CN103367979B - Connector assembly - Google Patents
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- CN103367979B CN103367979B CN201310120080.XA CN201310120080A CN103367979B CN 103367979 B CN103367979 B CN 103367979B CN 201310120080 A CN201310120080 A CN 201310120080A CN 103367979 B CN103367979 B CN 103367979B
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Abstract
The invention provides a kind of connector assembly, comprising: the first connector, be electrically connected with the first object, comprise: the first connector, be electrically connected with the first object, comprise: the first fuselage, be formed with the first engagement groove in side; First signal pin, is inserted in the inside of above-mentioned first fuselage, and end is positioned on above-mentioned first engagement groove, and insulate with above-mentioned first fuselage; And connecting connector, comprising: connect fuselage, one end is combined in above-mentioned first engagement groove, in order to be electrically connected above-mentioned first fuselage; Bonding conductor, is inserted in the inside of above-mentioned connection fuselage, and above-mentioned first engagement groove contacts with above-mentioned first signal pin, in order to be electrically connected above-mentioned first signal pin, and insulate with the above-mentioned fuselage that is connected; Wherein, in above-mentioned first fuselage, the inner peripheral surface contacted with the outer peripheral face of above-mentioned connection fuselage in the inner peripheral surface of above-mentioned first engagement groove obtains the gradient (grade).Be formed with the first contact site in above-mentioned connection fuselage, above-mentioned first contact site protrudes from outer peripheral face, and contacts with the inner peripheral surface of above-mentioned first fuselage; Be formed with fixture block in above-mentioned first fuselage, above-mentioned fixture block protrudes from inner peripheral surface, in order to above-mentioned first contact site of buckle, is separated with above-mentioned first connector to prevent above-mentioned connection fuselage.
Description
Technical field
The present invention relates to connector assembly, more specifically relate to a kind of when object is electrically connected, can compensate while misprinting row, avoid connector assembly to damage and stably carry out the connector assembly that connects.
Background technology
Transmit between wire-wireless communication device and have multi-signal.Mutually be electrically connected between the communicator of transmission signal, usually utilize the connector with public connector portion and female connectors portion.Further, the internal circuit of radio communication device is generally presented on substrate (such as, printed circuit board (PCB) (PrintedCircuitBoard)).This matrix technique, with the development of very fast speed, except the printed circuit board (PCB) of hard character, can realize the flexible printed circuit board (FlexiblePCB moved freely; FPCB) be also widely used.
But, when being electrically connected by connector assembly between object, particularly by when carrying out between substrate being electrically connected, have following problem, that is, if slightly stagger and misprint row in the position being arranged on the connector of substrate, the electrical connection between substrate will make a mistake.Further, when connecting connector assembly between object, if apply necessary above pressure in order to stable connection, connector assembly will be caused to damage.
Summary of the invention
The invention provides a kind of connector assembly, it when being electrically connected object, can compensating and misprinting row, and connector assembly can be avoided to damage and stably connect simultaneously.
According to an embodiment of the present invention, the invention provides a kind of connector assembly, its feature is, comprising: the first connector, and it is electrically connected with the first object, and described first connector comprises: the first fuselage, and it is formed with the first engagement groove in side; First signal pin, it is inserted in the inside of described first fuselage, and end is positioned on described first engagement groove, and insulate with described first fuselage; And, connecting connector, it comprises: connect fuselage, its one end is combined in described first engagement groove, in order to be electrically connected described first fuselage; Bonding conductor, is inserted in the inside of described connection fuselage, and described first engagement groove contacts with described first signal pin, in order to be electrically connected described first signal pin, and insulate with the described fuselage that is connected; Wherein, in described first fuselage, the inner peripheral surface contacted with the outer peripheral face of described connection fuselage in the inner peripheral surface of described first engagement groove obtains the gradient.
The present invention also provides a kind of connector assembly, and its feature is, comprising: the first connector, and it is electrically connected with the first object, and described first connector comprises: the first fuselage, and it is formed with the first engagement groove in side; First signal pin, it is inserted in the inside of described first fuselage, and end is positioned on described first engagement groove, and insulate with described first fuselage; Holding wire, it, at described first fuselage form right angle or straight line, is electrically connected with described first signal pin; And, connecting connector, it comprises: connect fuselage, one end is combined in described first engagement groove, in order to be electrically connected described first fuselage; Bonding conductor, is inserted in the inside of described connection fuselage, and described first engagement groove contacts with described first signal pin, in order to be electrically connected described first signal pin, and insulate with the described fuselage that is connected; Wherein, in described first fuselage, the inner peripheral surface contacted with the outer peripheral face of described connection fuselage in the inner peripheral surface of described first engagement groove obtains the gradient.
Be formed with the first contact site in described connection fuselage, described first contact site protrudes from outer peripheral face and is formed, and contacts with the inner peripheral surface of described first fuselage; Be formed with fixture block in described first fuselage, described fixture block protrudes from inner peripheral surface and is formed, and in order to the first contact site described in buckle, is separated with described first connector to prevent described connection fuselage.
Be connected with the second connector at the other end of described connection fuselage, described second connector is electrically connected with the second object, and it comprises: the second fuselage, and it is formed with the second engagement groove in side; And, secondary signal pin, it is inserted in the inside of described second fuselage, and its end is positioned on described second engagement groove, and insulate with described second fuselage; The other end of described connection fuselage is combined in described second engagement groove, and in order to be electrically connected described second fuselage, described bonding conductor contacts with described secondary signal pin on described second engagement groove, in order to be electrically connected described secondary signal pin.
