Information
-
Patent Grant
-
6719593
-
Patent Number
6,719,593
-
Date Filed
Thursday, June 6, 200222 years ago
-
Date Issued
Tuesday, April 13, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Ta; Tho D.
- Tsukerman; Larisa
Agents
- Parkhurst & Wendel, L.L.P.
-
CPC
-
US Classifications
Field of Search
US
- 174 84 C
- 174 40 CC
- 403 362
- 361 355
-
International Classifications
-
Abstract
Screw terminal connected to a conductor device mounted on a piece of electrical equipment to connect at least one conductor, composed of a connection cage and a screw, the cage and/or the screw being movable inside the terminal housing.A pressure device (30) composed of a head plate (31) and a pressure plate (32) connected to each other by two elastic symmetrical wings (33, 34) designed to store torque energy, the head plate being convex in shape and attached by the screw neck. The pressure plate can be applied against a conductor or against the conductor device on the equipment, and the elastic wings are concave in shape, with a concavity that is reduced as the pressure on the screw is increased.
Description
This invention concerns a screw terminal connected to a conductor device on electrical equipment for connecting at least one electrical conductor to this device.
In particular, it concerns a screw terminal composed of a connection cage equipped with a tapped hole, a screw with a threaded head and stem that screw into the tapped hole, and an elastic pressure device for application against the electrical conductor. The cage and/or the screw are moveable inside the housing on the electrical equipment, and the pressure device is composed of a head plate and a pressure plate connected to each other by an elastic wing that is designed to store torque energy, the head plate being subject to pressure from the screw head, and the pressure plate being applicable against the conductor or the equipment's conductor part.
The document DE U 1 935 560 describes a terminal of this type. A U-shaped stirrup pressure device, composed of a high wing and a low wing connected by a core is engaged by the high wing under the screw head and is applicable through the low wing against a conductor introduced into the cage; the stirrup core is a little higher than the length of the threaded portion in order to create pressurization. Because of the pressure exercised under the screw head, this pressurization prevents terminal loosening and/or after application of the screw stem against the low wing, to recover the creep of the conductor screw tightened by the terminal.
However, the U-shape of the pressure device leads to an unbalance during terminal use.
Document DE 40 13 225 also illustrates a screw terminal equipped with a pressure device in the form of a closed cage, where the deformation method is not described.
This invention is aimed at improving the balance of a screw terminal such as those described, while at the same time ensuring improved deformation for the pressure device, partly for the space occupied by the terminal, and partly to respect the elastic limit of the pressure device.
According to this invention the pressure device is composed of two elastic wings symmetrical with the axial plane of the screw, the elastic wings are concave shaped and the head of the screw acts on the head plate to place the pressure device under compression symmetrically when the screw is tightened. The pressure device provides an advantage by forming an interlocked ring with the rigid cage.
The conception of the pressure device is preferably designed so that the concave elastic wings change shape reducing the concavity when the strain created by the screw is increased. The head plate has a sloping or convex shape and the screw head presses on the head plate at a slight distance from the screw axis to facilitate the described reduction effect in the concavity of the sides. The pressure device can be engaged on the neck of the screw through an assembly plate composed of two circular half-sectors, and this can form or act with the elements that maintain the terminal in open position and improved insulation on the side of the opening where the conductor is inserted.
The description that follows is the non-limiting method for the production of this invention, with reference to the enclosed technical drawings.
FIG. 1
is a partial cross section of the screw terminal according to this invention.
FIG. 2
is the side view of the terminal as described in FIG.
1
.
FIG. 3
is the bird's eye view of the terminal as described in
FIG. 1
with a partial cross section according to sectional view
3
—
3
.
FIG. 4
illustrates the screw terminal action.
The screw terminal A shown in the drawing is destined for being mounted on a piece of electrical equipment. The only elements of this equipment shown in
FIG. 1
are the insulating housing
10
envisaged for the terminal, and a fixed connection branch from the rigid conductor
11
conductor device against which one or several conductors can be screwed in contact. In this manner,
FIG. 1
shows the two conductors C
1
and C
2
designed to be inserted respectively above and below the branch. Housing
10
is located in the piece of electrical equipment, which means that it is envisaged inside some part of the equipment casing or in a terminal strip attached to the equipment casing.
Terminal A is composed of a cage
12
of familiar type, composed of a strip of metal cut and folded to form a rigid ring of rectangular shape. On the short side
12
a
, the rigid cage
12
has a tapped hole
12
b
and the connecting branch of the conductor device
11
is inserted crosswise in the elongated opening
12
c
, rectangular in shape, of cage
12
.
Screw
20
is composed of a maneuver head
21
, a threaded stem
22
and a neck
23
that connects the threaded stem to the head. The threaded stem, or the non-threaded extension of this stem is terminated at the end with a boss
24
.
A pressure device
30
is coupled with the screw
20
so that both move together. Device
30
is a single elastic part closed in on itself to form a ring, and symmetrical with the axial plane P of the screw. It is composed of a head plate
31
located under the head
21
and it encircles the neck
23
of the screw, a pressure plate
32
applicable on the conductor C
1
or the contact branch of the conductor device
11
, and on each side of the screw axis, a concave wing
33
,
34
that is connected with the plates
31
,
32
through a connection zone that forms a protruding angle
35
. The concavity of the wings (refer to
FIGS. 1 and 4
to view the concavity) is designed so that the wings approach the screw axis at their centres. The head plate
31
is composed of two circular half sectors
31
a
,
31
b
that are engaged in the neck
23
of the screw to maintain the pressure device
30
in a balanced position. The half-sectors that form the head plate
31
are positioned so that they rise towards the head of the screw, providing the head plate with a generally sloping or convex form, and plate
31
terminates over these half-sectors with folded over axial joins
31
c
that meet at the axial plane P of the screw.
