ROTARY CYLINDER DEVICE

BACKGROUND OF THE INVENTION

The present invention relates to a rotary type cylinder device capable of dealing with interconversion of reciprocating motions of pistons in cylinders and a rotary motion of a shaft, more precisely relates to a rotary type cylinder device which can be applied to internal-combustion engines, compressors, vacuum pumps, hydraulic rotary machines, etc.

In each of internal-combustion engines, compressors, vacuum pumps, hydraulic rotary machines, etc., various types of driving mechanisms are employed. For example, a reciprocal type driving mechanism in which a fluid is repeatedly sucked and discharged by reciprocating motions of piston units connected to a crank shaft, a scroll type driving mechanism in which a fluid is repeatedly sucked and discharged by revolving a movable scroll with respect to a fixed scroll, a rotary type driving mechanism in which a fluid is repeatedly sucked and discharged by rotary motion of a roller (see Japanese Laid-open Patent Publication No. P2004-190613A), a screw type driving mechanism, and a vane type driving mechanism are employed according to usage.

Especially, the reciprocal type driving mechanism is mainly used for internal-combustion engines, compressors, vacuum pumps, etc., each of which is rotated at a medium speed, e.g., 10000 rpm, and in each of which high airtightness is required.

In the reciprocal type driving mechanism, energy converting efficiency is easily lowered by energy loss caused by reciprocating motion of piston units in cylinders. Further, a connection rod for supporting the piston units reciprocally moved in the cylinders, a crank shaft being connected to the connecting rod and a crank arm being connected to the crank shaft are required, so an energy converting device, which converts the reciprocating motion of the piston units into a rotary motion, must be large in size. Vibration, which is caused by deviations of mass balances (gravity centers) of rotatable members while the piston units are reciprocally moved, must be absorbed by a damper, etc.

SUMMARY OF THE INVENTION

Accordingly, it is an object in one aspect of the invention to provide a rotary type cylinder device, in which rotatable members which are capable of revolving around a shaft at fixed rotational speeds can be compactly assembled in the axial and radial directions, piston units can be linearly reciprocally moved by combination of rotary motions around a plurality of crank shafts, and imbalance of masses of the rotatable members, which is caused by deviations of gravity centers caused by the linear and reciprocal motions of the piston units, can be repaired so as to restrain rotational vibration and reduce noise.

To produce the object, the rotary type cylinder device, which is capable of dealing with interconversion of reciprocating motions of pistons in cylinders and a rotary motion of a shaft, comprises:

a first crank shaft being eccentrically provided with respect to an axis of the shaft, the first crank shaft being revolved around the shaft by a first virtual crank arm having a radius of r from the shaft;

a composite piston assembly having an eccentric cylindrical body, which is constituted by a first cylindrical section, to which the first crank shaft is coaxially fitted, and second cylindrical sections, whose axes are second virtual crank shafts made eccentric with respect to an axis of the first cylindrical section and which are integrated with the first cylindrical section and located on the axial both sides of the first cylindrical section respectively, the composite piston assembly being revolved, around the first crank shaft, by a second virtual crank arm having a radius of r in a state where a first piston unit fitted to the one of the second cylindrical sections and a second piston unit fitted to the other second cylindrical section intersect each other;

a first balance weight and a second balance weight for producing rotational balances of rotatable members which are provided around the shaft and can be rotated at fixed rotational speeds, the first balance weight and the second balance weight being respectively provided to both end parts of the first clank shaft, to which the composite piston unit is attached; and

a main body case rotatably holding the shaft, the main body case rotatably accommodating the first crank shaft, the first balance weight and the second balance weight, which are revolved around the shaft, and the composite piston unit, which is revolved around the first crank shaft, and

wherein the first crank shaft is revolved around the shaft and the composite piston assembly is revolved around the first crank shaft in a state where first rotational mass balance relating to the first and second piston units around the second virtual crank shafts, second rotational mass balance relating to the composite piston assembly around the first crank shaft and third rotational mass balance relating to the first crank shaft and the composite piston assembly around the shaft are uniformly produced by only the first and second balance weights which are attached to the both end parts of the first crank shaft, thereby the first and second piston units, which are attached to the second cylindrical sections, are linearly reciprocally moved in radial directions of a circular orbit of the second virtual crank shafts, which has radius of 2 r, with relatively revolving around the shaft.

Note that, the first virtual crank arm means a part connecting the shaft to the axis of the first crank shaft. Even if there is no dedicated crank arm, a structure which can act as a crank arm is regarded as the first virtual crank arm. The second virtual crank arm means a part connecting the axis of the first crank shaft to the second virtual crank shafts. Even if there is no crank arm, a structure which can act as a crank arm is regarded as the second virtual crank arm. The second virtual crank shafts are virtual axes of revolution. Even if there are no physical axes of revolution, the virtual axes which can act as axes of revolution are regarded as the second virtual crank shafts. Further, each of the piston units means a unit in which a seal cap, a seal cap retainer, a piston ring, etc. are integrally attached to a piston head section.

Preferably, in the rotary type cylinder device, pinholes are formed in both end parts of the first crank shaft respectively, axes of the pinholes are perpendicular to the axis of the first crank shaft,

axial holes and pinholes are formed in shaft sections of the first and second balance weights respectively, axes of the pinholes of the first and second balance weights are perpendicular to the axes of the first and second balance weights, and

the both end parts of the first crank shaft are respectively fitted in the axial holes of the first and second balance weights in a state where the pinholes of the first crank shaft correspond to the pinholes of the first and second balance weights so as to integrate the first crank shaft with the first and second balance weights.

Preferably, in the rotary type cylinder device, at least one of the first and second balance weights is integrated with the shaft.

Preferably, in the rotary type cylinder device, each of the second cylindrical sections has bearing retainer parts, which are respectively formed in an inner circumferential face and an outer circumferential face, an inner bearing is retained by the bearing retainer parts formed in the inner circumferential face, an outer bearing is retained by the bearing retainer parts formed in the outer circumferential face, and

the first crank shaft is rotatably held by the inner bearings, the first and second piston units are held by the outer bearings.

In the rotary type cylinder device of the present invention, the first crank shaft is revolved around the shaft by rotating the shaft, and the first and second piston units attached to the second cylindrical sections are linearly reciprocally moved along the radial directions of the circular orbit of the second virtual crank shafts, which has radius of 2 r, by revolving the composite piston assembly around the first crank shaft.

While the operation, the first rotational mass balance relating to the first and second piston units around the second virtual crank shafts, the second rotational mass balance relating to the composite piston assembly around the first crank shaft and the third rotational mass balance relating to the first crank shaft and the composite piston assembly around the shaft are uniformly produced by only the first and second balance weights. Further, imbalance, which is caused by deviations of gravity centers caused by the linear and reciprocal motions of the piston units, can be repaired, so that rotational vibration of the rotary type cylinder device can be restrained and operation noise can be reduced.

In the rotary type cylinder device of the invention, energy loss can be reduced and energy converting efficiency can be improved by restraining the rotational vibration caused by revolving the rotatable members around the shaft. Further, a vibration-proof mechanism can be simplified.

In comparison with conventional devices, number of crank shafts and crank arms can be reduced, so that the structure of the rotary type cylinder device of the invention can be simplified.

In case that the both end parts of the first crank shaft are respectively fitted in the axial holes of the first and second balance weights in the state where the pinholes of the first crank shaft correspond to the pinholes of the first and second balance weights, pins can be fitted and fixed in the pinholes, accuracy of attaching the first and second weights, in the directions perpendicular to their axes, to the both end parts of the first crank shaft can be improved.

In case that at least one of the first and second balance weights is integrated with the shaft, number of parts can be reduced. The first crank shaft can be compactly attached, in the axial and radial directions, to the shaft by adjusting a length of the first virtual crank arm, which connects the shaft to the first crank shaft. The length of the first virtual crank arm is adjusted by adjusting the revolving radius of the first and second balance weights.

In case that each of the second cylindrical sections has bearing retainer parts, which are respectively formed in the inner circumferential face and the outer circumferential face, the inner bearing is retained by the bearing retainer parts formed in the inner circumferential face, the outer bearing is retained by the bearing retainer parts formed in the outer circumferential face, and the first crank shaft is rotatably held by the inner bearings, the first and second piston units are held by the outer bearings, the composite piston assembly including the eccentric cylindrical body can be compactly attached, in the axial and radial directions, to the first crank shaft by adjusting a length of the second virtual crank arm, which connects the first crank shaft to the second virtual crank shafts. The length of the second virtual crank arm is adjusted by adjusting the revolving radius of the second cylindrical sections.

BRIEF DESCRIPTION OF THE DRAWINGS

Embodiments of the present invention will now be described by way of examples and with reference to the accompanying drawings, in which:

FIG. 1 is a perspective view of the rotary type cylinder device of the present invention;

FIG. 2 is a perspective view of the rotary type cylinder device shown in FIG. 1, wherein a first case is detached;

FIG. 3 is a sectional perspective view of the rotary type cylinder device shown in FIG. 1;

FIG. 4 is an exploded perspective view of the rotary type cylinder device;

FIGS. 5A-5L are explanation views showing rotary motions of a first crank shaft and second virtual crank shafts and linear reciprocal motions of crank arms;

FIG. 6A is a plan view of a compressor to which the rotary type cylinder device is applied, wherein the first case is detached;

FIG. 6B is a sectional view of the compressor taken along the Z-axis;

FIG. 6C is a sectional view of the compressor taken along the Z-axis, wherein piston units are crisscrossed;

FIG. 7 is a front view of the first crank shaft;

FIG. 8A is a front view of a first balance weight;

FIG. 8B is a plan view of the first balance weight;

FIG. 8C is a bottom view of the first balance weight;

FIG. 9A is a front view of a second balance weight;

FIG. 9B is a plan view of the second balance weight;

FIG. 9C is a bottom view of the second balance weight;

FIG. 10A is a plan view of an eccentric cylindrical body;

FIG. 10B is a sectional view of the eccentric cylindrical body taken along the X-axis;

FIG. 11A is a plan view of the first case;

FIG. 11B is a sectional view of the first case taken along the X-axis;

FIG. 12A is a plan view of a second case;

FIG. 12B is a sectional view of the second case taken along the X-axis;

FIG. 13A is a partially cutaway plan view of a first piston main body;

FIG. 13B is a sectional view of the first piston main body taken along the Z-axis;

FIG. 13C is a right side view of the first piston main body;

FIG. 13D is a bottom view of the first piston main body;

FIG. 14A is a front view of the piston unit, to which a piston ring of an internal-combustion engine is attached;

FIG. 14B is a partial sectional view of the piston unit, which is accommodated in a main body case;

FIG. 15A is a plan view of a cylinder;

FIG. 15B is a sectional view of the cylinder taken along the X-axis;

FIG. 16A is a plan view of a cylinder seal cap;

FIG. 16B is a sectional view of the cylinder seal cap taken along the X-axis;

FIG. 17A is a plan view of a seal retainer;

FIG. 17B is a sectional view of the seal retainer taken along the X-axis;

FIG. 18 is a partial sectional view of a cylinder seal cap assembly of a vacuum pump;

FIG. 19 is a plan explanation view showing the piston unit and a rotational position of the shaft, wherein the first case is detached;

FIG. 20 is a plan explanation view showing the piston unit and a rotational position of the shaft, wherein the first case is detached;

FIG. 21 is a plan explanation view showing the piston unit and a rotational position of the shaft, wherein the first case is detached;

FIG. 22 is a plan explanation view showing the piston unit and a rotational position of the shaft, wherein the first case is detached; and

FIGS. 23A and 23B are partial sectional views of the piston unit and the cylinder.

DETAILED DESCRIPTION OF THE EMBODIMENTS

Preferred embodiments of the present invention will now be described in detail with reference to the accompanying drawings. A rotary type cylinder device, which will be assembled in a compressor, will be explained as an embodiment of the present invention with reference to FIGS. 1-23B. The rotary type cylinder device is capable of dealing with interconversion of reciprocating motions of pistons in cylinders and a rotary motion of a shaft.

In FIG. 1, a shaft (input/output shaft) 4 is rotatably held in a main body case 3, which is constituted by a first case 1 and a second case 2. The first case 1 and the second case 2 are integrated by bolts 3a, which are respectively provided to four corners of the main body case 3. In the main body case 3, as shown in FIG. 3, an eccentric cylindrical body 6, which can be revolved around a first crank shaft 5, and a first piston unit 7 and a second piston unit 8, which constitute a composite piston assembly P (see FIG. 2) and which can be revolved around the first crank shaft 5, are rotatably accommodated in the main body case 3. Details of the structural members will explained.

In FIG. 3, the first crank shaft 5 is eccentrically attached to the shaft 4. In the present embodiment, the shaft 4 is integrated with a first balance weight 9. Note that, a shaft may be integrated with a second balance weight 10. The first and second balance weights 9 and 10 are respectively fitted with end parts of the first crank shaft 5. In FIG. 7, slits 5a are respectively formed in the both end parts of the first crank shaft 5 and extended in the axial direction thereof. A pinhole 5b, whose axial line is perpendicular to that of the first crank shaft 5, is formed in each of the slits 5a. A diameter of the pinhole 5b is larger than a width of the slit 5a, and the pinhole 5b overlaps a part of the slit 5a. D-shaped parts 5c, whose end faces are formed into D-shape, are respectively formed in the both end parts of the first crank shaft 5. The first and second balance weights 9 and 10 are respectively fitted with the both end parts of the first crank shaft 5 in a state where the pinholes 5a correspond to pinholes 9b and 10b of the first and second balance weights 9 and 10 (see FIGS. 8A and 9A).

In FIGS. 8A-8C and 9A-9C, a bolt hole 9a and the pinhole 9b are formed in a shaft section of the first balance weight 9; a bolt hole 10a and the pinhole 10b are formed in a shaft section of the second balance weight 10. The first and second balance weights 9 and 10 are fitted with the first crank shaft 5 in a state where the pinholes 5b of the first crank shaft 5 (see FIG. 7) correspond to the pinholes 9b and 10b. A pin 11a (see FIG. 3) is fitted in the pinholes 5b and 9b, which are mutually communicated; a pin 11b (see FIG. 3) is fitted in the pinholes 5b and 10b, which are mutually communicated. Bolts 12a and 12b are respectively fitted in the bolt holes 9a and 10a so as to narrow the slits 5a and the pinholes 5b. Therefore, the pins 11a and 11b are retained, and the first and second balance weights 9 and 10 can be integrated with the both end parts of the first crank shaft 5 (see FIG. 4). With this structure, accuracy of attaching the first and second balance weights 9 and 10 to the both end parts of the first crank shaft 5, in the direction perpendicular to the axial line of the first crank shaft 5, can be improved.

In FIG. 3, the shaft 4, which is integrated with the first balance weight 9, is rotatably supported by a first bearing 13a; a shaft section 10c, which is formed coaxially with the shaft 4 of the second balance weight 10, is rotatably supported by a second bearing 13b. For example, the first and second balance weights 9 and 10 are fan-shaped blocks (see FIGS. 8B, 8C, 9B and 9C). The first and second balance weights 9 and 10 are used for producing rotational balance between rotatable members attached around the shaft 4, e.g., the first crank shaft 5, the composite piston assembly P.

As described above, the shaft 4 is integrated with at least one of the first and second balance weights 9 and 10, so that number of parts can be reduced. Further, the first crank shaft 5 can be compactly attached to the shaft 4, in the axial direction and the radial direction, by adjusting a length of a first virtual crank arm, which connects the shaft 4 to the first crank shaft 5. The length of the first virtual crank arm is adjusted by adjusting, for example, revolving radius r of the first and second balance weights 9 and 10.

As shown in FIG. 10B, the eccentric cylindrical body 6 has a plurality of second virtual crank shafts 14a and 14b, which are eccentrically disposed with respect to the axis of the first crank shaft 5. In the present embodiment, the two piston units 7 and 8 are crisscrossed, so the second virtual crank shafts 14a and 14b are disposed around the first crank shaft 5 with a phase difference of 180 degrees.

As shown in FIG. 3, the crisscrossed piston units 7 and 8 is attached to the eccentric cylindrical body 6, which is capable of revolving around the first crank shaft 5. As shown in FIG. 10B, the eccentric cylindrical body 6 is constituted by a first cylindrical section 6a, through which the first crank shaft 5 acting as a rotary shaft is pierced, and second cylindrical sections 6b, which are extended from both axial ends of the first cylindrical section 6a. The first crank shaft 5 is coaxially fitted in the first cylindrical section 6a and acts as a rotary shaft of the eccentric cylindrical body 6. Axial lines of the second cylindrical sections 6b correspond to the second virtual crank shafts 14a and 14b, which are eccentrically disposed with respect to the axial line of the first crank shaft 5 (the first cylindrical section 6a). As shown in FIG. 3, the first and second piston units 7 and 8, which are crisscrossed each other, are rotatably attached to the second cylindrical sections 6b by outer bearings 16a and 16b.

In FIGS. 10A and 10B, each of the second cylindrical sections 6b has a bearing retainer part 6c, which is formed in an inner circumferential face, and a bearing retainer part 6d, which is formed in an outer circumferential face. As shown in FIG. 3, inner bearings 15a and 15b are respectively retained by the bearing retainer parts 6c; the outer bearings 16a and 16b are respectively retained by the bearing retainer parts 6d. The inner bearings 15a and 15b rotatably support the first crank shaft 5. As shown in FIG. 3, the first and second piston units 7 and 8 are rotatably supported by the outer bearings 16a and 16b in a state where the first and second piston units 7 and 8 are fitted to the second cylindrical sections 6b and their axial lines are perpendicular to the second virtual crank shafts 14a and 14b.

With this structure, the composite piston assembly P including the eccentric cylindrical body 6 can be compactly attached to the first crank shaft 5, in the axial direction and the radial direction, by adjusting a length of a second virtual crank arm, which connects the first crank shaft 5 to the second virtual crank shafts 14a and 14b. The length of a second virtual crank arm is adjusted by adjusting revolving radius of the second cylindrical sections 6b.

The first and second piston units 7 and 8 are fitted to the second cylindrical sections 6b of the eccentric cylindrical body 6, their axial lines are perpendicular to the second virtual crank shaft 14a and 14b, and first piston head sections 7c and second piston head sections 8c are reciprocally moved in the same plane. Therefore, the composite piston assembly P (see FIG. 2) can be compactly assembled, so that the device can be downsized and its installation space can be made smaller.

In FIG. 2, the first piston head sections 7c are provided to both axial ends of a first piston main body 7A; the second piston heads 8c are provided to both axial ends of a second piston main body 8A. Ring-shaped seal caps 17a and 17b (see FIGS. 16A and 16B) and seal cap retainers 18a and 18b (see FIGS. 17A and 17B) are fixed to the first and second piston head sections 7c and 8c by bolts 19. The seal caps 17a and 17b are composed of an oil-free sealing material, e.g., polyether ether ketone (PEEK). Erecting sections 17c are formed along outer circumferential edges and extended in the moving directions of the piston heads (see FIGS. 16A and 16B). In a compressor, a hydraulic rotary machine, etc., the erecting sections 17c are extended in the moving directions of the first and second piston head sections 7c and 8c and headed outside (see FIG. 23A).

In FIGS. 2 and 3, cylinders 21 are fitted in opening parts 20, which are formed in four side faces of the main body case 3 constituted by the first and second cases 1 and 2, by bolts 22. In FIG. 2, the first and second piston units 7 and 8 slide on inner faces 21f of the cylinders 21 (see FIG. 15B) with sealing clearances therebetween by the seal caps 17a and 17b (the erecting sections 17c). Note that, the seal caps 17a and 17b are very light and their revolving masses can be ignored, so function of balancing first to third rotational balances to be described later, which is performed by the first and second balance weights 9 and 10, is not influenced.

FIG. 13A is a partially cutaway plan view of the first piston main body 7A, wherein the seal caps and the seal cap retainers are detached; FIG. 13B is a sectional view thereof taken along the Z-axis; FIG. 13C is a right side view thereof; and FIG. 13D is a bottom view thereof. The first and second piston main bodies 7A and 8A have the same configuration, so only the first piston main body 7A will be explained. Note that, structural elements of the second piston main body 8A (see FIG. 2) are the same as those of the first piston main body 7A. An escape hole 7a (see FIG. 13A), which is formed for preventing interference with a main part 9c of the shaft 4 (see FIG. 8A), is formed in the center of the first piston main body 7A. The center of the escape hole 7a corresponds to the second virtual crank shaft 14a. A bearing retainer part 7b, which retains the outer bearing 16a, is formed to enclose the escape hole 7a (see FIGS. 13B and 13D).

The first piston head sections 7c, each of which is formed into a circular plate, are respectively provided to the axial both ends of the first piston main body 7A. Base plates 7d, which have bolt holes 7e, are provided to the first piston main body 7A (see FIG. 13C). As shown in FIG. 13A, the base plates 7d are respectively provided to the both end faces of the first piston main body 7A, the seal caps 17a shown in FIG. 4 are fitted to stepped parts 7f, each of which is formed on the radially outer side of the base plate 7d, and then the seal cap retainers 18a are stacked on the seal caps 17a in a state where bolt holes 18c correspond to bolt holes 7e (see FIG. 13C). By screwing the bolts 19 in the bolt holes 18c and 7e, the seal caps 17a are clamped and integrated between the seal cap retainers 18a and the first piston head 17c. Further, the seal caps 17b are clamped and integrated between the seal cap retainers 18b and the second piston head 18c as well.

An example of the structure of the first piston unit 7 is shown in FIGS. 14A and 14B. A plurality of circular grooves 7g are formed in an outer circumferential face of each of the first piston head sections 7c. A piston ring (sealing member) 7h is fitted in each of the circular grooves 7g. The first piston unit 7 is attached to the opening part 20 of the main body case 3. The sealing members 7h slide on the inner faces 21f of the cylinders 21. By fitting cylinder heads (not shown) to the cylinders 21, airtightness of cylinder chambers can be highly maintained.

FIG. 18 shows an example of the first piston unit 7 which is attached in a vacuum pump for air suction. The erecting section 17c of the seal cap 17a is headed inside and fitted to the stepped part 7f formed on the end face of the first piston head section 7c. The seal cap retainer 18a is stacked on the seal cap 17a and the bolt 19 is screwed, so that the seal cap 17a is clamped and integrated between the seal cap retainer 18a and the first piston head 7s (see FIG. 4).

As shown in FIGS. 15A and 15B, the cylinder 21 has a flange 21e, which is formed along an edge of an opening part 21a, and a cylindrical body part 21c is extended from the flange 21e. The first piston head sections 7c of the first piston unit 7 and the second piston heads 8c of the second piston unit 8 slide on the inner faces 21f of the cylindrical body parts 21c and the flanges 21b (see FIGS. 1 and 2).

Two through-holes 21d are formed in the flange 21b. The cylindrical body part 21c is inserted into the opening part 20 of the main body case 3 (see FIG. 3), and the flange 21b is brought into contact with the side face of the main body case 3. At that time, the through-holes 21d correspond to bolt holes 1d of the first case 1 and bold holes 2d of the second case 2. Therefore, the cylinders 21 are fixed to the main body case 3 by screwing bolts 22 into the through-holes 21e and the bolt holes 1d and 2d (see FIG. 4).

In FIGS. 15A and 15B, a plurality of bolt holes 21e are formed in the flange 21b. The bolt holes 21e are used when the cylinder head is stacked on and fixed to the cylinder 21 by bolts.

In FIGS. 11A and 11B, an opening part 20a is formed in each of four side faces of the first case 1. A bearing retainer part 1a is formed at an axial end of the first case 1. A first bearing 13a is fitted to the bearing retainer part 1a (see FIG. 3). An opening part 1b is formed in the center of the bearing retainer part 1a. The shaft 4, which is integrated with the first balance weight 9, is pierced through the first bearing 13a, which is retained by the bearing retainer part 1a, and outwardly projected from the main body case 3 via the opening part 1b (see FIG. 3). Bolt holes 1c are respectively formed at four corners of the first case 1, and bolts 3a (see FIG. 1) will be screwed into the bolt holes 1c. Further, bolt holes 1d are formed in the four side faces of the first case 1, and bolts 22 (see FIG. 1) will be screwed into the hold holes 1d.

In FIGS. 12A and 12B, an opening part 20b is formed in each of four side faces of the second case 2. A bearing retainer part 2a is formed at an axial end of the second case 2. A second bearing 13b is fitted to the bearing retainer part 2a (see FIG. 3). An opening part 2b is formed in the center of the bearing retainer part 2a. The shaft section 10c, which is integrated with the second balance weight 10, is pierced through the second bearing 13b, which is retained by the bearing retainer part 2a (see FIG. 3). Bolt holes 2c are respectively formed at four corners of the second case 2, and the bolts 3a (see FIG. 1) will be screwed into the bolt holes 2c in a state where the bolt holes 2c correspond to the bolt holes 1c of the first case 1. Further, bolt holes 2d are formed in the four side faces of the second case 2, and the bolts 22 (see FIG. 1) will be screwed into the hold holes 2d.

Next, the assembly structure of the rotary type cylinder device will be explained with reference to FIG. 4.

The inner bearings 15a and 15b are attached to the bearing retainer parts 6c. The first crank shaft 5 is fitted in the center hole of the first cylindrical section 6a, to which the inner bearings 15a and 15b have been attached (see FIG. 3). The first and second piston units 7 and 8 are fitted, in the second cylindrical sections 6b respectively, with the outer bearings 16a and 16b, to form crisscross arrangement.

The first and second balance weights 9 and 10 are respectively fitted to the both ends of the first crank shaft 5. The pins 11a and 11b are fitted in the pinholes 5b and the bolts 12a and 12b are screwed so as to integrate the first and second balance weights 9 and 10 to the first crank shaft 5. The first bearing 13a is fitted in the bearing retainer part 1a of the first case 1, and the second bearing 13b is fitted in the bearing retainer part 2a of the second case 2. The shaft 4 is fitted in the first bearing 13a, the shaft section 10c of the second balance weight 10 is fitted in the second bearing 13b, and the first and second cases 1 and 2 are combined to form the main body case 3. Therefore, the first crank shaft 5, the first and second balance weights 9 and 10 and the composite piston assembly P (see FIG. 2) are accommodated in the main body case 3 (see FIG. 1). The bolt holes 1c are corresponded to the bolt holes 2c, and then the bolts 3a are screwed thereinto, so that the main body case 3 (see FIG. 1) can be completely assembled. Finally, the cylinders 21 are fitted into the opening parts 20 (see FIGS. 2 and 3) respectively formed in the four side faces of the main body case 3, and then the first and second cylinder head parts 7c and 8c are slidably fitted into the opening parts 21a of the cylinders 21 respectively (see FIG. 2), so that the rotary type cylinder device can be completed.

In the above described rotary type cylinder device, first rotational balance of the first and second piston units 7 and 8 around the second virtual crank shafts 14a and 14b, second rotational balance of the composite piston assembly P around the first crank shaft 5 and third rotational balance of the first crank shaft 5 and the composite piston assembly P around the shaft 4 are uniformly produced by only the first and second balance weights 9 and 10.

With this structure, even if the first and second piston units 7 and 8, which are attached to the second cylindrical sections 6b, are linearly reciprocally moved in the radial directions of a circle 23 (see FIG. 5A) around the shaft 4 (i.e., a circular orbit of the second virtual crank shafts 14a and 14b) by revolving the first crank shaft 5 around the shaft 4 and revolving the composite piston assembly P around the first crank shaft 5. Deviations of the center of gravities of the first and second piston units 7 and 8, which are caused by the linear reciprocating motions thereof, are repaired by producing balances, so that noise can be reduced. By reducing rotational vibration, mechanical loss caused by the linear reciprocating motions of the piston heads can be prevented, so that energy converting efficiency of the first and second piston units 7 and 8 can be greater than that of the conventional reciprocal type driving mechanism. Further, a vibration-proof mechanism, e.g., damper, can be simplified.

The rotary motions of the first crank shaft 5 and the second virtual crank shafts 14a and 14b around the shaft 4 and the linear reciprocating motions of the first and second piston units 7 and 8 will be explained with reference to FIGS. 5A-5L. In FIGS. 5A-5L, the center O of the circle 23 corresponds to the axis of the shaft 4. The first crank shaft 5 is shifted from the center O. The second virtual crank shafts 14a and 14b are revolved, without slip, by revolving the first crank shaft 5. Number of the second virtual crank shafts 14a and 14b is equal to that of the piston units 7 and 8.

A distance r between the center O (the shaft 4) and the axis of the first crank shaft 5 is an arm length (revolving radius) of the first virtual crank arm and the second virtual crank arm. The first crank shaft 5 is revolved around the shaft 4 (the center O) along a circular orbit 30 whose radius is equal to the arm length r of the first virtual crank arm. The second virtual crank shafts 14a and 14b are apparently revolved around the first crank shaft 5 along a circular orbit (virtual circle) 24 whose radius is equal to the arm length r of the second virtual crank arm. Therefore, the first and second piston units 7 and 8 can be reciprocally moved in the radial directions of the circle 23 whose center is the center O and whose radius R is equal to the diameter 2r of the virtual circle 24.

In the present embodiment, the axes of the second cylindrical sections 6b, to which the first and second piston units 7 and 8 are fitted in the crisscross form, are the second virtual crank shafts 14a and 14b. In FIG. 5A, the second virtual crank shafts 14a and 14b are disposed on the virtual circle 24, having the radius of r, around the first crank shaft 5 with a phase difference of 180 degrees. The second virtual crank shaft 14a is located at an intersection point (the lowermost point) of the circle 23 and the diameter R1; the second virtual crank shaft 14b is located at the center O of the circle 23 (the axis of the shaft 4). The first crank shaft 5 is separated the distance r from the center O of the circle 23.

In case of revolving the first crank shaft 5 around the center O of the circle 23 in the counterclockwise direction will be explained. Note that, the virtual circle 24 revolves, without slip, along the circle 23 in the clockwise direction. In each of FIGS. 5A-5L, the first crank shaft 5 is shifted by 30 degrees.

When the first crank shaft 5 is revolved 90 degrees, in the counterclockwise direction, from the position shown in FIG. 5A, the first crank shaft 5 is moved to the position shown in FIG. 5D. While this operation, the second virtual crank shaft 14a is moved, along the diameter R1 of the circle 23, to the center O, and the second virtual crank shaft 14b is moved to an intersection point (the rightmost point) of the diameter R2, which perpendicularly crosses the diameter R1, and the circle 23.

When the first crank shaft 5 is further revolved 90 degrees, in the counterclockwise direction, from the position shown in FIG. 5D, the first crank shaft 5 is moved to the position shown in FIG. 5G. While this operation, the second virtual crank shaft 14a is moved to an intersection point (the uppermost point) of the circle 23 and the diameter R1, and the second virtual crank shaft 14b is moved to the center O of the circle 23.

When the first crank shaft 5 is further revolved 90 degrees, in the counterclockwise direction, from the position shown in FIG. 5G, the first crank shaft 5 is moved to the position shown in FIG. 5J. While this operation, the second virtual crank shaft 14a is moved to the center O of the circle 23, and the second virtual crank shaft 14b is moved to an intersection point (the leftmost point) of the circle 23 and the diameter R2.

When the first crank shaft 5 is further revolved 90 degrees, in the counterclockwise direction, from the position shown in FIG. 5J, the first crank shaft 5 is moved to the position shown in FIG. 5A. While this operation, the second virtual crank shaft 14a is moved to an intersection point (the lowermost point) of the circle 23 and the diameter R1, and the second virtual crank shaft 14b is moved to the center O of the circle 23.

By revolving the first crank shaft 5 around the center O (the shaft 4), the second virtual crank shaft 14a is reciprocally moved along the diameter R1 of the circle 23, which is the circular orbit of the virtual circle 24, and the second virtual crank shaft 14b is reciprocally moved along the diameter R2 of the circle 23.

With the rotary motion of the first crank shaft 5 along the circular orbit 30, which has the radius r from the shaft 4 (the center O), and the rotary motions of the second virtual crank shafts 14a and 14b along the circular orbit, which has the radius r from the first crank shaft 5, the first piston unit 7, which is fitted to the second cylindrical section 6b whose axis corresponds to the second virtual crank shaft 14a, is repeatedly reciprocally moved along the diameter R1 of the circle 23, whose radius is 2r and whose center corresponds to the axis of the shaft 4; the second piston unit 8, which is fitted to the second cylindrical section 6b whose axis corresponds to the second virtual crank shaft 14b, is repeatedly reciprocally moved along the diameter R2 of the circle 23, whose radius is 2 r and whose center corresponds to the axis of the shaft 4.

As shown in FIGS. 6A-6C, for example, first and second cylinder heads 25 and 26 are respectively attached to the cylinders 21, in which the first and second piston head sections 7c and 8c are accommodated respectively, by using the bolt holes 21e (see FIGS. 15A and 15B) to respectively face the first and second piston head sections 7c and 8c, so that cylinder chambers 27a, 27b, 27c and 27d are formed. A fluid outlet 28 and a fluid inlet 29 are provided to each of the cylinder chambers 27a, 27b, 27c and 27d.

For example, by rotating the shaft 4 by a motor, etc., the first crank shaft 5 and the eccentric cylindrical body 6 are revolved. The eccentric cylindrical body 6 is revolved around the first crank shaft 5, so that the first and second piston units 7 and 8 are linearly reciprocally moved in the radial directions of the circle 23 (see FIG. 5A), which has the radius of r from the shaft 4. While this operation, a fluid is sucked into the cylinder chambers 27a, 27b, 27c and 27d via the fluid inlets 29 and discharged therefrom via the fluid outlets 28. Therefore, a compressor or a pump can be realized.

