[0001] This invention relates to a fluid displacement apparatus of the scroll type,such
as a compressor,expander,or pump.
[0002] Scroll type fluid displacement apparatus are well known in the prior art. For example,
U.S.Patent No. 801,182 discloses a scroll type fluid displacement apparatus 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 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. The
volume of the fluid pockets increases or decreases depending on the direction of the
orbiting motion. Therefore, the scroll type fluid displacement apparatus is applicable
to compress,expand or pump fluids. The discussion which follows deals only with scroll
type devices used as compressors for the sake of convenience.
[0003] In comparison with a conventional compressor of the piston-type, the scroll type
compressor has certain advantages,such as fewer parts and continuous compression of
fluid. However, there have been several problems,primarily in the sealing of the fluid
pockets. Sealing of the fluid pockets must be sufficiently maintained at axial and
radial interfaces in the scroll type fluid apparatus, because the fluid pockets are
defined by the line contacts between the interfitting spiral elements and axial contact
between the axial end surfaces of the spiral elements and the inner end surfaces of
the end plates.
[0004] The principles of operation of a typical scroll type compressor will be described
with reference to Figs. 1a-1d,Fig. 2 and Fig. 3. Figs. 1a-1d schematically illustrate
the relative movement of interfitting spiral elements to compress the fluid. Fig.
2 diagrammatically illustrates the compression cycle in the each of the fluid pockets.
Fig. 3 schematically illustrates the typical interfitting relationship of prior art
spiral elements. Figs.1a-1d may be considered to be end view of a compressor wherein
the end plates are removed and only the spiral elements are shown.
[0005] .Two spiral elements 1 and 2 are angularly offset and interfit with one another.
As shown in Fig. 1a, the orbiting spiral element 1 and fixed spiral element 2 make
four line contacts as shown at four points A-D. A pair of fluid pockets 3a and 3b
are defined between line contacts D-C and line contacts A-B, as shown by the dotted
regions. The fluid pockets 3a and 3b are defined not only by the wall of spiral elements
1 and 2 but also by the end plates from which these spiral elements extend. When orbiting
spiral element 1 is moved in relation to fixed spiral element 2 so that the center
0' of orbiting spiral element 1 revolves around the center 0 of fixed spiral element
2 with a radius of 0-0', while the rotation of orbiting spiral element 1 is prevented,a
pair of fluid pockets 3a and 3b shift angularly towards the center of the interfitted
spiral elements with the volume of each fluid pockets 3a and 3b being gradually reduced,as
shown in Figs. 1a-1d. Therefore, the fluid in each pockets is compressed.
[0006] Now, the pair of fluid pockets 3a and 3b are connected to one another while passing
the stage from Fig. 1c.to Fig. 1d and as shown in Fig. 1a, both pockets 3a and 3b
merge at the center portion 5 and are completely connected to one another to form
a single pocket. The volume of the connected single pocket is further reduced by further
revolution of 90° as shown in Figs. 1b,1c and 1d. During the course of rotation, outer
spaces which open in the state shown in Fig. 1b change as shown in Figs. 1c,1d and
1a, to form new sealed off pockets in which fluid is newly enclosed.
[0007] Accordingly, if circular end plates are disposed on,and sealed to, the axial facing
ends of spiral elements 1 and 2, respectively, and if one of the end plates is provided
with a discharge port 4 at the center thereof as shown in figures, fluid is taken
into the fluid pockets at the radial outer portion and is discharged from the discharge
portion 4 after compression.
[0008] Referring to Fig.2 and Fig.1, the compression cycle of fluid in one fluid pocket
will be described. Fig.2 shows the relationship of fluid pressure in the fluid pocket
to crank angle, and shows that the one compression cycle is completed at a crank angle
of 4π in this case.
[0009] The compression cycle begins (Fig.1a) with the outer end of each spiral element in
contact with the opposite spiral element, the suction stroke having finished. The
state of fluid pressure in the fluid pocket is shown at point K in Fig.2. The volume
of the fluid pocket is reduced and compressed by the revolution of the orbiting scroll
member until the crank angle reaches 2π, which state is shown by the point L in Fig.
