CN108767418B - Height storage is than winding ribbed deployable antenna structure - Google Patents
Height storage is than winding ribbed deployable antenna structure Download PDFInfo
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- CN108767418B CN108767418B CN201810357111.6A CN201810357111A CN108767418B CN 108767418 B CN108767418 B CN 108767418B CN 201810357111 A CN201810357111 A CN 201810357111A CN 108767418 B CN108767418 B CN 108767418B
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/08—Means for collapsing antennas or parts thereof
- H01Q1/10—Telescopic elements
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/08—Means for collapsing antennas or parts thereof
- H01Q1/10—Telescopic elements
- H01Q1/103—Latching means; ensuring extension or retraction thereof
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
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- Details Of Aerials (AREA)
Abstract
The present invention relates to a kind of high storages than winding ribbed deployable antenna structure, comprising: mounting seat；Centerbody: its inner hollow, and be arranged in mounting seat；Scalable feed: it is mounted in centerbody；Muti-piece elastically wraps rib: it is installed around the centerbody bottom outside；Metal wire side: tensioning, which is laid on, to be elastically wrapped on rib, and the rib that elastically wraps of expansion is cooperated to form parabolic reflecting surface；Locking assembly: including be arranged in mounting seat around the centerbody kerve, elastically wrap rib expansion and the locking hoop that bottom is placed in kerve, the upper plate that scalable feed top is set and pushes down locking hoop upper end described in constraint, and locking rope；Release component: including the hot knife of round bar and external power supply contacted with the locking rope.Compared with prior art, the present invention forms parabolic reflecting surface using rib tensioning metal wire side is elastically wrapped, be capable of providing the storage ratio of superelevation, reliability is unfolded and has enough type faces precision etc..
Description
Technical field
The invention belongs to space structure fields, are related to a kind of high storage ratio winding ribbed deployable antenna structure.
Background technique
In recent years, Small Satellite Technology development is swift and violent, wherein it is new to have developed to the space flight in functional application stage at initial stage in foreign countries
Mark also can be used in addition to having the advantages that develop the moonlets such as launch cost is low, the period is short in elegant cube satellite (CubeSat)
Standardization, modularized design, scalability is strong, and transmitting flexibly, can quickly networking.Cube satellite distributed three-dimensional system it is comprehensive at
This is low, high-efficient, can scout in terms of play a significant role, therefore its strategic value is higher.
Cube satellite antenna structure is based on unipole antenna.Unipole antenna gain is low, can if antenna gain can be improved
Greatly improve satellite communication quality.For cube satellite develop reflector antenna, can effectively increase antenna gain, can make its
X, the band operations such as S, greatly improve data transmission bauds, have high scientific research value and strategic value.
External cube satellite communication module is quickly grown.U.S. USC (University of Southern in 2012
California/Space Engineering Research Center) design cube satellite AENEAS successful launch,
Satellite antenna is radial rib paraboloid, and bore 0.5m stores volume 2U, and working frequency range is S-band；JPL has then started to research and develop work
Working frequency reaches the high-speed subminaturization high-gain aerial of 37.5GHz, and bore 0.5m stores volume 1.5U, and obtains 46dBi's
High-gain；Boeing winds rib reflector antenna in proposition microminiature in 2011, and bore 0.5m, service band is S-band,
Storage volume is then decreased to 0.5U, but the reflector antenna is only conceptual model, and type face precision is poor, and locking and method for releasing are not
It is bright.The research of domestic satellite antenna concentrates on heavy caliber reflector antenna, and the reflector antenna suitable for cube satellite is at present still
In the starting stage.Exploitation is suitable for the micromation high-gain reflecting surface Deployable antenna of cube satellite, compiles to cube satellite
Team's communication is of great significance.
Summary of the invention
It is an object of the present invention to overcome the above-mentioned drawbacks of the prior art and provide a kind of high storages than winding
Ribbed deployable antenna structure forms parabolic reflecting surface using rib tensioning metal wire side is elastically wrapped, is capable of providing the receipts of superelevation
Receive ratio, reliability is unfolded and has enough type faces precision.
