CN101950055B - Optical fiber connector - Google Patents

Optical fiber connector Download PDF

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Publication number
CN101950055B
CN101950055B CN2010102783277A CN201010278327A CN101950055B CN 101950055 B CN101950055 B CN 101950055B CN 2010102783277 A CN2010102783277 A CN 2010102783277A CN 201010278327 A CN201010278327 A CN 201010278327A CN 101950055 B CN101950055 B CN 101950055B
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China
Prior art keywords
thrust unit
contact pin
hole
rear end
guide
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Application number
CN2010102783277A
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Chinese (zh)
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CN101950055A (en
Inventor
黄澄
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China Aviation Optical Electrical Technology Co Ltd
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China Aviation Optical Electrical Technology Co Ltd
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Application filed by China Aviation Optical Electrical Technology Co Ltd filed Critical China Aviation Optical Electrical Technology Co Ltd
Priority to CN2010102783277A priority Critical patent/CN101950055B/en
Publication of CN101950055A publication Critical patent/CN101950055A/en
Application granted granted Critical
Publication of CN101950055B publication Critical patent/CN101950055B/en
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Abstract

The invention discloses an optical fiber connector. The rear end of a contact pin locating seat integrally extends backwards to be provided with two guide posts which are symmetrically arranged at both sides of a cable passage, each guide hole is internally provided with a spring which abuts between the corresponding pushing end surfaces of the rear end of the guide post and the rear end of the guide hole when in thrust, a long hole extending from front to back is arranged around either guide post, a limit part penetrating through the long hole is extended and arranged in the guide hole of a thrust device along the radial direction of the guide hole, and hole walls at the front end and the rear end of the long hole are pushed and blocked by the limit part when the hole walls move to the position of the limit part. The contact pin locating seat and the thrust device which are arranged front and back in the invention are glidingly matched front and back through the guide posts and the guide holes correspondingly spliced in between and stop gliding match through hook parts on the guide posts and the long holes on the thrust device, and the springs abutting on the guide posts and the thrust device elastically stop the connection between the locating seat and the thrust device in the fore-and-after direction.