2. Immediately after passing this state,and hence,passing point L, the pair of fluid
pockets are connected to one another and simultaneously are connected to the space
filled with high pressure,which is connected to the discharge chamber and is formed
at the center of both spiral elements At this time,if the compressor is not provoded
with a discharge valve,the fluid pressure in the connected fluid pockets suddenly
rises to equal the pressure in the discharge chamber. If, however,the compressor is
provided with a discharge valve, the fluid pressure in the connected fluid pockets
rises slightly due to the mixing of the high pressure fluid and the fluid in the connecting
fluid pockets. This state is shown at point M in Fig.2. The fluid in the high pressure
space is further compressed by revolution of the orbiting scroll member until it reaches
the discharge pressure. This state is shown at point N in Fig. 2. When the fluid pressure
in the high pressure space reaches the discharge pressure, the fluid is discharged
to the discharge chamber through the discharge hole by the operation of the discharge
valve. Therefore,fluid pressure in the high pressure space is maintained at the discharge
pressure until a crank angle of 4
1T (point 0).
[0010] Accordingly,one cycle of compression is completed at a crank angle of 4π ,but the
next cycle begins at the mid-point of compression of the first cycle as shown by point
K',L' and M',and the dot-dash . line in Fig.2. Therefore,fluid compression proceeds
continuously by the operation of these cycle.
[0011] Line contact between spiral elements is dinned by several pairs of points, as shown
in Fig.3. However,it is very difficult to attain complete contact at all points. If
the line contact between spiral elements is imperfect at one or more points to form
a gap,fluid leakage through the gap will occur during operation to allow the outer
pockets to contain gas with high pressure than the ideal case. The volumetric efficiency
of the compressor and, hence, its refrigeration capacity will thereby be reduced.
Especially, fluid leakage across the line contact separating pair of fluid pockets
from the high pressure space is very serious problem. If such leakage occurs,the pressure
in the fluid pocket rises, as shown by the dotted lines and letters l,m,n in Fig.2;therefore,the
torque or the power required in the compressing operation is increased as a result,
the energy efficiency ratio (refrigeration capacity performed by a unit horse power)
is greatly reduced. Thus , sealing of the high pressure space must be tightly secured.
[0012] The curve of the spiral elements is usually an involute curve of a circle,each spiral
having the same pitch (the pitch shown as distance a
1-a
2, a
2-a
n, or b
1-b
2, b
2-b
n in Fig.3),and these two spiral elements interfit at an angular and radial offset,so
that the spiral elements make a plurality of line contacts which are represented by
points a
1-a
n and b
1-b
n in Fig.3. Therefore,if the pitch of the spiral element is slightly different or if
the inner and outer wall curve deviates from a true involut curve due to manufacturing
inaccuracies the line contacts will be imperfect, and the apparatus which uses these
spiral elements'will suffer fluid leakage. In order to avoid this problem,high accuracy
is reouired in manufactureing of the spiral elements, resulting in high cost.
[0013] Even when two perfect spiral elements (having no dimentional errors) are interfitted
and used in a compressor,heat developed during operation creats a thermal expansion
of the elements. If the temperature is uniform throughout the spiral elements, the
line contacts between both spiral elements change uniformely, and sealing. of the
fluid pockets is maintained. However, under actualoperating conditions, thermal expansion
of the spiral elements is nouniform due to the temperature gradient,material nouniformitz
or other imperfection resulting in a nouniform pitch variation or deviation of wall
curves from a true involut. This causes a gap at the line contacts between the spiral
elements, resulting in fluid leakage from the high pressure space.
[0014] It is a primary object of this invention to provide an efficient scroll type fluid
displacement apparatus.
[0015] It is another object of this invention to provide a scroll type fluid displacement
apparatus wherein the line contact between the two spiral elements is insured in order
to seal the high pressure space.
[0016] It is still another object of this invention to realize the above objects with a
simple construction,a simple production method and low cost.