The purpose of the present invention can be achieved through the following technical solutions:
A kind of high storage ratio winding ribbed deployable antenna structure, comprising:
Mounting seat；
Centerbody: its inner hollow, and be arranged in mounting seat；
Scalable feed: it is mounted in centerbody；
More elastically wrap rib: it is installed around the centerbody bottom outside, and when elastically wrapping rib expansion, is constituted
The skeletal support of parabolic reflecting surface；
Metal wire side: tensioning, which is laid on, to be elastically wrapped on rib, and the rib that elastically wraps of expansion is cooperated to form parabolic reflecting surface；
Locking assembly: including be arranged in mounting seat around the centerbody kerve, elastically wrap rib described in constraint
It is unfolded and bottom is placed in the locking hoop in kerve, and scalable feed top is set and pushes down the upper top of locking hoop upper end
Plate, the locking hoop are spliced by multi-disc hoop shell, and the locking rope that one end is secured to, institute are additionally provided on the upper plate
The other end for stating locking rope passes through the centerbody, is pierced by from mounting seat side, and is being installed with tension connection setting
Rope fixing end on pedestal；
Release component: including the hot knife of round bar and external power supply contacted with the locking rope.
Further, the lower part of the centerbody is in prismatic structure, and number of planes elastically wraps rib quantity with described
It is corresponding consistent.Top can be in cylindrical type, can use aluminium alloy element.When centerbody has wave transparent requirement, upper and lower two
Dividing may be designed to assembling form, and Upper cylindrical type structure uses the material with wave transparent performance, such as polyimide material instead.
Further, the lesser strip thin plate of thickness can be selected by elastically wrapping rib, and cross section is straight or it is certain to have
Radian is to increase bending stiffness, in addition, elastically wrapping, rib is longitudinally parabolic, the burnt diameter of specific parabolic equation and reflecting surface
Than related.The edge for elastically wrapping rib, which can according to need, is equipped with several apertures, convenient for sewing up later with metal wire side.Elasticity twines
It can be carried out preferably around the quantity of rib, to reach balance between the required precision of type face and storage ratio require.Further, bullet
Property winding rib material stainless steel, beryllium-bronze, carbon fiber can be used and other there is high-intensitive, high resiliency and high-low temperature resistant
Material.
Further, the scalable feed is feed forward type feed, feedback type feed or spiral shell with Telescopic
Revolve spring antenna.
Further, metal wire side should be the dedicated metal mirror wire side of spacecraft, may be selected to use nickel plating stainless steel wire
Wire side, gold-plated molybdenum filament wire side or particular fabric wire side.
Further, locking hoop uses the notched cylindrical shell of two panels.Locking rope can be using Di Nima rope etc..
Further, the scalable feed is helical spring antenna comprising is arranged in the spring of upper plate lower end
Insulated leg, the feed undersetting being arranged in mounting seat and both ends are separately connected the spring insulated leg and feedback
The feed spring and structure rope of source undersetting.
Further, it is closely connected between the spring insulated leg and upper plate using structure glue, the feed
The upper and lower ends of spring are respectively fitted on spring insulated leg and feed undersetting, and use structure glue connection.
Further, the kerve includes the shell being fixed in mounting seat, upper part be machined with circumferentially and
For being caught in the locating slot of locking hoop lower end, also hollow out to form mounting hole at the middle part of shell, the inner casing is placed in installation
It in hole and can move up and down along it, compressed spring is additionally provided between inner casing and mounting seat.
Further, the mounting hole is processed into the inverted T-type structure for preventing inner casing from deviating from, and when compressed spring pushes
When inner casing is jacked along mounting hole to maximum, the prominent upper shell face of inner casing.The isostructural setting of compressed spring can guarantee lock
Surely hoop lower end ejects kerve, and then will not influence the expansion for elastically wrapping rib.
Further, the hot knife of the round bar is vacantly arranged in mounting seat by hot knife support, and the hot knife of round bar passes through
Heater circuit is connect with external power supply, and after external power supply power supply, the hot knife heating of round bar, which restricts locking to fuse, realizes release.
Further, the marginal position of the upper plate is also downwardly extending the card of constraint locking hoop upper end freedom degree
Pawl.
High storage of the invention is than winding ribbed deployable antenna structure, before satellier injection, will elastically wrap rib and
Metal wire side is wound on centerbody, meanwhile, locked component will elastically wrap rib and be constrained to rounding state, after entering the orbit when receive exhibition
When opening instruction, release component operation unlocks constraint of the component to deployable antenna, elastically wraps rib and is expanded to working condition.
Compared with prior art, the invention has the characteristics that:
(1) present invention uses the rib of high-strength high-elasticity material, and the reflecting surface rigidity of complexed metal reflector net, formation is big.