On the direction that described connection fuselage inserts, described first engagement groove reduces gradually with the diameter of the inner peripheral surface that the outer peripheral face of described connection fuselage contacts.
Be formed with the second contact site in described connection fuselage, described second contact site protrudes from the outer peripheral face of described connection fuselage and is formed, and contacts with the inner peripheral surface of described second fuselage.
The outer peripheral face of described first contact site and described second contact site is formed with circular shape.
Described first connector also comprises the first insulator, described first insulator is combined between described first fuselage and described first signal pin, in order to described first signal pin be electrically connected with the holding wire of described first object and described first fuselage be electrically connected with the earth connection of described first object of insulating.
Described second connector also comprises the second insulator, described second insulator is combined between described second fuselage and described secondary signal pin, in order to the described secondary signal pin be electrically connected with the holding wire of described second object and described second fuselage be electrically connected with the earth connection of described second object of insulating.
Described connecting connector also comprises connection insulator, and described connection insulator is combined between described connection fuselage and described bonding conductor, in order to described connection fuselage and the described bonding conductor of insulating.
Described bonding conductor is formed with link slot at two ends, inserts described first signal pin to be electrically connected, insert described secondary signal pin to be electrically connected in the described link slot that another end is formed in the described link slot that an end is formed.
The conglobate spherical state of part structure that described first signal pin and described secondary signal pin are electrically connected with described bonding conductor, and protrude formation from outer peripheral face.
Be formed with at least one groove in described connection fuselage, at least one groove described is formed from end to third side to through inner peripheral surface and outer peripheral face.
Described connector assembly also comprises: conductive elastomer, is inserted in described second engagement groove, and when pressurizeing described connection fuselage to described second connector direction from described first connector, described conductive elastomer is in order to provide elasticity to described connection fuselage.
Described conductive elastomer is ring-type, in order to provide elasticity between the end and described second fuselage of described connection fuselage.
Described connector assembly also comprises: at least one conductive rubber, and at least one conductive rubber described is inserted in the outer peripheral face of described connection fuselage, in order to mask the RF signal of leakage.
Described connector assembly also comprises: the first conductive rubber, between the outer peripheral face of its inner peripheral surface at described first engagement groove and described connection fuselage, in order to mask the RF signal of leakage; And the second conductive rubber, between the outer peripheral face of its inner peripheral surface at described second engagement groove and described connection fuselage, in order to mask the RF signal of leakage.
Described connector assembly also comprises: conductive elastomer, and it is inserted in described second engagement groove, when pressurizeing described connection fuselage to described second connector direction from described first connector, in order to provide elasticity to described connection fuselage; And at least one conductive rubber, it is inserted in the outer peripheral face of described connection fuselage, in order to mask the RF signal of leakage.
Be formed in the lower end of described first fuselage of described first connector and conclude fuselage, be formed with the screw hole of joint bolt at described both ends of concluding fuselage, or be formed with the rivet hole of binding rivet, fixing for described first object.
Described holding wire is connected with at the described sidepiece concluding fuselage, ' L ' shape and form right angle is formed to make described holding wire and described first fuselage, or be connected with described holding wire in described bottom of concluding fuselage, form ' I ' shape to make described holding wire and described first fuselage and formed straight line.
Tool of the present invention has the following advantages: even if need the part that connects consistent not between object, also stably can realize electrical connection, thus can compensate and misprint row, can make to be electrically connected between object simultaneously.Such as, if object is substrate, though connector be arranged on substrate position and inconsistent when, also can avoid the damage of connector assembly and compensate misprinting row, and stably connection substrate.And, even if the electrical characteristics caused to prevent the connection of object reduce, apply necessary above pressure and when concluding connector, also can make the state that connector assembly maintenance is best when removing pressure, thus the damage of connector assembly can be prevented and keep best state.
Accompanying drawing explanation
Fig. 1 is the stereogram of the first embodiment of connector assembly of the present invention;
Fig. 2 to Fig. 4 is the profile of the cohesive process of connector assembly in Fig. 1;
Fig. 5 is the profile while row are misprinted in compensation, object being carried out the connector assembly in the Fig. 1 be electrically connected;
Fig. 6 is the exploded perspective view of connecting connector in Fig. 1 and the second connector and conductive rubber;
Fig. 7 is the profile of the connector assembly of the conductive rubber be inserted with in Fig. 6;
Fig. 8 is the exploded perspective view of connecting connector in Fig. 1 and the second connector and conductive elastomer;
Fig. 9 is the profile of the connector assembly of the conductive elastomer be inserted with in Fig. 8;
Figure 10 is the profile of the connector assembly of the conductive elastomer being inserted with conductive rubber in Fig. 6 and Fig. 8;
Figure 11 is the stereogram of the second embodiment of connector assembly of the present invention;
Figure 12 is another stereogram of the second embodiment of connector assembly of the present invention;
Figure 13 is the profile of the bonding state of the connector assembly of Figure 11;
Figure 14 is another profile of the bonding state of the connector assembly of Figure 11;
Figure 15 is another profile of the connector assembly of Figure 11 and the bonding state of first and second object.
Embodiment
Below, be described embodiments of the invention with reference to accompanying drawing, meanwhile, the identical Reference numeral marked in each accompanying drawing represents identical parts.
first embodiment
Fig. 1 is the stereogram of the first embodiment of connector assembly 100 of the present invention.Fig. 2 to Fig. 4 is the profile of the cohesive process of connector assembly 100 in Fig. 1.
