Summary of the invention
The technical matters that the present invention solves is the deficiency that overcomes prior art, and a kind of passive phase compensation structure of full optical fiber interferometer with high stable level and preparation method thereof is provided.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is following:
The passive phase compensation structure of a kind of full optical fiber interferometer; Comprise that inside offers the foamed rubber-plastic heat insulation material body of annular groove; Accommodate the fiber optic interferometric ring in the said annular groove, external unlined aluminium foil paper layer, the first composite ceramic adiabatic coating layer, a DOK polyester glass medium flaggy, special polyurethane high molecule sound-absorbing insulation material layer, the 2nd DOK polyester glass medium flaggy, the second composite ceramic adiabatic coating layer, heat-insulating material layer, foamed rubber-plastic heat insulation material layer and the outer foil ply of paper of being enclosed with successively of said foamed rubber-plastic heat insulation material; The optical fiber that is used to be connected to the external signal input and output on the said full optical fiber interferometer passes from layers of material.The bipeltate that foamed rubber-plastic heat insulation material body among the present invention and foamed rubber-plastic heat insulation material layer are adopted; Be the nitrile rubber with excellent performance, PVC is a primary raw material, through banburying; Special process such as sulfur foam are processed, and have good thermal insulation, insulation effect.The aluminium foil ply of paper has characteristics such as light reflectivity height, airtight, waterproof, good seal performance and heat reflectivity height, thereby possesses thermal radiation resistant, heat-blocking action.Composite ceramic adiabatic coating layer has the adiabatic heat-insulation effect.DOK polyester glass medium flaggy can completely cut off the infrared ray up to 90%; Have fast light, water-fast, moisture-proof, characteristic such as high temperature resistant; Play the effect of sealing, thermal insulation and support structure, as the media that depends on of special polyurethane high molecule sound-absorbing insulation material layer and composite ceramic adiabatic coating layer.Special polyurethane high molecule sound-absorbing insulation material layer plays deadening, and sound transmission loss is up to 42dB.Composite ceramic adiabatic coating layer plays thermal insulation, insulation effect.The present invention has adopted the good macromolecule sound-proof material of multiple coefficient of heat conductivity very low special thermal insulation, insulation material and sound insulation value; And adopted multi-layer sealed technology to handle; Be sealed in the inside one deck to the full optical fiber interference ring of required protection; By the lining toward various heat-insulating materials of sealed package in layer and sound insulation, radiation proof material; Thereby greatly reduce to place innermost fiber optic interferometric ring because of external environment condition changes suffered influence, reached a passive phase compensation level of high stable.
The fiber optic interferometric ring that full optical fiber interferometer is turned to ring-type can improve the integrated level of structure, but must be too severe if optical fiber is crooked, and its loss meeting becomes very big; And around crossing the final size that conference increases structure; Therefore under the prerequisite that guarantees enough integrated levels, that tries one's best encompasses one than circlet, through the experiment proof; Preferred sizes does; Internal diameter>=the 9cm of said fiber optic interferometric ring, external diameter≤20cm, the radial width scope 0.1-0.5cm of said fiber optic interferometric ring; The internal diameter of said annular groove is less than the internal diameter of fiber optic interferometric ring, and external diameter is greater than the external diameter of fiber optic interferometric ring.The magnitude relationship of the internal diameter of fiber optic interferometric ring, external diameter and radial width is: (outside dimension) deducts (internal diameter size) and equals (radial width 2 times).
Foamed rubber-plastic heat insulation material layer thickness scope is 0.5-1cm; Wet resistance factor mu>=10000 of said foamed rubber-plastic heat insulation material body and foamed rubber-plastic heat insulation material layer, coefficient of heat conductivity λ≤0.034W/ (mK).
The thickness range of the said first composite ceramic adiabatic coating layer and the second composite ceramic adiabatic coating layer is 0.2-0.4cm, coefficient of heat conductivity≤0.054 W/ (mK).
The thickness range of a said DOK polyester glass medium flaggy and the 2nd DOK polyester glass medium flaggy is 0.3-0.4cm.
The thickness range of unlined aluminium foil paper layer and outer foil ply of paper is 0.03-0.05cm, and light reflectivity and heat reflectivity are all greater than 90%.
The material of said heat-insulating material layer is an aerosil; Aerosil is known as " blue smoke ", " solid cigarette " again; It is present the lightest known solid material; Also be heat-insulating property best material up to now, coefficient of heat conductivity is 0.013-0.025 W/ (mK), and thickness range is 0.5-2cm.And aerosil lightweight, transparent is very good heat-insulating material.Obviously, other the solid, powdery material littler than aerosil coefficient of heat conductivity is applicable to the present invention too.