The quantity of rib can optimize, and realization type face is high-precision while realizing efficiently storage.It is realized using the elasticity for elastically wrapping rib
Parabolic reflecting surface expansion is unfolded fast and reliable and is not necessarily to extra power.
(2) present invention is compared with the monopole and microstrip antenna for being traditionally used for the communication of cube star, because its provide it is biggish
Parabolic reflecting surface, therefore it is capable of providing higher gain, there is higher data transmission efficiency.
(3) for the present invention compared with the folding rib wire side antenna being applied on cube star, used elastically wraps shaft of rib product more
It is small and wound around centerbody, therefore it can be realized bigger storage ratio.
(4) locking mechanism and relieving mechanism of the invention, structure is simple, compact, is formed using least configuration closed
Loose winding ribbed antenna can be stored completely, limit its freedom degree completely, form stable gathering shape by space
State；In unlock, it can be realized feed and wind the synchronous release of ribbed reflecting surface, the structure of relieving mechanism is simple, and effect can
It leans on.
Detailed description of the invention
Fig. 1 is the schematic front view of unfolded state of the invention；
Fig. 2 is the schematic top plan view of unfolded state of the invention；
Fig. 3 is that the axis side of unfolded state of the invention tries to be intended to；
Fig. 4 is the elevational schematic view of unfolded state of the invention；
Fig. 5 is that the axis side of receiving state of the invention tries to be intended to；
Fig. 6 is the diagrammatic cross-section of receiving state of the invention；
Fig. 7 is the A-A diagrammatic cross-section of Fig. 1 mark；
Fig. 8 is the schematic front view of center body；
Fig. 9 is the B-B diagrammatic cross-section that Fig. 8 indicates part；
Figure 10 is the schematic front view for elastically wrapping rib；
Figure 11 is the structural schematic diagram of feed；
Figure 12 is that the axis side of kerve tries to be intended to；
Figure 13 is the schematic top plan view of kerve；
Figure 14 is the schematic diagram that inner casing jacks state in kerve；
Figure 15 is the schematic diagram that inner casing declines state in kerve；
Description of symbols in figure:
1 is center body, and 1-1 is center body lower part, and 1-2 is center body top, and 2 is elastically wrap rib, and 3 be metal wire side, 4
For scalable feed, 4-1 is upper plate, and 4-2 is spring insulated leg, and 4-3 is feed spring, and 4-4 is structure rope, and 4-5 is feedback
Source undersetting, 5 be mounting seat, and 6 be locking hoop, and 7 be kerve, and 7-1 is shell, and 7-2 is inner casing, and 7-3 is compressed spring, and 8 are
Locking rope, 9 be rope fixing end, and 10 be the hot knife of round bar, and 11 be hot knife support.
Specific embodiment
The present invention is described in detail with specific embodiment below in conjunction with the accompanying drawings.The present embodiment is with technical solution of the present invention
Premised on implemented, the detailed implementation method and specific operation process are given, but protection scope of the present invention is not limited to
Following embodiments.
A kind of high storage provided in the present invention is than winding ribbed deployable antenna structure, referring to shown in Fig. 1-4, Fig. 7,
Include:
Mounting seat 5；
Centerbody 1: its inner hollow, and be arranged in mounting seat 5；
Scalable feed 4: it is mounted in centerbody 1；
More elastically wrap rib 2: it is installed around 1 bottom outside of centerbody, and when elastically wrapping the expansion of rib 2,
Constitute the skeletal support of parabolic reflecting surface；
Metal wire side 3: tensioning, which is laid on, to be elastically wrapped on rib 2, and the rib 2 that elastically wraps of expansion is cooperated to form parabolic reflective
Face；
Locking assembly: mounting seat 5 is arranged in referring to shown in Fig. 5, Fig. 6, Figure 12-Figure 15, including around the centerbody 1
On kerve 7, elastically wrap the expansion of rib 2 described in constraint and bottom is placed in locking hoop 6 in kerve 7, and be arranged scalable
4 top of feed and the upper plate 4-1 for pushing down 6 upper ends of locking hoop, the locking hoop 6 is spliced by multi-disc hoop shell, described
The locking rope 8 that one end is secured to is additionally provided on upper plate 4-1, the other end of the locking rope 8 passes through the centerbody 1, from
5 side of mounting seat is pierced by, and connects the rope fixing end 9 being arranged in mounting seat 5 with tension；
Discharge component: it is shown in Figure 6, including the hot knife 10 of round bar and external power supply contacted with the locking rope 8.
In a preferred embodiment of the invention, referring to shown in Fig. 8-Fig. 9, the centerbody 1 divides for center
Body top 1-2 and centerbody lower part 1-1, wherein centerbody lower part 1-1 is in prismatic structure, and number of planes is twined with the elasticity
Corresponding consistent around 2 quantity of rib, such as elastically wrapping 2 quantity of rib is 16, then the number of planes of centerbody lower part 1-1 is 16, that is, is in
16 arris are cylindrical.Meanwhile the root for elastically wrapping rib 2 can also be beaten there are two circular hole, referring to Figure 10, use bolt to facilitate
It is connected with the side panels of centerbody lower part 1-1.Centerbody top 1-2 can be in cylindrical type, can use aluminium alloy element.
When centerbody 1 has wave transparent requirement, upper and lower two parts may be designed to assembling form, and Upper cylindrical type structure is used instead with wave
The material of energy, such as polyimide material.
In a preferred embodiment of the invention ,-Fig. 4, Figure 10 referring to fig. 2, thickness can be selected by elastically wrapping rib 2
Lesser strip thin plate is spent, cross section is straight or has certain radian to increase bending stiffness, in addition, it is vertical to elastically wrap rib 2
To parabolic, specific parabolic equation is related with the burnt diameter ratio of reflecting surface.The edge for elastically wrapping rib 2 can according to need
Several apertures are equipped with, convenient for sewing up later with metal wire side 3.The quantity for elastically wrapping rib 2 can carry out preferably, in type face essence
Degree requires and storage is than reaching balance between requiring.Further, stainless steel, beryllium blueness can be used in the material for elastically wrapping rib 2
Copper, carbon fiber and other materials with high-intensitive, high resiliency and high-low temperature resistant.
In a preferred embodiment of the invention, shown in Figure 11, the scalable feed 4 is with stretching
Feed forward type feed, feedback type feed or the helical spring antenna of contracting function.It is further preferred that the scalable feed 4
For helical spring antenna comprising be arranged in the spring insulated leg 4-2 of the lower end upper plate 4-1, be arranged in mounting seat 5
Feed undersetting 4-5 and both ends are separately connected the feed spring of the spring insulated leg 4-2 and feed undersetting 4-5
4-3 and structure rope 4-4.Still more preferably, feed spring 4-3 is made by phosphor-copper with good conductivity, and structural parameters are such as
Central diameter, line footpath, circle number, screw pitch etc. are calculated by structural mechanics and radio frequency analog calculated result determines jointly.In addition, spring insulation branch
Seat 4-2 then can be using materials such as polyimides.Further, between the spring insulated leg 4-2 and upper plate 4-1
It is closely connected using structure glue, the upper and lower ends of the feed spring 4-3 are respectively fitted under spring insulated leg 4-2 and feed and prop up
On seat 4-5, and use structure glue connection.Further, structure rope 4-4 can use stainless steel 304 cable wire, in this way, passing through
The rope hole that upper plate 4-1 and feed undersetting 4-5 is reserved can be through entire scalable feed 4, and then can effectively increase
The lateral rigidity of feed increases the vibration frequency of feed.
In a preferred embodiment of the invention, metal wire side 3 should be the dedicated metallic reflection veil of spacecraft
Face may be selected to use nickel plating stainless steel wire wire side, gold-plated molybdenum filament wire side or particular fabric wire side.Metal wire side 3 is preferably in its recommendation
Tensioning is carried out under stretching force, metal wire side 3 can cut out net stencil with acrylic under tensile state and be cut out.By what is reduced
Metal wire side 3, which is layered on, to be elastically wrapped on rib 2, is stitched metal wire side 3 by elastically wrapping the aperture Kev bracing wire reserved on rib 2
On rib.After sewing it up, tensioning is carried out with a continuous Kev bracing wire in 3 outer edge of metal wire side, and finally use polyimides
Adhesive tape edge sealing, in case 3 flash of metal wire side is wound mutually.
In a preferred embodiment of the invention, locking hoop 6 uses the notched cylindrical shell of two panels.Locking rope 8
It can be using Di Nima rope etc..
In a preferred embodiment of the invention, the kerve 7 includes the shell being fixed in mounting seat 5
7-1, upper part be machined with circumferentially and for be caught in it is described locking hoop 6 lower ends locating slot, also dug at the middle part of shell 7-1
Sky forms mounting hole, and the inner casing 7-2 is placed in mounting hole and can move up and down along it, between inner casing 7-2 and mounting seat 5
It is additionally provided with compressed spring 7-3.When installation, the lower end of locking hoop 6 can enter in locating slot, meanwhile, inner casing 7-2 is in compressed spring 7-3
Active force under withstand upwards always locking hoop 6 lower ends.When 6 non-stress are bound round in locking, i.e. the upper end is not raised plate 4-1 and pushes down
When, inner casing 7-2 is jacked under compressed spring 7-3 effect, until inner casing 7-2 shell rostellum goes out the top surface shell 7-1, when locking hoop 6
When forced compression, compressed spring 7-3 is shunk, inner casing 7-2 decline, until its shell top is flushed with locating slot bottom end.In this way, when that will lock
Surely it binds round in 6 lower ends indentation locating slot, the elasticity stored in compressed spring 7-3 can be when end pressure disappears on locking hoop 6, will
Locking hoop 6 pops up, it is made not to be stuck in kerve 7, in case influence elastically wraps the expansion of rib 2.
Further, the mounting hole is processed into inverted T shaped anti-taking off structure, and when compressed spring 7-3 is pushed
When inner casing 7-2 is jacked along mounting hole to maximum, the prominent upper surface shell 7-1 inner casing 7-2.The isostructural setting of compressed spring 7-3
It can guarantee locking hoop 6 lower ends ejection kerve 7, and then will not influence the expansion for elastically wrapping rib 2.The setting of anti-taking off structure
Primarily to avoid making inner casing 7-2 be ejected and be kept completely separate with shell 7-1 under the action of compressed spring 7-3,
Can use common inverted T-type structure, at this point, inner casing 7-2 shape be also provided with into it is similar to mounting hole.
In a preferred embodiment of the invention, the hot knife 10 of the round bar is vacantly arranged by hot knife support 11
In mounting seat 5, the hot knife 10 of round bar is connect by heater circuit with external power supply, after external power supply power supply, the hot knife of round bar
8 fusing of locking rope is realized release by 10 heating.The component of two middle with hole can be set into hot knife support 11, using polyamides Asia
Amine material is mounted in mounting seat 5 by bolt, in this way, the hot knife 10 of round bar is two interstitial holes across hot knife support 11,
It adopts and is screwed, the purpose is to separate hot knife vacantly with bottom plate, external power supply can be provided by celestial body.
In a preferred embodiment of the invention, shown in referring to figs. 5 and 6, the edge of the upper plate 4-1
Position is also downwardly extending the claw of constraint locking 6 upper lateral freedom degrees of hoop.
Embodiment 1
A kind of high storage ratio winding ribbed deployable antenna structure, referring to shown in Fig. 1-4, Fig. 7, comprising:
Mounting seat 5；
Centerbody 1: its inner hollow, and be arranged in mounting seat 5；
Scalable feed 4: it is mounted in centerbody 1；
More elastically wrap rib 2: it is installed around 1 bottom outside of centerbody, and when elastically wrapping the expansion of rib 2,
Constitute the skeletal support of parabolic reflecting surface；
Metal wire side 3: tensioning, which is laid on, to be elastically wrapped on rib 2, and the rib 2 that elastically wraps of expansion is cooperated to form parabolic reflective
Face；
Locking assembly: mounting seat 5 is arranged in referring to shown in Fig. 5, Fig. 6, Figure 12-Figure 15, including around the centerbody 1
On kerve 7, elastically wrap the expansion of rib 2 described in constraint and bottom is placed in locking hoop 6 in kerve 7, and be arranged scalable
4 top of feed and the upper plate 4-1 for pushing down 6 upper ends of locking hoop, the locking hoop 6 is spliced by multi-disc hoop shell, described
The locking rope 8 that one end is secured to is additionally provided on upper plate 4-1, the other end of the locking rope 8 passes through the centerbody 1, from
5 side of mounting seat is pierced by, and connects the rope fixing end 9 being arranged in mounting seat 5 with tension；
Discharge component: it is shown in Figure 6, including the hot knife 10 of round bar and external power supply contacted with the locking rope 8.
Referring to shown in Fig. 8-Fig. 9, the centerbody 1 divides for centerbody top 1-2 and centerbody lower part 1-1, wherein in
Heart body lower part 1-1 is in prismatic structure, and number of planes and 2 quantity of rib that elastically wraps are corresponding consistent, such as elastically wraps the number of rib 2
Amount is 16, then the number of planes of centerbody lower part 1-1 is 16, i.e., cylindrical in 16 arris.Meanwhile elastically wrapping the root of rib 2
Portion can also be beaten there are two circular hole, referring to Figure 10, use bolt to be connected with the side panels of centerbody lower part 1-1 to facilitate.In
Heart body top 1-2 can be in cylindrical type, can use aluminium alloy element.When centerbody 1 has wave transparent requirement, upper and lower two parts
It may be designed to assembling form, Upper cylindrical type structure uses the material with wave transparent performance, such as polyimide material instead.
It referring to Figure 10, elastically wraps rib 2 and selects the lesser strip thin plate of thickness, cross section is straight or has certain radian
To increase bending stiffness, in addition, elastically wrapping longitudinal parabolic, the burnt diameter ratio of specific parabolic equation and reflecting surface of rib 2
It is related.The edge for elastically wrapping rib 2, which can according to need, is equipped with several apertures, convenient for sewing up later with metal wire side 3.Elasticity twines
It can be carried out preferably around the quantity of rib 2, to reach balance between the required precision of type face and storage ratio require.Further,
The material for elastically wrapping rib 2 can be used stainless steel, beryllium-bronze, carbon fiber and other have high-intensitive, high resiliency and resistance to height
The material of temperature.
Shown in Figure 11, the scalable feed 4 is helical spring antenna comprising is arranged under upper plate 4-1
The spring insulated leg 4-2 at end, the feed undersetting 4-5 being arranged in mounting seat 5 and both ends are separately connected the bullet
The feed spring 4-3 and structure rope 4-4 of spring insulated leg 4-2 and feed undersetting 4-5.Feed spring 4-3 is good by electric conductivity
Phosphor-copper production, structural parameters such as central diameter, line footpath, circle number, screw pitch etc. is calculated by structural mechanics and radio frequency analog calculated result
It is common to determine.In addition, spring insulated leg 4-2 then can be using materials such as polyimides.The spring insulated leg 4-2 with
It is closely connected between upper plate 4-1 using structure glue, the upper and lower ends of the feed spring 4-3 are respectively fitted over spring insulated leg
On 4-2 and feed undersetting 4-5, and use structure glue connection.Structure rope 4-4 can use stainless steel 304 cable wire, in this way, logical
Entire scalable feed 4 can be run through by crossing the rope hole that upper plate 4-1 and feed undersetting 4-5 is reserved, and then can effectively be increased
The lateral rigidity for adding feed increases the vibration frequency of feed.
Metal wire side 3 should be the dedicated metal mirror wire side of spacecraft, may be selected with nickel plating stainless steel wire wire side, gold-plated
Molybdenum filament wire side or particular fabric wire side.Metal wire side 3 is preferably recommended to carry out tensioning under stretching force at it, and metal wire side 3 is in tensioning
Net stencil can be cut out with acrylic under state to be cut out.The metal wire side 3 reduced is layered on and is elastically wrapped on rib 2, is passed through
It elastically wraps the aperture Kev bracing wire reserved on rib 2 metal wire side 3 is sewn on rib.After sewing it up, in 3 outer edge of metal wire side
Tensioning is carried out with a continuous Kev bracing wire, and finally uses Kapton Tape edge sealing, in case 3 flash of metal wire side twines mutually
Around.
Locking hoop 6 uses the notched cylindrical shell of two panels.Locking rope 8 can be using Di Nima rope etc..
The kerve 7 includes the shell 7-1 that is fixed in mounting seat 5, upper part be machined with circumferentially and be used for
It is caught in the locating slot of 6 lower ends of the locking hoop, also hollows out to form mounting hole at the middle part of shell 7-1, the inner casing 7-2 is placed in peace
It in dress hole and can move up and down along it, compressed spring 7-3 is additionally provided between inner casing 7-2 and mounting seat 5.When installation, locking
The lower end of hoop 6 can enter in locating slot, meanwhile, inner casing 7-2 withstands locking hoop 6 upwards always under the active force of compressed spring 7-3
Lower end.When 6 non-stress are bound round in locking, i.e., when the upper end is not raised plate 4-1 and pushes down, inner casing 7-2 is i.e. under compressed spring 7-3 effect
Jacking, until inner casing 7-2 shell rostellum goes out the top surface shell 7-1, when 6 forced compression is bound round in locking, compressed spring 7-3 is shunk, inner casing
7-2 decline, until its shell top is flushed with locating slot bottom end.In this way, when that will lock in 6 lower ends of hoop indentation locating slot, compressed spring
Locking hoop 6 can be popped up when end pressure disappears on locking hoop 6, it is made not to be stuck by the elasticity stored in 7-3
In kerve 7, in case influence elastically wraps the expansion of rib 2.
