[0001] This invention relates to a scroll type fluid displacement apparatus including a
pair of scroll members each comprising an end plate and a spiral wrap extending from
one side of said end plate, said spiral wrap having a groove formed in the axial end
surface thereof along the spiral curve, a seal element being fitted within said groove
and said spiral wraps interfitting at an angular and radial offset to make a plurality
of line contacts which define at least one pair of fluid pockets, driving means operatively
connected to one of said scroll member for orbiting said one scroll member relative
to the other scroll member and for preventing rotation of said one scroll member to
change the volume of the fluid pockets.
[0002] Scroll type fluid displacement apparatus are well known in the prior art. For example,
U.S. Patent No. 801,182 (Creux) discloses a device including two scroll members each
having a circular end plate and a spiroidal or involute spiral element. These scroll
members are maintained angularly and radially offset so that both spiral elements
interfit to make a plurality of line contacts between their spiral curved surfaces
to thereby seal off and define at least one pair of fluid pockets. The relative orbital
motion of the two scroll members shifts the line contacts along the spiral curved
surfaces and, therefore, the fluid pockets change in volume. Since the volume of the
fluid pockets increases or decreases dependent on the direction of the orbiting motion,
the scroll type fluid displacement apparatus is applicable to compress, expand or
pump fluids.
[0003] In comparison with conventional fluid displacement apparatus of the piston type,
the scroll type fluid displacement apparatus has certain advantages, such as reduced
parts and continuous compression of fluid. However, one of the problems encountered
in prior art scroll type fluid displacement apparatus is the ineffective sealing of
the fluid pockets. Axial and radial sealing of the fluid pockets must be maintained
in a scroll type fluid displacement apparatus in order to achieve efficient operation.
The fluid pockets in the scroll type fluid displacement apparatus are defined by both
line contacts between the interfitting spiral elements and axial contacts between
the axial end surfaces of the spiral elements and the inner end surface of the end
plates.
[0004] Figs. 1 to 5 illustrate a simple construction of an axial sealing mechanism. Fig.
1 shows a diagrammatic sectional view illustrating the spiral element of the fixed
and orbiting scroll members and Fig. 2 shows a sectional view taken along a line II-II
in Fig. 1. !n the construction, a seal element 1 is loosely fitted into a groove 2
formed in the axial end surface of each spiral element 3, i.e., the width W
2 of seal element 1 is formed smaller than the width W, of groove 2 and also the depth
D
2 of seal element 1 is formed smaller than the depth D, of groove 2, as shown in Fig.
2. As a substitute for a mechanical axial force urging device, the pressurized fluid
then is introduced into groove 2 from adjacent pockets through the gap C, which is
defined between the side surface of seal element 1 and the inner end surface of groove
2, and seal element 1 is urged toward the axial and radial direction to contact with
the facing end plate 4 and the one side surface of groove 2. The urging force towards
radial direction is shown by arrow in Fig. 1.
[0005] As shown in Fig. 1, the fluid within a high pressure chamber A, which is defined
by the center portions of the spiral elements, leaks into the adjacent lower pressure
chambers B, and B
2, and also fluid within lower pressure chambers B, and B
2 leaks into the suction chamber defined by the outer peripheral portion of the scroll
members. Since groove 2 in which seal element 1 is disposed extends from the center
of spiral element to near the terminal end thereof. Furthermore, as shown in Fig.
4 which is a sectional view taken along a line IV-IV in Fig. 1, the fluid within the
high pressure chamber A or lower pressure chambers B, and B
2 leaks into the adjacent lower chambers B, and B
2 or the suction chamber through the contact surface between the axial end surface
of seal element 1 and the inner end surface of facing end plate 4. Therefore, the
volume efficiency of the compressor is reduced.
[0006] A scroll type fluid displacement apparatus of the above-mentioned kind using another
technique for improving the axial seal is known from the US Patent 3,994,636. In the
apparatus described therein the end surface of each spiral element facing the end
plate of the other scroll member is provided with a groove formed along the spiral.
A seal element is placed within the groove and an axial force urging device, such
as a spring, is placed behind the seal element to urge the seal element toward the
facing end surface of the end plate to thereby effect axial sealing.
[0007] In both types of apparatus shown, in order to avoid the fluid leakage from the high
pressure chamber or lower pressure chambers to lower pressure chamber or suction chamber,
the clearance between the axial end surface of spiral element and the inner end surface
of facing end plate will be made as small as possible to reduce the gap C. However,
during the operation of the compressor, the axial end surface of the spiral element
comes into contact with the inner end surface of the facing end plate and thereby
cause the abnormal wearing. These disadvantages arise because of the following conditions.
Intrinsically, both scroll members are expanded each other by the pressure within
the fluid pockets and the orbiting scroll member is pushed against an axial thrust
bearing device. However, the driving point of the orbiting scroll member, which point
is placed on the side surface of the end plate opposite the spiral element extending,
is offset from the acting point of the reaction force caused by the compression of
gas, which point is placed on the intermediate along the height of spiral element
of the orbiting scroll member. Therefore, the resultant moment causes the axial slant
of the orbiting scroll member. Also, in a transit condition, such as the moment of
turning on or off the magnetic clutch or sudden change of the operating condition,
the orbiting scroll member is not uniformly pushed against the axial thrust bearing
which is placed between the end plate of the orbiting scroll member and the fixed
plate portion. Therefore, the axial slant of the orbiting scroll member is caused.
[0008] Furthermore, the seal element is disposed within the groove in an axially and radially
floating condition, and pushed against the facing end plate by pressurized fluid.
However, as shown in Fig. 1 and Fig. 5 which is a sectional view taken along a line
V-V in Fig. 1, a part of seal element 1 extends to the no pressure differential area.
The area is shown by a part of D in Fig. 1. In this condition, the seal element 1
cannot receive the urging force toward the axial and radial direction, and seal element
1 can therefore freely move within the groove 2 and comes into contact with the inner
end surface of facing end plate 4, as shown in Fig. 5, to thereby cause the abnormal
wear.
[0009] It is a primary object of this invention to provide an improvement in a scroll type
fluid displacement apparatus with high volumetric efficiency and thus with high energy
efficiency.
[0010] It is another object of this invention to provide a scroll type fluid displacement
apparatus wherein the abnormal wear of the axial seal element is prevented and the
axial sealing of the fluid pockets is enhanced to attain a long life.
[0011] It is still another object of this invention to provide a scroIs type fluid displacement
apparatus wherein the wear of the scroll member is prevented and the endurance life
of the apparatus is improved.
[0012] It is a further object of this invention to provide a scroll type fluid displacement
apparatus which is simple in construction and simple in manufacturing to achieve the
above objects.
[0013] A scroll type fluid displacement apparatus according to this invention includes a
pair of scroll members each comprising a circular end plate and a spiral wrap extending
from one side of the circular end plate. A groove is formed in the axial end surface
of each spiral wrap and extends along the spiral curve of the wrap. A seal element
is fitted in the groove. The axial dimension of the seal element is greater than the
depth of the groove. The axial end surface of seal element is, therefore, usually
contact with the inner end surface of the facing end plate without any axial force
urging device, after assembling the compressor. Accordingly, the gap between the seal
element and the groove which defines the channel of leakage fluid is reduced.
[0014] Further objects, features and other aspects of this invention will be understood
from the detailed description of the preferred embodiment of this invention referring
to the annexed drawings.
Fig. 1 is a diagrammatic sectional view illustrating the spiral element of the fixed
and orbiting scroll members;
Fig. 2 is a sectional view taken along a line II-II in Fig. 1;
Fig. 3 is a perspective view of an axial end portion of the spiral element illustrating
the leakage channel of the high pressure fluid;
Fig. 4 is a sectional view taken along a line IV-IV in Fig. 1;
Fig. 5 is a sectional view taken along a line V-V in Fig. 1;
Fig. 6 is a vertical sectional view of the compressor unit type of fluid displacement
apparatus according to one embodiment of this invention;
Fig. 7 is an exploded perspective view of the driving mechanism of the embodiment
of Fig. 6;
Fig. 8 is a perspective view of the scroll member in the embodiment of Fig. 6;
Fig. 9 is a sectional view taken along a line IX-IX in Fig. 8; and
Fig. 10 is a sectional view of an axial end portion of the spiral element according
to another embodiment of this invention.
[0015] Referring to Fig. 6, a fluid displacement apparatus in accordance with the present
invention is shown which is a scroll type refrigerant compressor. The compressor includes
a compressor housing 10 having a front end plate 11 and a cup shaped casing 12 fastened
to an end surface of front end plate 11. An opening 111 is formed in the center of
front end plate 11 for supporting a drive shaft 13. An annular projection 112, concentric
with opening 111, is formed on the rear end surface of front end plate 11 facing cup
shaped casing 12. An outer peripheral surface of annular projection 112 fits into
an inner wall of the opening of cup shaped casing 12. Cup shaped casing 12 is fixed
on the rear end surface of front end plate 11 by a fastening device, such as bolts
and nuts, so that the opening of cup shaped casing 12 is covered by front end plate
11. An 0- ring 14 is placed between the outer peripheral surface of annular projection
112 and the inner wall of cup shaped casing 12. Front end plate 11 has an annular
sleeve 15 projecting from the front end surface thereof; this sleeve 15 surrounds
drive shaft 13 to define a shaft seal cavity. As shown in Fig. 6, sleeve 15 is attached
to the front end surface of front end plate 11 by screws 16, one of which is shown
in Fig. 6. An O-ring 17 is placed between the front end surface of front end plate
11 and an end surface of sleeve 15 to seal the mating surface of front end plate 11
and sleeve 15. Alternatively, sleeve 15 may be formed integral with front end plate
11.
[0016] Drive shaft 13 is rotatably supported by sleeve 15 through a bearing 18 disposed
within the front end of sleeve 15. Drive shaft 13 has a disk shaped rotor 19 at its
inner end; disk shaped rotor 19 is rotatably supported by front end plate 11 through
a bearing 20 disposed within opening 111 of front end plate 11. A shaft seal assembly
21 is assembled on drive shaft 13 within the shaft seal cavity of sleeve 15.
[0017] A pulley 22 is rotatably supported by a bearing 23 on the outer surface of sleeve
15. An electromagnetic coil 24, which is received in an annular cavity of pulley 22,
is mounted on the outer surface of sleeve 15 by a supported plate 241. An armature
plate 25 is elastically supported on the outer end of drive shaft 13 which extends
from sleeve 15. A magnetic clutch is formed by pulley 22, magnetic coil 24 and armature
plate 25. Thus, drive shaft 13 is driven by an external power source, for example,
an engine of vehicle, through a rotation transmitting device, such as the above described
magnetic clutch.
[0018] A number of elements are located within the inner chamber of cup shaped casing 12
including a fixed scroll 26, an orbiting scroll 27, a driving mechanism for orbiting
scroll 27 and a rotation preventing/thrust bearing device 28 for orbiting scroll 27.
The inner chamber of cup shaped casing 12 is formed between the inner wall of cup
shaped casing 12 and front end plate 11.
[0019] Fixed scroll 26 includes a circular end plate 261, a wrap or spiral element 262 affixed
to or extending from one end surface of circular end plate 261, and a plurality of
internal bosses 263 axially projecting from the end surface of circular end plate
261 on the side opposite spiral element 262 extending. The end surface of each boss
263 is seated on the inner surface of end plate portion 121 of cup shaped casing 12
and is fixed to end plate portion 121 by a plurality of bolts 29, one of which is
shown in Fig. 6. Hence, fixed scroll 26 is fixedly disposed within cup shaped casing
12. Circular end plate 261 of fixed scroll 26 partitions the inner chamber of cup
shaped casing 12 into a rear chamber 30 having bosses 263, and a front chamber 31,
in which spiral element 262 of fixed scroll 26 is located. A sealing member 32 is
disposed within circumferential groove 264 of circular end plate 261 for sealing the
outer peripheral surface of circular end plate 261 and the inner wall of cup shaped
casing 12. A hole or discharge port 265 is formed through circular end plate 261 at
a position near the center of spiral element 262; discharge port 265 connects the
fluid pockets at the center of spiral element 262 and rear chamber 30.
[0020] Orbiting scroll 27, which is disposed in front chamber 31, includes a circular end
plate 271 and a wrap or spiral element 272 affixed to or extending from one end surface
of circular end plate 271. The spiral elements 262 and 272 interfit at an angular
offset of 180° and a predetermined radial offset. The spiral elements define at least
a pair of fluid pockets between their interfitting surfaces. Orbiting scroll 27 is
connected to the driving mechanism and the rotation preventing/thrust bearing device
28. The driving mechanism and the rotation preventing/thrust bearing device 28 effect
orbital motion of orbiting scroll 27 by the rotation of drive shaft 13 to thereby
compress fluid passing through the compressor.
[0021] Referring to Figs. 6 and 7, the driving mechanism of orbiting scroll 27 will now
be described. As described above, drive shaft 13, which is rotatably supported by
sleeve 15 through bearing 18, has disk shaped rotor 19 at its inner end. Disk shaped
rotor 19 is also rotatably supported by front end plate 11 through bearing 20. A crank
pin or drive pin 191 projects axially from an axial end surface of disk shaped rotor
19 and is radially offset from the center of drive shaft 13. Circular end plate 271
of orbiting scroll 27 is provided with a tubular boss 273 axially projecting from
the surface opposite to the end surface from which spiral element 272 extends. A discoid
or short axial bushing 33 fits into boss 273, and is rotatably supported therein by
a bearing, such as needle bearing 34. An eccentric hole is formed on bushing 33; the
eccentric hole is radially offset from the center of bushing 33. Drive pin 191, which
is surrounded by bearing 39, fits into the eccentric hole. Therefore, bushing 33 is
driven by the revolution of drive pin 191 to thereby rotate within bearing 34. The
spiral element of orbiting scroll 27 is thus pushed against the spiral element of
fixed scroll 26 due to the moment created by the differential of the driving point
and the reaction point of pressure gas for securing the line contacts.
[0022] Rotation preventing/thrust bearing device 28 is placed between the inner end surface
of front end plate 11 and the end surface of circular end plate 271 which faces the
inner end surface of front end plate 11, as shown in Fig. 6, and includes a fixed
ring 281, which is fastened against the axial end surface of annular projection 112,
an orbiting ring 282, which is fastened against the end surface of circular end plate
272 by a fastening device, and a bearing element, such as a plurality of spherical
balls 283. Rings 281 and 282 have a plurality of indentations 284 and 285 and one
of spherical ball 283 is retained between each of these indentations 284 and 285.
Therefore, the rotation of orbiting scroll 27 is prevented by balls 283, which interact
with the edges of indentations 284 and 285 to prevent rotation. Also, these balls
283 carry the axial thrust load from orbiting scroll 27. Therefore, orbiting scroll
27 orbits while maintaining its angular orientation to fixed scroll 26.
[0023] As orbiting scroll 27 orbits, the line contacts between spiral element 262 and 272
shift toward the center of the spiral elements along the surfaces of the spiral elements.
The fluid pockets defined by the line contacts between spiral elements 262 and 272
move toward the center with a consequent reduction of volume, to thereby compress
the fluid in the fluid pockets. Therefore, fluid or refrigerant gas introduced into
front chamber 31 from an external fluid circuit through an inlet port 35 mounted on
the outside of cup shaped casing 12 is taken into the fluid pockets formed at the
outer portion of spiral elements 262 and 272. As orbiting scroll 27 orbits, the fluid
in the fluid pockets is compressed as the pockets move toward the center of the spiral
element. Finally, the compressed fluid is discharged into rear chamber 30 through
hole 265, and thereafter, the fluid is discharged to the external fluid circuit through
an outlet port 36 formed on cup shaped casing 12.
