Information
-
Patent Grant
-
6736609
-
Patent Number
6,736,609
-
Date Filed
Tuesday, March 19, 200222 years ago
-
Date Issued
Tuesday, May 18, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Yu; Justine R.
- Liu; Han L
Agents
- Wenderoth, Lind & Ponack, L.L.P.
-
CPC
-
US Classifications
Field of Search
US
- 417 365
- 418 2067
- 418 2068
- 418 2069
- 427 230
- 427 249
- 384 114
- 384 121
- 384 107
- 384 387
- 384 9071
- 508 109
-
International Classifications
-
Abstract
A pump apparatus of simple construction has a bearing structure for which a lubricant is unnecessary. A flow passage for a refrigerant (liquid ammonia) is formed in a housing to provide communication between a suction port and a discharge port, and slide bearing members formed of amorphous carbon are provided in the housing to be fitted into the flow passage to support a rotating shaft. A drive for rotating the rotating shaft is constituted by a rotor, which is fitted into the flow passage and provided with the rotating shaft, and a stator, which is provided outside the housing to surround the rotor, and a pump body is provided midway the flow passage and connected to the rotating shaft to pump a fluid.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The invention relates to a support apparatus provided with a member for displaceably supporting a movable member such as a rotating shaft, and a pump apparatus.
2. Description of the Related Art
Space equipment such as artificial satellites, space stations or the like, and other equipment used in outer space include many kinds of drive mechanisms in which a support apparatus, such as ball-and-roller bearing apparatuses, ball screw apparatuses, linear guide apparatuses and the like, for displaceably supporting a movable member is used. Fluoro grease is used as a lubricant in a support apparatus for use on earth, but evaporates in outer space is responsible for contamination of various equipment and decomposition due to radioactive rays, and so cannot be used there. In a support apparatus for equipment used in outer space, molybdenum dioxide, lead or silver is used, which is low in torque and stable.
As described above, equipment used in outer space, in particular, equipment used over a long term in artificial satellites, space stations or the like, are exceedingly difficult in the exchange of parts, and required high durability. A support apparatus for supporting a movable member provided in such equipment is desirably made simple in construction for the purpose of less failure, and constructed to dispense with the use of lubricant for preventing a degraded performance due to changes in the lubricant.
SUMMARY OF THE INVENTION
It is an object of the invention to provide a support apparatus which is simple in construction and dispenses with lubricant.
Also, it is an object of the invention to provide a pump apparatus which is simple in construction and provided with a bearing structure for supporting a rotating shaft, and which dispenses with lubricant.
The invention provides a support apparatus for displaceably supporting a movable member comprising slide members for slidably supporting the movable member, the slide members being formed of amorphous carbon.
According to the invention, a movable member can be supported by slide members formed of amorphous carbon. Amorphous carbon is high in abrasion resistance and possesses a low frictional property called a self-lubricating property, and slide members formed of amorphous carbon are used to smoothly slide relative to a movable member to, without using lubricant, enable supporting the movable member so that the movable member can be smoothly displaced. Accordingly, it is possible to obtain a support apparatus that is simple in construction and supports a movable member without the use of lubricant to enhance the durability of the support apparatus.
In the invention, it is preferable that the movable member comprises a rotating shaft and the slide members are slide bearing members for rotatably supporting the rotating shaft.
According to the invention, the slide bearing members formed of amorphous carbon can support the rotating shaft. It thereby is possible to reduce a gap between the rotating shaft and the slide bearing members and rotatably support the rotating shaft so as to cause stable rotation of the rotating shaft.
In the invention it is preferable that the slide members are arranged in a space in which a fluid is contained.
According to the invention, the slide members are formed of amorphous carbon and possess chemical resistance, so they are not subjected to chemical change by a fluid even when being provided in a space in which a fluid is contained. Besides, even if the fluid is one, either a strong acid or strong base, liable to chemically affect a mating member, the slide members are not subjected to chemical change by the fluid. The slide members can thereby preserve the function as slide members over a long term without being damaged by the fluid. Accordingly, the slide members can be suitably used in fluid flow passages.
In the invention, it is preferable that a gap between the movable member and the slide members is dimensioned to allow entry of the fluid due to the capillary phenomenon.
According to the invention, a fluid in the space enters between the movable member and the slide members. The slide members formed of amorphous carbon are not restricted in lubricant as in the case of slide members of metal, but can use a wide variety of fluids as lubricant. As described above, while lubricant is essentially unnecessary, the use of lubricant makes it possible to support the movable member in a further smoothly displaceable manner. Accordingly, a fluid in the gap can be used as lubricant so that a supporting state can be achieved to realize smooth displacement of the movable member.
In the invention, it is preferable that the fluid is liquid ammonia. According to the invention, the slide members possess chemical resistance, and are not subjected to chemical change even when a fluid is liquid ammonia, so that they can preserve their function as slide members over a long term. Moreover, it is possible to make use of liquid ammonia as a favorable lubricant. Accordingly, the slide bearing members can be favorably used in a space in which liquid ammonia is contained.
In the invention it is preferable that the support apparatus is mounted on equipment used in outer space.
According to the invention, the support apparatus can be enhanced in durability, so that it is suitably usable for equipment, such as artificial satellites, space stations or the like, which are used in outer space, and whose parts are difficult to exchange.
The invention provides a pump apparatus comprising a rotating shaft, slide bearing members formed of amorphous carbon for rotatably supporting the rotating shaft, drive means for drivingly rotating the rotating shaft and a pump body connected to the rotating shaft, for pumping a fluid.
