CN106602203A - Portable satellite antenna - Google Patents
Portable satellite antenna Download PDFInfo
- Publication number
- CN106602203A CN106602203A CN201610958856.9A CN201610958856A CN106602203A CN 106602203 A CN106602203 A CN 106602203A CN 201610958856 A CN201610958856 A CN 201610958856A CN 106602203 A CN106602203 A CN 106602203A
- Authority
- CN
- China
- Prior art keywords
- base
- reflecting plate
- feed
- source device
- portable satellite
- 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.)
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Classifications
-
- 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
-
- 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
- H01Q1/084—Pivotable antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/16—Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal
- H01Q15/161—Collapsible reflectors
- H01Q15/162—Collapsible reflectors composed of a plurality of rigid panels
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
- H01Q19/12—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/12—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems
- H01Q3/16—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/12—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems
- H01Q3/16—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device
- H01Q3/20—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device wherein the primary active element is fixed and the reflecting device is movable
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aerials With Secondary Devices (AREA)
- Details Of Aerials (AREA)
Abstract
The invention relates to a portable satellite antenna. The portable satellite antenna includes a base, a reflecting plate detachably connected with the base, and a feed source device detachably connected with the base, the included angle between the reflecting plate and the base is adjustable, the reflecting plate is made of carbon fiber materials, the included angle between the feed source device and the base is adjustable, and the relative position between the feed source device and the reflecting plate can be adjusted through the included angle between the feed source device and the base. The portable satellite antenna is portable and meets the needs for outdoor portable use while guaranteeing the easy adjustment of satellite antenna reflection position through the angle adjustable design and the detachable design between the reflecting plate and the base and the feed source device and the base.
Description
Technical field
The present invention relates to communication technique field, and in particular to a kind of Portable satellite aerial.
Background technology
With the development of mechanics of communication, communication tool has become the with oneself indispensable article of people, no matter to which, Ren Mendou
Too busy to get away communication tool.But the use of communication tool be unable to do without satellite-signal, signal difference understands making for extreme influence communication tool
With.For especially for some outdoor activities personnel, when being frequently encountered signal difference, outdoor personnel and the external world are affected
Contact in time.Communication signal is bad when especially outdoor activities personnel face a danger outside can cause very big impact.
Therefore, the use of Portable satellite aerial is more and more extensive.But existing Portable satellite aerial is typically all monoblock type knot
Structure, to outdoor personnel very big inconvenience is brought.
The content of the invention
In consideration of it, being necessary the problem for above-mentioned existing Portable satellite aerial portability difference, there is provided one kind is more convenient for
The Portable satellite aerial of carrying.
In view of this, the embodiment of the present invention provides a kind of Portable satellite aerial, including：
Base；
The reflecting plate being detachably connected with the base, the angle scalable between the reflecting plate and the base, and
The reflecting plate is made up of carbon fibre material；
The feed source device being detachably connected with the base, the angle between the feed source device and the base is adjustable
Section, and can pass through to adjust between angle regulation feed source device and the reflecting plate between the feed source device and the base
Relative position.
Wherein in one embodiment, also include the connecting seat being detachably connected with the base；The expelling plate and institute
State feed source device to be connected with the base by the connecting seat；
The connecting seat includes support column and connecting shaft；
Described support column one end is detachably connected with the base, and the other end connects the connecting shaft by connecting hole；
The reflecting plate is rotated by bracing frame and the connecting shaft and be connected, the feed source device by feed support bar and
The connecting shaft rotates connection.
Wherein in one embodiment, the support column is rotatably connected by bottom link slot with the base post of base.
Wherein in one embodiment, orientation locking device is provided with the support column, the orientation locking device sets
Put in the outside of the bottom link slot, it is adaptable to the relative position between the fixation connecting seat and base post.
Wherein in one embodiment, pitching locking device and/or pitching micromatic setting are provided with the connecting shaft；
The pitching locking device, it is adaptable between fixed support frame as described above and the feed support bar and the connecting shaft
Relative position；
The pitching micromatic setting, it is adaptable to support frame as described above and the feed support bar are adjusted in the first preset range
Angle of inclination between base.
Wherein in one embodiment, described feed support bar one end is connected by fixed part with feed in the connecting shaft
Portion is fixedly connected, and the feed connecting portion is rotatably connected with the connecting shaft；
The other end of the feed support bar is provided with chute, and the feed source device is matched by feed seat with the chute
Connection；And the chute is horizontal during the Portable satellite aerial work.