[0017] A scroll type fluid displacement apparatus according to this invention includes a
housing and a pair of scroll members. One of the scroll members is fixedly disposed
relative to the housing and has an end plate from which a first spiral wrap extends
into the interior of the housing. The other scroll member is movably disposed for
non-rotative orbital movement within the interior of the housing and has an end plate
from which a second spiral wrap extends. The first and second wrap are interfitted
at an angular and radial offset to make a plurality of line contacts to define at
least one pair of sealed off fluid pockets. A driving mechanism is operatively connected
to the other scroll member to effect its orbital motion, whereby the fluid pockets
move inwardly and change in volume. The two innermost pockets eventually are merged
into a single pocket near the center of the wrap. The center portions of the wrap
are thicker than the remaining portions thereof. The center portions. extend substantially
from the inner ends of the wrap outwardly at least throughout the portions thereof
which contact one another when the two innermost fluid pockets are merged into a single
fluid pocket.
[0018] Therefore,sealing of the high pressure space which is formed at center of the wraps
is maintained without being affected by dimensional errors of the wraps or by thermal
expansion with help of the compliant drive mechanism.
[0019] Further objects, features and other aspects of this invention will be understood
from the following detailed description of the preferred embodiments of this invention
referring to the annexed drawings. The description relates to a scroll type compressor
for the sake of convenience, but the invention is not limited to compressors.
Figs. 1a-1d are schematic views illustrating the relative movement of interfitting
spiral elements to compress the fluid;
Fig. 2 is a pressure-crank angle diagram illustrating the compression cycle in each
of the fluid pockets;
Fig. 3 is a schematic view illustrating the interfitting relationship of prior art
spiral elements;
Fig. 4 is vertical sectional view of a compressor of the scroll type according to
the invention;
Fig. 5 is an exploded perspective view of the driving mechanism used in the compressor
of Fig. 4;
Fig. 6 is an explanatory dingram of the motion of the eccentric bushing illustrated
in Fig. 4;
Fig. 7 is an exploded perspective view of the rotation preventing/thrust bearing mechanism
used in the compressor of Fig.4;
Fig. 8 is a schematic view illustrating the interfitting relationship of spiral elements
according to one embodiment of this invention;
Fig. 9 is a schematic view similar to Fig. 8 illustrating a modified interfitting
relationship of spiral elements according to this invention;
Fig. 10 is a schematic view illustrating the configuration of the transition portion
of a spiral element;and
Figs. 11a-11c are schematic view illustrating the configuration of spiral elements
according to a third embodiment of this invention.
[0020] Referring to Fig.4,a refrigerant compressor unit according to the invention is shown
which includes a compressor housing 10 comprising a front end plate 11 and a cup-shaped
casing 12 disposed on the end surface of front end plate 11.
[0021] A fixed scroll member 13,an orbiting scroll member'14, a driving mechanism and a
rotation preventing/thrust bearing mechanism of orbiting scroll member 14 are disposed
within an inner suction chamber of cup-shaped casing 12. These mechanisms are-described
in detail below. The inner chamber is defined by the side wall of cup-shaped casing
12, the inner end surface of front end plate 11, and fixed scroll member 13.
[0022] Fixed scroll member 13 includes a circular end plate 131 and a involute wrap or spiral
element 132 affixed to and extending from one major end surface of end plate 131.
End plate 131 of fixed scroll member 13 is formed with a plurality of internally threaded
bosses 133 axially projecting from a major end surface of plate 131 opposite the side
thereof from which spiral element 132 extends. The end of each boss 133 abuts the
inner surface 121 of cup-shaped casing 12, and is fixed to casing 12 by screws 15
which screw into bosses 133 from the outside of casing 12. Hence, fixed scroll member
13 is fixedly disposed within cup shaped casing 12. End plate 131 of fixed scroll
member 13 partitions the interior of cup-shaped casing 12 into two chambers,a discharge
chamber 16 and a suction chamber 17,and a sealing member 135 is disposed between the
outer periphery of end plate 131 and the inner wall of cup-shaped casing 12 to isolate
these two chambers.