According to the invention, the drive means is used to drive the rotating shaft to drive the pump body connected to the rotating shaft to discharge a fluid. The rotating shaft is rotatably supported by a bearing apparatus having slide bearing members. The slide bearing members are formed of amorphous carbon. Amorphous carbon is high in abrasion resistance and possesses a low frictional property called a self-lubricating property, and slide bearing members formed of amorphous carbon are used to smoothly slide relative to the rotating shaft to, without using lubricant, enable supporting the rotating shaft so that the rotating shaft can be smoothly rotated. Accordingly, it is possible to obtain a bearing apparatus which is simple in construction and supports the rotating shaft without the use of lubricant to enhance durability of the bearing apparatus, thus of the pump apparatus.
In the invention it is preferable that the pump apparatus further comprises a housing having a fluid flow passage which provides communication between a suction port and a discharge port, and that the rotating shaft is arranged in the housing, the slide bearing members are fitted in the fluid flow passage in the housing, the drive means comprises a rotor fitted in the fluid flow passage to be provided on the rotating shaft and a stator provided outside the housing to surround the rotor, and the pump body is provided midway of the fluid flow passage.
According to the invention, the drive means is used to drive the rotating shaft to drive the pump body connected to the rotating shaft so that a fluid sucked through a suction port is made to flow down the flow passage to be discharged through a discharge port. In this pump apparatus, the rotating shaft, the slide bearing members and the rotor are fitted into the flow passage. In this manner, the provision of the rotating shaft, the slide bearing members and the rotor in the flow passage eliminates the need of providing rotating constituents both inside and outside the flow passage through the housing, so that the whole pump apparatus can be made favorable in sealing quality relative to leakage of the fluid, the sealing construction can be made simple, and the pump apparatus can be made small in size.
With such construction, the slide bearing members are formed of amorphous carbon and possess chemical resistance, so they are not subjected to chemical change by a fluid even when being provided in a space in which a fluid is contained. Besides, even if the fluid is one, either strong acid or strong base, liable to chemically affect a mating member, the slide members are not subjected to chemical change by the fluid. The slide bearing members can thereby preserve the function as slide bearing members over a long term without damage by the fluid.
In the invention, it is preferable that a gap between the rotating shaft and the slide bearing members is dimensioned to allow entry of the fluid due to the capillary phenomenon.
According to the invention, a fluid in the flow passage enters between the rotating shaft and the slide bearing members. The slide bearing members formed of amorphous carbon are not restricted in lubricant as in the case of slide bearing members of metal, but can use a wide variety of fluids as lubricant. As described above, while lubricant is essentially unnecessary, the use of lubricant makes it possible to support the rotating shaft in a further smoothly displaceable manner. Accordingly, the fluid in the flow passage can be used as lubricant and so a pump apparatus can be achieved to provide for further smooth rotation of the rotating shaft.
In the invention it is preferable that the pump apparatus is a pump for circulating a refrigerant and the fluid is liquid ammonia as the refrigerant.
According to the invention, the slide bearing members possess chemical resistance, and are not subjected to chemical change even when the fluid is liquid ammonia, so that they can preserve the function as slide bearing members over a long term. Moreover, the slide bearing members can make use of liquid ammonia as a favorable lubricant. Without the use of freon gas, for the sake of global environmental protection, such liquid ammonia is used as a refrigerant favorably in the pump apparatus, in which the refrigerant is circulated.
Also, liquid ammonia as refrigerant can be used to cool the rotating shaft, the slide bearing members and the rotor and to maintain a stable performance of the pump.
In the invention it is preferable that the pump body is formed of amorphous carbon.
According to the invention, the pump body is formed of amorphous carbon, and so is not susceptible to chemical influences, whereby it is possible to realize a favorable pump apparatus that keeps the function of the pump body over a long term.
In the invention, it is preferable that the slide bearing members are radial bearings to bear the radial load of the rotating shaft, and the pump body is formed of amorphous carbon to bear the thrust load of the rotating shaft.
According to the invention, formation of the pump body of amorphous carbon can have the pump body fulfilling the function of thrust bearings and bearing the thrust load of the rotating shaft. Therefore, the load on the slide bearing members can be reduced. In this manner, load is imposed on the pump body to make it possible to reduce the slide bearing members in size and enhance durability of the pump apparatus.
In the invention, it is preferable that the pump apparatus is mounted on equipment used in outer space.
According to the invention, the pump apparatus can be enhanced in durability so that it is suitably usable for equipment, such as artificial satellites, space stations or the like, which are used in outer space, of which parts are difficult to exchange.