Referring to figs. 1 through Fig. 4, connector assembly 100 comprises the first connector 200 and connecting connector 300.
Above-mentioned first connector 200 comprises the first fuselage 210, first signal pin 270 and the first insulator 250.First fuselage 210 is formed with the first engagement groove 220 in its side, and opposite side is electrically connected with the earth connection of the first object (not shown).
Above-mentioned first object can be substrate, coaxial cable etc., if above-mentioned first object is substrate, multiple earth connections of substrate are electrically connected with the first fuselage 210 respectively.The first signal pin 270 is inserted with in the inside of the first fuselage 210.
First signal pin 270 is positioned at the hollow position of the inside being formed in the first fuselage 210, to insulate with the first fuselage 210.One end of first signal pin 270 is positioned at the inside of the first engagement groove 220, and the other end is electrically connected with the holding wire of above-mentioned first object.Such as, if above-mentioned first object is substrate, then multiple signal pins of substrate are electrically connected with the first signal pin 270 respectively.
First insulator 250 is combined between the first signal pin 270 and the first fuselage 210, insulate to make the first signal pin 270 and the first fuselage 210.
Such as, the first insulator 250 is inserted in the hollow position of the inside being formed at the first fuselage 210 and combines, and the first signal pin 270 is inserted in the through hole that is formed at the first insulator 250 inside and combines.
Further, fixture block 215 is formed with at the medial surface of above-mentioned first engagement groove 220.The effect of above-mentioned fixture block 215 will be described hereinafter.
In addition, also comprise the second connector 400 in the present invention, above-mentioned second connector 400 is incorporated into the opposite side of above-mentioned first connector 200 and connecting connector 300.
Above-mentioned second connector 400 comprises the second fuselage 410, secondary signal pin 470 and the second insulator 450.Above-mentioned second fuselage 410 is formed with the second engagement groove 420 in its side, and its opposite side is electrically connected with the earth connection of the second object (not shown).
Above-mentioned second object can be substrate, coaxial cable etc., if above-mentioned second object is substrate, multiple earth connections of substrate are electrically connected with the second fuselage 410 respectively.
Secondary signal pin 470 is inserted with in the inside of the second fuselage 410.
Secondary signal pin 470 is positioned at the hollow position being formed in the second fuselage 410 inside, to insulate with the second fuselage 410.One end of secondary signal pin 470 is positioned at the inside of the second engagement groove 420, and the other end is electrically connected with the holding wire of above-mentioned second object.Such as, if above-mentioned second object is substrate, multiple signal pins of substrate are electrically connected with secondary signal pin 470 respectively.
Second insulator 450 is combined between secondary signal pin 470 and the second fuselage 410, insulate to make secondary signal pin 470 and the second fuselage 410.
Such as, the second insulator 450 is inserted in the hollow position that is formed at the second fuselage 410 inside and combines, and secondary signal pin 470 is inserted in the through hole that is formed at the second insulator 450 inside and combines.
In addition, above-mentioned connecting connector 300 comprises and connects fuselage 310, bonding conductor 370,380 and connection insulator 350.
Above-mentioned connection fuselage 310 is combined in the first engagement groove 220 and the second engagement groove 420, in order to be electrically connected the first fuselage 210 and the second fuselage 410.
Namely, the first engagement groove 220 is inserted in by the side connecting fuselage 310, to make connection fuselage 310 and the first fuselage 210 be electrically connected, be inserted in the second engagement groove 420 by the opposite side connecting fuselage 310, be electrically connected to make connection fuselage 310 and the second fuselage 410.
The outer peripheral face connecting the direction, side of fuselage 310 contacts with the inner peripheral surface of the first engagement groove 220, is electrically connected to make connection fuselage 310 and the first fuselage 210.
The part contacted with the outer peripheral face connecting fuselage 310 in the inner peripheral surface of the first engagement groove 220 obtains the gradient (grade).That is, the inner peripheral surface of the first engagement groove 220 contacted with the outer peripheral face connecting fuselage 310 is formed obliquely.
In the first engagement groove 220, the diameter of the inner peripheral surface of the first engagement groove 220 contacted with the outer peripheral face connecting fuselage 310, reduces gradually to the direction (from the lower end of the first fuselage 210 to upper extreme direction in Fig. 2 to Fig. 4) connecting fuselage 310 insertion.
As mentioned above, because the inner peripheral surface of the first engagement groove 220 is reduced (tapered), therefore, even if apply pressure from the first connector 200 to the second connector 400 direction, make after reaching maximum compression as shown in Figure 4, when removing the pressure from the first connector 200 to the second connector 400 direction, by the effect of restoring force, as shown in Figure 2 or Figure 3, the position of connecting connector 300 is adjusted.
Two ends due to connecting connector 300 need to have with the first connector 200 or the second connector 400 to be less than appointed interval (such as, 1mm etc.) interval, just can have good characteristics of signals, the inner peripheral surface of the first engagement groove 220 reduced provides elastic force to connecting connector 300, appointed interval is less than (such as to make two ends of connecting connector 300 and the first connector 200 or the second connector 400 have, 1mm etc.) interval, thus keep best characteristics of signals.