The pressure plate
32
is curved to provide a generally convex form for the lower portion of device
30
and presents ridges
32
b
that correspond with the recess
11
a
of the conductor device
11
.
As illustrated in
FIGS. 1 and 4
, device
30
is designed so that the concavity of its wings
33
,
34
combines with the convex shape of the plates
31
,
32
permitting deformation through compression, with a curve that is reduced as the pressure is increased. It can be noted that the reduction of the concavity is simultaneous with the maintaining of the device
30
in the contour defined by the protruding angles
35
, this contour being less than the width b of housing
10
for guidance needs.
In rest position, a slight distance C is foreseen between the boss
24
of the screw and the internal face
32
a
of the pressure plate
32
. This distance has been calculated so that the compensation provides the required stress level of the pressure device. The minimal distance d (observed in rest position) between the internal faces
33
a
,
34
a
of the wings
33
,
34
is slightly larger than the width e of the cage
12
so that the cage can slide freely between the wings or vice-versa. The head
21
of the screw is applied against the head plate
31
of the pressure device in an area located at a very slight distance f from the screw axis so that, through the plate
31
it creates a lever arm that accentuates the torque exercised on device
30
.
The internal walls of the insulating housing
10
have at least one blocking rim
10
a
that act with the heading formed by the upper angle of the pressure device to block the terminal in open position. At the same time, the insulating flap
36
that reduces the danger of over-rapid contact is fixed to wing
34
so that it moves with the pressure device and masks part of the conductor insertion opening. Stamped zones
36
can be provided in the strongly stressed region of angles
35
.
Below is a description of the terminal action. It can be noted that according to the piece of equipment on which this terminal is mounted, the terminal clamps an upper conductor C
1
, or a lower conductor C
2
, or both conductors C
1
and C
2
. The translation motion of the screw and the cage can be varied according to employment.
For example, when conductor C
1
is clamped, through the threaded action in the tapped hole
12
b
, the screw rotation makes cage
12
rise until it is in contact with the lower face of the fixed conductor branch
11
, at the same time as the descent of the screw in relation to cage
12
and to housing
10
. The descent continues until contact is made with the lower area of the pressure plate
32
against the face opposite branch
11
. Continuation of the screw rotation will provoke stress on the pressure device
30
through compression. This reduces the concavity of the wings
33
,
34
and the application of the boss
24
of the screw against the internal face
32
a
of the pressure plate
32
. (This action is illustrated by the dotted lines in FIG.
4
). It is worth noting that the head of the screw creates compression on the head plate, to facilitate the respecting of the elastic limit of device
30
. The torque energy stored in the wings
33
,
34
of device
30
contributes towards preventing the loosening of the screw by over-rapid rotation (action exercised by the head plate
31
on the head
21
) and towards recovering the creep play of conductor C
1
by moving the pressure plate
32
in relation to the boss
24
of the screw, with an amplitude that can attain c.
Claims
- 1. A screw terminal comprising:a connection cage having a tapped hole; a screw having a head, a neck, and a threaded part for threaded engagement with the tapped hole, wherein the cage threadingly travels along the screw while the screw rotates, and the cage and/or the screw is movable inside an equipment housing; and a pressure device comprising a head plate and a pressure plate connected to each other by two elastic wings for storage of torque energy, the head plate for compression by the head of the screw and the pressure plate for application of pressure against a conductor, wherein: the two elastic wings are symmetrical in relation to an axial plane of the screw, and are concave such that centers of said wings are closer to the axial plane of the screw than ends of said wings, and the head plate is compressed by the head of the screw to place the pressure device symmetrically in compression when the screw is tightened.
- 2. The screw terminal according to claim 1, wherein the pressure device has a predetermined shape and position for deforming the concave elastic wings to reduce curvature of said wings when strain by the screw on the head plate is increased.
- 3. The screw terminal according to claim 1, wherein the head plate of the pressure device comprises a convex shape or shape sloping towards the head of the screw and the head of the screw is for compressing the head plate at a predetermined distance from the screw axis.
- 4. The screw terminal according to claim 1, wherein the pressure plate of the pressure device comprises a convex shape located facing the conductor device.
- 5. The screw terminal according to claim 1, wherein the head plate of the pressure device comprises two circular half-sectors engaged in the neck of the screw and terminating with a fold over to form a join.
- 6. The screw terminal according to claim 1, wherein the pressure device comprises a ring interlaced with the connection cage, and internal faces of the concave wings have a predetermined distance therebetween slightly wider than the cage.
- 7. The screw terminal according to claim 1, further comprises a blocking ridge wherein a connection zone of a concave elastic wing with the head plate defines a protruding angle that acts with a blocking ridge created inside the terminal housing to maintain the terminal in open position.
- 8. The screw terminal according to claim 1, in which an insulating flap is fixed to one concave wing (34) of the pressure device.
Priority Claims (1)
Number |
Date |
Country |
Kind |
01 07624 |
Jun 2001 |
FR |
|
US Referenced Citations (12)
Foreign Referenced Citations (5)
Number |
Date |
Country |
325 260 |
Oct 1957 |
CH |
712 382 |
Oct 1941 |
DE |
733 024 |
Mar 1943 |
DE |
21 47 046 |
Apr 1973 |
DE |
63 870 |
Aug 1949 |
NL |