The rotary motion of the shaft 4 and the linear reciprocating motions of the first and second piston head sections 7c and 8c will be explained with reference to FIGS. 19-22.

In FIG. 19, the shaft 4 is located at the initial position; in FIG. 20, the shaft 4 is rotated 90 degrees from the initial position; in FIG. 21, the shaft 4 is rotated 180 degrees from the initial position; and in FIG. 22, the shaft 4 is rotated 270 degrees from the initial position. In FIGS. 19 and 20, the first piston unit 7 is moved upward, and the second piston unit 8 is moved rightward. The fluid is sucked into the cylinder chambers 27a and 27c; the fluid is discharged from the cylinder chambers 27b and 27d. In FIGS. 20 and 21, the first piston unit 7 is moved upward, and the second piston unit 8 is started to move leftward. The fluid is discharged from the cylinder chambers 27b and 27c; the fluid is sucked into the cylinder chambers 27a and 27d. In FIGS. 21 and 22, the first piston unit 7 is started to move downward, and the second piston unit 8 is moved leftward. The fluid is discharged from the cylinder chambers 27a and 27c; the fluid is sucked into the cylinder chambers 27b and 27d.

Note that, the first and second piston head sections 7c and 8c need not have the circular shapes, so they may have polygonal shapes. In case of using a part of the piston units assembled in a compressor as a vacuum pump, the device can be used as a hybrid type pump.

In this case, the seal caps 17a and 17b are attached to the piston head section, which is used as the compressor, and their erecting sections 17c are outwardly extended in the sliding direction; the seal caps 17a and 17b are also attached to the piston head section, which is used as the vacuum pump, preferably their erecting sections 17c are inwardly extended in the sliding direction (see FIG. 18). In case that the fluid is water or a liquid, the seal caps 17a and 17b may be omitted.

In the above described embodiment, the rotary type cylinder device has two piston units. Number of the piston units may be three or more. In case of the device having three piston units, for example, three second virtual crank shafts are disposed, on the virtual circle 24 shown in FIG. 5A, around the first crank shaft 5 with angular separation of 120 degrees.

In one of the piston units, the piston head sections may be omitted. If the second virtual crank shaft corresponds to the axis of the shaft 4 in one piston unit, a rotational dead point will occur. However, by omitting the piston head sections in one of the piston units, the occurrence of the rotational dead point in the one piston unit can be avoided, so that the rotary motion of the rotary type cylinder device can be continued.

In the above described embodiment, the first and second piston head sections 7c and 8c are attached to the eccentric cylindrical body 6 so as to reciprocally move in the same X-Y plane. In case that the eccentric cylindrical body is divided into a plurality of parts, a plurality of the piston units can be arranged in the height direction (the Z-axis direction) and crisscrossed at different heights.

In the above described embodiment, the first and second piston units 7 and 8 are crisscrossed, but their arrangement is not limited. For example, the first and second piston units 7 and 8 may be disposed around the first crank shaft 5 with a phase difference of 60 degrees, etc.

As shown in FIGS. 14A and 14B, piston rings 7h are respectively provided to the first and second piston head sections 7c and 8c. This structure may be applied to internal-combustion engines.

For example, if air intake valves, air release valves, an injector, a spark plug, etc. are provided to each of the cylinder chambers, which are formed by attaching the cylinder heads to the cylinders 21, this structure can be applied to engines. In this case, the first and second piston units 7 and 8 are linearly reciprocally moved by explosive-burning fuel in the cylinder chambers, so that the linear reciprocal motions of the piston units can be converted into and outputted as the rotary motions of the eccentric cylindrical body 6 and the first crank shaft 5 (the composite piston assembly P) around the shaft 4.

FIG. 23A is a partial sectional view of the cylinder 21 of the first piston unit 7 used for a compressor or a hydraulic rotary machine, and FIG. 23B is a partial sectional view of the cylinder 21 of the first piston unit 7 used for an internal-combustion engine. The second piston unit 8 has the same structure, so explanation will be omitted.

In FIG. 23A, a gap G between the inner face 21f of the cylinder 21 and outer circumferential faces 7j and 18d of the piston head section 7c and the seal cap retainer 18a is designed, with considering dimension change caused by machining error and temperature variation, so as to prevent mechanical interference. The gap G is minimized, so that the erecting section 17c of the seal cap 17a can slide, without biting the inner face 21 of the cylinder 21, and maintain sealing property.

In FIG. 23B, a gap G is formed between the circular groove 7g and the piston ring (sealing member) 7h so as to set the piston ring 7h in the circular groove 7g of the piston head section 7c. In case of balancing the third rotational balance of the first crank shaft 5 and the composite piston assembly P around the shaft 4, the motion of the piston ring 7h, in the radial direction, in the cylinder is limited, so the third rotational balance cannot be produced perfectly. Thus, a preferable error range of balancing design is 3% or less.

As shown in FIG. 6A, four cylinder heads are provided in a 2-piston/4-head rotary type cylinder device, so a part of the cylinder heads may be used for generating positive pressure and the rest cylinder heads may be used for generating negative pressure.

Further, multistage compression of air can be performed by four cylinder heads. In this case, strokes of the piston units cannot be changed, so diameters of a piston and a cylinder must be changed even in one piston unit. Preferably, the first to third rotational balances are produced by the first and second balance weights 9 and 10.

As described above, the first crank shaft is revolved around the shaft 4 and the eccentric cylindrical body 6 is revolved around the first crank shaft 5 by rotating the shaft 4, so that the first and second piston units 7 and 8, which are attached to the second cylindrical sections 6b whose axes correspond to the second virtual crank shaft 14a and 14b, are linearly reciprocally moved in the radial directions of the circle 23 (see FIG. 5A), which has the radius r from the shaft 4, along the circular orbit (hypocycloid) of the second virtual crank shafts 14a and 14b.

While the operation, the first rotational balance relating to the first and second piston units 7 and 8 around the second virtual crank shafts 14a and 14b (see FIG. 10B), the second rotational balance relating to the composite piston assembly P around the first crank shaft 5 and the third rotational balance relating to the first crank shaft 5 and the composite piston assembly P around the shaft 4 can be produced by the first and second balance weights 9 and 20. Further, deviations of gravity centers caused by the linear and reciprocal motions of the first and second piston units 7 and 8, can be repaired, so that a compact rotary type cylinder device, which is capable of reducing rotational vibration and noise, can be produced.

By reducing rotational vibration caused by rotation around the shaft 4, mechanical loss can be reduced and energy converting efficiency can be improved. Further, a vibration-proof mechanism, e.g., damper, can be simplified.

In comparison with conventional devices, number of elements constituting the crank shaft and the crank arms can be reduced, so that the simple crank mechanisms can be realized.

If the first rotational balance is lost, the second and third rotational balances are lost, too. Japanese Laid-open Patent Publication No. P63-24158A discloses a hypocycloid rotary type cylinder device capable of producing balances of rotatable members (see column 6, line 31-34). However, in the patent publication, only balances of a shaft and a crank shaft are produced. The technical idea of producing rotational balances of a slider connected to the crank shaft and rotatable members, including a piston assembly, connected to the slider is not disclosed, at all. Conventionally, there was no technical idea of repairing deviation of gravity center caused by linear and reciprocal motion of a piston unit, so vibration caused by the deviation of gravity center was absorbed by a vibration absorbing mechanism, e.g., damper.

On the other hand, in the rotary type cylinder device of the present invention, the rotatable members including the shaft 4, the first crank shaft 5 and the second virtual crank shafts 14a and 14b are capable of revolving at fixed revolving speeds with respect to the centers, the first to third rotational balances are produced by the first and second balance weights 9 and 10, so that a total balance is well maintained. Further, the deviations of gravity centers caused by the linear and reciprocal motions of the first and second piston units 7 and 8 can be repaired. Therefore, the hypocycloid rotary type cylinder device, which is capable of restraining rotational vibration caused by the rotary motions around the shaft 4 and the linear reciprocal motions of the first and second piston units 7 and 8, can be produced.

Balancing performance of a compressor of 46 cc displacement, which relates to the present invention, and a conventional similar mechanism will be explained. Note that, eccentric weight of the first crank shaft 5 around the shaft 4 is 10 g, and eccentric weight of the composite piston assembly P attached to the first crank shaft 5 is 210 g (including first and second piston units 7 and 8, the eccentric cylindrical body 6, the inner bearings 15a and 15b and the outer bearings 16a and 16b).

In the present invention, the first to third rotational balances are produced by the first and second balance weights 9 and 10, so that the rotary motion around the shaft 4 can be performed with balancing the eccentric weight of 220 g. Therefore, mechanical loss can be reduced, energy converting efficiency can be improved and noise can be reduced. On the other hand, in Japanese Laid-open Patent Publication No. P63-24158A, only a crank shaft revolved around a shaft is balanced. The balance of the crank shaft (10 g) around the shaft is poorly produced (about 5%). Therefore, rotational vibration must be great, mechanical loss must be great, and energy converting efficiency must be low. Further, the vibration must be absorbed by, for example, damper due to intense noise.

Since the shaft 4 is integrated with at least one of the first and second balance weights 9 and 10, number of parts can be reduced. Further, the first crank shaft 5 can be compactly attached around the shaft 4, in the axial direction and the radial direction, by adjusting the length of the first virtual crank arm, which connects the shaft 4 to the first crank shaft 5. The length of the first virtual crank arm is adjusted by adjusting the revolving radius of the first and second balance weights 9 and 10.

The inner and outer bearings 15a, 15b, 16a and 16b are respectively retained by the bearing retainer parts 6c and 6d, which are formed in the inner circumferential faces of the second cylindrical sections 6b. The first crank shaft 5 is rotatably held by the inner bearings 15a and 15b, and the first and second piston units 7 and 8 are rotatably held by the outer bearings 16a and 16b. Therefore, the composite piston assembly P including the eccentric cylindrical body 6 can be compactly attached, in the axial and radial directions, around the first crank shaft 5 by adjusting the length of the second virtual crank arm, which connects the first crank shaft 5 to the second virtual crank shafts 14a and 14b. The length of the second virtual crank arm is adjusted by adjusting the revolving radius of the second cylindrical sections 6b.

The first and second cylinder head sections 7c and 8c are respectively attached to front ends of the first and second piston units 7 and 8, and the cylinder heads 25 and 26, which respectively face the first and second cylinder head sections 7c and 8c and which form the cylinder chambers 27a-27d, are attached to the main body case 3. In the rotary type cylinder device, the fluid can be introduced into and discharged from the cylinder chambers 27a-27d by the reciprocal motions of the two piston units. Therefore, the rotary type cylinder device can be applied to variety of driving mechanisms, e.g., hydraulic rotary machines, vacuum sucking machines, internal-combustion engines.

All examples and conditional language recited herein are intended for pedagogical purposes to aid the reader in understanding the invention and the concepts contributed by the inventor to furthering the art, and are to be construed as being without limitation to such specifically recited examples and conditions, nor does the organization of such examples in the specification relate to a showing of the superiority and inferiority of the invention. Although the embodiments of the present invention has been described in detail, it should be understood that the various changes, substitutions, and alternations could be made hereto without departing from the spirit and scope of the invention.

Number	Date	Country	Kind
2009-245920	Oct 2009	JP	national
2010-053633	Mar 2010	JP	national

ROTARY CYLINDER DEVICE

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CPC

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