of Figure 1 and showing a pressure loading plate in the end cover; Figure 14 is a central sectional view like Figure 1 but including a star pointed annulus; Figure 15 is a sectional view taken along line 15--15 in Figure 14; Figure 16 is a sectional view taken along line 16-16 in Figure 14; Figure 17 is a central sectional view of a hydraulic device like Figure 8 having shortened through passage and differing manifold passages; Figure 18 is a sectional view of the hydraulic device of Figure 17 taken along lines 18-18 of that Figure; Figure 19 is a sectional view of the manifold plate of Figure 17 taken generally along lines 19-19 of that Figure; Figure 20 is a central sectional view like Figure 14 of a bilateral ported hydraulic device; Figure 21 is a sectional view of the manifold plate of the bilateral ported hydraulic device of Figure 20 taken generally along lines 21-21 of that Figure; Figure 22 is a central sectional view like Figure 8 of an inverse valved hydraulic device; Figure 23 is a sectional view of the manifold plate of the inverse valved hydraulic device of Figure 22 taken generally along lines 23-23 of that Figure; Figure 24 is a central sectional view like Figure 14 of a manifold plate ported hydraulic device; Figure 25 is a sectional view of the manifold plate of Figure 24 taken generally along lines 25-25 of that Figure; Figure 26 is a sectional view of the manifold plate of Figure 24 taken generally along lines 26-26 of that Figure; Figure 27 is a sectional view of the channel closure plate of Figure 24 taken generally along lines 27-27 of that Figure; Figure 28 is a sectional view of the end plate of Figure 24taken generally along lines 28-28 of that Figure; Figure 29 is a central sectional view similar to Figure 14 of an intermediate plate gerotor porting.
The gerotor is contained in a power steering unit.
The unit is of multi-plate construction; Figure 30 is a view of the porting passages of Figure 29 taken generally along lines 30--30 of that Figure; 120 Figure 31 is a view of the porting passages of Figure 29 taken along lines 31-31- of that Figure; Figure 32 is a view of the porting passages of Figure 29 taken generally along lines 32-32 of that Figure; 125 Figure 33 is a view of the porting passages of Figure 29 taken generally along lines 33-33 of that Figure; 2 GB 2 155 108 A 2 Figure 34 is a view of the porting passages of Figure 29 taken generally along lines 34-34 of that Figure; Figure 35 is a central sectional view of a power steering unit similar to that of Figure 29. This Figure 35 unit further utilizing multi-plates to simplify the construction of the body of the unit; Figure 36 is a view of the plates of Figure 35 taken generally along lines 36-36 of that Figure; Figure 37 is a view of the plates of Figure 35 taken generally along lines 37-37 of that Figure; Figure 38 is a view of the plates of Figure 35 taken generally along lines 38-38 of that Figure; and Figure 39 is a view of the plates of Figure 35 taken generally along lines 39-39 of that Figure.
Those familiar with this type of apparatus will understand that while the present invention is being described as a pump using a fluid inlet and a fluid outlet, nevertheless, the same structure may be used as a motor by merely reversing the fluid inlet and outlet so that the high pressure fluid now enters at what was previously the inlet and the device operates as, a motor.
In the description and claims occurring hereinafter, the term "housing" is used to include not only the main housing member, but also the pressure plate, gerotor set, manifold and end cap, all of these latter parts being connected to the main housing portion by bolts.
Referring now to Figure 1, the first embodiment of this invention comprises a main housing unit 20 having a radially flat inner end to which is respectively attached a wear plate 21, a gerotor set 22, a manifold 23 and an end cap 24, all of these being secured together by bolts 25, which are shown in the various sectional views but omitted from Figure 1, but those skilled in this art will recognize that the bolts have heads pressing against the outer righthand end of the end cap 24 and extending through the members 21,22 and 23 and threaded tightly into the main housing portion 20. Sealing rings 26 seal all of the members against leakage between them.
The gerotor set 22, best seen in Figures 1 and 4, comprises an internal toothed member 27 which is a stator inside of which a coacting externally toothed member 28, a rotor, which rotates about its own axis A as seen in Figure 4, but which is eccentric relative to the center of the stator 27 by the distance shown between A and B, on the line of eccentricity C, and the rotor orbits about the center B. During this movement of the rotor and stator a series of cells 29 and 29a form a series of cells of constantly changing size between the rotor and stator, the size of the cells becoming greater on one side of the line of eccentricity, and the cell size becoming smaller on the opposite side. In Figure 4the minimum size cell at 29a approaches zero. The rotor rotates in the direction of the arrow shown in Figure 4. The rotor hastWo flat axial end surfaces.
The inlet means to the housing is indicated at 30.
The fluid outlet means is shown at 31. The inlet means is connected by means indicated only in dot-dash lines through a continuous annulus or distribution channel 32 in the main housing portion130 20. This annulus opens through the wear plate 21 which has a number of through openings or fluid travelways 33, the number of which is not important, but suff icient to take care of the flow of fluid necessary. These openings 33 are connected by connecting passages 33a to the annulus or annular ring transfer channel 34 of smaller diameter on the opposite face of the wear plate and opening into the rotor cavity toward the gerotor 22.
