Information
-
Patent Grant
-
6272862
-
Patent Number
6,272,862
-
Date Filed
Monday, March 27, 200024 years ago
-
Date Issued
Tuesday, August 14, 200123 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Andrus, Sceales, Starke & Sawall
-
CPC
-
US Classifications
Field of Search
US
- 060 696
- 092 1691
- 092 150
- 092 151
-
International Classifications
-
Abstract
An actuator having a body defining an internal cavity and a gland disposed within the cavity, the gland being secured against movement relative to the actuator body in a direction along the internal cavity by a securing element located in an opening of which respective parts are defined by the actuator body and the gland, and which allows insertion of the securing element into the opening along a substantially linear path.
Description
This invention relates to the retention of a gland within the body of an actuator, for example an hydraulic actuator for use in aerospace applications.
In a known type of hydraulic actuator, a gland is mounted about an actuator rod that extends through a cavity defined by the actuator body, the gland forming a fluid-tight partition dividing the cavity into two chambers which, typically, in use, contain hydraulic fluid under pressure. The known gland is retained axially in position within the actuator body by a wire ring located in a passageway formed by opposed grooves extending circumferentially respectively around the outer periphery of the gland and an inner surface of the actuator body defining the cavity.
However, a clearance must be provided between the wire ring and the surfaces defining the circumferentially extending grooves to allow the wire ring to be fed into the grooves during assembly of the actuator. This can result in an undesirable degree of play in the wire ring when located in the grooves leading to possible fretting fatigue problems during the life of the unit. Moreover the space envelope required by the cylinder to accommodate the wire ring necessitates an increase in cylinder diameter around its entire circumference, which can be undesirable for some aerospace applications.
An actuator is provided in accordance with the invention comprising a body defining an internal cavity and a gland disposed within the cavity, the gland being secured against movement relative to the actuator body in a direction along the internal cavity by a securing element located in an opening of which respective parts are defined by the actuator body and the gland, and which allows insertion of the securing element into the opening along a substantially linear path.
In one convenient arrangement, the opening part in the actuator body is formed by a hole and the opening part in the gland is a groove in the outer periphery thereof aligned with the hole, the securing element extending through the hole and lying along the groove.
Alternatively the opening part in the gland is a hole extending through the gland in alignment with the hole in the body, the securing element extending through at least a part of both of the holes.
Conveniently the securing element is locked in position by fastening devices extending axially and/or transversely of the securing element.
The securing element may be configured and arranged to provide in the opening a vent passage extending between the outer peripheral surface of the gland and the body exterior by way of the opening part in the body.
In order that the invention may be well understood, two embodiments thereof, which are given by way of example only, will now be described with reference to the accompanying drawings, in which:
FIG. 1
shows a first embodiment of the invention in the form of an hydraulic actuator containing a gland retained in place within the actuator body;
FIG. 2
shows a sectional view along the line (II—II) in
FIG. 1
;
FIG. 3
shows a perspective view of the gland shown in
FIGS. 1 and 2
;
FIG. 4
is a sectional view, corresponding to the sectional view in
FIG. 2
, of another of the actuator; and
FIG. 5
is a sectional view along the line (V—V) in FIG.
4
.
The actuator
1
in
FIG. 1
has a hollow body
2
defining a cavity
3
through which extends an actuator rod
4
. The actuator rod
4
is of a known type and is slidably mounted within the actuator body
2
in a known manner. A gland
5
is fitted within the body
2
so as to form a fluid-tight partition dividing the cavity
3
into two chambers
3
A and
3
B. The rod
4
divides each chamber into separate portions that can be connected to a variety of fluid pressure sources for controlling the position of the rod within the actuator body
2
. This aspect of the actuator
1
is known and will not be described in further detail. The gland
5
is secured in position within the actuator body
2
against the action of a pressure differential between chambers
3
A and
3
B by means of two securing elements, shown as pins
6
. The pins
6
are made of metal, but may alternatively be made of another sufficiently strong and rigid material.
FIG. 2
shows a partial cross-section through the actuator
1
viewed along the line (II—II) in FIG.
1
. The actuator body
2
is provided with a transversely extending rectangular flange
10
containing transversely and substantially linearly extending upper and lower bores
11
in which the securing pins
6
are received. One end portion
11
A of each of the bores
11
(the right hand end portion in
FIG. 2
) provides a through-hole in the actuator body
2
communicating with the cavity
3
and the outside of the actuator body
2
. The opposite end portion
11
B of each of the bores
11
(the left hand end portion in
FIG. 2
) opens into the cavity
3
and is closed at its distal end by an end wall
12
. The securing pins
6
are inserted respectively in the open end portions
11
A of the bores
11
and the respective leading end portions of the pins
6
are held in place in the opposite end portions
11
B of the respective bores
11
by screws
13
which engage threaded bores extending axially within the leading end portions of the pins
6
. A head of each screw
13
abuts a recessed outer surface of a respective one of the walls
12
.