Description

The joints of optical fibre
Technical field
The present invention relates to the joints of optical fibre.
Background technology
Existing one type of joints of optical fibre that the multi-core optical fiber contact pins body with optical fiber ribbon cable and flat pattern is used; Generally comprise the contact pin positioning seat and the pushing in device that is used for the staff push operation that is arranged at contact pin positioning seat back that are fixed on the optical fiber contact pins tail end through the location pilot pin; The normal employing is connected or integrative-structure is realized being connected of contact pin positioning seat rear end and pushing in device front end in existing this type of fibre-optic connector structure, can't realize the elastic compression of contact pin front end face when grafting.
Summary of the invention
The object of the present invention is to provide a kind of simple in structure, joints of optical fibre that the contact pin positioning seat is connected with pushing in device elasticity.
Technical scheme of the present invention is: a kind of joints of optical fibre; Comprise by the contact pin body, contact pin positioning seat, the thrust unit that are used to be connected the optical cable end that set gradually behind the forward direction; Be respectively equipped with in contact pin positioning seat, the thrust unit and connect the cable passage that confession optical cable both front/rear ends, that mutual correspondence communicates wears; The rear end one of contact pin positioning seat extends back and is provided with two guide pillars that are symmetricly set in the both sides, cable passage; The front end correspondence of thrust unit is provided with two pilot holes; The rearward end of said each guide pillar is slided and is inserted in the corresponding pilot hole, and the spring between the corresponding pushing tow end face that top when being used to receive thrust is assigned in guide pillar rear end and pilot hole rear end is housed in each pilot hole; Said guide pillar side face offers the slotted hole that extends from front to back; Be provided with the limiting section that is threaded onto in the said slotted hole along radially extending of pilot hole in the pilot hole of said thrust unit, the hole wall of slotted hole rear and front end is limited pushing tow block when moving to said limiting section position.
Said limiting section is the pin that radially inserts said pilot hole, and said pin is threaded onto in the slotted hole on the guide pillar that gets in the corresponding pilot hole simultaneously.
Said slotted hole connects the side face of the relative both sides of guide pillar.
Elasticity is fixed with symmetrically arranged two locking keys that are used for the spacing cooperation of adaptive jack buckle on the outside surface of the relative both sides of said thrust unit; Each locking key front end is connected on the thrust unit; Rear end elasticity backward is suspended in thrust unit outside surface top; The outside, the rear end of locking key is provided with and refers to touch convexity, and the outside, middle part of locking key is provided with and is used for the hangnail that the spacing recess with adaptive jack is clasped.
The outside surface of said thrust unit front end is provided with and places the said locking key feather key along the fore-and-aft direction extension before.
Said contact pin body, contact pin positioning seat, thrust unit are the bluff body of the height dimension in cross section greater than width dimensions, and said guide pillar, pilot hole are arranged near the edge part on the height dimension direction of contact pin positioning seat, thrust unit.
Contact pin positioning seat that front and back of the present invention are provided with and pushing in device are through corresponding guide pillar of pegging graft and pilot hole are slidingly matched before and after realizing between the two; And the limiting section through corresponding setting on the slotted hole on the guide pillar and the pushing in device and anti-avulsion is slidingly matched; And the top is furnished with spring and has realized that the flexible anti-avulsion on the fore-and-aft direction between positioning seat and the pushing in device is connected between guide pillar and pushing in device, thereby the contact pin positioning seat that satisfies the joints of optical fibre can and be linked to be the demand of integral body simultaneously with respect to the pushing in device elastic floating.
Description of drawings
Fig. 1 is the structural representation of embodiments of the invention;
Fig. 2 is the vertical view of Fig. 1;
Fig. 3 is the cut-open view of embodiments of the invention;
Fig. 4 is the schematic perspective view of embodiments of the invention.
Embodiment
Like Fig. 1~shown in Figure 4; The joints of optical fibre of the present invention comprise contact pin body 1, contact pin positioning seat 2, the thrust unit 3 that is connected the end of adaptive optical cable by being used to of setting gradually behind the forward direction; Contact pin body 1, contact pin positioning seat 2, thrust unit 3 are the bluff body of the height dimension in cross section greater than width dimensions; Be respectively equipped with in contact pin positioning seat 2, the thrust unit 3 and connect the cable passage 9 that confession optical cable both front/rear ends, that mutual correspondence communicates wears; Contact pin body 1 rear end is fixed on the front end of contact pin positioning seat 2 through the location pilot pin 6 of its both sides, ribbon fiber 4 insert and insert from the cable inlet of thrust unit 3 tail ends wear thrust unit 3, contact pin positioning seat 2 is connected with contact pin body 1.Elasticity is fixed with symmetrically arranged two locking keys that extend back 7 on the outside surface of thrust unit 3 relative both sides.
The rear end one of contact pin positioning seat 2 extends back and is provided with two guide pillars 21 that are symmetricly set in the both sides, cable passage; The front end correspondence of thrust unit 3 is provided with two pilot holes 31; The rearward end of described two guide pillars 21 is slided and is inserted in each corresponding pilot hole 31; The middle part of guide pillar 21 offers the slotted hole 22 of perforation guide pillar 21 relative two lateral circle surfaces that extend from front to back; Be fixed with the radially slotting pin 33 of wearing said pilot hole 31 on the said thrust unit 3 along pilot hole; Said pin 33 is threaded onto in the slotted hole 22 on the guide pillar 21 that gets in the corresponding pilot hole 31 simultaneously, the hole wall of the slotted hole 22 rear and front ends 33 pushing tow blocks of when moving to pin 33 positions, being pinned.In each pilot hole 31 spring 5 is housed, spring 5 is the flexible volute spring of fore-and-aft direction, and said guide pillar 21 rear end faces cooperate with spring 5 front end pushing tows, and the rear end of spring 5 cooperates with pushing tow end face 32 pushing tows that pilot hole 31 rear ends are provided with.
Because contact pin positioning seat 2 is bigger with the size of thrust unit 3 on short transverse, said guide pillar 21 and corresponding pilot hole 31 are arranged near near the edge of the dual-side on the height dimension direction of contact pin positioning seat, thrust unit.When the joints of optical fibre use, spring 5 can with contact pin positioning seat 2 and thrust unit 3 to be separated from each other forward, towards the rear to backing down, realize that contact pin positioning seat 2 is connected with the elasticity of thrust unit 3 on fore-and-aft direction.And the block between the pin of the slotted hole on the guide pillar and thrust unit cooperates and can guarantee that contact pin positioning seat 2 can not arbitrarily come off from thrust unit 3.
Be provided with two pin mounting grooves 23 on the outside surface of contact pin positioning seat 2 front ends one side side by side; Be provided with the axial limiting bayonet socket that cooperates with the eel-like figure axle journal of locating pilot pin 6 afterbodys in the pin mounting groove 23; Make location pilot pin 6 afterbodys pack in the pin mounting groove 23 and axially by locked, the head of location pilot pin 6 is plugged on the pin-and-hole corresponding on the contact pin body 1 after the front end face of contact pin positioning seat 2 passes.
Thrust unit 3 middle parts on the outside surface of the relative both sides on the short transverse respectively elasticity be fixed with the locking key 7 that is used for the spacing cooperation of adaptive jack buckle; Each locking key 7 front end is connected on the thrust unit 3; Locking key 7 rear ends elasticity backward are suspended in thrust unit 3 outside surfaces top; The outside, the rear end of locking key 7 is provided with the finger that has band and touches protrudingly 71, and the outside, middle part of locking key 7 is provided with and is used for the hangnail 72 that the spacing recess with adaptive jack is clasped.Thrust unit 3 front end outside surfaces are provided with and place said one of them locking key 7 feather key 8 along the fore-and-aft direction extension before.
Be used for and the spacing limiting section that cooperates of the slotted hole of guide pillar that is provided with in the pilot hole in the foregoing description is pin; Certainly in other embodiments limiting section also can adopt structures such as the hangnail that radially is convexly set on the pilot hole inwall, projection, and the slotted hole of guide pillar can be contained on the limiting section with strong dress mode or elasticity fashion of extrusion.

