Information
-
Patent Grant
-
6603229
-
Patent Number
6,603,229
-
Date Filed
Wednesday, November 15, 200025 years ago
-
Date Issued
Tuesday, August 5, 200323 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Ramirez; Nestor
- Cuevas; Pedro J.
Agents
-
CPC
-
US Classifications
Field of Search
US
- 310 90
- 310 15
- 310 12
- 310 49 R
- 310 80
- 310 83
- 128 20524
- 251 12911
-
International Classifications
- H02K516
- H02K708
- H02K706
- H02K710
- H02K3700
- H02K4100
- H02K3300
- H02K3500
-
Abstract
In a preferred embodiment, a linear actuator, including: front and rear end bells; a stator structure; a rotor structure having first and second bearings journaled, respectively, in cavities formed in inner surfaces of the front and rear end bells; a captivation sleeve having its proximal end threadedly inserted in a cavity formed in an outer surface of the front end bell; and all foregoing elements being coaxially aligned to permit the insertion therethrough of a lead screw.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to motors generally and, more particularly, but not by way of limitation, to a novel linear actuator having a captivated lead screw and bearing pre-load adjustment.
2. Background Art
A linear actuator is a device used to perform operation along a linear path. One possible configuration of a linear actuator is one in which rotary motion is translated into linear motion by passing a lead screw through the threaded rotor of a rotary electric motor. In doing so, it is necessary to provide means to prevent rotation of the lead screw. This can be achieved using either external constraints or constraints internal to the actuator through captivation. The latter requires no external anti-rotation techniques.
Captive linear actuators provide anti-rotation by fastening anti-rotation shafts to the lead screw and passing this shaft through a bearing. The bearing is typically constrained with a sleeve mounted to a motor face. The shaft and bearing can be any configuration that allows linear translation without rotation of the shaft. Examples of this are splined, hexagonal, or butterfly shafts, etc. In motor applications using ball bearings for rotor rotation efficiency, it is necessary to pre-load the ball bearing between the inner and outer bearing race.
Accordingly, it is a principal object of the present invention to provide a linear motor with an internally captivated lead screw.
It is a further object of the invention to provide such a linear motor in which the pre-load of the ball bearings thereof is adjustable.
It is another object of the invention to provide such a linear motor that is economically constructed.
Other objects of the present invention, as well as particular features, elements, and advantages thereof, will be elucidated in, or be apparent from, the following description and the accompanying drawing figures.
SUMMARY OF THE INVENTION
The present invention achieves the above objects, among others, by providing, in a preferred embodiment, a linear actuator, comprising: front and rear end bells; a stator structure; a rotor structure having first and second bearings journaled, respectively, in cavities formed in inner surfaces of said front and rear end bells; a captivation sleeve having its proximal end threadedly inserted in a cavity formed in an outer surface of said front end bell; and all foregoing elements being coaxially aligned to permit the insertion therethrough of a lead screw.
BRIEF DESCRIPTION OF THE DRAWING
Understanding of the present invention and the various aspects thereof will be facilitated by reference to the accompanying drawing figures, submitted for purposes of illustration only and not intended to define the scope of the invention, on which:
FIG. 1
is an exploded, side elevational view, partially in cross-section, of a linear actuator constructed according to the present invention.
FIG. 2
is a cross-sectional side elevational view of the assembled linear actuator.
FIG. 3
is a side elevational view of the assembled linear actuator.
FIG. 4
is an exploded, isometric view of the captivation sleeve and anti-rotation bearing for the linear actuator.
FIG. 5
is a cross-sectional, isometric view of the captivation sleeve with the anti-rotation bearing inserted therein, but before rolling of the tabs of the sleeve.
FIG. 6
is a cross-sectional, isometric view of the sleeve of the present invention with locking tabs rolled over the anti-rotation bearing.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Reference should now be made to the drawing figures, on which similar or identical elements are given consistent identifying numerals throughout the various figures thereof, and on which parenthetical references to figure numbers direct the reader to the view(s) on which the element(s) being described is (are) best seen, although the element(s) may be seen also on other views.
FIGS. 1-3
illustrate the elements of a linear actuator, in this case an electric motor, constructed according to the present invention, and generally indicated by the reference numeral
20
. Motor
20
may be assumed to be a rotary hybrid stepper motor, incorporating both variable reluctance and permanent magnet motor characteristics. Motor
20
includes front and rear end bells
30
and
32
, respectively, a rotor assembly
34
, the latter having a permanent magnet structure
36
and first and second cylindrical ball bearing assemblies
38
and
40
, respectively, mounted on a shaft having a threaded portion
42
and a splined portion
44
, and a stator structure
45
surrounding the permanent magnet structure, all the foregoing elements being coaxially aligned. Lead wires
46
extend from stator structure
45
. When motor
20
is assembled (FIG.