The mounting hole is processed into inverted T shaped anti-taking off structure, and when compressed spring 7-3 pushes inner casing 7-2 along peace
When dress hole is jacked to maximum, the prominent upper surface shell 7-1 inner casing 7-2.The isostructural setting of compressed spring 7-3 can guarantee lock
Surely 6 lower ends ejection kerve 7 is bound round, and then will not influence the expansion for elastically wrapping rib 2.The setting of anti-taking off structure is primarily to keep away
Exempt to make inner casing 7-2 be ejected and be kept completely separate with shell 7-1 under the action of compressed spring 7-3, it can be using common
Inverted T-type structure, at this point, inner casing 7-2 shape be also provided with into it is similar to mounting hole.
The hot knife 10 of the round bar is vacantly arranged in mounting seat 5 by hot knife support 11, and the hot knife 10 of round bar is by adding
Heater circuit is connect with external power supply, and after external power supply power supply, 8 fusing of locking rope is realized release by the hot heating of knife 10 of round bar.Heat
The component of two middle with hole can be set into knife support 11, using polyimides material, is mounted on mounting seat 5 by bolt
On, in this way, the hot knife 10 of round bar is two interstitial holes across hot knife support 11, adopts and be screwed, the purpose is to keep hot knife outstanding
Sky is separated with bottom plate, and external power supply can be provided by celestial body.
Shown in referring to figs. 5 and 6, the marginal position of the upper plate 4-1 is also downwardly extending on constraint locking hoop 6
Hold the claw of lateral degrees of freedom.
The above description of the embodiments is intended to facilitate ordinary skill in the art to understand and use the invention.
Person skilled in the art obviously easily can make various modifications to these embodiments, and described herein general
Principle is applied in other embodiments without having to go through creative labor.Therefore, the present invention is not limited to the above embodiments, ability
Field technique personnel announcement according to the present invention, improvement and modification made without departing from the scope of the present invention all should be of the invention
Within protection scope.
Claims (10)
1. a kind of high storage is than winding ribbed deployable antenna structure characterized by comprising
Mounting seat (5)；
Centerbody (1): its inner hollow, and be arranged on mounting seat (5)；
Scalable feed (4): it is mounted in centerbody (1)；
More elastically wrap rib (2): it is installed around the centerbody (1) bottom outside, and is unfolded when elastically wrapping rib (2)
When, constitute the skeletal support of parabolic reflecting surface；
Metal wire side (3): tensioning is laid on and elastically wraps on rib (2), and it is anti-to cooperate the elastically wrapping of expansion rib (2) to form parabolic
Penetrate face；
Locking assembly: it is twined including the kerve (7) that is arranged on mounting seat (5) around the centerbody (1), the constraint elasticity
Around rib (2) expansion and bottom is placed in the locking hoop (6) in kerve (7), and is arranged on scalable feed (4) top and pushes down lock
The upper plate (4-1) of fixed hoop (6) upper end, the locking hoop (6) are spliced by multi-disc hoop shell, the upper plate (4-1)
On be additionally provided with the locking rope (8) that one end is secured to, the other end of the locking rope (8) passes through the centerbody (1), from installation
Pedestal (5) side is pierced by, and the rope fixing end (9) being arranged on mounting seat (5) with tension connection；
Release component: including the hot knife of round bar (10) and external power supply contacted with the locking rope (8).
2. a kind of high storage according to claim 1 is than winding ribbed deployable antenna structure, which is characterized in that described
The lower part of centerbody (1) be in prismatic structure, number of planes with it is described elastically wrap rib (2) quantity it is corresponding unanimously.
3. a kind of high storage according to claim 1 is than winding ribbed deployable antenna structure, which is characterized in that described
Rib (2) are elastically wrapped as elastic strip thin plate, longitudinal direction is parabolic.
4. a kind of high storage according to claim 1 is than winding ribbed deployable antenna structure, which is characterized in that described
Scalable feed (4) is feed forward type feed, feedback type feed or helical spring antenna with Telescopic.