BRIEF DESCRIPTION OF THE DRAWINGS
Other and further objects, features, and advantages of the invention will be more explicit from the following detailed description taken with reference to the drawings wherein:
FIG. 1
is a cross sectional view showing a pump apparatus
1
according to an embodiment of the invention;
FIG. 2
is a cross sectional view of the pump apparatus
1
of
FIG. 1
as viewed from above of
FIG. 1
;
FIG. 3
is a left side view of the pump apparatus
1
of
FIG. 1
;
FIG. 4
is a right side view of the pump apparatus
1
of
FIG. 1
;
FIG. 5
is a front view showing a cylindrical-shaped member
11
constituting a housing
3
;
FIG. 6
is a right side view of the cylindrical-shaped member
11
of
FIG. 5
;
FIG. 7
is a cross sectional view showing a pump chamber forming member
12
constituting the housing
3
;
FIG. 8
is a plan view of the pump chamber forming member
12
of
FIG. 7
;
FIG. 9
is a left side view of the pump chamber forming member
12
of
FIG. 7
;
FIG. 10
is a right side view of the pump chamber forming member
12
of
FIG. 7
;
FIG. 11
is a cross sectional view of a suction port forming member
13
constituting the housing
3
;
FIG. 12
is a left side view of the suction port forming member
13
of
FIG. 11
;
FIG. 13
is a right side view of the suction port forming member
13
of
FIG. 11
;
FIG. 14
is a cross sectional view showing a discharge port forming member
14
constituting the housing
3
;
FIG. 15
is a right side view of the discharge port forming member
14
of
FIG. 14
;
FIG. 16
is a front view showing a rotating shaft
4
;
FIG. 17
is a left side view of the rotating shaft
4
of
FIG. 16
;
FIG. 18
is a cross sectional view showing slide bearing members
5
;
FIG. 19
is a left side view of the slide bearing members
5
of
FIG. 18
;
FIG. 20
is a front view showing an inner gear
60
;
FIG. 21
is a cross sectional view taken along cutting plane line S
21
—S
21
in
FIG. 20
;
FIG. 22
is a front view showing an outer gear
61
;
FIG. 23
is a cross sectional view taken along cutting plane line S
23
—S
23
in
FIG. 22
;
FIG. 24
is a cross sectional view showing a pump body
10
on an enlarged scale;
FIG. 25
is a cross sectional view of the pump body
10
as viewed from leftward of
FIG. 24
;
FIG. 26
is an exploded, perspective view showing the pump body
10
;
FIG. 27
is a cross sectional view showing an apparatus for measuring coefficients of friction;
FIGS. 28A and 28B
are graphs showing results of tests for measuring coefficients of friction;
FIG. 29
is a cross sectional view showing an apparatus for measuring wear in the air;
FIGS. 30A and 30B
are graphs showing results of tests for measuring wear in the air;
FIG. 31
is a cross sectional view showing an apparatus for measuring wear in the water;
FIGS. 32A and 32B
are graphs showing results of tests for measuring wear in the water;
FIG. 33
is a graph showing wear coefficients of various materials including AC;
FIG. 34
is a graph showing coefficients of thermal expansion of various materials including AC;
FIG. 35
is a graph showing bulk densities of various materials including AC;
FIG. 36
is a graph showing melting points or temperatures of thermal deformation of various materials including AC;
FIG. 37
is a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of water at 5.5° C.;
FIG. 38
is a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of ethyl ether;
FIG. 39
is a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of liquid ammonia at 8° C.;
FIG. 40
is a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of ethyl ether at 10° C.;
FIG. 41
is a graph showing the relationship between input power to a drive means and flow rate of the pump apparatus
1
making use of ethyl ether at 10° C.; and
FIG. 42
is a graph showing the relationship between number of revolutions and flow rate of the pump apparatus
1
making use of ethyl ether at 10° C.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Now referring to the drawings, preferred embodiments of the invention are described below.
FIG. 1
is a cross sectional view showing a pump apparatus
1
according to an embodiment of the invention,
FIG. 2
being a cross sectional view showing the pump apparatus
1
as viewed from above
FIG. 1
,
FIG. 3
being a left side view showing the pump apparatus
1
of
FIG. 1
, and
FIG. 4
being a right side view showing the pump apparatus
1
of FIG.
1
. The pump apparatus
1
is an apparatus for feeding a liquid, the apparatus being mounted on, for example, space equipment such as artificial satellites, space stations or the like, and equipment used in outer space outside the stratosphere, and serves to circulate a refrigerant which makes heat exchange with other apparatuses mounted on the equipment. The pump apparatus
1
comprises a housing
3
formed with a refrigerant flow passage
2
, a rotating shaft
4
provided in the housing
3
, a bearing structure
6
having slide bearing members
5
which rotatably support the rotating shaft
4
, a motor
9
having a rotor
7
and a stator
8
, and a pump body
10
connected to the rotating shaft
4
. For the sake of global environmental conservation, iron freon gas is not used for the refrigerant, but liquid ammonia is used.
Assembled to the housing
3
are a cylindrical-shaped member
11
shown in
FIGS. 5 and 6
, a pump chamber forming member
12
shown in
FIGS. 7
,
8
,
9
and
10
, a suction port forming member
13
shown in
FIGS. 11
,
12
and
13
, and a discharge port forming member
14
shown in
FIGS. 14 and 15
. The cylindrical-shaped member
11
is thin-walled and cylindrical-shaped, and both axial ends
15
and
16
thereof are formed with a plurality of, for example, circumferentially three, through holes
17
,
18
, respectively.
The pump chamber forming member
12
is formed at its one axial end
19
with an axially opened fitting recess
20
, in which a pump chamber
22
having a cylindrical-shaped, inner peripheral surface is formed to be contiguous to the other axial end of the fitting recess
20
. The fitting recess
20
is coaxial with an axis L
12
of the pump chamber forming member
12
, and the pump chamber
22
is of a smaller diameter than that of the fitting recess
20
to be formed offset from the axis L
12
of the pump chamber forming member
12
.
Also, the pump chamber forming member
12
is formed at the other axial end
21
with an axially opened bearing recess
23
, which is coaxial with the axis L
12
of the pump chamber forming member
12
, and with a shaft insertion hole
24
, which passes through the pump chamber forming member
12
along the axis L
12
to provide communication between the pump chamber
22
and the bearing recess
23
. Further, the pump chamber forming member
12
is formed with an inside pump port
25
, which is contiguous to the pump chamber
22
on a side of the other axial end
21
, and an inside pump passage
26
, which is offset from the axis L
12
of the pump chamber forming member
12
to pass in parallel to the axis L
12
. The inside pump port
25
is formed in an arc extending about an axis of the pump chamber
22
, that is, an axis L
22
of an inner peripheral surface facing the pump chamber
22
, the inside pump passage
26
being axially opened at the other axial end
21
of the pump chamber forming member
12
.