2
), first and second ball bearings
38
and
40
will be journaled, respectively, in inner cavities
50
and
52
provided, respectively, in front and rear end bells
30
and
32
.
Threaded portion
42
is extendable through front and rear end bells
30
and
32
and the inner surface of rotor assembly
34
is threaded complementarily with the outer surface of the threaded portion.
Front end bell
30
includes an outer cavity
60
having its surface threaded so as to accept therein a threaded outer surface
62
of the proximal end of a cylindrical capitivation sleeve
64
. A spanner nut
66
disposed on threaded outer surface
62
bears against a cylindrical shoulder
68
formed on the front surface of front end bell
30
and secures captivation sleeve
64
in place. Formed at the distal end of captivation sleeve
64
is a cavity
70
having a shoulder
72
formed at the base thereof for the insertion into the cavity of an anti-rotation bearing
80
(FIG.
2
). One or more optional spring washers
86
are disposed between the outer end of first ball bearing
38
and the proximal end of captivation sleeve
64
. Again, all the foregoing elements of motor
20
, except of course lead wires
46
, are coaxially aligned.
Screwing captivation sleeve
64
into front end bell
30
against the outer surface of first ball bearing
38
permits first and second ball bearings
38
and
40
to be pre-loaded to a desired degree. This arrangement allows the pre-load to be adjusted after assembly of motor
20
and can even be achieved in the field, by changing the degree of torque of captivation sleeve
64
as it is threaded into cavity
60
. Spring washer(s)
86
may be provided to accommodate tolerances. This arrangement also permits the strength of spring washer(s)
86
, when used, and/or the degree of torque of captivation sleeve
64
to be changed for a particular motor
20
during manufacture, so that different degrees of pre-load can be obtained in a single motor size. The length of captivation sleeve
64
is determined by the desired stroke actuation of the lead screw which can easily be changed.
The distal end of splined portion
44
has a threaded section
90
extending therefrom. This is provided for attachment to an apparatus (not shown) with which motor
20
may be used, although such is not part of the present invention and other attachment means may be employed as well.
Splined portion
44
has, respectively, external and internal stops
100
and
102
fixedly attached thereto to limit the degree of travel of splined portion
44
and, concomitantly, threaded portion
42
.
Machine screws
98
(
FIG. 1
) extend through end bells
30
and
32
and stator structure
45
to secure together those elements of motor
20
.
FIG. 4
illustrates in more detail the construction of the distal end of captivation sleeve
64
and anti-rotation bearing
80
. The inner surface of anti-rotation bearing
80
has an involute splined surface
104
complementary to that of the outer surface of splined portion
44
(
FIGS. 1-3
) to prevent rotation of splined portion
44
and, concomitantly, threaded portion
42
.
The distal end of captivation sleeve
64
has three, equally spaced apart slots, as at
100
, formed therein to closely engage anti-rotation tabs
108
formed on the outer surface of anti-rotation bearing
80
when the anti-rotation bearing is inserted into cavity
70
to prevent the anti-rotation bearing from rotating with respect to the captivation sleeve. Also formed on the distal end of captivation sleeve
64
are three, equally spaced locking tabs, as at
110
, the function of which is described below.
FIG. 5
illustrates anti-rotation bearing
80
inserted into the distal end of captivation sleeve
64
and shows that the inner surface of the anti-rotation bearing bottoms out against shoulder
72
.
FIG. 6
is the same as
FIG. 5
, except that locking tabs
110
have been bent over the outer surface of anti-rotation bearing
80
by a rolling process to securely and fixedly hold the anti-rotation bearing in place in the distal end of captivation sleeve
64
.
The use of anti-rotation tabs
108
(
FIGS. 5 and 6
) and locking tabs
110
is very economical. Anti-rotation tabs
102
may be formed integrally with anti-rotation bearing
80
in a thermoplastic molding operation. Captivation sleeve
64
is preferably formed of aluminum. The other components of motor
20
can be formed of any suitable, conventional materials.
It will be understood that anti-rotation bearing
80
prevents splined portion
44
from rotating, while rotation of threaded portion
42
, due to the engagement of the threaded inner surface of rotor assembly
34
with the threaded outer surface of threaded portion
42
, will cause the splined portion to move out of the distal end of captivation sleeve
64
or to move into the distal end of the captivation sleeve as the rotor structure is caused to selectively rotate one direction or the other.