5. a kind of high storage according to claim 1 or 4 is than winding ribbed deployable antenna structure, which is characterized in that institute
The scalable feed (4) stated is helical spring antenna comprising is arranged in the spring insulated leg (4- of the lower end upper plate (4-1)
2) the feed undersetting (4-5) and both ends, being arranged on mounting seat (5) are separately connected the spring insulated leg (4-
And the feed spring (4-3) and structure rope (4-4) of feed undersetting (4-5) 2).
6. a kind of high storage according to claim 5 is than winding ribbed deployable antenna structure, which is characterized in that described
It is closely connect between spring insulated leg (4-2) and upper plate (4-1) using structure glue, above and below the feed spring (4-3)
Both ends are respectively fitted on spring insulated leg (4-2) and feed undersetting (4-5), and use structure glue connection.
7. a kind of high storage according to claim 1 is than winding ribbed deployable antenna structure, which is characterized in that described
Kerve (7) includes the shell (7-1) and inner casing (7-2) that are fixed on mounting seat (5), and upper part is machined with being used in combination circumferentially
In the locating slot for being caught in the locking hoop (6) lower end, also hollow out to form mounting hole at the middle part of shell (7-1), the inner casing (7-
2) it is placed in mounting hole and can move up and down along it, be additionally provided with compressed spring (7- between inner casing (7-2) and mounting seat (5)
3).
8. a kind of high storage according to claim 7 is than winding ribbed deployable antenna structure, which is characterized in that described
Mounting hole is processed into the inverted T-type structure for preventing inner casing (7-2) from deviating from, and when compressed spring (7-3) pushes inner casing (7-2) along installation
When hole is jacked to maximum, the prominent upper surface shell (7-1) of inner casing (7-2).
9. a kind of high storage according to claim 1 is than winding ribbed deployable antenna structure, which is characterized in that described
The hot knife of round bar (10) is vacantly arranged on mounting seat (5) by hot knife support (11).
10. a kind of high storage according to claim 1 is than winding ribbed deployable antenna structure, which is characterized in that described
Upper plate (4-1) marginal position be also downwardly extending constraint locking hoop (6) upper end freedom degree claw.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810357111.6A CN108767418B (en) | 2018-04-20 | 2018-04-20 | Height storage is than winding ribbed deployable antenna structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810357111.6A CN108767418B (en) | 2018-04-20 | 2018-04-20 | Height storage is than winding ribbed deployable antenna structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108767418A CN108767418A (en) | 2018-11-06 |
| CN108767418B true CN108767418B (en) | 2019-08-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810357111.6A Active CN108767418B (en) | 2018-04-20 | 2018-04-20 | Height storage is than winding ribbed deployable antenna structure |
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Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109818151B (en) * | 2019-02-19 | 2021-05-21 | 上海卫星工程研究所 | Satellite-borne deployable mesh antenna |
| CN110120576B (en) * | 2019-05-11 | 2021-12-28 | 西安电子科技大学 | Umbrella-shaped antenna unfolding mechanism combining fixed-axis wheel train and lead screw |
| CN110994118B (en) * | 2019-11-18 | 2021-07-02 | 西安电子科技大学 | Rope-driven umbrella-shaped Cassegrain antenna main and auxiliary surface stable unfolding mechanism |
| CN112164856B (en) * | 2020-08-13 | 2024-05-28 | 中国石油天然气集团有限公司 | Directional antenna skeleton structure and three-degree-of-freedom frame type winding tool |
| CN114069188B (en) * | 2021-12-27 | 2024-06-04 | 浙江众星志连科技有限责任公司 | Expansion and locking device for pico-nano satellite antenna |
| CN114678677A (en) * | 2022-03-21 | 2022-06-28 | 同济大学 | Feed mechanism of winding rib type deployable antenna |
| CN116505224B (en) * | 2023-06-29 | 2023-09-05 | 齐鲁空天信息研究院 | Antenna and aerospace device composed of expandable winding ribs |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104269657B (en) * | 2014-09-19 | 2017-06-13 | 上海跃盛信息技术有限公司 | A kind of umbrella antenna reflector |
| US10170843B2 (en) * | 2015-05-29 | 2019-01-01 | California Institute Of Technology | Parabolic deployable antenna |
| CN107799867A (en) * | 2016-08-29 | 2018-03-13 | 何志杰 | New deployable antenna structure |
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