CN108594399A - Supporting structure and supporting component of large-diameter reflector - Google Patents
Supporting structure and supporting component of large-diameter reflector Download PDFInfo
- Publication number
- CN108594399A CN108594399A CN201810588812.0A CN201810588812A CN108594399A CN 108594399 A CN108594399 A CN 108594399A CN 201810588812 A CN201810588812 A CN 201810588812A CN 108594399 A CN108594399 A CN 108594399A
- Authority
- CN
- China
- Prior art keywords
- nested
- straight slot
- face
- loop connecting
- reflecting mirror
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000003292 glue Substances 0.000 claims description 74
- 230000009975 flexible effect Effects 0.000 claims description 60
- 238000010276 construction Methods 0.000 claims description 32
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 26
- 238000002347 injection Methods 0.000 claims description 15
- 239000007924 injection Substances 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 10
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 claims description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims 1
- 229910052760 oxygen Inorganic materials 0.000 claims 1
- 239000001301 oxygen Substances 0.000 claims 1
- 239000011347 resin Substances 0.000 claims 1
- 229920005989 resin Polymers 0.000 claims 1
- 230000035882 stress Effects 0.000 abstract description 22
- 230000008646 thermal stress Effects 0.000 abstract description 11
- 230000003287 optical effect Effects 0.000 abstract description 2
- 239000007767 bonding agent Substances 0.000 description 8
- 239000000853 adhesive Substances 0.000 description 6
- 230000001070 adhesive effect Effects 0.000 description 6
- 239000012790 adhesive layer Substances 0.000 description 6
- 239000003822 epoxy resin Substances 0.000 description 6
- 229920000647 polyepoxide Polymers 0.000 description 6
- 238000009825 accumulation Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000004026 adhesive bonding Methods 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 239000010426 asphalt Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000005350 fused silica glass Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
- G02B7/183—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors specially adapted for very large mirrors, e.g. for astronomy, or solar concentrators
Landscapes
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Astronomy & Astrophysics (AREA)
- Sustainable Development (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Mounting And Adjusting Of Optical Elements (AREA)
- Endoscopes (AREA)
Abstract
the invention relates to a supporting structure and a supporting assembly of a large-aperture reflector, which relate to the technical field of space optical remote sensors, and solve the problem that the thermal stress of the existing supporting structure influences the surface shape precision of the reflector, and further solve the problem that the bonding stress and the assembly stress influence the surface shape precision of the reflector.
Description
Technical field
The present invention relates to space optical remote sensor technical fields, and in particular to a kind of support construction of large caliber reflecting mirror and
Support component.
Background technology
With the development of earth observation from space technology, increasingly higher demands are proposed to the resolution ratio of Space Remote Sensors.
Core element of the large caliber reflecting mirror as high resolution space remote sensor, surface figure accuracy directly affect Space Remote Sensors
Image quality.To reduce launch cost, high light-weight design usually is carried out to large caliber reflecting mirror, this weakens speculum resistance
The ability of the external environments such as gravity, temperature and erection stress, to influence the surface figure accuracy of speculum.The surface figure accuracy of speculum
There are prodigious relationship, good support construction that can reduce face shape and answer gravity, temperature and assembly with the support construction of speculum
The susceptibility of the extraneous loads such as power, therefore reflecting mirror support structure is designed to ensure the important link of surface figure accuracy.
The widely used support construction as described in Figure 1 of support of large caliber reflecting mirror, including nesting 101, nesting 101 it is outer
Anchor ring A is bonding with speculum endoporus progress gross area;It further include the flexible support bar being connected by screw with speculum backboard
102, flexible support bar 102 is connect by screw with nesting 101, the soft slot 103 of L-type is provided on flexible support bar 102, for releasing
Put the thermal stress and erection stress that external mirror unit installing board is brought.
Above-mentioned support construction has a defect that:
1, it is thermal stress caused by weakening temperature loading, nested 101 use the iron-nickel alloy that linear expansion coefficient is adjusted, with
Reflecting mirror material linear expansion coefficient is matched, and the compatibility of deformation of Mirror blank materials, nested material and bonding agent three is reached.However
Under wide temperature case (such as range of temperature is more than ± 5 DEG C) or the smaller ULE of linear expansion coefficient is applied to (close to zero
Expansion) and when crystallite mirror body, the deformation of mirror body, nesting and bonding agent three is difficult to coordinate, to generate larger thermal stress, band
Carry out the problem of face shape stability difference.Meanwhile glue-line contraction will produce tensile stress when curable adhesive layer, will be respectively acting on nested and anti-
Mirror is penetrated, 101 rigidity of nesting is larger, and non-deformability is strong, to easily lead to speculum bonding region minute surface deformation of cylindrical.
