CN109239858A - A kind of optical fiber collimator docking style single optical rotary joint and installation method - Google Patents

A kind of optical fiber collimator docking style single optical rotary joint and installation method Download PDF

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Publication number
CN109239858A
CN109239858A CN201811435850.9A CN201811435850A CN109239858A CN 109239858 A CN109239858 A CN 109239858A CN 201811435850 A CN201811435850 A CN 201811435850A CN 109239858 A CN109239858 A CN 109239858A
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CN
China
Prior art keywords
optical fiber
fiber collimator
rotor
bearing
rotary joint
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Granted
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CN201811435850.9A
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CN109239858B (en
Inventor
王芳
钱路
胡志涛
梁礼晔
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Shanghai Transmission Line Research Institute (china Electronic Technology Group Corp Twenty-Third Institute)
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Shanghai Transmission Line Research Institute (china Electronic Technology Group Corp Twenty-Third Institute)
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Priority to CN201811435850.9A priority Critical patent/CN109239858B/en
Publication of CN109239858A publication Critical patent/CN109239858A/en
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    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/38Mechanical coupling means having fibre to fibre mating means
    • G02B6/3807Dismountable connectors, i.e. comprising plugs
    • G02B6/381Dismountable connectors, i.e. comprising plugs of the ferrule type, e.g. fibre ends embedded in ferrules, connecting a pair of fibres
    • G02B6/3818Dismountable connectors, i.e. comprising plugs of the ferrule type, e.g. fibre ends embedded in ferrules, connecting a pair of fibres of a low-reflection-loss type
    • G02B6/3821Dismountable connectors, i.e. comprising plugs of the ferrule type, e.g. fibre ends embedded in ferrules, connecting a pair of fibres of a low-reflection-loss type with axial spring biasing or loading means
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/26Optical coupling means
    • G02B6/34Optical coupling means utilising prism or grating
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/38Mechanical coupling means having fibre to fibre mating means
    • G02B6/3807Dismountable connectors, i.e. comprising plugs
    • G02B6/3833Details of mounting fibres in ferrules; Assembly methods; Manufacture
    • G02B6/3834Means for centering or aligning the light guide within the ferrule

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Optical Couplings Of Light Guides (AREA)

Abstract

The invention discloses a kind of optical fiber collimator docking style single optical rotary joint and installation methods, the optical fiber collimator docking style single optical rotary joint includes turning end optical fiber collimator, stationary end optical fiber collimator, rotor, bearing assembly, stationary end installation lid and installation shell, the bearing assembly includes first bearing, second bearing and end ring, it is characterized in that, the bearing assembly is fixed between the rotor and the installation shell, and the elastic element is located between the bearing and the installation shell;The present invention can compress bearing, reduce axial gap, promote stability of device when by temperature change, vibratory impulse, installation method of the present invention solves the problems, such as such optical rotary joint, and there are angles and location error between rotation axis during the installation process, and can fast and effeciently be installed collimation device.