Such pump chamber forming member
12
is inserted into the cylindrical-shaped member
11
from a side of the other axial end
21
, and mounted to the one axial end
15
of the cylindrical-shaped member
11
by inserting bolts
28
through the respective through holes
17
and screwing the same to the pump chamber forming member
12
with the use of threaded holes
27
. In this state, an O-ring
31
is provided between the cylindrical-shaped member
11
and the pump chamber forming member
12
to be fitted into an annular groove
30
, which is formed in an outer peripheral portion at the other axial end
21
of the pump chamber forming member
12
, thus attaining sealing.
Formed in the suction port forming member
13
are an axially opened suction port
33
, which is disposed at a one axial end
32
to be offset from an axis L
13
of the suction port forming member
13
, and a suction passage
34
contiguous to the suction port
33
to extend axially in parallel to the axis L
13
of the suction port forming member
13
, the suction passage
34
being axially opened at the other axial end
35
of the suction port forming member
13
. Also, formed in the suction port forming member
13
are an axially opened bearing recess
36
, which is disposed at the other axial end
35
to be coaxial with the axis L
13
of the suction port forming member
13
, and a shaft insertion recess
37
contiguous to the bearing recess
36
to extend near a center in the axial direction along the axis L
13
of the suction port forming member
13
.
Such suction port forming member
13
is inserted into the cylindrical-shaped member
11
from a side of the other axial end
35
, and mounted to the other axial end
16
of the cylindrical-shaped member
11
by inserting bolts
38
through the respective through holes
18
and screwing the same to the suction port forming member
13
with the use of threaded holes
39
. In this state, an O-ring
41
is provided between the cylindrical-shaped member
11
and the suction port forming member
13
to be fitted into an annular groove
40
, which is formed in an outer peripheral portion at the other axial end
35
of the suction port forming member
13
, thus attaining sealing.
Formed in the discharge port forming member
14
is an axially opened discharge port
43
, which is disposed at the one axial end
42
thereof to be offset from an axis L
14
of the discharge port forming member
14
. Further, formed in the discharge port forming member
14
is an outside pump port
45
, which is disposed at the other axial end
44
thereof to be offset from the axis L
14
of the discharge port forming member
14
. The outside pump port
45
is disposed in a position corresponding to the discharge port
43
with respect to in a circumferential direction to extend circumferentially arcuately. Further, formed in the discharge port forming member
14
is a discharge passage
46
, which is offset from the axis L
14
of the discharge port forming member
14
to extend through the discharge port forming member
14
in parallel to the axis L
14
.
Such discharge port forming member
14
has the other axial end
44
fitted into the fitting recess
20
of the pump chamber forming member
12
to plug the pump chamber
22
in the axial direction. The pump chamber forming member
12
is provided at its one axial end
19
with a flange
47
, which extends radially outward and is formed with a plurality of (for example, four) threaded holes
46
, and the discharge port forming member
14
is provided at its one axial end
42
with a flange
49
, which extends radially outward and is formed with a plurality of (for example, four) through holes
48
. Bolts
50
inserted through the respective through holes
48
are screwed into the flange
47
with the use of the threaded holes
46
, whereby the discharge port forming member
14
is mounted to the pump chamber forming member
12
with its other axial end
44
fitted into the fitting recess
20
. In this state, an O-ring
52
is provided between the pump chamber forming member
12
and the discharge port forming member
14
to be fitted into an annular groove
51
, which is formed in an outer peripheral portion at the other axial end
44
of the discharge port forming member
14
, thus attaining sealing.
In this manner, the housing
3
is constructed, in which state the axis L
11
of the cylindrical-shaped member
11
, the axis L
12
of the pump chamber forming member
12
, the axis L
13
of the suction port forming member
13
, and the axis L
14
of the discharge port forming member
14
are in accord with the axis L
3
of the housing
3
. A rotor chamber
55
is formed in the housing
3
to be disposed between the pump chamber forming member
12
and the suction port forming member
13
, and the suction passage
34
and the inside pump passage
26
are communicated to the rotor chamber
55
. Accordingly, the suction port
33
and the discharge port
43
are formed in the housing
3
, and the flow passage
2
is formed to communicate with these ports
33
,
43
. The flow passage
2
of a fluid refrigerant is formed by connection of at least the suction passage
34
, the rotor chamber
55
, the inside pump passage
26
, the inside pump port
25
, the pump chamber
22
, the outside pump port
45
and the discharge passage
46
in this order. Such housing
3
is composed of, for example, stainless steel.
Provided within such housing
3
is the rotating shaft
4
being a movable member shown in
FIGS. 16 and 17
, the rotating shaft
4
being rotatably supported by the slide bearing members
5
, which are support members shown in
FIGS. 18 and 19
. The rotating shaft
4
is formed of stainless steel to be columnar-shaped, and its one axial end
69
is partially cut away in a circumferential direction to be oval-shaped in cross section to be adapted for latching. In this embodiment, two slide bearing members
5
are provided, each of which is formed of amorphous carbon to be made in the form of a short cylinder.
The respective slide bearing members
5
are press fitted into and fixed to the bearing recess
23
of the pump chamber forming member
12
and the bearing recess
36
of the suction port forming member
13
in such a way that the axis L
5
is in accord with the axis L
3
of the housing
3
. In this manner, the respective slide bearing members
5
are held by and provided in the housing
3
to be exposed to the rotor chamber
55
, which constitutes a part of the flow passage
2
. In a state of being inserted through the respective slide bearing members
5
, the rotating shaft
4
is inserted through the shaft insertion hole
24
of the pump chamber forming member
12
with one axial end thereof disposed in the pump chamber
22
and the other axial end thereof
56
inserted and disposed in the shaft insertion recess
37
.