2, Nian Jie with primary mirror hole annulus gross area in the faces the A gluing of nesting 101, combination interface connection is in blocks, lack of homogeneity,
It is also easy to produce local starved or glue accumulation in root is overflowed, larger local stress is generated at glue accumulation, is unfavorable for speculum acquisition
High surface figure accuracy.
3, when being deformed caused by unloading carrying force, the soft slot of L-type by its square crossing is limited flexible support bar 102, is only capable of
More single deformation is generated, therefore the erection stress that a part of external mirror unit installing board is brought can be remained, this is to small
The influence of type speculum is smaller, but surface figure accuracy is required for high large caliber reflecting mirror, then will produce obvious face
Shape error.
Drawbacks described above is all the surface figure accuracy due to influencing speculum in support construction there are stress, reduces speculum
The stability of face shape, to influence the image quality of Space Remote Sensors.
Invention content
The present invention provides a kind of support construction of large caliber reflecting mirror, to solve thermal stress present in existing support construction
The problem of influencing reflecting mirror surface shape precision, adhesive stress and erection stress are further also solved to reflecting mirror surface shape precision shadow
Loud problem is realized and is supported to the low stress high stability of large caliber reflecting mirror.
Technical solution of the invention is:A kind of support construction of large caliber reflecting mirror, including nested and supporting flexible are cut with scissors,
The nesting outer wall is connected with mirror hole, and one end of the supporting flexible hinge is fixedly connected with the nesting, supporting flexible hinge
The other end is fixedly connected with external mirror unit installing board, is characterized in that, described nested including nested ontology, nested
Be evenly distributed the radians equal in widths such as N sections on the end face of ontology and run through nested groove in the axial direction, wherein N be more than or equal to
2 natural number.Thermal stress present in support construction can effectively be eliminated using the above-mentioned arcuate furrow being evenly distributed.
Further, the distance between groove and nested outer wall are less than the distance between nested inner wall, groove with it is embedding
It is flexible thin sheet between set outer wall.The flexible thin sheet can reduce the local stiffness of support construction, and further release temperature changes
Mirror body when larger, the nested deformation with bonding agent three be difficult to coordinate and the thermal stress and curable adhesive layer that generate are shunk and generation
Stress.
In order to eliminate adhesive stress, nested ontology uses small area bonding way with mirror hole, specifically, in nesting
Several hole for injecting glue are arranged in outer wall, i.e.,:It opens up and several equidistantly arranges to what nested body central direction was recessed along trench wall
Keyway, the keyway is circumferentially arranged along nested ontology, and axially penetrates through nested ontology;It is provided on the lateral surface of nested ontology and key
Several hole for injecting glue that slot vertically communicates.
Further, N is equal to 3, and the radian of the groove is 90 °, and each section of groove opens up that there are four keys along its inner wall
Slot, each section of groove correspond to 2 × 4 injecting glue hole array, each keyway corresponds to two hole for injecting glue.
Further, the gap between the nested ontology and speculum is less than or equal to 0.02mm, after ensureing injecting glue
Glue-line is evenly distributed, it is ensured that bonding is reliable.
Further, the nesting further includes being arranged in the loop connecting face of nested end face;The supporting flexible is cut with scissors
Loop connecting pedestal, support tube and m flexible leg, wherein m are the natural number more than or equal to 3;Loop connecting pedestal with it is nested
Loop connecting face match and connect with nested encryptions face by screw;M flexible leg is set along the radial direction of loop connecting pedestal
It sets, and the circumferencial direction along loop connecting pedestal end face is uniformly distributed, one end of the flexible leg is fixed on loop connecting bottom
On the end face of seat, the other end of the flexible leg and the cylinder lateral wall of support tube are fixed;
There are one " L " type straight slot, several longitudinal straight slots being mutually parallel, " L " type straight slot to erect for setting on each flexible leg
To partial-length with longitudinal straight slot equal length and less than the height along support tube axial direction of flexible leg, " L " type straight slot erects
The end face parallel with longitudinal straight slot and being each perpendicular to loop connecting pedestal to part;The longitudinal direction straight slot includes first longitudinal direction straight slot
With second longitudinal direction straight slot, first longitudinal direction straight slot is down-set along the top of flexible leg, and second longitudinal direction straight slot is along flexible leg
Bottom end is set up;" L " type straight slot is located at the surface of the end face of loop connecting pedestal, the vertical section of " L " the type straight slot
It is contour with second longitudinal direction straight slot.