The annulus 34 may be ring-shaped (Figures 1 and 3) or star-pointed (Figures 14 and 16). The ring-shaped annulus 34 is symmetrical-a channel of uniform diameter and depth. The star-pointed annulus 34b, in contrast, has a shape dictated by the area swept bythe passageways 37 through the rotor 28 during the rotation of the rotor 28. The starpointed annulus 34b is of varying diameter and depth-widest and deepest at the points of the annulus 34b. The connecting passages 33a intersect with the star-pointed annulus 34b at the points of the annulus 34b.
The internal teeth 27a on the stator 27 are provided by cyli nders 27a inserted in recesses 27b over 180'in circumference so as to maintain the cylinders 27a in the positions shown in Figure 4. It will be understood that the cylinders 27a terminate at the level of the opposite faces of the stator 27. The rotor 28 has external teeth which are formed to fit almost exactly between the internal teeth of the stator, as shown in Figure 4. The rotor 28 has an open center 35 surrounded by a sealing strip 36 which is uninterrupted circumferential ly and laterally outside of which is an annular liquid intake passageway 37. The axis of rotation for the wobble stick 38 is marked Ain Figure 4. The axis of rotation for the orbiting movement of the wobble stick 38 relative to the stator is indicated at B in Figure 4. The line C passing through A and B is herein indicated as the line of eccentricity. The movement of the rotor herein described is as indicated by the arrow D in Figure 4. During this rotation the cells 29 on the lefthand side of the line of eccentricity increase in size gradually while the cells 29 on the righthand side of the line of eccentricity gradually decrease in size as indicated in Figure 4. The rotor functions as the main valve for the device. Six travel passageways or holes 37a are evenly spaced around the annulus 37 extending linearly through the rotor parallel to the axis of the rotor. These project radially inwardly from the annulus or annular channels 37 as seen at 37b, in one embodiment this being about 1/8 of an inch projection. The other travel passageway is generally on the central axis of the rotor, in the structure disclosed around the wobble stick-rotor device connection. There are sufficient openings in this type of drive connection thatfluid flow is relatively unimpeded by the spline-gear interfaces. The transfer channel 34 communicates with the annular channel as the device is operated.
A manifold 23 connects the rotor valve with the gerotor cells. The manifold 23 will be best shown in Figure 5, 5A, and 6. Seven parallel through openings to extend through the rotor facing surfaces of the manifold 23 parallel to its axis. This set of openings, 3 GB 2 155 108 A 3 as best seen in Figures 5 and 6, have a peculiar cross section. These openings 40 will be herein described as "double-trapezoidal". Referring to Figure 5, it will be seen that one of these openings appears substantially like two trapezoids facing each other with no middle partition and having opposite ends which are not quite parallel but instead are radial. The radially inner side of each opening is composed, not of straight lines, but of lines slightly concave inwardly meeting in a slight peak at the center 40a. The outer wall of this opening radially, as seen in Figure 5, may be composed of two straight lines meeting in the center or preferably a single line slightly convex radially outwardly. The size of each of these openings is such as to fit in the opening, seen in Figure 4, between two of the cylindrical openings 37a in a circumferential direction and between the central opening and the annulus 37 in a radial direction. These openings 40 are swept by the travel passageways in the rotor as the device is operated. This performs the primary valving function of the device. Each of the openings 41, as seen in Figures 5 and 6, of which there are seven evenly spaced, on the side of the manifold toward the gerotor are connected by fluid passageways 41 a and 42 sloping inwardly and downwardly to one end of the openings 40 just described.
The manifold 23, as seen in Figure 6, shows seven inclined passageways 42 in solid lines which coact with the structure described in connection with the openings 41, passageways 41 a and openings 40 as previously described. These coacting passageways are shown in broken lines in Figure 6 to show the cooperation. Seven of such passages 42 are provided extending part way through the manifold from side to side. These are at a slight angle to the axis of the gerotor and are spaced at a diameter to register, as shown in Figures 5 and 6. It will thus be seen that each passageway 42 in the manifold mates with one of the passages 41 a half-way through the manifold so that each of the seven passages 40 combines with one of the passages 41 a, 42.
The elongated rigid wobble stick 38 is clearly seen 110 in Figure 1 and shown in section in Figures 2 and 3.
One end of the wobble stick has a spline connection 44b with the drive shaft 44. It will be noted that this shaft has a solid outer end and a hollow inner end as indicated at 44a. The opposite end of the wobble stick has a spline connection 44c in a central bore in the rotor 28. These spline connections are provided in such a manner that the wobble stick may rotate and orbit around the center axes A, B and that fluid can continuously flow over and around them. The exhaust passageway includes the open center 35 of the rotor over and around the wobble stick- rotor drive connection and the open center 21 a of the wear plate and the hollow 44a, and is completed by four radial passageways 45 and 46 which are connected as shown in dot-dash lines, with the outlet 31.
Suitable needle bearings are shown at 47 and 48 supporting the drive shaft 44 in the main housing portion 20. Also suitable sealing means as shown at130 49 and 50 are provided where the drive shaft passes out of the main housing portion 20.
This embodiment has been described as a pump utilizing the drive shaft 44forthe attachment of powerwhich would cause intake of lower pressure fluid at 30 and exhaust of higher pressure fluid at 31. As previously explained, reversing the connections 30 and 31 will cause the device to operate as a motor producing power on the drive shaft 44.