When the connection fuselage 310 of connecting connector 300 moves with the form shown in Fig. 4, damaging to prevent connecting fuselage 310, connecting fuselage 310 at least one groove 320 being formed with through inner peripheral surface and outer peripheral face from end to the direction of centre.
That is, when pressurizeing as shown in Figure 4, will reduce the size of at least one groove 320, and avoid connection fuselage 310 damage and connection fuselage 310 is moved, when returning to Fig. 2 or Fig. 3 from Fig. 4, at least one groove 320 will return to original size.
In order in the second engagement groove 420 of the second connector 400, end and second connector 400 of connecting connector 300 have the interval being less than appointed interval, in the moment of form reaching Fig. 2 or Fig. 3, from the direction of the first connector 200 to the second connector 400, applied pressure can not stop, but until exert pressure reach the situation of Fig. 4.
Namely, if in the second engagement groove 420, end and second connector 400 of connecting connector 300 separate the interval being greater than appointed interval, and RF characteristics of signals will be caused to reduce, and because the coupling part of secondary signal pin 470 and bonding conductor 370 shortens, characteristics of signals will be caused to reduce.
Therefore, in order to the end of connecting connector 300 and the second connector 400 there is the interval that is less than appointed interval in the second engagement groove 420 and apply pressure time, form as shown in Figure 4 will be produced, when removing pressure under the state of fig. 4, connecting connector 300 will be restored as shown in Figure 2 or Figure 3, in the second engagement groove 420, the end of connecting connector 300 and the second connector 400 have the interval that is less than appointed interval and are close to, thus by connecting connector 300, first connector 200 and the second connector 400 are electrically connected.
Connect fuselage 310 to comprise: the first contact site 315, protrude from the outer peripheral face of above-mentioned connection fuselage 310, and carry out electrical contact with the inner peripheral surface of the first fuselage 210; Second contact site 415, protrudes from the outer peripheral face of above-mentioned connection fuselage 310, and carries out electrical contact with the inner peripheral surface of the second fuselage 410.
First contact site 315 is formed in the end towards the first connector 200 direction in the outer peripheral face connecting fuselage 310, and the second contact site 415 is formed in the end towards the second connector 400 direction in the outer peripheral face connecting fuselage 310.The outer peripheral face of the first contact site 315 and the second contact site 415 is formed with the form of circular arc.
Be formed with fixture block 215 in first fuselage 210, above-mentioned fixture block 215 protrudes and buckle first contact site 315 from the inner peripheral surface of above-mentioned first fuselage 210, is separated with the first connector 200 to prevent junctor body 310.
Namely, after the side of connecting connector 300 is inserted in the first connector 200, first contact site 315 is buckled in fixture block 215, thus prevent connecting connector 300 to be easily separated from the first connector 200, after connecting connector 300 is inserted in the first connector 200 and the second connector 400, when the first connector 200 and the second connector 400 will be separated from connecting connector 300, because the first contact site 315 is buckled in fixture block 215, thus the first connector 200 is prevented to be separated from connecting connector 300 prior to the second connector 400.
Bonding conductor 370,380 is inserted in the inside connecting fuselage 310, first engagement groove 220 contacts with the first signal pin 270, second engagement groove 420 contacts with secondary signal pin 470, to make the first signal pin 270 and secondary signal pin 470 be electrically connected, and be connected fuselage 310 and insulate.
Two ends of bonding conductor 370,380 are formed with link slot 379,389, first signal pin 270 is inserted in the link slot 379 of an end formation of bonding conductor 370,380 and is electrically connected, and secondary signal pin 470 is inserted in the link slot 389 of another end formation of bonding conductor 370,380 and is electrically connected.
In the first signal pin 270, to contact with link slot 379 and the part 275 be electrically connected has rounding top and bottom pattern, and protrude formation from the outer peripheral face of the first signal pin 270, in secondary signal pin 470, contact with link slot 389 and the part 475 that is electrically connected has rounding top and bottom pattern, and protrude from the outer peripheral face of secondary signal pin 470 and formed.
With regard to bonding conductor 370,380, the bonding conductor 370 corresponding with the first signal pin 270 and the bonding conductor 380 corresponding with secondary signal pin 470 form one, or bonding conductor 370 and each independent formation of bonding conductor 380 combine.
Form one or each independent formation and the bonding conductor 370,380 combined is inserted into and connects the inside of insulator 350, thus make bonding conductor 370,380 and be connected fuselage 310 and insulate.
When utilizing connector assembly 100 as above to make above-mentioned first object and above-mentioned second object be electrically connected, first connector 200 is installed in above-mentioned first object, and under the state combined in the side of the first connector 200 and connecting connector 300, start the opposite side in conjunction with connecting connector 300 in the second connector 200 being arranged on above-mentioned second object.In addition, in order to as mentioned above in conjunction with connecting connector 300 and the second connector 400, pressure is applied and after reaching state as shown in Figure 4 from the direction of the first connector 200 to the second connector 400, when removal is from the direction of the first connector 200 to the second connector 400 during applied pressure, connecting connector 300 moves with state as shown in Figure 2 or Figure 3, thus makes above-mentioned first object and above-mentioned second object electrical connection.
Fig. 5 makes object carry out the profile of the connector assembly 100 in the Fig. 1 be electrically connected while row are misprinted in compensation.
Referring to figs. 1 through Fig. 5, when the position that the first connector 200 in above-mentioned first object combines is different with the position that the second connector 400 in above-mentioned second object combines, as shown in Figure 5, according to the connector assembly 100 of the embodiment based on technological thought of the present invention, above-mentioned first object is stably connected with above-mentioned second object.