Description

A kind of optical fiber collimator docking style single optical rotary joint and installation method
Technical field
The invention belongs to technical field of optical fiber communication, and in particular to one kind is for relative rotation equipment in optical fiber telecommunications system Between optical signal transmission optical fiber collimator docking style single optical rotary joint and its installation method.
Background technique
Fiber optic communication makes it be used widely because of many merits such as its enormous bandwidth, common-path interference and minor losses. It needs to carry out fiber optic communication between the equipment mutually rotated at two in certain applications, such as marine towing fiber optic communication hawser Between lash ship, between vehicle and radar antenna between fire balloon and earth station etc..These application scenarios require light rotation Connector.The stationary parts and rotary part of optical rotary joint are individually fixed between the equipment that two mutually rotate, it can To realize the fiber optic communication between two equipment.
Common single optical rotary joint is aligned by the optical fiber collimator of two relative rotation, or passes through two naked light It is fine directly to dock.The optical rotary joint directly docked using bare fibre, at docking unavoidably there is because off-axis aberrations, Angular deviation and axial deviation and caused by power loss, cause since the core diameter of Standard single-mode fiber is smaller to these errors It is very sensitive, biggish fiber optic communication power loss therefore also is caused, is brought very to designing and manufacturing for optical rotary joint Big difficulty.Structure is complicated for the optical rotary joint of bare fibre Direct-type, and very high to part processing precision requirement, thus seldom It is used.United States Patent (USP) US23300281A proposes a kind of optical rotary joint of optical fiber collimator docking style, although can drop It is low that part processing precision is required, but the gap between bearing will cause the variation in collimator orientation, to cause to rotate The insertion loss variation of device in journey is bigger.
In addition, optical fiber collimator alignment of the common single optical rotary joint by two relative rotation, multi-core optical rotation Turning connector generally uses the optical path of mechanical axis of rotation as benchmark.In the manufacturing process of this optical rotary joint, need The orientation of optical fiber collimator is adjusted, so that turn of the central axis of optical fiber collimator output beam and optical rotary joint Moving axis is overlapped, this is a relatively difficult and complicated process.Common method has speckle analysis method and gradually proof method.
Speckle analysis method uses CCD monitoring device, and monitoring is mounted on the hair of the collimator of optical rotary joint centre bore Position and the angle parameter for penetrating hot spot, are then calculated according to related algorithm, and the angles and positions parameter of collimator is adjusted;Most After carrying out confirming performance using CCD monitoring device and stationary end collimator eventually, the collimator of round end is permanently fixed, this side Method needs to carry out expensive CCD monitoring device investment, and carries out the algorithm research of matched fixture exploitation and various products.
Gradually proof method step 1: first collimator is temporarily fixed in rotary shaft by mechanical precision with readily removable glue It in heart hole, is exchanged in the collimator of stationary end collimator and rotation, by the loss of the 360 degree rotation of the two collimators Variation is adjusted to minimum, and the general first step is adjustable to 10dB or so;Step 2: the collimator of rotation is removed and clears up glue Water, then loss is adjusted to minimum by turning end collimator on the basis of the collimator of stationary end, it is general to require to be less than 0.5dB, It is fixed in the centre bore of rotary shaft with readily removable glue again, at this time again by the Dissipation change tune of the 360 degree rotation of two collimators It is whole to arrive minimum, generally it is adjustable to 3dB or so;Step 3: repeating second step multipass, the Dissipation change of 360 degree rotation is adjusted To the required value of product, generally 0.5dB, while maximum insertion is less than the required value of product, generally 1.5dB.Gradually Proof method needs to expend a large amount of manpower and time, and fabrication cycle is long, does not have rapid throughput.
Therefore optical rotary joint needs a kind of low cost, quickly and effectively adjustment optical fiber collimator and mechanical rotary shaft same The method of axis.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of optical fiber collimator docking style single optical rotary joint, energy It is enough to solve the unstable situation of the device caused by optical rotary joint bearing clearance, and a kind of optical fiber collimator and mechanical is provided The installation method of concentric rotation axis, solving such optical rotary joint, there are angles between collimator and rotation axis during the installation process The problem of degree and location error.
The present invention is to solve above-mentioned technical problem and the technical solution adopted is that be achieved:
A kind of optical fiber collimator docking style single optical rotary joint, including turning end optical fiber collimator 1, stationary end optical fiber Collimator 2, rotor 3, bearing assembly and installation shell 7, the bearing assembly are located between rotor 3 and installation shell 7, feature Be: the bearing assembly includes first bearing 41, second bearing 42 and end ring 43, the first bearing 41 and the second axis 42 bearing outer rings are held with installation 7 interference connection of shell and bearing inner race is connect with 3 interference of rotor;The side of the bearing assembly is set It is equipped with for compressing bearing face and eliminating the elastic element 5 of bearing clearance.
Further, the elastic element 5 is the waveform spring being arranged between installation shell 7 and the side of bearing assembly Or butterfly spring.
Further, the optical fiber collimator docking style single optical rotary joint further includes being fixed in installation shell 7 Stationary end lid 6 is installed, the turning end optical fiber collimator 1 is fixed in the centre bore of the rotor 3, the stationary end optical fiber Collimator 2 is fixed in the centre bore of the stationary end installation lid 6.