Said foamed rubber-plastic heat insulation material shape is rectangular parallelepiped, cylinder or spheroid.For effective fixed fiber interference ring, reduce its influence of outer bound pair simultaneously to greatest extent, the space between said annular groove and fiber optic interferometric ring is filled with aerosil, to play the effect of direct more adiabatic heat-insulation, avoids ectocine.Simultaneously because and the space between the annular groove be filled full, also can be effectively shockproof, prevent that the fiber optic interferometric ring from rocking in annular groove.
The method for making of the passive phase compensation structure of above-mentioned full optical fiber interferometer may further comprise the steps:
Step 1 turns to the fiber optic interferometric ring of ring-type with full optical fiber interferometer, and draws the optical fiber that is used to connect the external signal input and output;
Step 2 is made the foamed rubber-plastic heat insulation material body, and within it portion offer with step 1 in fiber optic interferometric annular shape and the annular groove that is complementary, and the fiber optic interferometric ring placed this annular groove;
Step 3 is at the external unlined aluminium foil paper layer that superscribes of said foamed rubber-plastic heat insulation material;
Step 4; On a DOK polyester glass medium flaggy and the 2nd DOK polyester glass medium flaggy apparent surface, apply special polyurethane high molecule sound-absorbing insulation material layer; And respectively be coated with on a DOK polyester glass medium flaggy and the 2nd another surface of DOK polyester glass medium flaggy and be covered with the first composite ceramic adiabatic coating layer and the second composite ceramic adiabatic coating layer; Form composite layer; This composite layer is processed first box body, and formed structure is complementary in the shape of this first box body internal cavity and size and the step 3, the structure in the step 3 is placed in the cavity of this first box body;
Step 5 utilizes the foamed rubber-plastic heat insulation material layer to process second box body, cavity in second box body and the first box body external appearance matching in the step 4, and cavity volume is greater than first box body;
Step 6 places first box body in the cavity of second box body, and in first box body and the second box body space, fills full aerosil formation heat-insulating material layer;
Step 7 is at the second box body outerwrap outer foil ply of paper.
In the said step 2, full aerosil is filled in the space between annular groove and the fiber optic interferometric ring.
Compared with prior art; The beneficial effect of technical scheme of the present invention is: the present invention has adopted the good macromolecule sound-proof material of multiple coefficient of heat conductivity very low special thermal insulation, insulation material and sound insulation value; And adopted multi-layer sealed technology to handle; Be sealed in the inside one deck to the full optical fiber interference ring of required protection; By the lining toward various heat-insulating materials of sealed package in layer and sound insulation, radiation proof material, thereby greatly reduce to place innermost fiber optic interferometric ring because of the suffered influence of external environment condition variation, reached a passive phase compensation level of high stable.And simultaneously, experimental data also shows, adopts the stability of the full optical fiber interferometer of the passive phase compensation structure of the present invention to obtain very big raising than prior art.
Embodiment
Below in conjunction with accompanying drawing and embodiment technical scheme of the present invention is done further explanation.
Embodiment 1
As depicted in figs. 1 and 2 is the passive phase compensation structural representation of full optical fiber interferometer of the present invention; Make for ease; Be rectangular shape, concrete structure comprises that inside offers the foamed rubber-plastic heat insulation material body 10 of annular groove, accommodates fiber optic interferometric ring 11 in the annular groove.It is bigger slightly than fiber optic interferometric ring that annular groove is done, and the internal diameter of annular groove is less than the internal diameter of fiber optic interferometric ring, and external diameter is greater than the external diameter of fiber optic interferometric ring.The internal diameter of fiber optic interferometric ring 11 is 9cm, and external diameter is 9.2cm, and promptly the radial width of fiber optic interferometric ring is 0.1cm.The internal diameter of annular groove is 8cm, and external diameter is 10cm.Foamed rubber-plastic heat insulation material body 10 is a rectangular parallelepiped, and it is fixed that its size is come according to the fiber optic interferometric ring, is standard with receiving optical fiber interference ring fully.In the present embodiment, for economical with materials to a greater extent, the face of the foamed rubber-plastic heat insulation material body 10 that the anchor ring of fiber optic interferometric ring 11 is corresponding is designed to square, and foamed rubber-plastic heat insulation material body 10 is of a size of 12.6cm*12.6cm*2.6cm in the present embodiment.Outside foamed rubber-plastic heat insulation material body 10, be enclosed with unlined aluminium foil paper layer 9, the first composite ceramic adiabatic coating layer 8, a DOK polyester glass medium flaggy 7, special polyurethane high molecule sound-absorbing insulation material layer 6, the 2nd DOK polyester glass medium flaggy 5, the second composite ceramic adiabatic coating layer 4, heat-insulating material layer 3, foamed rubber-plastic heat insulation material layer 2 and outer foil ply of paper 1 successively.