Further, m is uniformly distributed equal to circumferencial direction of 3,3 flexible legs along loop connecting pedestal end face.
Further, the material of the nesting is iron-nickel alloy;The material of the supporting flexible hinge is TC17.
Further, nested ontology is Nian Jie with speculum endoporus by epoxide-resin glue.
The present invention also provides a kind of support component of large caliber reflecting mirror, including above-mentioned support construction, further include from it is different
The auxiliary injecting glue of the corresponding different length of hole for injecting glue of position height is followed closely, and the auxiliary injecting glue nail offers " L " type glue injection channel;
The outlet end diameter of glue injection channel is equal with injecting glue bore dia.By above-mentioned auxiliary hole for injecting glue be convenient for through hole for injecting glue to nesting with it is anti-
Injecting glue in the gap of mirror is penetrated, and remaining binders can be sheared, to effectively eliminate adhesive stress.
Compared with prior art, the beneficial effects of the invention are as follows:
1, groove is set in nesting, the distance between groove and nested outer wall are less than the distance between nested inner wall,
It is flexible thin sheet between groove and nested outer wall, groove and flexible thin sheet reduce the local stiffness of support construction, be released effectively
The thermal stress and curable adhesive layer that mirror body, the nested deformation with bonding agent three are difficult to coordinate and generate when temperature change is larger are shunk
And the stress generated, it realizes and the low stress high stability of large caliber reflecting mirror is supported.
2, the hole for injecting glue of array distribution is arranged in the support construction on flexible thin sheet, by assisting injecting glue nail to be noted through hole for injecting glue
Penetrate bonding agent, solve existing for traditional gluing mode bonded areas connection in flakes, glue amount is unable to control, glue-line is unevenly distributed
The problems such as even, bonding agent residual and bonding agent overflow, avoids influence of the bonding agent residual stress to reflecting mirror surface shape.
3, the end face of the supporting flexible hinge upper edge loop connecting pedestal of support construction is evenly distributed with multigroup flexible leg, provides along anti-
Mirror axial direction, radial and other any directions flexibility are penetrated, the thermal stress of external mirror unit installing board introducing can be fully discharged
And erection stress, it ensure that the surface figure accuracy of speculum.
Description of the drawings
Fig. 1 is the schematic diagram of the flexible support structure of existing large caliber reflecting mirror;
Fig. 2 is the sectional view of the large caliber reflecting mirror support construction of the present invention;
Fig. 3 is structural schematic diagram nested in support construction of the present invention;
Fig. 4 is that the auxiliary injecting glue nail of the present invention is inserted into the sectional view after keyway;
Fig. 5 is that the auxiliary injecting glue nail of the present invention removes the structural schematic diagram of remaining binders;
Fig. 6 is nested lateral surface expansion design sketch after the completion of injecting glue of the present invention;
Fig. 7 is the structure chart that supporting flexible is cut with scissors in support construction of the present invention;
Fig. 8 is the sectional view that supporting flexible is cut with scissors in support construction of the present invention;
Reference numeral is in figure:101- is nested;102- flexible support bars;The soft slot of 103-L types;1- speculums;2- supporting flexibles
Hinge;3- screws;4- is nested;5- epoxide-resin glues;The 6- conical surfaces;7- flexible thin sheets;8- grooves;9- keyways;10- hole for injecting glue;11- is rigid
Property linkage section;12- assists injecting glue nail;13- glue injection channels;The outlet end of 14- glue injection channels;The gap of 15- nestings and speculum;
16- gum spots;17- redundant adhesives;18- assists injecting glue to follow closely lateral surface;19- flanges;20- loop connectings face;21- loop connectings bottom
Seat;22- support tubes;23- flexible legs;24- first longitudinal direction straight slots;25- second longitudinal direction straight slots;26- " L " type straight slot.