That is, the connecting connector 300 of connector assembly 100 performs and misprints row compensate function, therefore, even if position is not too consistent, the first connector 200 also can be made stably to be connected with the second connector 400.And, in first signal pin 270 contact with link slot 379 and the part 275 be electrically connected with in secondary signal pin 470 contact with link slot 389 and the part be electrically connected is formed with rounding top and bottom pattern, therefore, when row are misprinted in compensation, cut, damaged equivalent damage in the first signal pin 270, secondary signal pin 470 and bonding conductor 370, can not be there is.In addition, the contact site 315 connecting fuselage 310 is also formed with arcuation, therefore, when row are misprinted in compensation, connects in fuselage 310, first fuselage 210 and the second fuselage 410 and cut, damaged equivalent damage can not occur.
Fig. 6 is the connecting connector 300 of Fig. 1 and the exploded perspective view of the second connector 400 and conductive rubber 910, and Fig. 7 is the profile of the connector assembly 100 ' of the conductive rubber 910 being inserted with Fig. 6.
Referring to figs. 1 through Fig. 7, connector assembly 100 ' comprises the first connector 200, connecting connector 300, second connector 400 and at least one conductive rubber 910.First connector 200 of connector assembly 100 ', connecting connector 300 and the second connector 400 are identical with the first connector 200 in Fig. 1 to Fig. 4, connecting connector 300 and the second connector 400, and the explanation therefore repeated replaces by the explanation relevant to Fig. 1 to Fig. 4.
At least one conductive rubber 910 is inserted in the outer peripheral face connecting fuselage 310, to mask the RF signal of leakage.Two conductive rubbers 910 shown in Fig. 7 are inserted in the situation of the outer peripheral face connecting fuselage 310, but the present invention is not defined in this situation, between the outer peripheral face that at least one conductive rubber 910 can be combined in connection fuselage 310 and the inner peripheral surface of the first engagement groove 220 or the second engagement groove 420.
In the case of fig. 7, be combined in the conductive rubber 910 between outer peripheral face and the inner peripheral surface of the first engagement groove 220 connecting fuselage 310 mask the inner peripheral surface of the first engagement groove 220 and connect the RF signal leaked between the outer peripheral face of fuselage 310, be combined in the conductive rubber 910 between outer peripheral face and the inner peripheral surface of the second engagement groove 420 connecting fuselage 310 and mask the inner peripheral surface of the second engagement groove 420 and connect the RF signal leaked between the outer peripheral face of fuselage 310.
Conductive rubber 910 can connect the outer peripheral face of fuselage 310 by Intercalation, and make connection fuselage 310 be combined in the first engagement groove 220 or the second engagement groove 420, or, under the state that also can be combined in the inner peripheral surface of at least one in the first engagement groove 220 and the second engagement groove 420 at conductive rubber 910, connection fuselage 310 is made to be combined in the first engagement groove 220 and the second engagement groove 420.
Fig. 8 is the connecting connector 300 of Fig. 1 and the exploded perspective view of the second connector 400 and conductive elastomer 1110, and Fig. 9 is the connector assembly 100 of the conductive elastomer 1110 being inserted with Fig. 8 " profile.
Referring to figs. 1 through Fig. 4, Fig. 8 and Fig. 9, connector assembly 100 " comprise the first connector 200, connecting connector 300, second connector 400 and conductive elastomer 1110.
Connector assembly 100 " the first connector 200, connecting connector 300 and the second connector 400 and Fig. 1 identical to the first connector 200 illustrated in fig. 4, connecting connector 300 and the second connector 400, the explanation therefore repeated replaces by the explanation relevant to Fig. 1 to Fig. 4.
Conductive elastomer 1110 is inserted in the second engagement groove 420, when connecting fuselage 310 from the first connector 200 to the second connector 400 direction pressurization, has good RF characteristic in order to provide flexible to connection fuselage 310 simultaneously.
Such as, conductive elastomer 1110 is combined in the bottom surface of the second engagement groove 420, when connecting fuselage 310 from the first connector 200 to the second connector 400 direction pressurization, in order to provide elasticity in the bottom surface of the second engagement groove 420, thus prevent from damaging between the end of connection fuselage 310 and the second fuselage 410.
Further, due to the effect of conductive elastomer 1110, the position obtained with the earth connection of the second connector 400 is promoted the effect be equal to the height size of conductive elastomer 1110, RF characteristic is also got a promotion.Conductive elastomer 110 is formed with ring-shaped as shown in Figure 8, but the present invention is not defined in this situation, as long as can provide elasticity to connection fuselage 310, it can have other various shape.
Figure 10 is the connector assembly 100 being inserted with the conductive rubber 910 of Fig. 6 and the conductive elastomer 1110 of Fig. 8 " ' profile.
Referring to figs. 1 through Figure 10, connector assembly 100 " ' comprise the first connector 200, connecting connector 300, second connector 400, conductive rubber 910 and conductive elastomer 1110.Connector assembly 100 " ' the first connector 200, connecting connector 300 and the second connector 400 and Fig. 1 identical to the first connector 200 illustrated in fig. 4, connecting connector 300 and the second connector 400, the explanation therefore repeated replaces by the explanation relevant to Fig. 1 to Fig. 4.