Two optical fiber A, B being used to be connected to the external signal input and output on the full optical fiber interferometer pass from layers of material, and wherein one is signal input port, and one is signal outlet.
Each layer thickness is following:
Unlined aluminium foil paper layer 9 is 0.05cm with outer foil ply of paper 1 thickness; What adopt is high-performance thermal radiation resistant aluminum foil paper material; Have characteristics such as light reflectivity height, airtight, waterproof, good seal performance, heat reflectivity height, light reflectivity and heat reflectivity are all up to more than 90%;
The first composite ceramic adiabatic coating layer 8 and the second composite ceramic adiabatic coating layer, 4 thickness are 0.3cm, employing be the composite ceramic adiabatic coating of the excellent performance of coefficient of heat conductivity≤0.054W/ (mK).
The thickness of the one DOK polyester glass medium flaggy 7 and the 2nd DOK polyester glass medium flaggy 5 is 0.4cm, and the DOK polyester glass medium sheet material material of this layer employing can completely cut off the infrared ray up to 90%, fast light, water-fast, moisture-proof, high temperature resistant.
Heat-insulating material layer 3 thickness are 1cm, and the material that adopts is an aerosil, and thermal conductivity is minimum in all solids material, and lightweight is transparent, and coefficient of heat conductivity is in 0.013~0.025 W/ (mK) scope.
Foamed rubber-plastic heat insulation material layer 2 thickness are 1cm, and this layer and foamed rubber-plastic heat insulation material body 10 have low-down coefficient of heat conductivity, and coefficient of heat conductivity λ≤0.034W/ (mK) has high wet resistance factor mu>=10000 simultaneously.
For the interferometer of different brachiums, the arm length difference between the dissimilar arm and the stability of interferometer are inversely proportional to, and promptly under the identical situation of other condition, arm length difference is big more, and stability is just poor more.If weigh the stability of interference ring with unit arm length difference phase drift speed, passive phase compensation technology at present both domestic and external, the level of stability that generally can accomplish is: the average of unit arm length difference phase drift speed is about 0.2rad/min.And shown in unit length arm length difference phase change test pattern among Fig. 3; The passive phase compensation structure of present embodiment; The average of unit length arm length difference phase drift speed is 0.06 rad/min, and unit length arm length difference phase drift speed can reach about 0.01 rad/min when more stable.This shows, improved the stability of full optical fiber interferometer than prior art the present invention greatly.
The method for making of the passive phase compensation structure of above-mentioned full optical fiber interferometer may further comprise the steps:
Step 1 turns to the fiber optic interferometric ring 11 of ring-type with full optical fiber interferometer, and draws two optical fiber A, the B that is used to connect the external signal input and output;
Step 2; Make foamed rubber-plastic heat insulation material body 10; And within it portion offer with step 1 in fiber optic interferometric annular shape and the annular groove that is complementary, and the fiber optic interferometric ring placed this annular groove, fill aerosil in the space between annular groove and the fiber optic interferometric ring;
Step 3, unlined aluminium foil paper layer on said foamed rubber-plastic heat insulation material body 10 outerwrap;
Step 4; On a DOK polyester glass medium flaggy 7 and the 2nd DOK polyester glass medium flaggy 5 apparent surfaces, apply special polyurethane high molecule sound-absorbing insulation material layer 6; And respectively be coated with on a DOK polyester glass medium flaggy 7 and the 2nd DOK polyester glass medium flaggy 5 another surfaces and be covered with the first composite ceramic adiabatic coating layer 8 and the second composite ceramic adiabatic coating layer 4; Form composite layer; This composite layer is processed first box body, and formed structure is complementary in the shape of this first box body internal cavity and size and the step 3, the structure in the step 3 is placed in the cavity of this first box body;
Step 5 utilizes foamed rubber-plastic heat insulation material layer 2 to process second box body, cavity in second box body and the first box body external appearance matching in the step 4, and cavity volume is greater than first box body;
Step 6 places first box body in the cavity of second box body, and in first box body and the second box body space, fills full aerosil formation heat-insulating material layer 3;
Step 7 is at the second box body outerwrap outer foil ply of paper 1.
Offering annular groove in the step 2 with the concrete grammar of laying the fiber optic interferometric ring is:
(2.1) become the foamed rubber-plastic material cut foamed rubber-plastic heat insulation material body 10 of the rectangular shape of above-mentioned size;
(2.2) be as the criterion 2/3 place of foamed rubber-plastic heat insulation material body 10 to cut into two halves with height;
(2.3) be cutting out thickness that 2/3 this piece is as the criterion with the center, dig an internal diameter and be 8cm, external diameter and be 10cm, the degree of depth annular groove for half the (first step cut out rectangular parallelepiped thickness 1/3) of this piece thickness; Above-mentioned size can be adjusted according to the size of fiber optic interferometric ring 11, as long as enough spaces that is used for the receiving optical fiber interference ring can be provided.
(2.4) put the fiber optic interferometric ring into annular groove, recharge full aerosil;
(2.5) use " NCC insulation glue " with foamed rubber-plastic material adapted to become original rectangular structure to this two-layer the sticking on that just is cut into two halves.
The concrete steps of making first box body in the step 4 are:
(4.1) coat special polyurethane high molecule sound-absorbing insulation material layer 6 at two blocks of DOK polyester glass medium plates (i.e. a DOK polyester glass medium flaggy 7 and the 2nd DOK polyester glass medium flaggy 5) opposite face; Same method is made six faces; Be glued together with the polyester glass glue then and make a rectangular parallelepiped box; It is earlier bonding without the polyester glass glue to reserve a face, keeps and does lid.
(4.2) be coated in the inside surface and the outside surface of each face of the rectangular parallelepiped of above making with the composite ceramic adiabatic coating; Form the first composite ceramic adiabatic coating layer 8 at inside surface; Outside surface forms the second composite ceramic adiabatic coating layer 4, is made into first box body.This first box body essence plays good sound-insulating effect, can be referred to as " sound-insulating box ".
(4.3) put the structure of the gained of step 3 in " sound-insulating box ", good behind the cover lid with " polyester glass glue " adhesive seal.
Because noise is very big to the influence of fibre optic interferometer, to handle so will do sound insulation, the special polyurethane high molecule sound-absorbing insulation material oise insulation factor in the step 4 has satisfied the sound insulation demand fully up to 42dB.DOK polyester glass medium plate plays the effect of sealing, thermal insulation, support structure, and can let special polyurethane high molecule sound-absorbing insulation material and composite ceramic adiabatic coating be coated in its surface and the very firm bonding effect of formation, difficult drop-off.
In the step 5 be utilize foamed rubber-plastic heat insulation material and with it the NCC insulation glue of adapted make second box body of rectangular shape, it is same that to reserve one side not bonding as lid.
When in the step 6 first box body being placed second box body,, also can in the space of first box body and second box body, fill the foam rubbery material of fritter in order better to process and locate second box body.So that first box body is positioned at the centre of second box body.After aerosil to be filled finishes, cover the lid of first box body of reserving in the step 5, and good with NCC insulation glue adhesive seal.
Embodiment 2
Present embodiment and embodiment 1 are similar, and difference only is that the size of layers of material is different:
The internal diameter of fiber optic interferometric ring 11 is 14cm, the 14.4cm of external diameter, and promptly the radial width of fiber optic interferometric ring is 0.2cm.The internal diameter of annular groove is 13cm, and external diameter is 15cm;
Unlined aluminium foil paper layer 9 is 0.03cm with outer foil ply of paper 1 thickness;
The first composite ceramic adiabatic coating layer 8 and the second composite ceramic adiabatic coating layer, 4 thickness are 0.2cm;
The thickness of the one DOK polyester glass medium flaggy 7 and the 2nd DOK polyester glass medium flaggy 5 is 0.3cm;
Heat-insulating material layer 3 thickness are 0.5cm;
Foamed rubber-plastic heat insulation material layer 2 thickness are 0.5cm.
Embodiment 3
Present embodiment and embodiment 1 are similar, and difference only is that the size of layers of material is different:
The internal diameter of fiber optic interferometric ring 11 is 19cm, the 20cm of external diameter, and promptly the radial width of fiber optic interferometric ring is 0.5cm.The internal diameter of annular groove is 18cm, and external diameter is 21cm;
Unlined aluminium foil paper layer 9 is 0.04cm with outer foil ply of paper 1 thickness;
The first composite ceramic adiabatic coating layer 8 and the second composite ceramic adiabatic coating layer, 4 thickness are 0.4cm;
The thickness of the one DOK polyester glass medium flaggy 7 and the 2nd DOK polyester glass medium flaggy 5 is 0.35cm;
Heat-insulating material layer 3 thickness are 2cm;
Foamed rubber-plastic heat insulation material layer 2 thickness are 0.9cm.
Embodiment 4
Present embodiment and embodiment 3 are similar, and difference only is that the internal diameter of said fiber optic interferometric ring 11 is 19.8cm, and external diameter still is 20cm, and promptly the radial width of fiber optic interferometric ring is 0.1cm.