Specific implementation mode
Below in conjunction with attached drawing, invention is further described in detail.
Figure it is seen that the support construction of the present invention includes nesting 4 and supporting flexible hinge 2, nested 4 outer walls and speculum
Mirror hole is connected, and one end of supporting flexible hinge 2 is connect by screw 3 with nesting 4, and the other end passes through the flange 19 on top and external reflection
Mirror assembly mounting plate connects;1 material of speculum is super-low expansion fused silica (ULE), and the material of nesting 4 is used to be expanded with ULE lines
The iron-nickel alloy of coefficients match, speculum 1 are Nian Jie with nesting 4 by epoxide-resin glue 5;The material of supporting flexible hinge 2 is TC17.Dress
Timing, speculum 1 are buckled to, and nesting 4 vertically is put into mirror hole, by the metal wire of a diameter of 0.02mm ensure it is nested and
Gap between mirror hole is 0.02mm, it is ensured that glue-line is evenly distributed after injecting glue, and bonding is reliable.
From figure 3, it can be seen that nesting 4 includes nested ontology and is arranged in the loop connecting face 20 of nested end face, nesting is originally
The lateral surface of body is the conical surface 6 compatible with mirror hole, and be evenly distributed three sections on the end face of nesting 4 runs through in the axial direction
The groove 8 (also referred to as slot) of the equal radians equal in width of nesting 4, the distance between groove 8 and nested 4 outer wall less than with it is embedding
Cover the distance between 4 inner walls so that the flexible thin sheet 7 of the radians such as outside formation of groove 8.By flexible thin sheet 7 and groove 8,
The rigidity for reducing nesting 4, because nesting 4, epoxide-resin glue 5 and the deformation of 1 three of speculum are difficult to when release temperature changes greatly
Coordinate and generates thermal stress and curable adhesive layer contraction and the stress of generation;Three sections of grooves 8 are not connected, to ensure that nesting 4 retains
Certain rigidity.
The radian of flexible thin sheet 7 and groove 8 is 90 °, and 2 × 4 injecting glue hole array is provided on flexible thin sheet;Along groove
8 inner walls open up four keyways 9 equidistantly arranged being recessed to nested body central direction, and four keyways 9 are along nested ontology week
To arrangement, and nested ontology is axially penetrated through, hole for injecting glue 10 is vertical with keyway 9 to be communicated, and each keyway in the present embodiment corresponds to two
A hole for injecting glue 10.
From fig. 4, it can be seen that the support component of the present invention includes support construction and auxiliary injecting glue nail 12, auxiliary injecting glue nail 12
Offer " L " type glue injection channel 13;14 diameter of outlet end of glue injection channel is equal with 10 diameter of hole for injecting glue.The auxiliary of different length
The hole for injecting glue of the corresponding different location height of injecting glue nail.The auxiliary injecting glue nail of two groups of different lengths is set in the present embodiment, is led to respectively
The hole for injecting glue for crossing corresponding position height inwardly carries out injecting glue.
When injecting glue, auxiliary injecting glue nail 12 is inserted into keyway 9, syringe passes through 13 inside injecting glue of glue injection channel, asphalt mixtures modified by epoxy resin
Fat glue enters after the outlet end of glue injection channel 14 flows into hole for injecting glue 10 in the gap 15 between nested and speculum, passes through control
Injection pressure and injecting glue amount make glue-line be in discrete gum spot formal distribution, the gum spot 16 of fixed diameter are formed after curable adhesive layer, such as Fig. 6
It is shown.The discrete gum spot of fixed diameter makes to use small area bonding way between nested ontology and mirror hole, avoid viscous
The problem of region connection is in blocks and glue-line is unevenly distributed is connect, to eliminate adhesive stress, while ensureing bonding quality,.
When it is implemented, the relationship between 16 diameter of gum spot and injection pressure and injecting glue amount, is tested by multiple injection and is marked
Fixed, epoxide-resin glue 5 uses black glue, so gum spot size is easy to measure.