The operation of the first embodiment as a pump will now be described. Power is supplied to the protruding left end of the drive shaft 44 as seen in Figure 1. This rotates the shaft, the wobble stick 38, the rotor 28, and also causes the rotor to orbit about the stator 27. This causes the cells 29 to the left of the line of eccentricity C to gradually increase in size causing a suction atthe intake 30. The cells 29 on the righthand side of the line of eccentricity C in Figure 3 are also caused to progressively decrease in size thus causing the fluid under increased pressure to exhaust at the outlet 31. The incoming fluid from intake 30 passes through the annular channel 32, the passageways 33a to the annular channel 34, then through the rotor 28 through the annular channels 37 and the cylindrical holes 37a, then through the double trapezoidal openings 40 in the manifold 23, then through the passageways 41 a and 42 in the manifold and through the openings 41 in the manifold and rotor and thus into the expanding cells 29. Other cells 29 are exhausted back through other openings 41 and other passageways 42 and 41 a and other double trapezoidal openings 40 in the manifold into the open center 35 of the rotor. The fluid then flows over and around clearances in the wobble stick-rotor drive connection, cooling and lubricating it, through the opening 21 a, through the hollow portion 44a of the shaft and through openings 45 and 46 and thus out through the outlet 31.
If the rotary fluid pressure gerotor device incorporates the star-pointed annulus 34b the commutation fluid passage is more direct and less constrained than with a ring-shaped annulus 34. Please note that other commutation channels in the gerotor device can also benefit from being starpoined-for example annular channel 37.
The second embodiment of this invention is shown in Figures 8,9, 10 and 11. Figure 8 is a central sectional view through the second embodiment with the bearings and seals resembling those seen in Figure 1 omitted for simplification of the drawings.
The main housing portion 60 has secured to it a wear plate 61, a gerotor set 62, a manifold 63 and an end cap 64, all secured rigidly together by a plurality of bolts 65 extending from the righthand end of the device as seen in Figure 8 into threads in the main housing portion 60. The main housing portion has an intake 66 connected by a passage 67 through the housing portion 60 with a continuous annulus chamber 68, which communicates with a plurality of radial openings 69 which lead inwardly to a hollow portion 70a of a drive shaft 70 which is rotatably mounted in the housing portion 60. An elongated rigid wobble stick 71 has a spline connection 71 a at 4 GB 2 155 108 A 4 one end with the drive shaft 70 and another spline connection 71b at the opposite end with the rotor member of the gerotor set 62. The spline connections 71 a and 71 b are so shaped as to permit the rotation of the wobble stick while at the same time permitting it to follow the orbiting movement of the rotor in the stator as will presently appear.
The wear plate 61 has a circular opening 61 a which permits the necessary movement of the wobble stick 71 and at the same time forms part of the intake passageway for fluid.
Six pairs of intake passageways 82 and 83 extending through the rotor 72 connecting the circular opening 61 a in the wear plate 61 with the annular passageway 84. The annular passageway 84 opens towards the manifold 63.
Figure 17 is of a device like that shown in Figure 8. In the device of Figure 17 the intake passageway 83 terminates in the area of the spline drive connection 71. This cools and lubricates this connection. In addition the manifold plate 23A uses surface channels 78A to connect the openings 40 and 41, respectively.
The intake 66A and passage 67A are of a greater diameter than in Figure 8. There are two staggered rows of radial openings 69A, 69B, in the drive shaft 70. See Figure 18. These in combination allow for the unimpeded fluid input into the area about the wobble stick without the need of a continuous annulus chamber 68 as in Figure 8.
The manifold plate 23A, instead of using angled holes 78 to connect the pairs of openings 40-41 respectively, uses channels 78A let into the surface of the manifold plate 23A away from the rotor. See Figure 19. The end plate covers the open side of the channels 78A. See Figure 17.
The gerotor 62 is best seen in Figure 9. It comprises a stator 62a which has a plurality of internally extending teeth formed partly by direct formation in the stator but also in part by six cylindrical members 62b which are firmly held in recesses 62c which extend for a distance greater than the radius of each of the cylinders 62b so that they are held firmly in the position shown in Figure 9. A rotor 72 is shown having a plurality of externally 110 extending teeth 72a which are shaped to fittingly coact with the internally extending teeth 62, 62a and 62b, these external teeth being one less in number than the internal teeth previously described. The rotor has an axis E which is eccentric relative to the 115 axis F of the stator and the line G passing through points E and F is herein designated as the line of eccentricity. The rotor is provided with a generally annular ring 84 forming part of the intake passageway for fluid. This passageway is concentric around the axis E. Inside the annular ring 84 is a circular opening 74, also concentric, for the exhaust of fluid from the rotary fluid pressure device.
Referring now to Figs. 9, 10 and 11, Fig. 11 shows the face of the manifold toward the gerotor structure 62. Centrally there is the exhaust opening 75 which communicates with the exhaust opening 74. In the next circle, and concentric, are seven rotor communicating openings 76, and in an outer concentric circle are seven passageway openings 77 130 so positioned that they cooperate circurnferentially with the cells 80 which are formed in changing fashion between the rotor and the stator as seen in Fig. 9.