The opposite end of each pin
6
(the right hand end in
FIG. 2
) is secured in location in its respective bore
11
by secondary retention means in the form of a pin or plug
14
. The pin or plug
14
is received partly in a secondary passage
15
extending from the bore
11
to the outside of the actuator body
2
and partly in a recess
16
in the securing pin
6
. The secondary bore
15
and the recess
16
both extend perpendicularly to the bore
11
in mutual alignment. The pin or plug
14
restricts movement of the securing pin
6
in the direction of its own axis.
The gland
5
has a substantially circular outer peripheral surface
20
engaging an inner peripheral surface of the body
2
, and a substantially circular inner peripheral surface
21
for slidably receiving the actuator rod
4
. The outer and inner peripheral surfaces
20
,
21
are concentrically arranged as shown in FIG.
3
. Mutually parallel linearly and transversely extending grooves
22
are formed on opposite sides of the gland
5
, being the top and bottom sides as seen in FIG.
2
. With the gland fitted inside the chamber
3
of the actuator body
2
the grooves
22
are aligned with respective ones of the bores
11
so that each groove and bore jointly form a respective opening in the form of a passageway in which the securing pins
6
are tightly fitted. The securing pins
6
thereby prevent movement of the gland
5
in the direction of the longitudinal axis of the actuator
1
. The pins
6
, bores
11
, and grooves
22
can be tightly toleranced, for example to within ±0.025 mm, for accurate location and secure retention of the gland within the actuator body
2
.
During assembly of the actuator
1
, the gland
5
is fitted into chamber
3
and its grooves
22
aligned with the respective bores
11
to form the resulting passageways. Securing pins
6
are inserted into respective passageways
11
,
22
and secured in place in the body
2
by the screws
13
. The secondary retaining pins or plugs
14
are then located in their respective recesses
16
and bores
15
. The gland
5
can be readily removed for replacement or repair by reversing these assembly steps.
Each groove
22
is disposed centrally between the axial ends of the gland
5
. Seals
23
are disposed to either side axially of the groove
22
for preventing egress of fluid from chambers
3
A,
3
B along the interface between the outer peripheral surface
20
of the gland
5
and the inner peripheral surface of the actuator body
2
. Each securing pin
6
has a flat face (not shown) extending along its entire length and is angularly orientated with respect to its longitudinal axis such that its flat face, together with the inner peripheral surface of a respective passageway
11
,
22
defines a vent passage providing fluid communication between the groove
22
and the exterior of the actuator
1
via the open ends
11
A of the passageways. Fluid leaking under pressure from one of the chambers
3
A,
3
B and reaching the groove
22
will thus be allowed to seep through the vent passage to atmosphere. In the embodiment of
FIGS. 1-3
, the provision of each flat face reduces the diameter of its pin
6
by the order of about 0.5 mm.
To further discourage fluid from leaking from one of the chambers
3
A,
3
B into the other, a respective auxiliary groove
25
extends from one end of each of the grooves
22
around the outer periphery of the gland
5
to a corresponding end of the other of the grooves
22
. Fluid migrating past one of the seals
23
along the interface between the outer peripheral surface
20
of the gland
5
and the inner peripheral surface of the actuator body
2
will be caught by the auxiliary grooves
25
and directed into the grooves
22
. The leaked fluid can then seep from the grooves
22
to atmosphere through the respective vent passages as described above.
Seals
26
are provided on the inner periphery of the gland
5
to prevent migration of fluid between the chambers
3
A,
3
B along the interface between the engaging peripheral surfaces of the gland
5
and the actuator rod
4
. Any fluid which does penetrate past one of the seals
26
is received in a groove
27
in the inner peripheral surface of the gland
5
which feeds to a bore
28
interconnecting the groove
27
and the lower one of the grooves
22
. The leaked fluid can thus be allowed to seep to atmosphere through the vent passage of the lower groove
22
.
FIGS. 4 and 5
show portions of a further actuator
50
embodying the invention. Actuator
50
is substantially identical to actuator
1
except that, instead of the grooves
22
, the gland
505
of actuator
50
has mutually parallel, linearly and transversely extending through-holes
522
for receiving the securing pins
6
.
By providing through-holes
522
in the glands
505
it is possible to provide a gland which is shorter in the direction of its longitudinal axis. This is because it is essential to maintain a predetermined minimum thickness of gland material between the groove
22
or through-hole
522
and the outer peripheral recesses in the gland which house the seals
23
. As best shown in
FIG. 5
, the thickness ‘t’ of material between the hole
522
and seal
23
becomes greater the further the hole is located towards the inner peripheral surface of the gland
505
. In the case where the groove
22
is located on the outer peripheral surface
20
of the gland
505
the thickness ‘t’ is a minimum, so that a longer gland
505
will be required to maintain a predetermined minimum thickness t. The transverse dimensions of the actuator in a direction along the pins and in a direction perpendicular thereto can both be reduced using a construction similar to that shown in
FIGS. 4 and 5
.