Wherein in one embodiment, support frame as described above is arcuate structure, and one end rotates with the connecting shaft and is connected, another
End is arranged on the reflecting plate and the another side of the feed source device opposite face.
Wherein in one embodiment, the base includes base post, the collar, cradling piece and expansion link；
The set ring set is penetrated on the base post, and the collar can relatively described base post slide up and down, and energy
It is enough to rotate relative to the base post；
The cradling piece and the foldable connection of the collar；
Described expansion link one end slidably connects with the foldable connection in the base post bottom, the other end with the cradling piece
Connect.
Wherein in one embodiment, the cradling piece and the expansion link are made up of aluminum alloy materials.
Wherein in one embodiment, also set has penetrated azimuth vernier adjusting device on the base post, it is adaptable to default second
In the range of adjust the rotational angle of the connecting seat.
Wherein in one embodiment, the reflecting plate be circular configuration, a diameter of 0.4 meter, core molding thickness
For 1.5 millimeters, edge thickness is 7 millimeters.
Using above-mentioned technical proposal, the present invention can at least obtain following technique effects：
The Portable satellite aerial of the present invention, by the design of adjustable angle between reflecting plate and feed source device and base and
Design for disassembly, while ensureing that satellite antenna reflection orientation is easy to adjust, makes satellite antenna quite convenient for carrying, and meets family
The demand of outer portable use.Further, the base of satellite antenna mainly adopts aluminum alloy materials, reduces satellite antenna TBW
Amount.
Description of the drawings
Technical scheme in order to be illustrated more clearly that the embodiment of the present invention, below will be to institute in embodiment of the present invention description
The accompanying drawing that needs are used is briefly described, it should be apparent that, drawings in the following description are only some enforcements of the present invention
Example, for those of ordinary skill in the art, on the premise of not paying creative work, can be with according to present invention enforcement
The content of example and these accompanying drawings obtain other accompanying drawings.
Fig. 1 is the Portable satellite aerial overall structure diagram described in the present embodiment；
Fig. 2 is top half (not including the base) structural representation of the Portable satellite aerial described in the present embodiment；
Fig. 3 is the Portable satellite aerial connecting base structure schematic diagram described in the present embodiment；
Fig. 4 is the feed supporting bar structure schematic diagram of the Portable satellite aerial described in the present embodiment
Fig. 5 is the understructure schematic diagram of the Portable satellite aerial described in the present embodiment；
Fig. 6 is the structural representation after the Portable satellite aerial of the present embodiment is folded.
Specific embodiment
The disclosure for describing to help comprehensive understanding to be limited by claim and its equivalent referring to the drawings is provided
Various embodiments.Hereinafter description includes the various details for helping understand, but these details will be considered only to be example
Property.Therefore, it will be appreciated by those of ordinary skill in the art that without departing from the scope of the present disclosure and spirit in the case of, can be right
Various embodiments described herein makes various changes and modifications.In addition, in order to clear and succinct, known function and construction are retouched
Stating to be omitted.
Term and vocabulary used in following description and claims is not limited to document implication, but only by inventor
For enabling the disclosure clearly and as one man to be understood.Therefore, to those skilled in the art it should be apparent that carrying
Description for following various embodiments of this disclosure merely to exemplary purpose, and it is unrestricted by claims and its
The purpose of the disclosure that equivalent is limited.
It should be understood that unless context is clearly indicated in addition, otherwise singulative also includes plural.Thus, for example,
Include the reference to one or more such surfaces to the reference of " assembly surface ".
Fig. 1 is the Portable satellite aerial overall structure diagram of the present embodiment.
With reference to Fig. 1, the Portable satellite aerial of the present embodiment includes base 100, reflecting plate 200 and feed source device 300.Its
In, base 100 is the supporting construction of whole Portable satellite aerial, supports reflecting plate 200 and feed source device 300.And reflecting plate
200 and feed source device 300 be detachably connected with passive base 100.So as to user can be by when carrying
Reflecting plate 200 and feed source device 300 are disassembled from base 100, and respectively packaging is carried, and greatly increases taking for satellite antenna
Band property.
Referring to Fig. 1, in the present embodiment, reflecting plate 200 links together with feed source device 300, and its entirety can be the bottom of with
Seat 100 is separated, and satellite antenna can be split into two parts and be carried respectively by user when carrying, or splits Final finishing one
Packaging is carried after rising.