[0023] Orbiting scroll member 14 is disposed in suction chamber 17 and also comprises a
circular end plate 141 and a involut wrap or spiral element 142 affixed to and extending
from one end surface of end plate 141. Spiral element 142 and spiral element 132 of
fixed scroll member 13 are interfitted at an angular offset of 180° and a predetermined
radial offset. A pair of fluid pockets are thereby defined between spiral elements
132,142. Orbiting scroll member 14 is connected to the driving mechanism and the rotaion
preventing/thrust bearing mechanism. These mechanisms effect the orbital motion of
orbiting scroll member 14 at a circular radius R
0 by the rotation of a drive shaft 18,to thereby compress the fluid in the fluid pockets,as
described in connection with Figs.1a-1d.
[0024] Thus,when orbiting scroll member 14 is allowed to undergo the orbital motion with
the radius R by rotation of drive shaft 18, fluid or refrigerant gas, introduced into
suction chamber 17 from an external fluid circuit through an inlet port 19 on casing
12, is taken into the fluid pockets formed between spiral elements 132,142. As orbiting
scroll member 14 orbits,fluid in the fluid pockets is moved to the center of the spiral
elements with a consequent reduction of volume thereof. Compressed fluid is discharged
into disharge chamber 16 from the fluid pocket at the center of the spiral element
through a hole 134 which is formed through circular plate 131 at a position near the
center of spiral element 132,and a reed-type valve 136,and therefrom is discharged
through an outlet port 20 to an external fluid circuit.
[0025] Referring to Figs. 4 and 5,the driving mechanism of orbiting scroll member 14 will
be described. Drive shaft 18 is rotatably supported by a sleeve portion 111 of front
end plate 11 through a bearing 21 and is formed with a disk portion 181 at its inner
end portion. Disk portion 181 is also rotatably supported by front end plate 11 through
a bearing 22 which is disposed within an opening of front end plate 11.
[0026] A crank pin or drive pin 182 projects axially from an end surface of disk portion
181 and,hence,from an end of drive shaft 18, and is radially offset from the center
of drive shaft 18. End plate 141 of orbiting scroll member 14 is provided with a tubular
boss 143 axially projecting from the end surface opposite to the surface thereof from
which spiral element 142 extends. A discoid or short axial bushing 23 is fitted into
boss 143,and is rotatably supported therein by bearing,such as a needle bearing 24.
Bushing 23 has a balance weight 231 which is shaped as a portion of a disc or ring
and extends radially from bushing 23 along a front surface thereof. An eccentric hole
232 is formed in bushing 23 radially offset from the center of.bushing 23. Drive pin
182 is fitted into the eccentrically disposed hole 232 within which bearing 25 may
be applied. Bushing 23 is therefore driven by the revolution of drive pin 182 and
permitted to rotate by the needle bearing 24.
[0027] Respective location of center 0 of drive shaft 18, center 0
c of bushing 23,and center 0
d of hole 232 and thus drive pin 182 is shown in Fig.6. In the position shown in Fig.6,the
distance between 0
s and 0
c is the representative radius R
o of orbital motion of the orbiting scroll member 14,and when drive pin 182 is placed
in eccentric hole 232,center 0
d of drive pin 182 is placed, with respect to 0
s, on the opposite side of a line L
1,which is through 0 and perpendicular to a line L
2 through 0 and 0
s, and also beyond the line through 0
c and 0 in direction of rotation A of drive shaft 18.
[0028] In this construction of the driving mechanism,center 0
c of bushing 23 is permitted to swing about the center 0
d of drive pin 182 at a radius E
2. As shown in Fig.6,such swing motion of center 0
c is illustrated as arc 0
c'-0
c" in Fig.6. This permitted swing motion allows the orbiting scroll member 14 to compensate
its motion for changes in radius R due to wear on the spiral elements or due to dimentional
inaccuracies of the spiral elements. When drive shaft 18 rotates, a drive force F
dis applied to the left at tenter 0
d of drive pin 182 and a reaction force F
r of gas compression appears to the right at center 0 of bushing 33, both forces being
parallel to line L
1. Therefore,the. arm 0
d-0
c can swing outwardly by creation of the movement generated by the two forces. Spiral
element 142 of orbiting scroll member 14 is thereby forced . toward spiral element
132 of fixed scroll member 13 to make at least one pair of contact among several pair
of sealing points which will be explained later,and the center of orbiting scroll
member 14 orbits with the representative radius R
o around center 0
s of drive shaft 18. The rotation of orbiting scroll member 14 is prevented by the
rotation preventing/thrust bearing mechanism 26 (Fig.7),whereby orbiting scroll member
14 orbits while maintaining its angular orientation relate to fixed scroll member
13.