Further, the end ring 43 is between first bearing 41 and second bearing 42;The stationary end installation Lid 6 is located at 42 left side of second bearing, and with installation shell 7 by being threadedly engaged;It is right that the elastic element 5 is located at first bearing 41 Side.
Further, the optical fiber collimator docking style single optical rotary joint includes auxiliary device 8, the auxiliary dress Setting 8 includes a sensing unit bracket and at least two fastening screws, and the sensing unit bracket is hollow cylindrical structure, Center is provided with mounting hole and is used for setting angle light beam sensing unit 811 or position light beam sensing unit 812, sets around centre bore There are at least two screw holes matched with the mounting screw hole site of 3 end face of rotor, the fastening screw is threaded through screw hole In for sensing unit bracket to be fixed on 3 end face of rotor with one heart.
Further, the angle light beam sensing unit (811) is plated film light transmission glass plate or rhombic prism.
A kind of optical fiber collimator docking style single optical rotary joint installation method, it is characterised in that:
The optical fiber collimator docking style single optical rotary joint is structure described in claim 1;The installation method Are as follows: turning end optical fiber collimator 1 and stationary end optical fiber collimator 2 are aligned using micropositioning stage first, other component is assembled into It is placed in after connector assembly on the micropositioning stage between two collimators, makes the light beam being emitted through turning end optical fiber collimator 1 through even It is received after connecing 3 centre bore of rotor of device assembly by stationary end optical fiber collimator 2.
Further, the micropositioning stage is auxiliary device 8, and auxiliary device 8 includes a sensing unit bracket and multiple tight Gu screw, the sensing unit bracket is hollow cylindrical structure, and center is provided with mounting hole for setting angle light beam sensitivity Unit 811 or position light beam sensing unit 812, are equipped with around centre bore and the mounting screw hole site of 3 end face of rotor matches Several screw holes closed, the fastening screw are threaded through in screw hole for sensing unit bracket to be fixed on rotor with one heart 3 end faces, the specific steps are as follows:
Step S1: angle light beam sensing unit 811 is fixed on 3 central hole of rotor using auxiliary device 8, rotates rotor 3, adjust connector assembly between two collimators so that rotor 3 during rotation when, through turning end optical fiber collimator The light beam of 1 outgoing is not changed after 3 centre bore of rotor by the optical power that stationary end optical fiber collimator 2 receives, then beam optical axis Just parallel with the rotation axis of the rotor 3;
Step S2: auxiliary device 8 is reused the angle light beam in 812 replacement step S1 of position light beam sensing unit is sensitive Unit 811 is fixed on 3 central hole of rotor, rotates rotor 3, adjusts the connector assembly between two collimators, so that turning Son 3 during rotation when, the light beam being emitted through turning end optical fiber collimator 1 is quasi- by stationary end optical fiber after 3 centre bore of rotor The optical power that straight device 2 receives does not change, then beam optical axis just rotation overlapping of axles with the rotor 3;
Step S3: the position light beam sensing unit 812 on auxiliary device 8 and auxiliary device 8 is removed, by the turning end light Fine collimator 1 is moved in the center mounting hole of rotor 3 and is fixed, and the stationary end optical fiber collimator 2 is moved to stationary end It installs in the center mounting hole of lid 5 and fixed completion is installed.
The present invention compare the prior art have it is following the utility model has the advantages that
The present invention uses novel fiber rotation connector structure, and elastic element is arranged in bearing assembly side, can press Mandrel is held, and reduces the gap between Bearing inner ball and bearing internal external circle, is also just reduced entire rotation simultaneously in this way and is connected Connect the axial gap inside device;Fiber rotation connector is in temperature change, vibratory impulse etc., due to expanding with heat and contract with cold for each part The gap that will lead between axial each part constantly changes, and fiber rotation connector may be made to rotate and have some setbacks or be inserted into Loss becomes larger, but due to the presence of elastic element, can continue the axial gap inside when holding rotary connector assembles, mention The high environmental stability of fiber rotation connector performance;Since elastic element can keep pressure certain in a big way In the range of, the machining accuracy of each part axial size can also be reduced in this way, reduce the cost of product.
In installation method of the present invention, eliminated respectively by angle light beam sensing element and position light beam sensing element Problem is judged in rotation when optical fiber collimator is mounted in rotary shaft by accident, is solved such optical rotary joint and is collimated during the installation process There are problems that angle and location error between device and rotation axis, has the characteristics that relative to spot method inexpensive, easy-operating;Phase For gradually proof method, skill, working hour can be greatly lowered.
The assistant apparatus structure used is simple, is easy to adjust, low cost.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of optical fiber collimator docking style single optical rotary joint of the present invention;
Fig. 2 is single optical rotary joint collimator scheme of installation provided by the present invention;
Fig. 3 is auxiliary device schematic diagram provided by the present invention;
Fig. 4 is the schematic illustration of angle light beam sensing element (rhombic prism) of the present invention;
Fig. 5 is the schematic illustration of angle light beam sensing element (plated film light transmission glass plate) of the present invention;
Fig. 6 is the schematic illustration of light beam sensing element in position of the present invention.
In figure:
1: turning end optical fiber collimator 2: stationary end optical fiber collimator 3: rotor
41: first bearing 42: second bearing 43: end ring
5: elastic element 6: stationary end installs lid 7: installation shell
8: auxiliary device 81: light beam sensing unit 811: angle light beam sensing unit
812: position light beam sensing unit 82: stationary plane 83: mounting hole
84: light hole
Specific embodiment
The invention will be further described with reference to the accompanying drawings and examples.