As shown in figure 5, after the completion of injecting glue, curable adhesive layer is waited for for a period of time, extract auxiliary injecting glue nail 12, at this time glue injection channel
13 and glue injection channel outlet end 14 accumulate redundant adhesive 17 will by auxiliary injecting glue follow closely 12 lateral surface 18 cut off, to
Reduce the local stress that glue accumulation generates more than injecting glue hole site.
Can be seen that supporting flexible hinge 2 from Fig. 7 and Fig. 8 includes loop connecting pedestal 21, support tube 22 and three flexible legs
23, loop connecting pedestal 21 is matched with nested loop connecting face 20 and is connect with loop connecting face 20 by screw;Three soft
Property supporting leg 23 along loop connecting pedestal 21 radial direction setting, and it is uniformly distributed along the circumferencial direction of 21 end face of loop connecting pedestal, it is flexible
One end of supporting leg 23 is fixed on loop connecting pedestal 21, and the other end of flexible leg 23 is solid with the cylinder lateral wall of support tube 22
It is fixed.Flexible leg 23, loop connecting pedestal 21 and support tube 22 are integrated setting in the present embodiment.
There are one " L " type straight slot 26, the first longitudinal direction straight slot 24 being mutually parallel and second longitudinal directions for setting on each flexible leg
Straight slot 25, the vertical section length of " L " type straight slot 26 and the equal length of first longitudinal direction straight slot 24 and second longitudinal direction straight slot 25 and
Less than flexible leg along the height of support tube axial direction;
First longitudinal direction straight slot 24 is down-set along the top of flexible leg 23, and second longitudinal direction straight slot 25 is along flexible leg 23
Bottom end is set up;" L " type straight slot 26 is located at the surface of the end face of loop connecting pedestal 21, the vertical section of " L " type straight slot
It is contour with second longitudinal direction straight slot;Herein, top with bottom end is described relative to direction shown in Fig. 7, when the direction of figure becomes
When change, top is with bottom end also with the direction change of figure.
In the case of by ambient temperature load or there are build-up tolerance, the lateral part of " L " type straight slot 26 is speculum
Flexibility in an axial direction is provided, vertical section, first longitudinal direction straight slot 24 and the second longitudinal direction straight slot 25 of " L " type straight slot 26 are speculum
Flexibility radially is provided, three groups of soft legs are mutually coordinated, can fully discharge in external mirror unit installing board assembling process
The thermal stress and erection stress of introducing.
Claims (10)
1. a kind of support construction of large caliber reflecting mirror, including nested (4) cut with scissors (2) with supporting flexible, nesting (4) outer wall with it is anti-
Mirror mirror hole is penetrated to be connected, one end of supporting flexible hinge (2) is fixedly connected with nested (4), supporting flexible cut with scissors (2) the other end and
External mirror unit installing board is fixedly connected, it is characterised in that:The nesting (4) includes nested ontology, the end of nested ontology
It is evenly distributed the radians equal in widths such as N sections on face and runs through the groove (8) of nested (4) in the axial direction, wherein N is more than or equal to 2
Natural number.
2. a kind of support construction of large caliber reflecting mirror according to claim 1, it is characterised in that:Groove (8) with it is nested
(4) the distance between outer wall is less than the distance between nested (4) inner wall.
3. a kind of support construction of large caliber reflecting mirror according to claim 1, it is characterised in that:Along groove (8) inner wall
Several keyways (9) equidistantly arranged being recessed to nested body central direction are opened up, the keyway (9) is along nested ontology circumferential direction
Arrangement, and axially penetrate through nested ontology;Several hole for injecting glue communicated vertical with keyway (9) are provided on the lateral surface of nested ontology
(10)。
4. a kind of support construction of large caliber reflecting mirror according to claim 3, it is characterised in that:N is equal to 3, the ditch
The radian of slot (8) is 90 °, and each section of groove (8) opens up along its inner wall there are four keyway (9), and each section of groove (8) corresponds to 2 × 4
Injecting glue hole array, each keyway (9) correspond to two hole for injecting glue (10).
5. a kind of support construction of large caliber reflecting mirror according to claim 1, it is characterised in that:Nested ontology and reflection
Gap between mirror (1) is less than or equal to 0.02mm.