In this manner, the rotating shaft
4
is rotatably supported about the axis L
3
from radially outward by the slide bearing members
5
with the axis L
4
in accord with the axis L
3
of the housing
3
. Thus the respective slide bearing members
5
are radial bearings for supporting the rotating shaft
4
in a radial direction. When the rotating shaft
4
has an outer diameter of, for example, 2 mm, a radial gap d between the rotating shaft
4
and the respective slide bearing members
5
is at least 0.75 mm and at most 2 mm with an inner diameter of the slide bearing members
5
being selected to be at most 2.015 mm and at least 2.004 mm. Such gap is dimensioned to allow a refrigerant in the rotor chamber
55
to enter thereinto due to the capillary phenomenon. Thus the gap is formed to be extremely small, thus enabling stably stable support of the rotating shaft
4
.
Fitted in the pump chamber
22
as shown in
FIGS. 24 and 25
are an inner gear
60
shown in
FIGS. 20 and 21
, and an outer gear
61
shown in
FIGS. 22 and 23
. The inner gear
60
is formed at an outer periphery thereof with a plurality of (for example, four) teeth
62
. The outer gear
61
is substantially cylindrical-shaped and formed at an inner periphery thereof with teeth
63
, the number of which is more by one than that of the teeth
62
of the inner gear
60
.
As shown in
FIG. 26
, the inner gear
60
is fixed to one end
69
of the rotating shaft
4
in a state in which a spacer
65
in the form of a substantially elliptical cylinder is press fitted onto one end
55
of the rotating shaft
4
and the inner gear is press fitted onto the spacer
65
. Accordingly, the inner gear
60
has its axis L
60
aligned with the axis L
3
of the housing
3
. The outer gear
61
is fitted onto the inner gear
60
in a state of meshing with the inner gear
60
. The outer gear
61
has an outer diameter slightly smaller than an inner periphery of the pump chamber
22
and has its axis L
61
aligned with the axis L
22
of the pump chamber
22
to be eccentric relative to the inner gear
60
.
These inner gear
60
, outer gear
61
and a portion surrounding the pump chamber
22
constitute a displacement pump, concretely a pump body
10
being a trochoidal gear pump. With the pump body
10
, a plurality of pressure chambers are defined between the inner gear
60
and the outer gear
61
, so that when the inner gear
60
is rotated by rotation of the rotating shaft
4
, the outer gear
61
correspondingly rotates to vary volumes of the pressure chambers. The pressure chambers are communicated to the inside pump port
25
in a position where volumes become large, and are made contiguous to the outside pump port
45
in a position where volumes become small.
Also, the inner gear
60
and the outer gear
61
are formed of amorphous carbon. The inner gear
60
also functions as a thrust bearing for axially supporting the rotating shaft
4
.
The rotor
7
fixed to the rotating shaft
4
and formed of a magnet is provided in the rotor chamber
55
, and the stator
8
is provided in a position surrounding the rotor
7
outside the housing
3
. Drive means
9
is constituted by the rotor and the stator. The stator
8
includes a coil, which is electrically energized to impart torque to the rotor
7
due to the magnetic action between it and the rotor
7
, thus rotatingly driving the rotating shaft
4
to rotate the inner gear
60
to drive the pump body
10
. Thereby, the pump body
10
causes a refrigerant to be sucked from the suction port
33
to flow down the flow passage
2
to be discharged from the discharge port
43
.
Amorphous carbon (referred below to as “AC”) is also called glass carbon, and is amorphous carbon to have a property of a low coefficient of friction.
FIGS. 28A and 28B
show results of a test in which a coefficient of friction was measured by sliding, for example a stationary test piece
70
formed of AC shown in
FIG. 27
, on an outer periphery of a rotating test piece formed of high carbon chromium bearing steel (SUJ2) or silicon nitride (Si
3
N
4
). In this manner, members formed of AC exhibit small coefficients of friction even when no lubricant exists between them and other members, and further exhibit extremely small coefficients of friction when a lubricant is present, irrespective of the kind of lubricant.
Also, members formed of AC have a property in that the coefficients of friction are small.
FIGS. 30A and 30B
show results of a test in which depth of severe-mild wear was measured by rotating, pushing and sliding a test shaft
74
, which was formed of stainless steel and had a semi-spherical shaped tip end, on, for example, a stationary test piece
73
formed of AC and shown in FIG.
29
. Also,
FIGS. 32A and 32B
show results of a test, in which severe-mild wear and surface roughness were measured by rotating, pushing and sliding a test piece
75
, which was formed of alumina ceramics, on a test piece composed of AC or several compounds in water as shown in FIG.
31
. As indicated by these test results and a graph in
FIG. 33
, members formed of AC are small in coefficient of friction as compared with other members formed of other materials, and so hard to abrade, and are small in surface roughness even in the case of wearing.
Further, members formed of AC are small in coefficient of thermal expansion as shown in
FIG. 34
, small in bulk density as shown in
FIG. 35
, and high in melting point or temperature thermal deformation to be high in heat resistance as shown FIG.
36
.
Also, Table 1 shows properties of AC and other materials in combination, Table 2 showing properties of AC, Table 3 showing contents of impurities in the slide bearing members
5
formed of AC, inner gear
60
and the outer gear
61
, and Table 4 showing hydrofluoric acid resistance of the slide bearing members
5
formed of AC, inner gear
60
and the outer gear
61
.
TABLE 1
|
|
ductility
coefficient
|
fusing
Young's
(breaking
of thermal
|
bonding
point or
strength
modulus
strain)
expansion
density
|
material
structure
strength
Tg (K)
(MPa)
(GPa)
(%)
×10
−6
/° C.