Fig. 1 is the structural schematic diagram of optical fiber collimator docking style single optical rotary joint of the present invention, as shown, including Turning end optical fiber collimator 1, stationary end optical fiber collimator 2, rotor 3, bearing assembly and installation shell 7, bearing assembly, which is located at, to be turned Between son 3 and installation shell 7, bearing outer ring is connect with installation 7 interference of shell, and bearing inner race is connect with 3 interference of rotor, in bearing The side of component uses elastic element 5.Elastic element 5 and two bearings are concentric, contact on one side with 41 outer ring of first bearing, another Side is contacted with installation shell 7;Elastic element 5 be arranged in installation shell 7 and the side of bearing assembly between waveform spring or Person's butterfly spring;Elastic part is compressed to suitable force value when installation, the inner ring of bearing and outer ring are respectively to two sides at this time To movement, the gap between the ball between inner ring and outer ring is eliminated, optical path is more stable when making to rotate.Optical fiber collimator docking Type single optical rotary joint further includes the stationary end installation lid 6 being fixed in installation shell 7, and turning end optical fiber collimator 1 is solid It is scheduled in the centre bore of rotor 3, stationary end optical fiber collimator 2 is fixed in the centre bore of stationary end installation lid 6.Bearing assembly packet Include first bearing 41, second bearing 42 and end ring 43;End ring 43 is between first bearing 41 and second bearing 42; Stationary end installation lid 6 is located at 42 left side of second bearing, and with installation shell 7 by being threadedly engaged;Elastic element 5 is located at first axle Hold 41 right sides.
Fig. 2 is optical rotary joint collimator scheme of installation provided by the present invention, and installation method is as follows:
The first step adjusts the connector assembly position on micropositioning stage, so that the light beam emitted through turning end optical fiber collimator 1 Optical axis is parallel with the rotation axis of rotor 3, the specific steps are as follows:
Using auxiliary device 8 (such as Fig. 3), mounting hole 83 is connect with rotor 3 with screw, by angle light beam sensing unit 811 (the present embodiment is rhombic prism or plated film light transmission glass plate, sees Fig. 4, Fig. 5) are fixed on stationary plane 82, and are melted by heat Glue or other glue easy to clean are fixed, angle light beam sensing unit 811, light hole 84,3 centre bore three of rotor of auxiliary device 8 Person is generally within same center.Adjust connector assembly between two collimators so that rotor 3 during rotation when, The optical power that the light beam being emitted through turning end optical fiber collimator 1 is received after 3 centre bore of rotor by stationary end optical fiber collimator 2 Do not change, then beam optical axis is just parallel with the rotation axis of the rotor 3;
Second step then adjusts the connector assembly position on micropositioning stage, so that emit through turning end optical fiber collimator 1 The rotation overlapping of axles of beam optical axis and the rotor 3, the specific steps are as follows:
Auxiliary device 8 is reused by the angle light beam sensing unit 811 in 812 replacement step S1 of position light beam sensing unit (the present embodiment is that Zhejiang becomes transmitance plate glass, sees Fig. 6) is fixed on 3 center of rotor by hot melt adhesive or other glue easy to clean At hole, rotate rotor 3, adjust connector assembly positioned at two collimators between so that rotor 3 during rotation when, through turn The optical power that the light beam that moved end optical fiber collimator 1 is emitted is received after 3 centre bore of rotor by stationary end optical fiber collimator 2 is constant Change, then beam optical axis just with the rotation overlapping of axles of rotor 3;
Third step removes the position light beam sensing unit 812 on auxiliary device 8 and auxiliary device, and turning end optical fiber is quasi- Straight device 1 is moved in the center mounting hole of rotor 3 and is fixed, and stationary end optical fiber collimator 2 is moved to stationary end installation lid 5 In center mounting hole and fixed completion is installed.
Fig. 4 is 811 schematic illustration of angular-sensitive unit provided by the present invention, and angular-sensitive unit 811 can be one Kind prism, left and right end face is parallel, and when light beam is after prism, the optical axis of beam propagation has a translation D.Incident beam with The angle of prism is different, and the translation distance D of optical axis also can be different.
Fig. 5 is another 811 schematic illustration of angular-sensitive unit provided by the present invention, angular-sensitive unit 811 It can be a kind of surface coating light transmission glass plate, the plated film of glass plate makes the transmitance of glass plate quick to the incident angle of light beam Sense, incident beam is different from the angle of glass plate, also different eventually by the power of glass plate.
Fig. 6 is 812 schematic illustration of position light beam sensing unit provided by the present invention.Position light beam sensing unit 812 It is a kind of light transmission glass plate, in the plated film or printing gradient pattern of glass plate, so that the light beam passed through from glass plate different location Loss is different.The optical power that final optical fiber collimator receives will change.
The present invention uses novel fiber rotation connector structure, due to the presence of elastic element, can continue to keep rotation Turn the axial gap inside connector device timing, improves the environmental stability of fiber rotation connector performance;Due to elastic member Part can keep in a big way pressure in a certain range, can also reduce the processing essence of each part axial size in this way Degree, reduces the cost of product.
In installation method of the present invention, eliminated respectively by angle light beam sensing element and position light beam sensing element Problem is judged in rotation when optical fiber collimator is mounted in rotary shaft by accident, is solved such optical rotary joint and is collimated during the installation process There are problems that angle and location error between device and rotation axis.The assistant apparatus structure that uses is simple, be easy to adjust, it is low at This.
Although the present invention is disclosed as above with preferred embodiment, however, it is not to limit the invention, any this field skill Art personnel, without departing from the spirit and scope of the present invention, when can make a little modification and perfect therefore of the invention protection model It encloses to work as and subject to the definition of the claims.