Fig. 10 shows the face of the manifold 63 toward the end cap 64. This shows the through passageways 76 each connected to one of the openings 77 by means of angular passageways 78 and 79, each pair of which joins at an opening 79a.
The cooperation of these parts is shown in dot-dash lines in Fig. 9 at 81. This shows one of the openings 77 in position to cooperate with a cell 80a at the top of Fig. 9 and it is in cooperation through passageways 78 and 79, here shown diagrammatically, with one of the openings 76, which you might say is about two and one-half positions away going around the circle. It will now be seen how the radially outward openings 84a in the annular ring 84 cooperate with the communicating passageways 76. There are six of the formations 84a and each comprises a central, radially outermost portion 84b which extends substantially circurnferentially and at each end of this outermost portion is a radially and circurnferentially inwardly sloping portion 84c which extends to a radially innermost separating portion 84d. Each of the passageways 76 is herein described as double trapezoidal in section inasmuch as the opposite halves of the section are approximately trapezoid with their wider edges opening toward each other in the center. It will now be seen in Fig. 9 that when the dead pocket 80a at the top of Fig. 9 is in communication with its associated opening 77, then the other end of the connection through the 78,79 connection and shown at 76 in dot-dash lines, will illustrate howthe exhaust pocket related to cell 80a is shut off before the fluid is transferred from the associated intake pocket 76. This gives the dead center pocket a higher pressure than the supply at 66 because the fluid is trapped at that particular moment. This higher pressure causes the rotor 72 to seal better against the cylindrical members 62b on the opposite side of the axis. This higher pressure in cell 80a also provides oil to pivot roll near the upper dead center in Figure 9 whereby the rotor floats on a hydrodynamic oil film thus giving a higher mechanical efficiency output. It will now be seen that the shape of each of the portions 84a of the annular ring 84 match fairly well with the radially outer edges of the double trapezoidal passageways 76.
A balancing ring 86 is on the opposite side of the rotorfrom the annular ring 84. Small passages 87 through the rotor connect the balancing ring 86 to the opening 74. The balancing ring 86 equalizes the hydraulic pressure on the rotor 72.
It should now be apparent how the operation of this device as shown in Figs. 8-11 operates. Power is applied to the shaft 70 causing the rotor 72 to rotate in the stator 62a in the direction of the arrow shown in Fig. 9. The intake flow is from the inlet 66 through passageways 67 and 68, then through the hollow shaft portion 70a and through the central opening 61a in the wear plate. Then the flow is GB 2 155 108 A 5 through passageways 82 and 83 to the annular passageway 84 which opens toward the manifold 63. Then the flow passes through an opening to passageway 76 on one side of the eccentricity line G through the manifold passages 78,79 to one of the 70 openings 77 which is in communication with one of the cells 80 between the rotor and stator. Mean while, one of the cells 80 on the other side of the eccentricity line G communicates back to the appropriate passageway 76 and back through the manifold 63 to the exhaust passageways 74,75 and to exhaust.
Figure 12 shows a portion of the righthand end of Fig. 1 where the same parts are given the same reference numbers. Otherwise, the device operates 80 as described in connection with Fig. 1. However, in Fig. 12 there has been added a pressure plate 90 inserted in a suitable recess in the end cap 240, and the end cap is pushed toward the left as viewed in Fig. 12 by means of pressure admitted through lines 85 91, connected with the exhaust 45, and line 92 connected with the intake 30. Each of the lines 91 and 92 has adjacent the pressure loading plate 90 a ball check valve 93 so that the loading plate 90 is always pressed inwardly toward the manifold 23 and the gerotor set 22 beyond it. This provides for a head force towards the manifold and rotor set. This will take care of any wear between the engaging rubbing portions 22 and 23.
Fig. 13 also shows a portion of the righthand end 95 of Fig. 1 and all of the same parts are given the same reference characters. The added feature here is a pressure loaded commutator ring 95 which extends inwardly, toward the left in Fig. 13, against a shoulder 96 with a wave spring 97 circular in shape and pressed between the commutator ring and the 100 shoulder 96 to give an initial pressure. The wave spring is made of spring metal which weaves back and forth from a generally common plane as one goes around the circle. A seal 98 prevents leakage between the parts. There is provided a pin 105 connection 99 which as seen in Fig. 13 is in general an axial extension of the splines 440b connecting the wobble stick 380 and the rotor of the gerotor set 22. This pin fits between the splines 440b and extends into a suitable opening 99a in a portion of 110 the commutator ring. This pin connection is somewhat loose so as to use the rotational component of the rotor as a means of timing the opening and closing of the connection indicated in dot-dash lines in Fig. 9.
Fig. 20 is of a bilateral ported hydraulic device. In this device the inner travelpassageway instead of running through the open center 35of the rotor doubles back through a series of holes 100 in the manifold plate 23B to exit the gerotor device 120 through port 101.
The holes 100 extend through the manifold plate 23B about the central axis A' of the gerotor device.
The wobble stick 38 makes any physical contact that it does with the manifold plate 23B in the center of 125 the circle defined by holes 100. See Figure 21.