(Mg/m
3
)
|
|
ceramics
aggregation
ionic bond
high
large
large
small
small
small to
|
of
and
800-3500
1000-20000
70-700
10
0
0-10
medium
|
compound-
covalent
1-5
|
based
bond
|
crystal
|
metal
crystal of
metallic
medium
medium
medium
medium
medium
medium to
|
simple
bond
400-3400
400-3000
70-400
10
0
-10
2
4-40
large
|
substance or
2-20
|
solid
|
solution
|
organic
amorphous
covalent
low
small
small
medium
large
small
|
polymer
substance
bond
350-600
10-100
10 or
10
0
-10
3
10
2
or more
1-2
|
composed of
less
|
molecular
|
chain
|
amorphous
simple,
covalent
2600
200
30
1
3
1.5
|
carbon
amorphous
bond
|
substance
|
isotropic
crystal
covalent
3600
40-90
10-15
10
0
4.6-6.5
1.7-1.9
|
high-
aggregation
bond
|
density
of simple
|
graphite
substance
|
|
TABLE 2
|
|
* properties
|
gas
Coefficient
heat
Charpy
ash
|
bulk
trans-
bending
tensil
tensil
elastic
Resist-
of thermal
con-
impact
con-
|
density
porosity
mittance
strength
strength
elon-
modulus
ibility
expansion
ductivity
Shore
strength
tent
|
g/cm
3
%
cm
2
/sec
MPa
MPa
gation %
GPa
μΩ · cm
×10
−6
/K
W/m · K
hardness
kg · cm/cm
2
ppm
|
|
1.46-1.60
0.6-0.9
2.4 × 10
−12
120
(40)
(1.1)
30
4400-
3.0
5-8
127-130
(2.1-3.6)
20
|
4500
|
|
TABLE 3
|
|
* analytical value of ash content (impurities)
|
impurities
|
total ash
|
Al
Ca
Cr
Ba
Fe
Co
Mn
Sr
Ni
V
Si
content
|
|
concentration
ND
1.5
<0.1
<0.1
2.5
0.1
ND
<0.1
1.4
<0.1
2.7
20
|
(ppm)
|
|
TABLE 4
|
|
hydrofluoric acid resistance
|
impurities
|
Al
Ca
Cr
Cu
Fe
K
Mg
Na
Ni
Pb
Si
|
|
concentration
0.14
<1
<0.1
<0.2
<0.5
<1
<0.05
0.3
<0.05
<0.2
<1000
|
(ppm)
|
|
As apparent from the above-mentioned respective test results and the respective Tables 1 to 4, AC possesses properties such as lightness, low coefficient of thermal expansion, high rigidity, high heat resistance, gas non-permeability, high hardness, abrasion resistance, low coefficient of friction, compact homogeneous structure, chemical resistance and carbon powder non-falling or the like, and is much suitable as a material for members, which slide relative to other members. That is, AC can be much suitably used as the above-mentioned slide bearing member.
FIG. 37
is a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of water at 5.5° C.,
FIG. 38
being a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of ethyl ether, and
FIG. 39
being a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of liquid ammonia at 8° C. Also,
FIG. 40
is a graph showing the relationship between discharge pressure and flow rate of the pump apparatus
1
making use of ethyl ether at 10° C.,
FIG. 41
being a graph showing the relationship between input power to the drive means and flow rate of the pump apparatus
1
making use of ethyl ether at 10° C.,
FIG. 42
being a graph showing the relationship between number of revolutions and flow rate of the pump apparatus
1
making use of ethyl ether at 10° C. In addition,
FIGS. 40
to
42
show results in the case of using ethyl ether easy to handle while the inventors of this application have confirmed that similar results can be obtained in the case of using liquid ammonia.
Table 5 shows results of the performance test of the pump apparatus
1
making use of ethyl ether at temperature of 10° C., Table 6 showing results of the performance test of the pump apparatus
1
making use of ethyl ether at temperature of 20° C., Table 7 showing results of the performance test of the pump apparatus
1
making use of ethyl ether at temperature of 40° C., Table 8 showing results of the performance test of the pump apparatus
1
making use of ethyl ether at temperature of 60° C., Tables 9 and 10 showing results of the performance test of the pump apparatus
1
making use of ethyl ether at temperature of 60° C., and Tables 11 to 13 showing results of the performance test of the pump apparatus
1
making use of liquid ammonia at 8° C.
TABLE 5
|
|
number of
input side
discharge side
differential
|
current
input
revolution
pressure
pressure
pressure
flow rate
|
A
W
msec
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.188
3.01
3.74
4011
−0.196
−284
−0.075
−109
175
3.89
233
10.12
|
0.209
3.34
4.02
3731
−0.193
−279
−0.020
−29
250
3.30
198
8.60
|
0.218
3.49
4.14
3623
−0.193
−280
0.003
5
285
2.85
171
7.42
|
0.235
3.76
4.38
3425
−0.190
−274
0.044
64
338
2.13
128
5.54
|
0.279
4.46
5.14
2918
−0.180
−261
0.118
171
431
0.00
0
0.00
|
|
TABLE 6
|
|
number of
input side
discharge side
differential
|
current
input
revolutions
pressure
pressure
pressure
flow rate
|
A
W
msec
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.167
2.67
3.46
4335
−0.096
−137
0.044
63
201
4.19
251
10.76
|
0.196
3.14
3.84
3906
−0.086
−123
0.148
211
334
3.08
185
7.91
|
0.211
3.38
4.08
3676
−0.079
−112
0.209
298
410
2.07
124
5.32
|
0.226
3.62
4.38
3425
−0.073
−104
0.255
363
467
1.02
61
2.61
|
0.243
3.89
4.56
3289
−0.071
−102
0.289
413
515
0.00
0
0.00
|
|
TABLE 7
|
|
number of
input side
discharge side
differential
|
current
input
revolutions
pressure
pressure
pressure
flow rate
|
A
W
msec
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.197
3.15
3.88
3866
0.246
342
0.381
530
188
4.40
264
11.02
|
0.206
3.30
4.06
3695
0.236
328
0.421
585
257
3.68
221
9.20
|
0.215
3.44
4.16
3606
0.243
338
0.455
632
294
2.99
179
7.48
|
0.225
3.60
4.38
3425
0.246
342
0.486
676
334
2.29
137
5.73
|
0.238
3.81
4.56
3289
0.255
354
0.530
737
383
1.39
84
3.48
|
0.262
4.19
5.00
3000
0.256
356
0.576
801
445
0.00
0
0.00
|
|
TABLE 8
|
|
number of
input side
discharge side
differential
|
current
input
revolution
pressure
pressure
pressure
flow rate
|
A
W
msec
Rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.206
3.30
4.08
3676
0.789
1065
0.943
1273
208
4.23
254
10.27
|
0.215
3.44
4.22
3555
0.785
1059
0.969
1308
249
3.60
216
8.74
|
0.220
3.52
4.34
3456
0.787
1062
0.996
1345
283
3.06
184
7.44
|
0.236
3.78
4.60
3261
0.804
1085
1.056
1425
340
2.03
122
4.93
|
0.248
3.97
4.84
3099
0.820
1107
1.102
1488
381
1.13
68
2.74
|
0.269
4.30
5.20
2885
0.783
1057
1.096
1480
423
0.00
0
0.00
|
|
TABLE 9
|
|
number of
input side
discharge side
differential
|
current
input
revolution
pressure
pressure
pressure
flow rate
|
A
W
Hz
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.215
3.44
59.10
3546
−141
131
272
310
|
0.229
3.66
55.86
3352
−90
380
470
250
|
0.240
3.84
53.47
3208
−59
544
603
200
|
0.253
4.05
50.76
3046
−36
699
735
150
|
0.266
4.26
48.07
2884
−22
826
848
100
|
0.282
4.51
44.64
2678
−8
966
974
50
|
0.295
4.72
42.73
2564
−3
0
|
|
TABLE 10
|
|
number of
input side
discharge side
differential
|
current
input
revolutions
pressure
pressure
pressure
flow rate
|
A
W
Hz
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.286
4.58
39.06
2344
−162
157
319
330
|
0.300
4.80
37.03
2222
−134
330
464
300
|
0.325
5.20
33.33
2000
−92
587
679
250
|
0.351
5.62
30.12
1807
−66
828
894
200
|
0.384
6.14
26.10
1566
−39
150
|
0.416
6.66
22.72
1363
−22
100
|
0.459
7.34
18.31
1099
−7
50
|
0.490
7.84
15.33
920
−2
0
|
|
TABLE 11
|
|
number of
input side
discharge side
differential
|
current
input
revolution
pressure
pressure
pressure
flow rate
|
A
W
Hz
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.145
2.32
64.10
3846
2.398
3309
2.569
3545
236
4.52
271
11.22
|
0.160
2.56
59.17
3550
2.393
3303
2.659
3669
366
3.05
183
7.58
|
0.193
3.09
56.17
3370
2.417
3335
2.742
3784
449
2.26
136
5.62
|
0.250
4.00
45.45
2727
2.412
3329
2.818
3889
560
0.18
11
0.44
|
|
TABLE 12
|
|
number of
input side
discharge side
differential
|
current
input
revolutions
pressure
pressure
pressure
flow rate
|
A
W
V
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.150
2.40
3.99
3660
2.486
3431
2.630
3629
198
5.24
315
13.03
|
0.160
2.56
3.85
3531
2.469
3407
2.649
3656
249
4.29
257
10.65
|
0.170
2.72
3.75
3439
2.464
3400
2.704
3732
332
3.15
189
7.83
|
|
TABLE 13
|
|
number of
input side
discharge side
differential
|
current
input
revolutions
pressure
pressure
pressure
flow rate
|
A
W
Hz
rpm
V
gf/cm
2
V
gf/cm
2
gf/cm
2
V
cc/min
kg/h
|
|
0.120
1.92
91.90
5514
2.550
3519
2.620
3616
97
5.00
300
12.42
|
|
The pump apparatus
1
makes use of the slide bearing members
5
formed of the above-mentioned AC to support the rotating shaft
4
, and so the above-mentioned construction can realize a pump apparatus of high efficiency involving a small consumption power required for operation as shown in
FIGS. 37
to
42
and Tables 5 to 13.
With the above-mentioned pump apparatus
1
, the drive means
9
drives the rotating shaft
4
to drive the pump body
10
connected to the rotating shaft
4
so that the refrigerant sucked through the suction port
33
can be made to flow down the flow passage
2
to be discharged from the discharge port
43
. The rotating shaft
4
is rotatably supported by the bearing apparatus
6
having the slide bearing members
5
. The slide bearing members
5
are formed of amorphous carbon, which possesses the above-mentioned properties and can support the rotating shaft
4
for smooth rotation. Besides, amorphous carbon possesses high chemical resistance and so is free of damage even in the case of being fitted into the fluid flow passage. Further, the rotating shaft
4
, the slide bearing members
5
and the rotor
7
are fitted into the flow passage
2
. The gap between the rotating shaft
4
and the slide bearing members
5
is formed to be exceedingly small as described above to further stabilize rotation of the rotating shaft
4
.
Such exceedingly small gap allows entering of liquid ammonia as the refrigerant due to the capillary phenomenon. As AC possesses high chemical resistance, it is free of damage even in the case of being fitted into the fluid flow passage. Also, the slide bearing members
5
formed of AC are made irrespective of the kind of a fluid used, and accordingly liquid ammonia can be made use of as a favorable lubricant. Accordingly, the pump apparatus makes it possible to use a refrigerant being fed as a lubricant and to achieve smooth rotation of the rotating shaft. Further, since the bearing structure
6
can be formed by means of slide bearing members, it can be made simple and undergoes less failure.