Claims (8)

1. a kind of optical fiber collimator docking style single optical rotary joint, including turning end optical fiber collimator (1), stationary end optical fiber Collimator (2), rotor (3), bearing assembly and installation shell (7), the bearing assembly are located at rotor (3) and installation shell (7) Between, it is characterised in that: the bearing assembly includes first bearing (41), second bearing (42) and end ring (43), described First bearing (41) and second bearing (42) bearing outer ring and installation shell (7) interference connection and bearing inner race and rotor (3) mistake It is full of connection;The side of the bearing assembly is provided with for compressing bearing face and eliminating the elastic element (5) of bearing clearance.
2. a kind of optical fiber collimator docking style single optical rotary joint as described in claim 1, it is characterised in that: the elasticity Element (5) is waveform spring or butterfly spring of the setting between installation shell (7) and the side of bearing assembly.
3. a kind of optical fiber collimator docking style single optical rotary joint as claimed in claim 1 or 2, it is characterised in that: described Optical fiber collimator docking style single optical rotary joint further includes the stationary end installation lid (6) being fixed in installation shell (7), institute It states turning end optical fiber collimator (1) to be fixed in the centre bore of the rotor (3), the stationary end optical fiber collimator (2) is fixed In the centre bore that the stationary end installs lid (6).
4. a kind of optical fiber collimator docking style single optical rotary joint as claimed in claim 3, it is characterised in that: the axis Retaining ring (43) is held to be located between first bearing (41) and second bearing (42);The stationary end installation lid (6) is located at second bearing (42) left side, and with installation shell (7) by being threadedly engaged;The elastic element (5) is located on the right side of first bearing (41).
5. a kind of optical fiber collimator docking style single optical rotary joint as claimed in claim 4, it is characterised in that: the light Fine collimator docking style single optical rotary joint includes auxiliary device (8), and the auxiliary device (8) includes a sensing unit Bracket and at least two fastening screws, the sensing unit bracket are hollow cylindrical structure, and center is provided with mounting hole and is used for Setting angle light beam sensing unit (811) or position light beam sensing unit (812), are equipped with around centre bore and rotor (3) are held At least two screw holes that the mounting screw hole site in face matches, the fastening screw are threaded through in screw hole for will be sensitive Unit rack is fixed on rotor (3) end face with one heart.
6. a kind of optical fiber collimator docking style single optical rotary joint as claimed in claim 5, it is characterised in that: the angle Spending light beam sensing unit (811) is plated film light transmission glass plate or rhombic prism.
7. a kind of optical fiber collimator docking style single optical rotary joint installation method, it is characterised in that:
The optical fiber collimator docking style single optical rotary joint is structure described in claim 1;The installation method are as follows: first First turning end optical fiber collimator (1) and stationary end optical fiber collimator (2) are aligned using micropositioning stage, other component is assembled into company It is placed on the micropositioning stage between two collimators after connecing device assembly, makes the light beam being emitted through turning end optical fiber collimator (1) through even It is received after connecing rotor (3) centre bore of device assembly by stationary end optical fiber collimator (2).
8. a kind of optical fiber collimator docking style single optical rotary joint installation method as claimed in claim 7, it is characterised in that: The micropositioning stage is auxiliary device (8) structure described in claim 5, the specific steps are as follows:
Step S1: angle light beam sensing unit (811) is fixed on rotor (3) central hole using auxiliary device (8), rotation turns Sub (3) adjust the connector assembly between two collimators so that rotor (3) during rotation when, through turning end optical fiber The optical power that the light beam of collimator (1) outgoing is received after rotor (3) centre bore by stationary end optical fiber collimator (2) is constant Change, then beam optical axis is just parallel with the rotation axis of the rotor (3);
Step S2: auxiliary device (8) is reused the angle light beam in position light beam sensing unit (812) replacement step S1 is sensitive Unit (811) is fixed on rotor (3) central hole, rotates rotor (3), adjusts the connector assembly between two collimators, So that rotor (3) during rotation when, through turning end optical fiber collimator (1) outgoing light beam after rotor (3) centre bore quilt The optical power that stationary end optical fiber collimator (2) receives does not change, then the beam optical axis just rotation axis weight with the rotor (3) It closes;
Step S3: the position light beam sensing unit (812) on auxiliary device (8) and auxiliary device (8) is removed, by the turning end Optical fiber collimator (1) is moved in the center mounting hole of rotor (3) and is fixed, and the stationary end optical fiber collimator (2) is translated It installs in the center mounting hole of lid (5) and fixes to stationary end and complete installation.
CN201811435850.9A 2018-11-28 2018-11-28 Optical fiber collimator butt joint type single-core optical rotary connector and installation method Active CN109239858B (en)