6. a kind of support construction of large caliber reflecting mirror according to claim 1, it is characterised in that:The nesting (4) is also
Including the loop connecting face (20) in nested (4) end face is arranged;
The supporting flexible hinge (2) includes loop connecting pedestal (21), support tube (22) and m flexible leg (23), and wherein m is big
In the natural number equal to 3;Loop connecting pedestal (21) matched with the loop connecting face (20) of nested (4) and by screw with it is described
Loop connecting face (20) connects;M flexible leg (23) is arranged along the radial direction of loop connecting pedestal (21), and along loop connecting bottom
The circumferencial direction of seat (21) end face is uniformly distributed, and one end of the flexible leg (23) is fixed on the end of loop connecting pedestal (21)
On face, the cylinder lateral wall of the other end and support tube (22) of the flexible leg (23) is fixed;
There are one " L " type straight slot (26) and several longitudinal straight slots being mutually parallel, " L " type straight slots for setting on each flexible leg (23)
(26) equal length of vertical section length and longitudinal straight slot and less than flexible leg (23) along the height of support tube (22) axial direction
Degree, the vertical section of " L " type straight slot (26) is parallel with longitudinal straight slot and is each perpendicular to the end face of loop connecting pedestal (21);
The longitudinal direction straight slot includes first longitudinal direction straight slot (24) and second longitudinal direction straight slot (25), and first longitudinal direction straight slot (24) is along flexibility
The top of supporting leg (23) is down-set, and second longitudinal direction straight slot (25) is set up along the bottom end of flexible leg (23);
" L " type straight slot is located at the surface of the end face of loop connecting pedestal (21), the vertical section of " L " the type straight slot (26) with
Second longitudinal direction straight slot (25) is contour.
7. a kind of support construction of large caliber reflecting mirror according to claim 6, it is characterised in that:M is equal to 3,3 flexibilities
Circumferencial direction of the supporting leg (23) along loop connecting pedestal (21) end face is uniformly distributed.
8. a kind of support construction of large caliber reflecting mirror according to claim 1~7 any claim, feature exist
In:The material of the nesting (4) is iron-nickel alloy;The material of the supporting flexible hinge (2) is TC17.
9. a kind of support construction of large caliber reflecting mirror according to claim 8, it is characterised in that:Nested ontology passes through ring
Oxygen resin glue (5) is Nian Jie with speculum endoporus.
10. a kind of support component of large caliber reflecting mirror, it is characterised in that:Including any claim in such as claim 3~9
The support construction further includes the auxiliary injecting glue nail of different length corresponding with the hole for injecting glue of different location height (10)
(12), the auxiliary injecting glue nail (12) offers " L " type glue injection channel (13);Outlet end (14) diameter and injecting glue of glue injection channel
Hole (10) diameter is equal.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810588812.0A CN108594399B (en) | 2018-06-08 | 2018-06-08 | Supporting structure and supporting assembly of large-caliber reflector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810588812.0A CN108594399B (en) | 2018-06-08 | 2018-06-08 | Supporting structure and supporting assembly of large-caliber reflector |
Publications (2)
Publication Number | Publication Date |
---|---|
CN108594399A true CN108594399A (en) | 2018-09-28 |
CN108594399B CN108594399B (en) | 2024-05-14 |
Family
ID=63623337
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810588812.0A Active CN108594399B (en) | 2018-06-08 | 2018-06-08 | Supporting structure and supporting assembly of large-caliber reflector |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108594399B (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109765672A (en) * | 2019-02-27 | 2019-05-17 | 中国科学院西安光学精密机械研究所 | The splicing assembly method of reflecting mirror and support |