[0024] Referring to Fig. 8, each spiral element 262 and 272 is provided with a groove 37
formed in its axial end surface along the spiral curve of the spiral element. Groove
37 extends from the inner end portion of the spiral element to a position close to
the terminal end of the spiral element. A seal element 38 is fitted within each groove
37. In this construction, as shown in Fig. 9, at least the axial dimension D
2 of seal element 38 is formed greater than the depth D, of groove 37. Seal element
38 thus usually contacts with the inner end surface of facing circular end plate without
any axial force urging device. Therefore, axial sealing of the fluid pockets will
be secured.
[0025] In this construction, the gap C defined by the end plate 261, side wall of the spiral
element 262, the axial end surface of facing spiral element 272 and seal element 38
fitted in the groove 37 of facing spiral element 272 will be reduced, and the amount
of the fluid leakage from the high pressure chamber to lower pressure chamber is reduced.
Therefore, the volume efficiency of the compressor is improved.
[0026] Furthermore, the width of the groove will be made as large as possible and the width
of the seal element is made larger dependent on the width of the groove. Therefore,
the width of contact surface between the seal element and the inner end surface of
facing end plate will be made larger, so that the fluid leakage through the contact
surface will be reduced.
[0027] In this construction, the width W
2 of seal element 38 is formed smaller than the width W, of groove 37. Therefore, the
problem in that the assembling of the seal element into the groove would be in difficulty
which is caused by the limit of the tolerance to surface roughness or width of the
groove to be worked, or the width of seal element, is resolved. Also, ,if seal element
is formed of hard plastic and/or self-lubricating material, the deformation of the
seal element would occur in the long operation of the compressor. That is, the axial
dimension of the seal element is reduced by the axial slant of the scroll, while the
width of the seal element is increased. The increase of the width can be permitted
by the differential of the width, and thereby secures the long life sealing of the
fluid pockets.
[0028] Fig. 10 shows an alternative embodiment of the present invention which is characterized
in that the width W
2 of seal element 38 is formed substantially same as the width W, of groove 37. The
construction will more reduce the gap C, and therefore, the amount of fluid leakage
is reduced and volume efficiency of the compressor is improved.
1. Spiralfluidverdrängereinrichtung mit einem Paar Spiralteile (26, 27), von denen
jedes eine Endplatte (261, 271) und einen spiralförmig gewundenen Steg (262, 272)
der aus der einen Seite der Endplatte (262, 272) herausragt, aufweist, wobei der spiralförmig
gewundene Steg (262, 272) eine Nut (37), die in der axialen Endoberfläche desselben
entlang der Spiralkurve gebildet ist und ein Dichtelement (38), das in die Nut (37)
eingepaßt ist, aufweist und die spiralförmig gewundenen Stege (262, 272) unter einem
Winkel und einem radialen Abstand so zusammengepaßt sind, daß eine Mehrzahl von Linienberührungsstellen
entstehen, die mindestens ein Paar von Fluidtaschen bilden, einer Antriebseinrichtung
(13, 19, 28), die betriebsmäßig mit dem einen Spiralteil (27) verbunden ist, um das
eine Spiralteil (27) relativ zu dem anderen Spiralteil (26) umlaufen zu lassen und
zum Verhindern der Rotation des einen Spiralteils (27) zum Ändern des Volumens der
Fluidtaschen, dadurch gekennzeichnet, daß mindestens die axiale Ausdehnung des Dichtelements
(38) größer gebildet ist also die Tiefe der Nut (37).
2. Spiralfluidverdrängereinrichtung nach Anspruch 1, dadurch gekennzeichnet, daß die
Breite des Dichtelements (38) im wesentlichen der Breite der Nut (37) entspricht.