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CN109239858B CN109239858B (en) 2024-04-05

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110939515A (en) * 2019-11-29 2020-03-31 西安航天动力研究所 Method for expanding axial force adjusting capability of rotor shaft system
CN115097574A (en) * 2022-06-10 2022-09-23 中航光电科技股份有限公司 Optical fiber rotary connector
CN109239858B (en) * 2018-11-28 2024-04-05 上海传输线研究所(中国电子科技集团公司第二十三研究所) Optical fiber collimator butt joint type single-core optical rotary connector and installation method

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JP2005070710A (en) * 2003-08-28 2005-03-17 Hitachi Maxell Ltd Optical attenuator
US6904223B1 (en) * 2003-04-04 2005-06-07 Optiworks, Inc. Tilted-translation variable optical attenuator
US20090263085A1 (en) * 2006-10-20 2009-10-22 Bornmann Volker Device for injecting light into an optical wave guide
CN207796977U (en) * 2016-08-26 2018-08-31 翠达有限公司 Lamp decoration

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Publication number Priority date Publication date Assignee Title
CN109239858B (en) * 2018-11-28 2024-04-05 上海传输线研究所(中国电子科技集团公司第二十三研究所) Optical fiber collimator butt joint type single-core optical rotary connector and installation method

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6904223B1 (en) * 2003-04-04 2005-06-07 Optiworks, Inc. Tilted-translation variable optical attenuator
JP2005070710A (en) * 2003-08-28 2005-03-17 Hitachi Maxell Ltd Optical attenuator
US20090263085A1 (en) * 2006-10-20 2009-10-22 Bornmann Volker Device for injecting light into an optical wave guide
CN207796977U (en) * 2016-08-26 2018-08-31 翠达有限公司 Lamp decoration

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109239858B (en) * 2018-11-28 2024-04-05 上海传输线研究所(中国电子科技集团公司第二十三研究所) Optical fiber collimator butt joint type single-core optical rotary connector and installation method
CN110939515A (en) * 2019-11-29 2020-03-31 西安航天动力研究所 Method for expanding axial force adjusting capability of rotor shaft system
CN115097574A (en) * 2022-06-10 2022-09-23 中航光电科技股份有限公司 Optical fiber rotary connector
CN115097574B (en) * 2022-06-10 2023-11-14 中航光电科技股份有限公司 Optical fiber rotary connector

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