The embodiment of
FIGS. 4 and 5
facilitates the provision of a smaller gland
505
which is lighter and cheaper to produce whilst providing an actuator
50
having similar advantages to the actuator
1
of
FIGS. 1
to
3
.
Claims
- 1. An actuator comprising a body defining an internal cavity and a gland disposed within the cavity, the gland being secured against movement relative to the actuator body in a direction along the internal cavity by a securing element located in an opening of which respective parts are defined by the actuator body and the gland, and which allows insertion of the securing element into the opening along a substantially linear path, wherein the securing element is locked in position by fastening devices extending axially and/or transversely of the securing element.
- 2. An actuator as claimed in claim 1, wherein the opening part in the actuator body is formed by a hole and the opening part in the gland is a groove in the outer periphery thereof aligned with the hole, the securing element extending through the hole and lying along the groove.
- 3. An actuator as claimed in claim 1, wherein the opening part in the gland is a hole extending through the gland in alignment with the hole in the body, the securing element extending through at least a part of both of the holes.
- 4. An actuator as claimed in claim 1, wherein the securing element is configured and arranged to provide in the opening a vent passage extending between the outer periphery of the gland and the body exterior by way of the opening part in the body.
- 5. An actuator as claimed in claim 4, wherein the securing element is provided with a flat face which forms a wall of the vent passage when the securing element is inserted in a said opening having a substantially circular configuration.
- 6. An actuator as claimed in claim 1, wherein said opening part in the gland is interconnected for fluid communication with an auxiliary groove in the gland's outer periphery.
- 7. An actuator as claimed in claim 1, having more than one said opening, each opening allowing insertion therein of a respective said securing element.
- 8. An actuator comprising a body defining an internal cavity and a gland disposed within the cavity, the gland being secured against movement relative to the actuator body in a direction along the internal cavity by a securing element located in an opening of which respective parts are defined by the actuator body and the gland, and which allows insertion of the securing element into the opening along a substantially linear path, wherein the opening part in the actuator body is formed by a hole and the opening part in the gland is a groove in the outer periphery thereof aligned with the hole, the securing element extending through the hole and lying along the groove, the securing element configured and arranged to provide in the opening a vent passage extending between the outer periphery of the gland and the body exterior by way of the opening part in the body.
- 9. An actuator as claimed in claim 8, wherein the opening part in the gland is a hole extending through the gland in alignment with the hole in the body, the securing element extending through at least a part of both of the holes.
- 10. An actuator as claimed in claim 8, wherein the securing element is provided with a flat face which forms a wall of the vent passage when the securing element is inserted in a said opening having a substantially circular configuration.
- 11. An actuator as claimed in claim 8, wherein said opening part in the gland is interconnected for fluid communication with an auxiliary groove in the gland's outer periphery.
- 12. An actuator as claimed in claim 8, having more than one said opening, each opening allowing insertion therein of a respective said securing element.
- 13. An actuator comprising a body defining an internal cavity and a gland disposed within the cavity, the gland being secured against movement relative to the actuator body in a direction along the internal cavity by a securing element located in the opening of which respective parts are defined by the actuator body and the gland, and which allows insertion of the securing element into the opening along a substantially linear path, wherein the securing element is configured and arranged to provide in the opening a vent passage extending between the outer periphery of the gland and the body exterior by way of the opening part in the body.
- 14. An actuator as claimed in claim 13, wherein the opening part in the gland is a hole extending through the gland in alignment with the hole in the body, the securing element extending through at least a part of both of the holes.
- 15. An actuator as claimed in claim 14, wherein the securing element is provided with a flat face which forms a wall of the vent passage when the securing element is inserted in a said opening having a substantially circular configuration.
- 16. An actuator as claimed in claim 14, wherein said opening part in the gland is interconnected for fluid communication with an auxiliary groove in the gland's outer periphery.
- 17. An actuator as claimed in claim 14, having more than one said opening, each opening allowing insertion therein of a respective said securing element.
- 18. An actuator comprising a body defining an internal cavity and a gland disposed within the cavity, the gland being secured against movement relative to the actuator body in a direction along the internal cavity by a securing element located in an opening of which respective parts are defined by the actuator body and the gland, and which allows insertion of the securing element into the opening along a substantially linear path, wherein said opening part in the gland is interconnected for fluid communication with an auxiliary groove in the outer periphery of the gland.
Priority Claims (1)
Number |
Date |
Country |
Kind |
9907328 |
Mar 1999 |
GB |
|
US Referenced Citations (7)
Foreign Referenced Citations (6)
Number |
Date |
Country |
606819 |
Apr 1977 |
CH |
21 58 720 |
May 1973 |
DE |
38 31 909 |
Mar 1990 |
DE |
298 14 578 |
Oct 1998 |
DE |
0 348 687 |
Jan 1990 |
EP |
0 662 568 |
Jul 1995 |
EP |