Due to the pressures and volumes of fluid in motion in the gerotor device, there is a constant backwater type fluid flow at all times over the wobble stick 38-rotor drive connection 44c and throughout the central cavity 102 of the gerotor device. This fluid lubricates and removes contaminants from the gerotor device.
Figure 22 is of an inverse valved hydraulic device. In this inverse valved device an outer ring channel 103 on one side of the rotor 28A is connected through a diagonal passageway 104 to the open center 35 of the rotor. A star shaped annulus 34 communicating with the outer ring channel 103 connects the fluid passageway to one of the fluid ports 30. The other fluid passage is a second ring channel 105. Another star-shaped annulus 106 communicating with the second ring channel 105 connects this fluid passage to the other of the fluid ports 107. This annulus 106 is on the manifold plate 23C between openings 40 and 41. See Fig. 23. (These openings 40 and 41 are connected together respectively by a series of channels 108 on the opposite side of the manifold plate 23C). A series ofholes 109, the location of which is not critical, extend from the annulus 106 through the manifold plate 23C and through the channel closure plate 110 to connect with cavity 111. The port 107 is connected to the cavity 111.
In operation the open center 35 of the rotor and the second ring channel 105 selectively communicate with the manifold openings 40 to valve the gerotor device.
Figure 24 is of a manifold plate ported hydraulic device. In this device both the porting commutation and the valving occur between a single surface of the rotor and the manifold plate 23D.
In this device port 112 connects through ring channel 113 in the end plate 115, and holes 114 through the closure plate 116, median plates 117, 118 and manifold plate 23D to star-shaped commutation annulus 119. The annulus 119 communicates with ring channel 37B on the rotor. Port 120 connects through hole 121 in the closure plate 116 to the series of holes 122 in the median plates 117,118 and the manifold plate 23D. The series of holes 122 communicate with the open center 35 of the rotor.
Passages 37A and the other ring channel 37 hydraulically balance the rotor for fluid pressure in the ring channel 37. The opposite end of the open center of the rotor hydraulically balances the open centerfluid passage.
The manifold plate has openings 41 and 41.
Openings 40 extend through the manifold plate. Holes 127 extend off of openings 41 through the manifold plate. Respective pairs of openings 40 and holes 127 are connected together by a series of channels 108 on the median plate 117.
In operation the ring channel 37 and the open center 35 of the rotor selectively communicate with openings 40 to valve the device.
The actual porting in the manifold ported hydraulic device of Figure 25 is accomplished through the use of a series of successive plates 115-118 and 23D. Each of the plates is designed for ease of individual manufacture. See Figures 25-28. During assembly each plate is located in proper 6 GB 2 155 108 A 6 sequence in respect to the other plates to together form the porting passages of the device.
If necessary to insure an acceptable quantity of leakage between neighboring passages, a sealing compound can be inserted between the plates, the plates after assembly may be brazed together to form a single unit or other appropriate steps taken.
Figure 29 is of a multi-plate intermediate plate ported hydraulic device. The device is disclosed in a power steering unit 127. Figure 35 is of a similar unit 127a having multi- plate body construction. The fluid passages within these multi-plate construction devices are identical in function. The devices will be described together.
The fluid recesses 128,128a are arranged about the slide member 129,129a in a cylinder 2(C2), return 2(R2), cylinder 1 (Cl), media 1 (Ml), pressure 2(P2), return 1 (131) and pressure 1 (Pl) layout.
The cylinder 1 (Cl) and cylinder 2(C2) recesses are connected through passages 150, 151 and ports 152, 153 in the power steering unit 127,127a and high pressure hydraulic hoses to opposing sides of a double acting hydraulic steering cylinder (all not shown). The pressure 1 (Pl) and pressure 2(P2) recesses are connected through passages 154,155 and port 156 in the power steering unit 127, 127a and high pressure hydraulic hoses to the high pressure outlet of a hydraulic pump driven by an engine (all not shown). The return 1 (131) and return 2(R2) recesses are connected together through passage 157 and through passage 158 and port 159 in the power steering unit 127,127a and high pressure hydraulic hoses to the low pressure inlet of the hydraulic pump (all not shown).
The center passage 131 of the power steering unit 127,127a communicates to the drive hole 141 and inner fluid passageway of the device. The media (1 M1) recess of the power steering unit 127,127a communicates to passage 130 and the outer fluid passageway of the device.
In operation the selective rotation of the input shaft 142 is transformed into axial movement of the slide member 129,129a through a pin-helical groove connection 143 within the limits of motion allowed by the torsion spring connection 144 to the wobble stick and thereafter into direct rotation of the wobble stick 145.
The axial movement of the slide member 129, 129a interconnects the recesses 128,128a and passages 130-131 selectively. In the turning position shown in drawing 29, passage 130 is connected through the media 1 (Ml) recess to pressure 2(P2) and the center passage 131 of the device 127 is connected to the cylinder 2.
The fluid from passage 130 travels through holes 132 in plates 133,134 and 135 and the commutation 120 passages 138 in plate 136 to the seven outer annulus holes 139 in plate 137.
From the outer holes 139 in the plate 137 the fluid communicates through annular channels 37 to some of the openings 34 that are located inside the outer holes 139. The openings 34 extend through plates 137,136 and 135 to connect with the spiral passages 140 in plate 134, and through the spiral passages 140 to connect with openings 41, respectively. Openings 41 extend through plates 135,136 and 137 to open into the gerotor cells of the device 127,127a.
While the outer holes 139 are communicating by openings 34 to openings 41 leading to expanding gerotor cells, fluid from openings 41 leading contracting fluid cells communicates directly with the center passage 131 of the device through the drive hole 141 in the center of the rotor.
In an opposite turn the reverse would be true.
Figure 35 is shown in a neutral unturned position.
In these hydraulic devices plates 133-137 are brazed together to form a single unitary structure.
In the hydraulic device of Figure 29, the fluid ports, the recesses (P1, R1, P2, M1, C1, R2 and C2) and the respective fluid passages therebetween in the body 127 of the steering unit must be cast and/or machined. These are time and labor consuming manufacturing operations.
In the alternate device of Figure 35, a series of plates 146 simplify the construction of the fluid passages in the device between the port openings and the recesses (P1, R1, P2, M1, C1, R2 and C2) in the housing 127a of the device; this in addition to go the series of plate 147 that simplifies the construction of the fluid passages connecting the 130 recess, respectively, with the gerotor cells.
Each plate of the series of plates 146,147 is designed for ease of individual manfuacture (usually by stamping) and to reduce or to simplify the construction of the remainder of the device. (For example in the device disclosed, the fluid passages 148 and 149 in the housing 127a are designed for construction in one perpendicular drilling operation from the flat face of the housing 127a). The series of plates are then brazed together to form a single unitary structure.
The multi-plate construction of the gerotor porting, plates 147, and of the body of the steering unit, plates 146, greatly reduces the cost of construction while increasing the flexibility of power steering units.
While I have illustrated and described a preferred embodiment of my invention, itwill be understood thatthis is byway of example only and notto be construed as limiting.
Claims (17)
1. In a gerotor hydraulic pressure device having a housing, a rotor with a certain eccentric rotary motion and full revolution commutation between a fluid passage in the housing and a fluid passage in the rotor, the improvement of one of the fluid passage in the housing or the fluid passage in the rotor being laid out in a pattern substantially following the certain eccentric rotary motion of the rotor, said pattern facilitating the fluid commutation between the passages.
2. The improved gerotor hydraulic pressure device of Claim 1 wherein the fluid passage laid out in a pattern substantially following the certain eccentric rotary motion of the rotor is a ring channel and characterized in that the ring channel is starshaped, the points of which are directed towards the cells of the gerotor device.
7 GB 2 155 108 A 7
3. In a gerotor hydraulic pressure device having a housing, a rotorwith two flat axial end surfaces, gerotor cells and two fluid connections, an improved fluid control comprising a pair of travel passageways, 100% of the fluid traveling through both of said pair of travel passageways, a bore extending substantially on the axis of the rotor part way through the rotor from one of the two flat axial end surfaces of the rotor, one of said pair of travel passageways extending from the other of the two flat axial end surfaces of the rotor to said bore, the other of said pair of travel passageways being in the rotor, means to connect one of said pair of travel passageways to one of the two fluid connections, means to connect the other of said pair of travel passageways to the other of the two fluid connections and means within the housing to connect said pair of travel passageways to the gerotor cells selectively as the device is operated.
4. The gerot.Or hydraulic device of Claim 3 characteried in that the other of said pair of travel passageways is a second bore extending substantially on the axis of the rotor part way through the rotor from the other of the two flat axial end surfaces of the rotor, said second bore in the rotor being distinct from said bore in the rotor.
5. The gerotor hydraulic device of Claim 3, characterized in that the other of said pair of travel passageways extends through the rotor, including at one end a bore extending substantially on the axis of the rotor part way through the rotorfrom the other of the two flat axial end surfaces of the rotor, said second bore in the rotor being distinct from said bore in the rotor.
6. in a gerotor hydraulic pressure device having a housing, a rotorwith two flat axial end surfaces, gerotor cells and two fluid connections, an improved fluid control comprising a pair of travel passageways, one of said pair of travel passageways extending straight through the rotor from one surface to the other, the other of said pair of travel passageways being in the rotor, means on one side of the rotor to connect one of said pair of travel passageways to one of the fluid connections, means on the other side of the rotor to connect the other of said pair of travel passageways to the other of the fluid connections, and means within the housing to connect said pair of travel passageways to the gerotor cell selectively as the device is operated.
7. The gerotor hydraulic pressure device of Claim 6 characterized in that said one of said pair of travel 115 passageways surrounds said other of said pair of travel passageways.
8. The gerotor hydraulic pressure device of Claim 6 characterized in that said other of said pair of travel passageways surrounds said one of said pair of travel passageways.
9. In a gerotor hydraulic pressure device having a housing, a rotorwith a flat axial end surface rotatively engaging the housing at a plane, gerotor cells and two fluid connections, an improved fluid control comprising a pair of travel passageways, said pair of travel passageways being in the rotor, one of said pair of travel passageways surrounding the other of said pair of travel passageways, means at the plane to connect one of said pair of travel passageways to one of the fluid connections, means at the same plane to connect the other of said pair of travel passageways to the other of the fluid connections and means within the housing at the same plane to connect said pair of travel passageways to the gerotor cells selectively as the device is operated such that the commutation and valving of the device occurs on a single side of the rotor.
10. The gerotor hydraulic pressure device of Claim 9 characterized by the addition of an input-output shaft and a wobble stick and wherein the plane of commutation and valving is on the same side of the rotor as the wobblestick drive connection with the input-output shaft.
11. The gerotor hydraulic pressure device of Claim 9 characterized by the addition of an input-output shaft and a wobble-stick and wherein the plane of commutation and valving is on the opposite side of the rotor as the wobble-stick drive connection with the input-output shaft.
12. In a gerotor hydraulic pressure device having fluid passages within the device next to a rotor cavity, the improvement comprising three or more plates, said plate being selectively consecutively located next to the rotor cavity, and the fluid passages being in said plates thereby reducing the cost of constructing the fluid passages.
13. The gerotor hydraulic pressure device of Claim 12 wherein the device is the centering member of a hydrostatic steering unit, the hydrostatic steering unit having a body with fluid ports, valving passages and fluid passages therebetween separate from the gerotor hydraulic pressure device, and characterized by the further improvement of the body of the steering unit being of multi-plate construction substantially at the location of the valving passages, said multi-plates containing the valving passages and substantially all of the fluid passages of the unit.
14. In a hydrostatic steering device having fluid ports, valving passages and fluid passages therebetween in the device, respectively, the improvement of the device being of multi-plate construction substantially at the location of the valving passages said multi-plates containing the valving passages and substantially all of the fluid passages of the device.
15. A method for constructing the valving passages and substantially all of the fluid passages in a hydraulic steering device, said method comprising stamping individual plates each containing a selected cross-sectional pattern of passages, positioning the individual plates in the proper sequential position and brazing the plates together to form a single unitary structure.
16. A method substantially as herein described with reference to the accompanying drawings.
17. A device substantially as herein described as shown in the accompanying drawings.
8 GB 2 155 108 A 8 Amendments to the claims have been filed, and have the following effect: (a) Claims 1, 2 & 12 to 15 above have been deleted.
(c) Claims 3 to 11, 16 & 17 above have been 5 re-numberedaslto9, 10&llandtheir appendancies corrected.
Printed for Her Majesty's Stationery Office by Courier Press, Leamington Spa. 911985. Demand No. 8817443. Published by the Patent Office, 25 Southampton Buildings, London, WC2A lAY, from which copies may be obtained.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/360,832 US4474544A (en) | 1980-01-18 | 1982-03-23 | Rotary gerotor hydraulic device with fluid control passageways through the rotor |
US39032882A | 1982-06-21 | 1982-06-21 |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8506824D0 GB8506824D0 (en) | 1985-04-17 |
GB2155108A true GB2155108A (en) | 1985-09-18 |
GB2155108B GB2155108B (en) | 1986-10-01 |
Family
ID=27001036
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08307701A Expired GB2119444B (en) | 1982-03-23 | 1983-03-21 | Gerotor hydraulic machine with fluid-control passageway through the rotor |
GB08506825A Expired GB2155109B (en) | 1982-03-23 | 1985-03-15 | Gerotor device in or for a hydrostatic steering unit |
GB08506824A Expired GB2155108B (en) | 1982-03-23 | 1985-03-15 | Gerotor hydraulic device with fluid control passageways through the rotor |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08307701A Expired GB2119444B (en) | 1982-03-23 | 1983-03-21 | Gerotor hydraulic machine with fluid-control passageway through the rotor |
GB08506825A Expired GB2155109B (en) | 1982-03-23 | 1985-03-15 | Gerotor device in or for a hydrostatic steering unit |
Country Status (5)
Country | Link |
---|---|
JP (5) | JPH0694870B2 (en) |
BR (1) | BR8301453A (en) |
CA (1) | CA1217089A (en) |
DE (1) | DE3310593C3 (en) |
GB (3) | GB2119444B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2240365A (en) * | 1990-01-29 | 1991-07-31 | White Hollis Newcomb Jun | Reduced sized rotary hydraulic motor |
GB2275084A (en) * | 1990-01-29 | 1994-08-17 | White Hollis Newcomb Jun | Reduced sized hydraulic motor |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3626379A1 (en) * | 1985-08-06 | 1987-02-12 | White Jun Hollis Newcomb | Hydrostatic steering device |
DE3626381A1 (en) * | 1985-08-06 | 1987-02-12 | White Jun Hollis Newcomb | Hydrostatic steering device |
GB2219631B (en) * | 1988-06-09 | 1992-08-05 | Concentric Pumps Ltd | Improvements relating to gerotor pumps |
DE19637822C1 (en) * | 1996-09-17 | 1998-03-26 | Deutsch Zentr Luft & Raumfahrt | Micromechanical tool |
DE19843161C2 (en) * | 1998-09-21 | 2000-11-23 | Hnp Mikrosysteme Gmbh | Layer structure housing construction |
DE102011051486B4 (en) | 2011-06-30 | 2023-06-01 | Hnp Mikrosysteme Gmbh | Pump arrangement with micropump and bearing element |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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GB1012112A (en) * | ||||
GB1062646A (en) * | 1962-09-05 | 1967-03-22 | Germane Corp | Rotary fluid pressure motors and pumps |
GB1232686A (en) * | 1967-07-21 | 1971-05-19 | ||
GB2023738A (en) * | 1978-05-26 | 1980-01-03 | White H | Rotary positive-displacement fluid-machines |
GB2024949A (en) * | 1978-07-05 | 1980-01-16 | Rexroth Gmbh G L | Rotary positive - displacement fluidmachines |
EP0054161A2 (en) * | 1980-12-15 | 1982-06-23 | Trw Inc. | Gerotor gear set device with integral rotor and commutator |
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US2023738A (en) | 1931-01-30 | 1935-12-10 | Bush Mfg Company | Means for assembling and securing radiating fins on tubes |
US3106163A (en) | 1960-04-04 | 1963-10-08 | Roper Hydraulics Inc | Pumps, motors and like devices |
US3452680A (en) * | 1967-08-11 | 1969-07-01 | Trw Inc | Hydraulic motor-pump assembly |
DE2240632C2 (en) * | 1972-08-18 | 1983-09-01 | Danfoss A/S, 6430 Nordborg | Rotary piston machine for liquids |
US3799201A (en) * | 1973-04-05 | 1974-03-26 | Danfoss As | Distributor valve for an internally shafted orbital piston machine |
JPS5332525A (en) * | 1976-09-07 | 1978-03-27 | Mitsubishi Motors Corp | Automobile power transmission apparatus |
JPS5417505A (en) * | 1977-07-08 | 1979-02-08 | Aisin Seiki Co Ltd | Motor of internal gear pump of hydrostatic power steering device |
US4219313A (en) | 1978-07-28 | 1980-08-26 | Trw Inc. | Commutator valve construction |
-
1983
- 1983-02-23 CA CA000422267A patent/CA1217089A/en not_active Expired
- 1983-03-21 GB GB08307701A patent/GB2119444B/en not_active Expired
- 1983-03-22 BR BR8301453A patent/BR8301453A/en not_active IP Right Cessation
- 1983-03-23 DE DE19833310593 patent/DE3310593C3/en not_active Expired - Lifetime
- 1983-03-23 JP JP58047357A patent/JPH0694870B2/en not_active Expired - Lifetime
-
1985
- 1985-03-15 GB GB08506825A patent/GB2155109B/en not_active Expired
- 1985-03-15 GB GB08506824A patent/GB2155108B/en not_active Expired
-
1994
- 1994-01-04 JP JP82159483A patent/JP3090835B2/en not_active Expired - Lifetime
- 1994-01-04 JP JP6008216A patent/JP2832796B2/en not_active Expired - Lifetime
- 1994-01-04 JP JP821594A patent/JPH0742678A/en active Pending
-
1995
- 1995-09-28 JP JP07273683A patent/JP3100539B2/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1012112A (en) * | ||||
GB1062646A (en) * | 1962-09-05 | 1967-03-22 | Germane Corp | Rotary fluid pressure motors and pumps |
GB1232686A (en) * | 1967-07-21 | 1971-05-19 | ||
GB2023738A (en) * | 1978-05-26 | 1980-01-03 | White H | Rotary positive-displacement fluid-machines |
GB2024949A (en) * | 1978-07-05 | 1980-01-16 | Rexroth Gmbh G L | Rotary positive - displacement fluidmachines |
EP0054161A2 (en) * | 1980-12-15 | 1982-06-23 | Trw Inc. | Gerotor gear set device with integral rotor and commutator |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2240365A (en) * | 1990-01-29 | 1991-07-31 | White Hollis Newcomb Jun | Reduced sized rotary hydraulic motor |
GB2275084A (en) * | 1990-01-29 | 1994-08-17 | White Hollis Newcomb Jun | Reduced sized hydraulic motor |
GB2240365B (en) * | 1990-01-29 | 1994-10-12 | White Hollis Newcomb Jun | Orbiting valve hydraulic motor |
GB2275084B (en) * | 1990-01-29 | 1994-10-26 | White Hollis Newcomb Jun | Reduced sized hydraulic motor |
Also Published As
Publication number | Publication date |
---|---|
DE3310593C2 (en) | 1991-04-11 |
DE3310593A1 (en) | 1983-10-06 |
GB2155108B (en) | 1986-10-01 |
JP3090835B2 (en) | 2000-09-25 |
BR8301453A (en) | 1983-11-29 |
GB2155109B (en) | 1986-10-01 |
CA1217089A (en) | 1987-01-27 |
JP3100539B2 (en) | 2000-10-16 |
JPH06323260A (en) | 1994-11-22 |
GB8506825D0 (en) | 1985-04-17 |
JP2832796B2 (en) | 1998-12-09 |
DE3310593C3 (en) | 1995-07-13 |
GB8307701D0 (en) | 1983-04-27 |
JPH08254188A (en) | 1996-10-01 |
GB8506824D0 (en) | 1985-04-17 |
GB2119444A (en) | 1983-11-16 |
JPH0742678A (en) | 1995-02-10 |
GB2119444B (en) | 1986-10-01 |
GB2155109A (en) | 1985-09-18 |
JPH0694870B2 (en) | 1994-11-24 |
JPS58172481A (en) | 1983-10-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PE20 | Patent expired after termination of 20 years |
Effective date: 20030320 |