Claims (6)

1. joints of optical fibre; Comprise by the contact pin body, contact pin positioning seat, the thrust unit that are used to be connected the optical cable end that set gradually behind the forward direction; Be respectively equipped with in contact pin positioning seat, the thrust unit and connect the cable passage that confession optical cable both front/rear ends, that mutual correspondence communicates wears; It is characterized in that: the rear end one of contact pin positioning seat extends back and is provided with two guide pillars that are symmetricly set in the both sides, cable passage; The front end correspondence of thrust unit is provided with two pilot holes; The rearward end of said each guide pillar is slided and is inserted in the corresponding pilot hole, and the spring between the corresponding pushing tow end face that top when being used to receive thrust is assigned in guide pillar rear end and pilot hole rear end is housed in each pilot hole; Said guide pillar side face offers the slotted hole that extends from front to back; Be provided with the limiting section that is threaded onto in the said slotted hole along radially extending of pilot hole in the pilot hole of said thrust unit, the hole wall of slotted hole rear and front end is limited pushing tow block when moving to said limiting section position.
2. the joints of optical fibre according to claim 1 is characterized in that: said limiting section is the pin that radially inserts said pilot hole, and said pin is threaded onto in the slotted hole on the guide pillar that gets in the corresponding pilot hole simultaneously.
3. the joints of optical fibre according to claim 2 is characterized in that: said slotted hole connects the side face of the relative both sides of guide pillar.
4. the joints of optical fibre according to claim 1; It is characterized in that: elasticity is fixed with symmetrically arranged two locking keys that are used for the spacing cooperation of adaptive jack buckle on the outside surface of the relative both sides of said thrust unit; Each locking key front end is connected on the thrust unit; Rear end elasticity backward is suspended in thrust unit outside surface top, and the outside, rear end of locking key is provided with and refers to touch convexity, and the outside, middle part of locking key is provided with and is used for the hangnail that the spacing recess with adaptive jack is clasped.
5. the joints of optical fibre according to claim 4 is characterized in that: the outside surface of said thrust unit front end is provided with and places the said locking key feather key along the fore-and-aft direction extension before.
6. according to any described joints of optical fibre in the claim 1~5; It is characterized in that: said contact pin body, contact pin positioning seat, thrust unit are the bluff body of the height dimension in cross section greater than width dimensions, and said guide pillar, pilot hole are arranged near the edge part on the height dimension direction of contact pin positioning seat, thrust unit.
CN2010102783277A 2010-09-10 2010-09-10 Optical fiber connector Active CN101950055B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010102783277A CN101950055B (en) 2010-09-10 2010-09-10 Optical fiber connector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010102783277A CN101950055B (en) 2010-09-10 2010-09-10 Optical fiber connector

Publications (2)

Publication Number Publication Date
CN101950055A CN101950055A (en) 2011-01-19
CN101950055B true CN101950055B (en) 2012-02-29

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104216060A (en) * 2013-07-05 2014-12-17 中航光电科技股份有限公司 MT (mechanical transfer) contact and optical connector with same
CN113189711B (en) * 2021-04-20 2023-03-24 武汉光迅科技股份有限公司 Small MPO type optical fiber connector

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3066739B2 (en) * 1996-07-15 2000-07-17 セイコーインスツルメンツ株式会社 General-purpose optical connector and basic plug
US6287018B1 (en) * 1999-07-28 2001-09-11 Lucent Technologies Inc. Tunable optical fiber connector
CN201804139U (en) * 2010-09-10 2011-04-20 中航光电科技股份有限公司 Optical fiber connector

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