In other embodiments, reflecting plate 200 can also separate to be respectively installed to base with the feed source device 300
On 100.When carrying, reflecting plate 200 and feed source device 300 can respectively be disassembled packaging and be carried.
Further, in the present embodiment, reflecting plate 200 is made up of carbon fibre material, and reflecting plate 200 and base 100
Between angle scalable, the angle between feed source device 300 and base 100 can also adjust.As shown in figure 1, anti-when adjusting
The angle penetrated between plate 200 and base 100, or when adjusting the angle between feed source device 300 and base 100, reflecting plate 200
Can change with the relative position between feed source device 300.Especially by reflecting plate 200 and feed source device 300 from the base 100
On when disassemble, can be by adjusting the angle that the angle between reflecting plate 200 and feed source device 300 makes between the two
Minimum, so as to convenient use person's carrying.
As seen from the above description, the Portable satellite aerial base 100 of the present embodiment and reflecting plate 200 and feed source device
300 are detachably connected, so as to connect reflecting plate 200 and feed source device 300 when in use to base 100, and carry
When reflecting plate 200 and feed source device 300 are disassembled from base 100, so as to be convenient for carrying.Can adjust when carrying
Section feed source device 300 and and the angle between reflecting plate 200 to minimum.And scalable reflecting plate 200 and base when use
Angle between 100, makes the signal reception of satellite to most preferably.Improve the performance of the Portable satellite aerial.
It is further to note that the angle between reflecting plate 200 and base 100 refers to the edge plane of reflecting plate 200
With the angle between the plane of base 100.And the plane of base 100 is flat with horizontal plane or ground when satellite antenna is used
OK.Angle between the feed source device 300 and base 100 refers to that feed source device 300 is connected to base 100 by junction point
When upper, feed source device 300 being capable of the angle that rotates upwardly and downwardly of the plane of respect thereto 100.Equally, reflecting plate 200 also can be the bottom of with respect to
100 planes of seat rotate upwardly and downwardly move angle.
Wherein in one embodiment, as shown in Fig. 2 reflecting plate 200 is circular configuration, a diameter of 0.4 meter, it is antenna
One of core component of reflector sections.In the present embodiment, all many factors such as comprehensive collection assembling and manufacturing process, this
In embodiment, 200 points of reflecting plate is four pieces of designs, and piecemeal size reasonable, each piecemeal adopts buckle type rapid and convenient assembling method,
Mechanism's design science.The material of main part of reflecting plate 200 selects carbon fiber, and face plate center molding thickness is 1.5 millimeters, and panel periphery is thick
Spend for 7 millimeters.This structure is effectively increased the bulk strength of panel, reduces the process-cycle.So as to reduce the system of reflecting plate 200
Make cost, so as to reduce the cost of the Portable satellite aerial of the present embodiment on the whole.
Referring to Fig. 2 and Fig. 3, in the Portable satellite aerial of the present embodiment, reflecting plate 200 and feed source device 300 pass through
Intermediate member connecting seat 400 is connected with base 100.Wherein, connecting seat 400 includes support column 410 and connecting shaft 420.Support column
410 one end are detachably connected with base 100, and the other end connects connecting shaft 420 by connecting hole.In the present embodiment, support column 410
Into 90 jiaos between connecting shaft 420.When satellite antenna is used, the support column 410 is arranged perpendicular to the ground, so as to pass through the company
The horizontal support reflecting plate 200 of spindle 420 and feed source device 300.Specifically, reflecting plate 200 is by support column 410 and connecting shaft
420 rotate connection, and feed source device 300 is rotated with connecting shaft 420 by feed support bar 310 and is connected.
In the present embodiment, generally one non-dismountable structure of reflecting plate 200 and feed source device 300 and connecting seat 400, but
It is that reflecting plate 200 and feed source device 300 can be rotated relative to the connecting shaft on the connecting seat 400.As shown in fig. 6, work as taking
When band, together with reflecting plate 200 and feed source device 300 are turned folding around connecting shaft 420.Especially feed source device 300
The concave internal of reflecting plate 200 is folded into, saving takes up room, and makes satellite antenna easily portable.
Specifically, referring to Fig. 3, support column 410 is overall to be integrally formed, and bottom is cylindrical structural, and support column 410 is upper
Portion both sides ream, and make top into platy structure, are easily installed and fixed connection shaft 420.
Further, the lower interior portion of support column 410 makes hollow structure, that is, be internally formed a groove, referred to as bottom
End link slot.Connecting seat 400 is detachable with base 100 by the bottom link slot of the bottom of support column 410, is rotatably connected.Phase
Answer, in order to be connected with connecting seat 400, base 100 is provided with accordingly base post 110.When connection connecting seat 400 and base
When 100, base post 110 is placed in the link slot of bottom.
Wherein in one embodiment, for fixed connecting base 400 and base 100, in the bottom link slot of support column 410
Outside is additionally provided with orientation locking device.When the Portable satellite aerial of the present embodiment is installed, the post of base 100 is placed into and is propped up
After in the bottom link slot of dagger 410, the side for rotating the unitary rotation reflecting plate 200 of connecting seat 400 and feed source device 300 can be passed through
Position.Adjusting can be by the orientation locking device fixed connecting base 400, so as to anti-to satellite after the orientation of reflecting plate 200
Penetrate the orientation of plate 200 to be fixed, keep signal stabilization.
Referring to Fig. 3, as a kind of embodiment, just arrange described by the way of the first knob 4213 shown in Fig. 3
Orientation locking device.First knob 4213 is connected with rotary screw, and by rotary screw the base of seat 400 and inside is in clamping connection
Post 110, so as to the reflecting plate 200 of fixed satellite antenna.
In other embodiments, it is also possible to by arranging the side such as buckle for matching on base post 110 and support column 410
Formula fixed connecting base 400 and base 100.
Referring to Fig. 3, further, support column 410 is arranged on the middle part of connecting shaft 420, by midfoot support connecting shaft
420.Connection or the bracing frame 210 for supporting the reflecting plate 200 are two, rotatable installed in the two of connecting shaft respectively
End, at 423 positions as shown in Figure 3.And feed connecting portion 424 is additionally provided with connecting shaft 420, feed source device 300 leads to
Cross feed support bar 310 and connect the feed connecting portion 424 so as to reach the purpose that feed source device is connected to connecting seat 400.
The feed connecting portion 424 is also two, is separately positioned on the outside of bracing frame 210.The two ends of connecting shaft 420 are provided with fixation
Termination, for playing fixation, prevents feed connecting portion 424 from moving.
In relatively middle position, pitching locking device and pitching micromatic setting are additionally provided with connecting shaft.Referring to Fig. 3,
Pitching locking device, including first sleeve 4211, the second sleeve pipe 4212 and the second knob 4213.4211 sets of first sleeve is penetrated even
In spindle 420, the second 4212 sets of sleeve pipe is penetrated in the outside of the one end of first sleeve 4211, is partly overlapped with first sleeve 4211.When
During rotating second knob 4213, first sleeve 4211 is moved to the left, and is consolidated by extruding bracing frame 210 and feed connecting portion 424
Determine feed connecting portion 424 and bracing frame 210.I.e., it is possible to be adjusted by the pitching locking device and fixing support rack and feed
Relative position between support bar and connecting shaft.
It should be noted that referring to Fig. 1, it will be understood by those skilled in the art that when bracing frame 210 and feed support bar
310 relative to the connecting shaft 420 rotate when, the angle of pitch of reflecting plate 200 and feed source device 300, especially reflecting plate 200 are bowed
The elevation angle can change, therefore, by limiting bracing frame 210 and the relative position between feed support bar 310 and connecting shaft 420
The angle of pitch of fixation reflex plate 200 can be played a part of.Can be by adjusting loose pitching locking when needing so as to reach
Device adjusts the angle of pitch of reflecting plate 200, and is further stably received by locking the device after the angle of pitch is adjusted
Satellite-signal, it is ensured that the stability of the signal of the portable satellite nature.
For the pitching micromatic setting, referring to Fig. 3, including the 3rd sleeve pipe 4221, the first fixing axle 4222, the second fine setting
Axle 4223 and the part of the 3rd knob 4,224 4 constitute.4221 sets of 3rd sleeve pipe is penetrated at the middle part of the connecting shaft 420, described
First fixing axle 4222 is fixedly connected with the 3rd sleeve pipe 4221, second fine adjustment shaft 4223 and first fixing axle
4222 are rotatably connected.Fix can second fine adjustment shaft 4223 relatively described first by rotating the 3rd knob 4224
Axle 4222 is rotated clockwise or counterclockwise, and so as to drive support frame as described above 210 to rotate with feed connecting portion 424, reaches fine setting
The purpose of the angle of pitch of the reflecting plate 200.
It should be noted that the Main Function of the pitching micromatic setting is in the reflection for substantially adjusting reflecting plate 200
After angle the angle of pitch of reflecting plate 200 is finely adjusted when needing.So, in the present embodiment, it is provided with described micro-
Adjust the scope of device angle of pitch fine setting, set its can in certain angle, i.e. the first preset range, interior regulation bracing frame 210 and
Inclination angle between feed support bar 310 and base 100, so as to reach the adjustment reflection angle of reflecting plate 200 within the specific limits
Effect.
It also should be noted that, two bracing frames 210 are separately positioned on the two ends of connecting shaft in the present embodiment, two
Individual feed connecting portion 424 is also set, respectively on the two ends of connecting shaft 420.It can improve reflecting plate 200 and feed source device 300
The stability of support.But in other embodiments, bracing frame 210, feed connecting portion 424, pitching fine setting dress can be flexibly set
Put and orientation locking device position.Or can also omit the setting pitching micromatic setting.For the quantity of bracing frame,
In other enforcements, it is also possible to arrange a bracing frame 210, and the one end being connected with reflecting plate 200 in bracing frame 210 arranges and divides
Fork structure is in order to stabilize make the reflecting plate 200.Certainly, discounting for cost requirement, it is also possible to arrange multiple, such as arrange
Three the above bracing frames, for stably supporting the reflecting plate 200.
Wherein in one embodiment, referring to Fig. 4, feed support bar 310 includes fixed part 311 and connecting rod 312.Fixed part
311 one end for being connected to connecting rod 312, and be connected calmly with feed connecting portion in connecting shaft 420 solid 424 by the fixed part 311,
And feed connecting portion 424 is rotatably connected with connecting shaft 420.And the other end of the connecting rod 312 of feed support bar 310 is provided with cunning
Groove 3121, feed source device 300 is connected by feed seat with the matching of chute 3121.Referring to Fig. 1, slide when Portable satellite aerial works
Groove is horizontal.Specifically, referring to Fig. 2, the feed seat bottom being connected with feed support bar 310 in feed source device 300 sets
Be equipped with prominent bar, for being placed into the chute in.
Further, referring to Fig. 2, wherein in one embodiment, setting support frame as described above 210 be arcuate structure, one
End rotates with connecting shaft and is connected, and the other end is arranged on the another side of reflecting plate 200 and the opposite face of feed source device 300.Arc is tied
The bracing frame of structure matches with the arcuate structure of reflecting plate 200, when it is more stable to making for reflecting plate 200.
For the base 100 of Portable satellite aerial, referring to Fig. 5, wherein in one embodiment, base 100 includes bottom
Seat pillar 110, the collar 120, cradling piece 130 and expansion link 140.Wherein, 120 sets of the collar is penetrated on the post of base 100, and the collar 120
Can the post of respect thereto 100 slide up and down, and can respect thereto post 110 rotate；Cradling piece 130 and the foldable company of the collar 120
Connect；The one end of expansion link 140 and the foldable connection in the bottom of base post 110, the other end and the slidable connection of cradling piece 130.
Wherein, the cradling piece 130 refers to the foldable connection of the collar 120, referring to Fig. 6, cradling piece 130 and the collar 120
After folding, cradling piece 130 can fit with base post 110, or can be parallel with base post 110, so as to occupy minimum sky
Between.Equally, expansion link 140 also the main body bottom can be folded relatively, so as to be merged into the same axis of the base post 110
On, or closely arrange around same axis.
It is pointed out that the expansion link 140 can be free when the cradling piece 130 launches or folds
It is flexible, so as to coordinate the cradling piece to complete the expansion or folding of base.And referring to Fig. 5, be provided with the expansion link 140
Lock valve, when the stent is opened, can fix support frame as described above, it is ensured that portable satellite day by the locking lock valve
The supporting role of line base 100.
More preferably, referring to Fig. 5, the end of the cradling piece 130 is additionally provided with WidFin structure, for respectively to each
The height of cradling piece 130 is adjusted the horizontality for ensureing satellite nature.In order to ensure the effect of horizontal adjustment, can be with base
Spirit bubble 150 is installed, to check horizontal adjustment effect when horizontal adjustment on post 110.
Wherein, the cradling piece 130 and expansion link 140 of base 100 can be made by aluminum alloy materials.And miscellaneous part can be by
Stainless steel material is made.Whole device is lighter and handier.
Originally be embodiment Portable satellite aerial the deployment diameter of base 100 be 935 millimeters, a height of 152 millimeters, effectively
Reduce the height of C.G. of antenna.
The base 100 of the present embodiment includes the supporting expansion link 140 of three cradling pieces 130 and three.Each two cradling piece
130 in the horizontal direction between angle be 60 degree, the structure ensure that base 100 support stability.Certainly, at other
In embodiment, it is also possible to which greater number of cradling piece 130 and expansion link 140 are set.
More preferably, wherein in one embodiment, also set has penetrated azimuth vernier adjusting device on base post 110, it is adaptable to the
The rotational angle of connecting seat 400 is adjusted in two preset ranges.
The Portable satellite aerial of the present invention, after depletion region launches, installs feed source device 300, LNB (Low
Noise Block, tuner) and power amplifier, go out the substantially luffing angle and orientation angles of antenna alignment satellite using lining,
Star finder is correctly connected with LNB, antenna pitching and orientation angles are finely tuned, and satellite is accurately aimed at using star finder.It is directed at it
Star finder can be pulled down afterwards, and connect corresponding rear end modulation /demodulation equipment, you can what realization was communicated by satellite
Function.Whole device adopts Split type structure, and collection small volume (after folding, 518 millimeters of total length, 107 millimeters of height), weight
Gently, quite convenient for carrying.
Part in various embodiments above, in the case where not conflicting can combination in any, in the scope of protection of the invention
It is interior.
Although illustrating and describing the disclosure with reference to the various embodiments of the disclosure, those skilled in the art will manage
Solution, in the case of without departing from the spirit and scope of the present disclosure being defined by the appended claims and the equivalents thereof, can enter to it
Various changes in row form and details.
Claims (11)
1. a kind of Portable satellite aerial, it is characterised in that include：
Base；
The reflecting plate being detachably connected with the base, the angle scalable between the reflecting plate and the base, and it is described
Reflecting plate is made up of carbon fibre material；
The feed source device being detachably connected with the base, the angle scalable between the feed source device and the base, and
The phase that angle is adjusted between feed source device and the reflecting plate adjusted between the feed source device and the base can be passed through
To position.
2. Portable satellite aerial as claimed in claim 1, it is characterised in that also include being detachably connected with the base
Connecting seat；The reflecting plate and the feed source device are connected by the connecting seat with the base；
The connecting seat includes support column and connecting shaft；
Described support column one end is detachably connected with the base, and the other end connects the connecting shaft by connecting hole；
The reflecting plate is rotated by bracing frame and the connecting shaft and be connected, the feed source device pass through feed support bar with it is described
Connecting shaft rotates connection.
3. Portable satellite aerial according to claim 2, it is characterised in that the support column by bottom link slot with
The base post of base is rotatably connected.
4. Portable satellite aerial according to claim 3, it is characterised in that orientation locking is provided with the support column
Device, the orientation locking device is arranged on the outside of the bottom link slot, it is adaptable to the fixation connecting seat and base post
Between relative position.
5. Portable satellite aerial according to claim 2, it is characterised in that pitching locking is provided with the connecting shaft
Device and/or pitching micromatic setting；
The pitching locking device, it is adaptable to fixed support frame as described above and the phase between the feed support bar and the connecting shaft
To position；
The pitching micromatic setting, it is adaptable to support frame as described above and the feed support bar and bottom are adjusted in the first preset range
Angle of inclination between seat.
6. Portable satellite aerial according to claim 2, it is characterised in that described feed support bar one end is by fixing
Portion is fixedly connected with feed connecting portion in the connecting shaft, and the feed connecting portion is rotatably connected with the connecting shaft；
The other end of the feed support bar is provided with chute, and the feed source device matches company by feed seat with the chute
Connect；And the chute is horizontal during the Portable satellite aerial work.
7. Portable satellite aerial according to claim 2, it is characterised in that support frame as described above is arcuate structure, one end
Rotate with the connecting shaft and be connected, the other end is arranged on the reflecting plate and the another side of the feed source device opposite face.
8. Portable satellite aerial according to claim 1, it is characterised in that the base include base post, the collar,
Hack lever and expansion link；
The set ring set is penetrated on the base post, and the collar can relatively described base post slide up and down, and being capable of phase
The base post is rotated；
The cradling piece and the foldable connection of the collar；
Described expansion link one end and the foldable connection in the base post bottom, the other end and the cradling piece slidable connection.
9. Portable satellite aerial according to claim 8, it is characterised in that the cradling piece and the expansion link are by aluminum
Alloy material is made.
10. Portable satellite aerial according to claim 3, it is characterised in that also set has penetrated orientation on the base post
Micromatic setting, it is adaptable to the rotational angle of the connecting seat is adjusted in the second preset range.
11. Portable satellite aerials according to claim 1, it is characterised in that the reflecting plate be circular configuration, diameter
For 0.4 meter, core molding thickness is 1.5 millimeters, and edge thickness is 7 millimeters.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610958856.9A CN106602203A (en) | 2016-11-03 | 2016-11-03 | Portable satellite antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610958856.9A CN106602203A (en) | 2016-11-03 | 2016-11-03 | Portable satellite antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106602203A true CN106602203A (en) | 2017-04-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610958856.9A Pending CN106602203A (en) | 2016-11-03 | 2016-11-03 | Portable satellite antenna |
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| CN (1) | CN106602203A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106990516A (en) * | 2017-05-26 | 2017-07-28 | 上海微小卫星工程中心 | Satellite-borne laser communication wide-angle pointing device |
| CN107655316A (en) * | 2017-08-30 | 2018-02-02 | 西安普腾电子科技有限公司 | A kind of system for drying grain during procedure of storing grain using radiation field of aerial |
| CN110212994A (en) * | 2019-06-25 | 2019-09-06 | 上海剀蕊得信息科技有限公司 | A kind of detection device of wireless telecom equipment |
| CN111799542A (en) * | 2020-06-28 | 2020-10-20 | 北京爱科迪通信技术股份有限公司 | Emergency communication satellite antenna |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101666235A (en) * | 2009-10-19 | 2010-03-10 | 三一集团有限公司 | Installation auxiliary device for arc beam |
| CN201994402U (en) * | 2011-02-24 | 2011-09-28 | 北京波尔通导科技有限公司 | Automatically folding-supporting frame |
| CN102683886A (en) * | 2012-04-28 | 2012-09-19 | 深圳光启创新技术有限公司 | Portable satellite antenna and satellite antenna receiving system |
| CN203813027U (en) * | 2014-04-16 | 2014-09-03 | 厦门九华通信设备厂 | Satellite antenna control rotary table |
| CN105406163A (en) * | 2015-12-15 | 2016-03-16 | 无锡华信雷达工程有限责任公司 | Single-personal portable antenna |
-
2016
- 2016-11-03 CN CN201610958856.9A patent/CN106602203A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101666235A (en) * | 2009-10-19 | 2010-03-10 | 三一集团有限公司 | Installation auxiliary device for arc beam |
| CN201994402U (en) * | 2011-02-24 | 2011-09-28 | 北京波尔通导科技有限公司 | Automatically folding-supporting frame |
| CN102683886A (en) * | 2012-04-28 | 2012-09-19 | 深圳光启创新技术有限公司 | Portable satellite antenna and satellite antenna receiving system |
| CN203813027U (en) * | 2014-04-16 | 2014-09-03 | 厦门九华通信设备厂 | Satellite antenna control rotary table |
| CN105406163A (en) * | 2015-12-15 | 2016-03-16 | 无锡华信雷达工程有限责任公司 | Single-personal portable antenna |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106990516A (en) * | 2017-05-26 | 2017-07-28 | 上海微小卫星工程中心 | Satellite-borne laser communication wide-angle pointing device |
| CN106990516B (en) * | 2017-05-26 | 2020-10-02 | 上海微小卫星工程中心 | Satellite-borne laser communication wide-angle pointing device |
| CN107655316A (en) * | 2017-08-30 | 2018-02-02 | 西安普腾电子科技有限公司 | A kind of system for drying grain during procedure of storing grain using radiation field of aerial |
| CN110212994A (en) * | 2019-06-25 | 2019-09-06 | 上海剀蕊得信息科技有限公司 | A kind of detection device of wireless telecom equipment |
| CN111799542A (en) * | 2020-06-28 | 2020-10-20 | 北京爱科迪通信技术股份有限公司 | Emergency communication satellite antenna |
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