Also, AC is small in coefficient of friction to suppress the generation of heat produced upon rotation of the rotating shaft
4
and can prevent thermal expansion of the rotating shaft
4
and the slide bearing members
5
. Besides, even if frictional heat is generated, stable rotation could be maintained because AC is small in coefficient of thermal expansion and the gap, between the rotating shaft
4
and the slide bearing members
5
is not varied in dimension. Further, AC is small in coefficient of friction, so that with the above-mentioned small gap smooth rotation is achieved even for fluids of high viscosity such as liquid ammonia. Also, owing to small wear, even over long term use, the fluid is prevented from being contaminated with abrasion powder and the above-mentioned gap is prevented from being varied in dimension, so that smooth and stable rotation can be realized over a long term without maintenance. Accordingly, the pump apparatus can be preferably mounted on equipment used in outer space outside the stratosphere to enhance durability.
Also, provision of such rotating members in the housing
3
makes the sealing properties favorable and simplifies the construction therefor, thus enabling making the pump apparatus
1
small in size. Also, it is possible to cool the rotating shaft
4
, the slide bearing members
5
and the rotor
7
to keep a stable performance of the pump. Further, the cylindrical-shaped member
11
is thin-walled to provide a cooling effect of the stator
8
surrounding the rotor chamber
55
. Besides, the drive means
9
including the slide bearing members
5
and the rotor
7
is located upstream of the pump body
10
in a flow direction of the refrigerant, so that the slide bearing members
5
and the rotor
7
can be cooled prior to fluid compression by the pump body
10
and so a stable and favorable cooling effect is obtained. In this manner, such excellent pump apparatus
1
can be realized.
Also, the pump body
10
is formed of amorphous carbon, which is hardly subjected to chemical influences by the fluid, and maintains the function of the pump body over a long term, thus realizing a favorable pump apparatus
1
. Further, formation of the pump body
10
of amorphous carbon can have the pump body
10
fulfilling the function of thrust bearings and bearing the thrust load of the rotating shaft
4
. Therefore, the load on the slide bearing members
5
can be reduced. In this manner, the load is imposed on the pump body
10
to make it possible to reduce the slide bearing members
5
in size and enhance durability of the pump apparatus.
The above-mentioned embodiment is only exemplary of the invention and can be modified within the scope of the invention. For example, the slide bearing members
5
may be one in number or three or more. Also, the fluid may be other on than liquid ammonia.
Also, the support apparatus and the pump apparatus may be used in other equipment, such as medical equipment, than equipment used in outer space outside the stratosphere.
The invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and the range of equivalency of the claims are therefore intended to be embraced therein.
Claims
- 1. A support apparatus for displaceably supporting a movable member, comprising:a movable member comprising a rotating shaft; and a plurality of self-lubricating slide bearing members formed of amorphous carbon rotatably supporting said rotating shaft, said slide bearing members being radial bearings bearing a radial load of said rotating shaft; wherein said slide bearing members are arranged in a space in which a fluid is contained.
- 2. The support apparatus of claim 1, wherein a gap between said rotating shaft and said slide bearing members is dimensioned to allow entry of said fluid due to capillary phenomenon.
- 3. The support apparatus of claim 2, wherein said fluid is liquid ammonia.
- 4. The support apparatus of claim 2, wherein said gap is at least 0.75 micrometers and at most 2 micrometers.
- 5. The support apparatus of claim 1, wherein said support apparatus is mounted on equipment used in outer space.
- 6. A pump apparatus, comprising:a rotating shaft; slide bearing members formed of amorphous carbon for rotatably supporting said rotating shaft; a drive for drivingly rotating said rotating shaft; and a pump connected to said rotating shaft for pumping a fluid; wherein said slide bearing members are radial bearings bearing a radial load of said rotating shaft, and said pump body is formed of amorphous carbon to bear a thrust load of said rotating shaft.
- 7. A pump apparatus, comprising:a rotating shaft; slide bearing members for rotatably supporting said rotating shaft; a drive for drivingly rotating said rotating shaft; and a pump connected to said rotating shaft for pumping a fluid; wherein said slide bearing members are radial bearings bearing a radial load of said rotating shaft, and said pump body is formed of amorphous carbon to bear a thrust load of said rotating shaft.
- 8. A pump apparatus, comprising:a rotating shaft; a plurality of self-lubricating slide bearing members formed of amorphous carbon for rotatably supporting said rotating shaft, said slide bearing members being radial bearings bearing a radial load of said rotating shaft; a drive for drivingly rotating said rotating shaft; and a pump connected to said rotating shaft for pumping a fluid; wherein said slide bearing members are arranged in a space in which said fluid is contained so as to be exposed to said fluid.
- 9. The pump apparatus of claim 8, and further comprising a housing having a fluid flow passage which provides communication between a suction port and a discharge port wherein:said rotating shaft is arranged in said housing; said slide bearing members are fitted in said fluid flow passage in said housing; said drive comprises a rotor fitted in said fluid flow passage on said rotating shaft and a stator outside of said housing and surrounding said rotor; and said pump body is provided between ends of said fluid flow passage.
- 10. The pump apparatus of claim 9, wherein a gap between said rotating shaft and said slide bearing members is dimensioned to allow entry of said fluid due to capillary phenomenon.
- 11. The pump apparatus of claim 10, wherein said fluid is a liquid ammonia refrigerant circulated by said pump body.
- 12. The pump apparatus of claim 11, wherein said pump body is formed of amorphous carbon.
- 13. The pump apparatus of claim 8, wherein said pump apparatus is mounted on equipment used in outer space.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2001-079595 |
Mar 2001 |
JP |
|
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