And, connector assembly 100 " conductive elastomer 1110 of ' conductive rubber 910 and identical with the conductive rubber 910 that Fig. 6 and Fig. 7 illustrates relatively; connector assembly 100 " ' is identical with the conductive elastomer 1110 of Fig. 8 and Fig. 9, and the explanation therefore repeated replaces by the explanation relevant to Fig. 6 to Fig. 9.
second embodiment
Figure 11 is the stereogram of the second embodiment of connector assembly of the present invention, and Figure 12 is another stereogram of the second embodiment of connector assembly of the present invention.
With reference to Figure 11 and Figure 12, connector assembly 101 of the present invention comprises the first connector 500 and connecting connector 300.
Above-mentioned first connector 500 is the structures being fixed on the first object.
Above-mentioned first connector 500 comprises the first fuselage 510, first signal pin 570 and holding wire 512.The first engagement groove 520 is formed in the side of above-mentioned first fuselage 510.Above-mentioned first engagement groove 520 launches ground laterally gradually and is formed.
Above-mentioned first signal pin 570 is inserted in the inside of above-mentioned first fuselage 510, and its end is positioned on above-mentioned first engagement groove 520, and insulate with above-mentioned first fuselage 510.
Above-mentioned holding wire 512 is connected to sidepiece or the bottom of above-mentioned first fuselage 510.Wherein, above-mentioned holding wire 512 is electrically connected with above-mentioned first signal pin 570.Above-mentioned holding wire 512 is the structures such as coaxial cable, and it is formed along the direction with above-mentioned first fuselage 510 form right angle or straight line.
Thus, look on the whole, above-mentioned first fuselage 510 and above-mentioned holding wire 512 form ' L ' or ' I ' shape.
Particularly, according to the first fuselage 510 of the first connector 500 of the second embodiment, the inner peripheral surface that the inner peripheral surface contacted with the outer peripheral face of above-mentioned connection fuselage 310 in the inner peripheral surface of above-mentioned first engagement groove 520 contacts obtains the gradient (grade).
Wherein, be formed with fixture block 515 in the face of reducing (taper) of above-mentioned first engagement groove 520, above-mentioned fixture block 515 protrudes to the inner side of the first engagement groove 520.
In addition, above-mentioned connecting connector 300 comprises: connect fuselage 310, its one end is combined in above-mentioned first engagement groove 520, in order to be electrically connected above-mentioned first fuselage 510; Bonding conductor 370, is inserted in the inside of above-mentioned connection fuselage 310, and above-mentioned first engagement groove 520 contacts with above-mentioned first signal pin 570, in order to be electrically connected above-mentioned first signal pin 570, and insulate with the above-mentioned fuselage 310 that is connected.
Wherein, the formation of above-mentioned connecting connector 300 is identical in fact with the structure be mentioned in the first embodiment, therefore will save in the following description.
Wherein, be formed with the first contact site 315 in the connection fuselage 310 of above-mentioned connecting connector 300, above-mentioned first contact site 315 protrudes from the outer peripheral face of above-mentioned connection fuselage 310 and is formed, and contacts with the inner peripheral surface of above-mentioned first fuselage 510.Further, above-mentioned fixture block 515 protrudes from the inner peripheral surface reduced of the first engagement groove 520 and is formed and above-mentioned first contact site 315 of buckle, is separated with above-mentioned first connector 500 to prevent above-mentioned connection fuselage 310.In addition, be formed in the lower end of above-mentioned first fuselage 510 of above-mentioned first connector 500 and conclude fuselage 511.
Be formed with fixing hole H at the above-mentioned fixed part concluding fuselage 511, above-mentioned fixing hole H is combined with the fixing fixed body B for above-mentioned first object.As embodiment, above-mentioned in fixed part is concluded fuselage 511 liang of end sections and extends, in order to the rivet hole with the fixing of above-mentioned first object and the screw hole that is formed in order to joint bolt or binding rivet.
The sidepiece concluding fuselage 511 above-mentioned or bottom are connected with above-mentioned holding wire 512, make above-mentioned letter, number line 512 and above-mentioned first fuselage 510 form ' L ' or ' I ' shape and form right angle or straight line.
Again in addition, the second connector 400 is also combined with in the upper end of the other end as above-mentioned connection fuselage 310.Above-mentioned second connector 400 is electrically connected with the second object and is fixed.As embodiment, the second connector is substrate.
Wherein, the structure of above-mentioned second connector 400 and with connect be mentioned in the integrated structure of fuselage and the first embodiment identical in fact, therefore indicate identical Reference numeral, and will save in the following description.
Certainly, although not shown, the second engagement groove 420 of above-mentioned second connector 400 can be identically formed with the first engagement groove 520 inner peripheral surface reduced.Further, the fixture block (not shown) protruded from the above-mentioned inner peripheral surface reduced of the second connector 400 can be also formed.
In the first connector 500, by forming the structure of above-mentioned fixture block 515, even if be applied with external force to connection fuselage 310, the first connector 500 also easily can keep the bonding state with the lower end being connected fuselage 310.
For the effect that above-mentioned fixture block 515 plays, be mentioned in the first embodiment identical in fact.
Further, though not shown in Figure 13 to Figure 15, also can be provided with at the first engagement groove 520 inner peripheral surface of the first connector 500 conductive rubber 910 be mentioned in first embodiment.Further, identical with the first embodiment, in the second connector 400, also can be provided with conductive elastomer 1110.