CN110196476A (en) * | 2019-05-09 | 2019-09-03 | 中国科学院西安光学精密机械研究所 | In one kind/long wave heavy caliber Infrared Lens flexible support structure |
CN110609373A (en) * | 2019-10-11 | 2019-12-24 | 赵智亮 | Micro-stress support adjustable optical lens frame structure and optical lens clamping method |
CN110764219A (en) * | 2019-11-08 | 2020-02-07 | 南昌航空大学 | Reflector bonding structure for reducing thermal stress |
CN111352209A (en) * | 2020-04-07 | 2020-06-30 | 中国科学院长春光学精密机械与物理研究所 | Support structure of large-caliber reflector component of space remote sensor |
CN111650717A (en) * | 2020-05-09 | 2020-09-11 | 中国科学院西安光学精密机械研究所 | Surface-shaped high-stability reflector assembly and assembling method thereof |
CN111929804A (en) * | 2020-08-31 | 2020-11-13 | 长光卫星技术有限公司 | Support structure of large length-width ratio space reflector |
CN112130277A (en) * | 2020-09-28 | 2020-12-25 | 吉林大学 | Flexible supporting structure suitable for space camera reflector |
CN112162380A (en) * | 2020-10-22 | 2021-01-01 | 中国科学院长春光学精密机械与物理研究所 | Flexible supporting structure of medium and small-diameter reflector |
CN112882185A (en) * | 2021-01-22 | 2021-06-01 | 西安应用光学研究所 | Glue joint fixing structure and fixing method suitable for adjustable lens group of reflecting system |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050254111A1 (en) * | 2003-10-20 | 2005-11-17 | Griffith Michael S | Deformable mirror holders |
CN201348670Y (en) * | 2009-01-22 | 2009-11-18 | 中国科学院西安光学精密机械研究所 | Three-point supporting device of large-diameter reflector |
CN101762855A (en) * | 2009-12-30 | 2010-06-30 | 北京空间机电研究所 | Radial multipoint glue joint axial three-point clamping and supporting method of spatial lens |
CN106443959A (en) * | 2016-12-07 | 2017-02-22 | 中国科学院长春光学精密机械与物理研究所 | Split type bi-material flexible mechanism of space-based large-calibre high-facial-contour-precision reflector assembly |
CN106526784A (en) * | 2016-11-30 | 2017-03-22 | 中国科学院长春光学精密机械与物理研究所 | Flexible supporting mechanism for plane mirror |
CN106646816A (en) * | 2017-01-16 | 2017-05-10 | 中国科学院长春光学精密机械与物理研究所 | High-precision bonding fixing device for spatial reflector |
CN107450154A (en) * | 2017-08-15 | 2017-12-08 | 北京空间机电研究所 | The tension and compression modulus modulus of shearing unloading supporting construction of spacing reflection mirror |
CN208270836U (en) * | 2018-06-08 | 2018-12-21 | 中国科学院西安光学精密机械研究所 | Supporting structure and supporting component of large-diameter reflector |
-
2018
- 2018-06-08 CN CN201810588812.0A patent/CN108594399B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050254111A1 (en) * | 2003-10-20 | 2005-11-17 | Griffith Michael S | Deformable mirror holders |
CN201348670Y (en) * | 2009-01-22 | 2009-11-18 | 中国科学院西安光学精密机械研究所 | Three-point supporting device of large-diameter reflector |
CN101762855A (en) * | 2009-12-30 | 2010-06-30 | 北京空间机电研究所 | Radial multipoint glue joint axial three-point clamping and supporting method of spatial lens |
CN106526784A (en) * | 2016-11-30 | 2017-03-22 | 中国科学院长春光学精密机械与物理研究所 | Flexible supporting mechanism for plane mirror |
CN106443959A (en) * | 2016-12-07 | 2017-02-22 | 中国科学院长春光学精密机械与物理研究所 | Split type bi-material flexible mechanism of space-based large-calibre high-facial-contour-precision reflector assembly |
CN106646816A (en) * | 2017-01-16 | 2017-05-10 | 中国科学院长春光学精密机械与物理研究所 | High-precision bonding fixing device for spatial reflector |
CN107450154A (en) * | 2017-08-15 | 2017-12-08 | 北京空间机电研究所 | The tension and compression modulus modulus of shearing unloading supporting construction of spacing reflection mirror |
CN208270836U (en) * | 2018-06-08 | 2018-12-21 | 中国科学院西安光学精密机械研究所 | Supporting structure and supporting component of large-diameter reflector |
Non-Patent Citations (1)
Title |
---|
关英俊;辛宏伟;: "大口径主反射镜支撑结构设计", 光电工程, no. 12, 15 December 2010 (2010-12-15) * |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109765672B (en) * | 2019-02-27 | 2020-09-01 | 中国科学院西安光学精密机械研究所 | Adhesive joint assembling method for reflector and support |
CN109765672A (en) * | 2019-02-27 | 2019-05-17 | 中国科学院西安光学精密机械研究所 | The splicing assembly method of reflecting mirror and support |