[0029] Referring to Figs.7and 4,a rotation preventing/thrust bearing mechanism 26 surrounds
boss 143 and comprises a fixed ring 261 and Oldham ring 262. Fixed ring 261 is secured
to an inner surface of housing 10. Fixed ring 261 is provided with a pair of keyways
261a,261b in an axial end surface facing orbiting scroll member
14. Oldham ring 262 is disposed in a hollow portion between fixed ring 261 and end
plate'141 of orbiting scroll member 14. Oldham ring 262 is provided with a pair of
keys 262a,262b on the surface facing fixed ring 261,which are received in keyways
261a,262b. Therefore,Oldham ring 262 is linearly slidable relative to fixed ring 261
by the guide of keys 262a,262b within keyways 261a,261b. Oldham ring 262 is also provided
with a pair of keys 262c,262d on its opposit surface. Keys 262c,262d are arranged
along a diameter perpendicular to the diameter along which keys 262a,262b are arranged.
Circular end plate 141 of orbiting scroll member 14 is provided with a pair of keyways
(in Fig.7 only one keyway 141a is shown; the other keyway is disposed diametrically
opposite keyway 141a) on the surface facing Oldham ring 262 in which are received
keys 262c,262d. Therefore,orbiting scroll member 14 is linearly slidable relative
to Oldham ring 262.by the guide of keys 262c,262d within the keyways of end plate
141.
[0030] Accordingly,orbiting scroll member 14 is slidable in one radial direction with Oldham
ring 262,and is independently slidable in another radial direction perpendicular to
the first radial direction. Therefore,rotation of orbiting scroll member 14 is prevented,while
its movement in two radial directions perpendicular to one another is permitted. Now,
Oldham ring 262 is provided with a plurality of holes or pockets 27, and a bearing
element , such as balls 28
)having a diameter which is greater than the thickness of Oldham ring 262,is retained
in each pocket 27. Balls 28 contact and roll on the surface of fixed ring 261 and
circular end plate 141 of orbiting scroll member 14. Therefore,the thrust load from
orbiting scroll member 14 is supported on fixed ring 261 through balls 28.
[0031] As explained below, the radius R of orbital motion is determined by one contact point
between the spiral elements having the minimum of the angle <0
c0
d0
s. Bushing 23 is supported to permit swing motion about drive pin 182,and this swing
motion allows the orbiting scroll member 14 to compensate its motion for variation
of radius R . On the other hand,spiral element 142 of orbiting scroll member 14 is
forced toward spiral element 132 of fixed scroll member 13 by the driving moment.
The radius R is determined by the combination of the errors of the spiral elements,
for example by,either a combination of the maximum inward deviation of the inner wall
of the fixed spiral element 132 and the maximum outward deviation of the outer wall
of the orbiting spiral element 142 or a combination of the maximum outward deviation
of the outer wall of the fixed spiral element 132 and the maximum inward deviation
of the inner wall of the orbiting spiral element 142, from the theoretical involute
curve for each wall. There are various manners in which the actual orbiting radius
various as the crank angle proceeds,but the first portion to contact the opposit wall
of the other spiral element,determines the radius R as a function of the crank angle,in
other words the orbiting scroll member 14 orbits with radius R which is determined
by the first contact point between spiral elements 132,142,and the actual contact
point to determine the radius can be near outer end of the spiral to form gaps between
the two spiral wall in the area of the high pressure space.
[0032] Fig.8 shows the configuration of spiral elements according to one embodiment of the
present invention. As shown in Fig.8,the wall of the center portion of each spiral
elements is made slightly thicker (by α in Fig.8) by making a slight step along the
inner wall thereof. The thicker portion of each spiral element extends from the inner,
end portion or tip of the spiral element (shown at point A in Fig.8) to a location
along the spiral which is spaced from the tip by an involut angle of at least 2
7F (shown at point B in Fig.8). The outer portion of each spiral element extends from
point B to the outermost end of the spiral element (shown at point D in Fig.8)with
a reduced thickness. When the two spiral elements are interfitted at an angular and
radial offset for the involut portions from A to B of both spiral elements to make
line contact,a small gap may arise at the point where the line contacts should between
the spiral elements in the involute range from B to D. However, the more important
seal of the high pressure space which is defined in the center of both spiral elements
is insured by the thicker portion from A to B(hereinafter designation A-B will be
used) of the inner wall of the spiral elements. The same effect may altanatively be
achieved by a step on the outer(rather than the inner)wall thereof at corresponding
points to B for each spiral.