Role is drawn for the setting because of above-mentioned conductive rubber 910 and conductive elastomer 1110, be mentioned in the first embodiment identical in fact.Further, the compensation shown in Figure 14 is misprinted and is arranged and connect the mode of first and second object, to arrange and to be electrically connected the mode of object identical in fact with compensating in Fig. 5 of the first embodiment to misprint.
Above, the specific embodiment relevant to connector assembly of the present invention is illustrated, but in the limit not exceeding scope of the present invention, multiple enforcement distortion can be realized.Therefore, scope of the present invention is not defined in described embodiment, but should limit by appending claims and with the scope of this claims equalization.
Namely, should be understood to aforesaid embodiment go up in all respects be all illustrate instead of limit, scope of the present invention describes in detail compared to it, to be limited by appending claims, the implication of these claims and scope, and from impartial all changes of concept derivation or the form of distortion are all covered by scope of the present invention with it.
Claims (17)
1. a connector assembly, is characterized in that, comprising:
First connector, it is electrically connected with the first object, and described first connector comprises:
First fuselage, it is formed with the first engagement groove in side;
First signal pin, it is inserted in the inside of described first fuselage, and end is positioned on described first engagement groove, and insulate with described first fuselage; And,
Connecting connector, it comprises:
Connect fuselage, its one end is combined in described first engagement groove, in order to be electrically connected described first fuselage;
Bonding conductor, is inserted in the inside of described connection fuselage, and described first engagement groove contacts with described first signal pin, in order to be electrically connected described first signal pin, and insulate with the described fuselage that is connected;
Wherein, in described first fuselage, the diameter of the inner peripheral surface contacted with the outer peripheral face of described connection fuselage in the inner peripheral surface of described first engagement groove is inserted into described first connector direction at described connection fuselage reduces gradually and obtains the gradient,
When described connection fuselage is inserted into described first connector, to be connected side that fuselage inserts to apply pressure in the opposite direction and after reaching maximum compression with described, when removing described pressure, the inner peripheral surface of described first engagement groove reduced provides elastic force to the outer peripheral face of described connection fuselage, and described connection fuselage is connected the side that fuselage inserts moves in the opposite direction towards with described.
2. a connector assembly, is characterized in that, comprising:
First connector, it is electrically connected with the first object, and described first connector comprises:
First fuselage, it is formed with the first engagement groove in side;
First signal pin, it is inserted in the inside of described first fuselage, and end is positioned on described first engagement groove, and insulate with described first fuselage;
Holding wire, it, at described first fuselage form right angle or straight line, is electrically connected with described first signal pin; And,
Connecting connector, it comprises:
Connect fuselage, one end is combined in described first engagement groove, in order to be electrically connected described first fuselage;
Bonding conductor, is inserted in the inside of described connection fuselage, and described first engagement groove contacts with described first signal pin, in order to be electrically connected described first signal pin, and insulate with the described fuselage that is connected;
Wherein, in described first fuselage, the diameter of the inner peripheral surface contacted with the outer peripheral face of described connection fuselage in the inner peripheral surface of described first engagement groove is inserted into described first connector direction at described connection fuselage reduces gradually and obtains the gradient,
When described connection fuselage is inserted into described first connector, to be connected side that fuselage inserts to apply pressure in the opposite direction and after reaching maximum compression with described, when removing described pressure, the inner peripheral surface of described first engagement groove reduced provides elastic force to the outer peripheral face of described connection fuselage, and described connection fuselage is connected the side that fuselage inserts moves in the opposite direction towards with described.
3. connector assembly according to claim 1 and 2, is characterized in that,
Be formed with the first contact site in described connection fuselage, described first contact site protrudes from outer peripheral face and is formed, and contacts with the inner peripheral surface of described first fuselage;
Be formed with fixture block in described first fuselage, described fixture block protrudes from inner peripheral surface and is formed, and in order to the first contact site described in buckle, is separated with described first connector to prevent described connection fuselage.
4. connector assembly according to claim 1 and 2, is characterized in that,
The second connector is connected with at the other end of described connection fuselage,
Described second connector is electrically connected with the second object, and it comprises:
Second fuselage, it is formed with the second engagement groove in side; And,
Secondary signal pin, it is inserted in the inside of described second fuselage, and its end is positioned on described second engagement groove, and insulate with described second fuselage;
The other end of described connection fuselage is combined in described second engagement groove, in order to be electrically connected described second fuselage,
Described bonding conductor contacts with described secondary signal pin on described second engagement groove, in order to be electrically connected described secondary signal pin.
5. connector assembly according to claim 4, is characterized in that, is formed with the second contact site in described connection fuselage, and described second contact site protrudes from the outer peripheral face of described connection fuselage and formed, and contacts with the inner peripheral surface of described second fuselage.
6. connector assembly according to claim 5, is characterized in that, the outer peripheral face of described second contact site is formed with circular shape.
7. connector assembly according to claim 4, is characterized in that,
Described first connector also comprises the first insulator, described first insulator is combined between described first fuselage and described first signal pin, in order to described first signal pin be electrically connected with the holding wire of described first object and described first fuselage be electrically connected with the earth connection of described first object of insulating;
Described second connector also comprises the second insulator, described second insulator is combined between described second fuselage and described secondary signal pin, in order to the described secondary signal pin be electrically connected with the holding wire of described second object and described second fuselage be electrically connected with the earth connection of described second object of insulating;
Described connecting connector also comprises connection insulator, and described connection insulator is combined between described connection fuselage and described bonding conductor, in order to described connection fuselage and the described bonding conductor of insulating.
8. connector assembly according to claim 4, it is characterized in that, described bonding conductor is formed with link slot at two ends, in the described link slot that an end is formed, insert described first signal pin to be electrically connected, in the described link slot that another end is formed, insert described secondary signal pin to be electrically connected;
The conglobate spherical state of part structure that described first signal pin and described secondary signal pin are electrically connected with described bonding conductor, and protrude formation from outer peripheral face.
9. connector assembly according to claim 1 and 2, is characterized in that, is formed with at least one groove in described connection fuselage, and at least one groove described is formed from end to third side to through inner peripheral surface and outer peripheral face.
10. connector assembly according to claim 4, is characterized in that, described connector assembly also comprises:
Conductive elastomer, is inserted in described second engagement groove, and when pressurizeing described connection fuselage to described second connector direction from described first connector, described conductive elastomer is in order to provide elasticity to described connection fuselage.
11. connector assemblies according to claim 10, is characterized in that, described conductive elastomer is ring-type, in order to provide elasticity between the end and described second fuselage of described connection fuselage.
12. connector assemblies according to claim 1 and 2, is characterized in that, described connector assembly also comprises:
At least one conductive rubber, at least one conductive rubber described is inserted in the outer peripheral face of described connection fuselage, in order to mask the RF signal of leakage.
13. connector assemblies according to claim 4, is characterized in that, described connector assembly also comprises:
First conductive rubber, between the outer peripheral face of its inner peripheral surface at described first engagement groove and described connection fuselage, in order to mask the RF signal of leakage; And,
Second conductive rubber, between the outer peripheral face of its inner peripheral surface at described second engagement groove and described connection fuselage, in order to mask the RF signal of leakage.
14. connector assemblies according to claim 4, is characterized in that, described connector assembly also comprises:
Conductive elastomer, it is inserted in described second engagement groove, when pressurizeing described connection fuselage to described second connector direction from described first connector, in order to provide elasticity to described connection fuselage; And,
At least one conductive rubber, it is inserted in the outer peripheral face of described connection fuselage, in order to mask the RF signal of leakage.
15. connector assemblies according to claim 1, is characterized in that, be formed conclude fuselage in the lower end of described first fuselage of described first connector,
Be formed with the screw hole of joint bolt at described both ends of concluding fuselage, or be formed with the rivet hole of binding rivet, fixing for described first object.
16. connector assemblies according to claim 2, is characterized in that, be formed conclude fuselage in the lower end of described first fuselage of described first connector,
Be formed with the screw hole of joint bolt at described both ends of concluding fuselage, or be formed with the rivet hole of binding rivet, fixing for described first object.
17. connector assemblies according to claim 16, it is characterized in that, described holding wire is connected with at the described sidepiece concluding fuselage, ' L ' shape and form right angle is formed to make described holding wire and described first fuselage, or be connected with described holding wire in described bottom of concluding fuselage, form ' I ' shape to make described holding wire and described first fuselage and formed straight line.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR20120035475 | 2012-04-05 | ||
| KR10-2012-0035475 | 2012-04-05 | ||
| KR1020130015771A KR101311724B1 (en) | 2012-04-05 | 2013-02-14 | Connector assembly |
| KR10-2013-0015771 | 2013-02-14 |
Publications (2)
| Publication Number | Publication Date |
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| CN103367979A CN103367979A (en) | 2013-10-23 |
| CN103367979B true CN103367979B (en) | 2016-02-17 |
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| CN201310120080.XA Active CN103367979B (en) | 2012-04-05 | 2013-04-08 | Connector assembly |
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Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102015100452A1 (en) * | 2015-01-14 | 2016-07-14 | Phoenix Contact E-Mobility Gmbh | Connector part with a compensation device |
| KR102163379B1 (en) * | 2019-12-27 | 2020-10-08 | 주식회사 기가레인 | Board mating connector |
| JP2022030015A (en) * | 2020-08-06 | 2022-02-18 | 株式会社オートネットワーク技術研究所 | Connector device |
| JP7417200B2 (en) | 2020-08-06 | 2024-01-18 | 株式会社オートネットワーク技術研究所 | connector device |
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| CN1685567A (en) * | 2002-08-22 | 2005-10-19 | 康宁吉伯股份有限公司 | High frequency, blind mate, coaxial interconnect |
| CN201369450Y (en) * | 2009-03-10 | 2009-12-23 | 镇江通达电子有限公司 | Coaxial connector capable of quickly inserting, pulling and self-locking |
| CN201450195U (en) * | 2009-08-04 | 2010-05-05 | 西安富士达科技股份有限公司 | Radiofrequency coaxial connector suitable for blind mating and floating connection |
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| CN202127117U (en) * | 2011-06-11 | 2012-01-25 | 安费诺凯杰科技(深圳)有限公司 | Radio-frequency connector capable of calibrating positions |
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| CN1685567A (en) * | 2002-08-22 | 2005-10-19 | 康宁吉伯股份有限公司 | High frequency, blind mate, coaxial interconnect |
| CN201369450Y (en) * | 2009-03-10 | 2009-12-23 | 镇江通达电子有限公司 | Coaxial connector capable of quickly inserting, pulling and self-locking |
| CN201450195U (en) * | 2009-08-04 | 2010-05-05 | 西安富士达科技股份有限公司 | Radiofrequency coaxial connector suitable for blind mating and floating connection |
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