CN110196476A (en) * | 2019-05-09 | 2019-09-03 | 中国科学院西安光学精密机械研究所 | In one kind/long wave heavy caliber Infrared Lens flexible support structure |
CN110609373B (en) * | 2019-10-11 | 2024-04-05 | 赵智亮 | Micro-stress supporting adjustable optical lens frame structure and optical lens clamping method |
CN110609373A (en) * | 2019-10-11 | 2019-12-24 | 赵智亮 | Micro-stress support adjustable optical lens frame structure and optical lens clamping method |
CN110764219A (en) * | 2019-11-08 | 2020-02-07 | 南昌航空大学 | Reflector bonding structure for reducing thermal stress |
CN111352209A (en) * | 2020-04-07 | 2020-06-30 | 中国科学院长春光学精密机械与物理研究所 | Support structure of large-caliber reflector component of space remote sensor |
CN111650717A (en) * | 2020-05-09 | 2020-09-11 | 中国科学院西安光学精密机械研究所 | Surface-shaped high-stability reflector assembly and assembling method thereof |
CN111929804A (en) * | 2020-08-31 | 2020-11-13 | 长光卫星技术有限公司 | Support structure of large length-width ratio space reflector |
CN112130277A (en) * | 2020-09-28 | 2020-12-25 | 吉林大学 | Flexible supporting structure suitable for space camera reflector |
CN112130277B (en) * | 2020-09-28 | 2021-06-25 | 吉林大学 | Flexible supporting structure suitable for space camera reflector |
CN112162380A (en) * | 2020-10-22 | 2021-01-01 | 中国科学院长春光学精密机械与物理研究所 | Flexible supporting structure of medium and small-diameter reflector |
CN112882185A (en) * | 2021-01-22 | 2021-06-01 | 西安应用光学研究所 | Glue joint fixing structure and fixing method suitable for adjustable lens group of reflecting system |
Also Published As
Publication number | Publication date |
---|---|
CN108594399B (en) | 2024-05-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN108594399A (en) | Supporting structure and supporting component of large-diameter reflector | |
CN208270836U (en) | Supporting structure and supporting component of large-diameter reflector | |
CN201344989Y (en) | An optical lens and lens group | |
CN106291864B (en) | Reflecting mirror support structure, mirror assembly and optical remote sensing camera | |
WO2013136972A1 (en) | Cemented lens, and manufacturing method for cemented lens | |
CN104749741B (en) | Spacing reflection mirror double stopper adhesive means | |
US10161810B2 (en) | Honeycomb sandwich structure and method of manufacturing honeycomb sandwich structure | |
CN106646816A (en) | High-precision bonding fixing device for spatial reflector | |
CN108508570A (en) | Multiaxis flexible supporting device of the aspect than rectangular mirror | |
CN106405785B (en) | A kind of programmable large caliber reflecting mirror component load-carrying construction of heat distortion amount | |
CN113340223B (en) | Fiber grating strain sensor with adjustable measuring range and preparation and use methods thereof | |
CN106371189A (en) | Mechanical structure for turning optical path optical system | |
CN109343198A (en) | A kind of microstress adhesive asserably method for large-diameter non-spherical reflecting mirror | |
CN101718899A (en) | Periphery supporting mechanism of reflecting mirror in space remote sensing camera | |
CN101571389A (en) | Method for precisely assembling space remote sensing camera body structure | |
CN106323515A (en) | Optical fiber F-P cavity stress relief pressure sensor | |
JP2005539240A (en) | Capacitive pressure sensor | |
EP3025177B1 (en) | Optical subassembly, optical system and method | |
CN206906666U (en) | The optical bracket with bonding gap with least one clamping unit | |
CN103472566B (en) | Zero-expansion flexible damping supporting device of space reflector | |
US9956651B2 (en) | Method for producing a fluidic connection component for chromatography | |
CN109273862B (en) | Carbon fiber parabolic antenna and focusing assembly method thereof | |
CN103718011B (en) | For the sensor of at least one characteristic of test fluid medium | |
CN114729799A (en) | Device and method for measuring the three-dimensional shape of a structure, in particular of a wind turbine blade | |
EP3798137A1 (en) | Pipe structure and truss structure, and artificial satellite using such structures |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |