Screw terminal

Information

  • Patent Grant
  • 6719593
  • Patent Number
    6,719,593
  • Date Filed
    Thursday, June 6, 2002
    22 years ago
  • Date Issued
    Tuesday, April 13, 2004
    20 years ago
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)
Number Name Date Kind
2602104 Hubbell et al. Jul 1952 A
2809363 Schertel et al. Oct 1957 A
3659253 Wiessner Apr 1972 A
3836941 Izraeli Sep 1974 A
3864005 Klein Feb 1975 A
4103986 Izraeli Aug 1978 A
4213669 Wittes et al. Jul 1980 A
4629281 Kruger Dec 1986 A
5747741 Alsch May 1998 A
5934818 Schmitt et al. Aug 1999 A
6004167 Hirakawa Dec 1999 A
6040525 Chauquet et al. Mar 2000 A
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