In the embodiments of the present invention described above, it will be recognized that individual elements and/or features thereof are not necessarily limited to a particular embodiment but, where applicable, are interchangeable and can be used in any selected embodiment even though such may not be specifically shown.
Terms such as “upper”, “lower”, “inner”, “outer”, “inwardly”, “outwardly”, “horizontal”, “vertical”, and the like, when used herein, refer to the positions of the respective elements shown on the accompanying drawing figures and the present invention is not necessarily limited to such positions.
It will thus be seen that the objects set forth above, among those elucidated in, or made apparent from, the preceding description, are efficiently attained and, since certain changes may be made in the above construction without departing from the scope of the invention, it is intended that all matter contained in the above description or shown on the accompanying drawing figures shall be interpreted as illustrative only and not in a limiting sense.
It is also to be understood that the following claims are intended to cover all of the generic and specific features of the invention herein described and all statements of the scope of the invention which, as a matter of language, might be said to fall therebetween.
Claims
- 1. A linear actuator, comprising:(a) front and rear end bells; (b) a stator structure; (c) a rotor structure having first and second bearings journaled, respectively, in cavities formed in inner surfaces of said front and rear end bells; (d) a captivation sleeve having its proximal end threadedly inserted in a cavity formed in an outer surface of said front end bell; (e) all foregoing elements being coaxially aligned to permit the insertion therethrough of a lead screw inserted through coaxially aligned foregoing elements, said lead screw having a threaded portion extending through said rotor structure and a splined portion extending through said captivation sleeve; and (f) a cylindrical anti-rotation bearing fixedly inserted in a distal end of said captivation sleeve, said anti-rotation bearing having an opening coaxial with said foregoing elements.
- 2. A linear actuator, as defined in claim 1, wherein: said proximal end of said captivation sleeve bears against an outer surface of said first bearing to impose a selected pre-load on said first and second bearings by selectively threadedly rotating said captivation sleeve inwardly or outwardly.
- 3. A linear actuator, as defined in claim 1, further comprising: a spring disposed between an outer surface of said first bearing and said proximal end of said captivation sleeve such that pre-load of said first and second bearings is determined by strength of said spring and degree of compression of said spring by said proximal end of said captivation sleeve being inserted into said cavity formed in an outer surface of said front end bell.
- 4. A linear actuator, as defined in claim 1, wherein:(a) said anti-rotation bearing has anti-rotation tabs molded integrally therewith; and (b) said captivation sleeve has slots formed in said distal end thereof into which sleeve said anti-rotation tabs closely fit to prevent rotation of said anti-rotation bearing with respect to said captivation sleeve.
- 5. A linear actuator, as defined in claim 1, wherein: said captivation sleeve has locking tabs formed in said distal end thereof and bent over an outer surface of said anti-rotation bearing to lock said anti-rotation bearing axially and radially in place in said captivation sleeve.
- 6. A linear actuator, comprising:(a) front and rear end bells; (b) a stator structure; (c) a rotor structure having first and second bearings journaled, respectively, in cavities formed in inner surfaces of said front and rear end bells; (d) a captivation sleeve having its proximal end threadedly inserted in a cavity formed in an outer surface of said front end bell; (e) a lead screw inserted through coaxially aligned foregoing elements, said lead screw having a threaded portion extending through said rotor structure and a splined portion extending through said captivation sleeve; and (f) a cylindrical anti-rotation bearing fixedly inserted in a distal end of said captivation sleeve, said anti-rotation bearing having an opening coaxial with said foregoing elements.
- 7. A linear actuator, as defined in claim 6, wherein: said proximal end of said captivation sleeve bears against an outer surface of said first bearing to impose a selected pre-load on said first and second bearings by selectively threadedly rotating said captivation sleeve inwardly or outwardly.
- 8. A linear actuator, as defined in claim 7, further comprising: a spring disposed between an outer surface of said first bearing and said proximal end of said captivation sleeve such that pre-load of said first and second bearings is determined by strength of said spring and degree of compression of said spring by said proximal end of said captivation sleeve being inserted into said cavity formed in an outer surface of said front end bell.
- 9. A linear actuator, as defined in claim 7, wherein:(a) said anti-rotation bearing has anti-rotation tabs molded integrally therewith; and (b) said captivation sleeve has slots formed in said distal end thereof into which sleeve said anti-rotation tabs closely fit to prevent rotation of said anti-rotation bearing with respect to said captivation sleeve.
- 10. A linear actuator, as defined in claim 7, wherein: said captivation sleeve has locking tabs formed in said distal end thereof and bent over an outer surface of said anti-rotation bearing to lock said anti-rotation bearing axially and radially in place in said captivation sleeve.
US Referenced Citations (26)