[0033] In accordance with the above construction of spiral elements, when the thickness
of portion B-D has a dimentional error (ΔE) of less than the step (α) between portion
A-B and portion B-D will not disturb the sealing of the high pressure space. The fluid
leakage across the gap at the line contacts between the outer portion (B-D) of the
spirals is considered to be minimal because the pressure difference between outer
fluid poukets is small. Deterioation of resultant volumetric efficiency of the compressor
is thereby permissible.
[0034] Fig.9 shows a modification of the embodiment shown in Fig.8, wherein the center portion
of each spiral element is made thicker by a slight step (α) on the inner and outer
walls thereof. These thicker portion extend from the inner end portion.or tip of each
spiral element 132,142 (shown at point A in Fig.9) at least throughout the portion
of the spiral elements which contact one another when the pair of fluid pockets are
connected to the high pressure space (shown at points B and C in Fig.9). The slightly
thinner outer portion extends from the points B or C to the terminal ends of both
spiral elements 132,142 (shown at point D and E in Fig. 9). Therefore,when'these two
spiral elements are interfitted with one another,a gap (shown as 2α in Fig.9) between
the portion B-D and the portion C-E of both spiral elements results. However, the
important seal of the high pressure space which is defined at the center of the spiral
elements is insured.
[0035] The transition between the thicker portion and the thinner portion of each spiral
is shown in Figs. 8 and 9 to be steplike. However,the transition can be arcuate,rather
than stepped,as shown in Fig.10. The radius of curvature of the arcuate transition
portion is determined by the radius of the milling tool M used to form the spiral
element. The arcuate transition portion is formed when the milling tool reaches the
end of its travel after forming an adjacent portion of spiral.
[0036] Fig.11a shows another embodiment of the present invention, which is charactrized
in that the inner wall of the outer portion of the spiral element starts deviating
from a true involut curve at point B to form a portion of gradually reduced thickness.
The wall thickness of the inner portion,which is between the inner end portion or
tip of each spiral element (point A) and point B, is uniform. Since the wall thickness
between point B and the outer terminal end (point D) gradually reduces, the gap (α)
between the spiral elements will be a function of the involut angle.
[0037] Figs. 11b and 11c show modifications of the embodiment shown in Fig.11a, wherein
the center portion of each spiral elements is formed to a true involute curve and
the outer wall of the outer portion of the spiral element starts deviating from a
true involute curve at point C to form a portion of gradually reduced thickness (shown
in Fig.11b) or the inner and outer wall of the outer portion of the spiral elements
starts devisting from a true involute curve at points B and C to form a portion of
gradually reduced thickness (shown in Fig.11c).
[0038] This invention has been described in detail in connection with preferred embodiments,
but these embodiments are merely for example only and this invention is not restricted
thereto. It will be easily understood by those skilled in the art that other variations
and modifications can be easily made within the scope of this invention,as defined
by the appended claims.
1. A scroll type fluid displacement apparatus including a housing (10, a pair of scroll
members (13, 14), one of said scroll members (13) fixedly disposed relative to said
housing (10) and having an end plate (131) from which a first wrap means (132) extends
into the interior of said housing and the other scroll member (14) movably disposed
for non-rotative orbital movement within the interior of said housing (10) and having
an end plate (141) from which a second spiral wrap means (142) extends, said first
and second wrap means (132, 142) interfitting at an angular and radial offset to make
a plurality of line contacts to define at least one pair of sealed off fluid pockets
(3), and a driving mechanism (18, 181, 182) operatively connected to said other scroll
member (14) to effect the orbital motion of said other scroll member (14), whereby
said fluid pockets (3) move inwardly and change in volume, the two innermost fluid
pockets eventually merging into a single pocket (5) near the center of said wrap means
(13, 14), characterized in that the center portions of said wrap means (13, 14) are
thicker than the remaining portions thereof, said center portions extending substantially
from the inner ends of said wrap means outwardly at least throughout the portions
thereof which contact one another when said two innermost fluid pockets are merged
into a single fluid pocket.
2. A scroll type fluid displacement apparatus as claimed in Claim 1, characterized
in that said thicker center portion of each wrap means is formed with a step on the
inner wall of said center portion.
3. A scroll type fluid displacement apparatus as claimed in Claim 1, characterized
in that said thicker center portion of each wrap means is formed with a step on the
outer wall of said center portion.
4. A scroll type fluid displacement apparatus as claimed in Claim 1, characterized
in that said thicker center portion of each wrap means is formed with a step on both
the inner and outer walls of said center portion.
5. A scroll type fluid displacement apparatus as claimed in Claim 1, 2, 3 or 4, characterized
in that a transition portion is formed on each of said wrap means between said thicker
center portion and the thinner remaining portion thereof.
6. A scroll type fluid displacement apparatus as claimed in Claim 5, characterized
in that said transition portion is stepped.
7. A scroll type fluid displacement apparatus as claimed in Claim 5, characterized
in that said transition portion is arcuate.
8. A scroll type fluid displacement apparatus as claimed in Claim 1, 2, 3 or 4, characterized
in that the thickness of the thinner outer portion of each of said wrap means gradually
diminishes toward the outer terminal end thereof.
9. A scroll type fluid compressor unit comprising:
a housing (10) having a fluid inlet port (19) and fluid outlet port (20);
a fixed scroll member (13) fixedly disposed relative to said housing (10) and having
an end plate (131) from which a first spiral wrap means (132) extends into the interior
of said housing;
an orbiting scroll member (14) movably disposed within said housing (10) and having
an end plate (141) from which a second spiral wrap (142) means extends, said first
and second wrap means (132, 142) interfitting at an angular and radial offset to make
a plurality of line contacts to define at least one pair of sealed off fluid pockets
(3a, 3b);
rotation preventing means for restraining said orbiting scroll member (14) to orbit
motion;
drive shaft (18) rotatably supported by said housing (10); and
drive means operatively coupling said drive shaft to said orbiting scroll member (14)
to effect orbital motion of said orbiting scroll member by rotation of said drive
shaft (18), whereby said fluid pockets (3a, 3b) move inwardly and change volume, the
two innermost fluid pockets eventually merging into a single pocket (5) near the center
of said wrap means (132, 142), characterized in that the center portion of said wrap
means (132, 142) being thicker than the remaining portion thereof, said center portions
extending substantially from the inner ends of said wrap means (132, 142) outwardly
at least throughout the portions thereof which contact one another when said two innermost
fluid pockets (3a, 3b) are merged into a single fluid pocket (5).
10. A scroll type fluid compressor unit as claimed in Claim 9, characterized in that
said thicker center portion of each wrap means (132, 142) is formed with a step on
the inner wall of said center portion.
11. A scroll type fluid compressor unit as claimed in Claim 9, characterized in that
said thicker center portion of each wrap means (132, 142) is formed with a step on
the outer wall of said center portion.
12. A scroll type fluid compressor unit as claimed in Claim 9, characterized in that
said thicker center portion of each wrap means (132, 142) is formed with a step on
both the inner and outer walls of said center portion.
13. A scroll type fluid compressor unit as claimed in Claim 9, 10, 11 or 12, characterized
in that a stepped transition portion is formed on each of said wrap means (132, 142)
between said thicker center portion and the thinner remaining portion thereof.
14. A scroll type fluid compressor unit as claimed in Claim 9, 10, 11 or 12, characterized
in that an arcuate transition portion is formed on each of said wrap means (132, 142)
between said thicker center portion and the thinner remaining portion thereof.
15. A scroll type fluid compressor unit as claimed in Claim 9, 10, 11 or 12, characterized
in that the thickness of the thinner remaining portion of each of said wrap means
gradually diminishes toward the outer terminal end thereof.