WO2017084403A1 - Antenne parabolique rotative de communication par satellite portable - Google Patents

Antenne parabolique rotative de communication par satellite portable Download PDF

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Publication number
WO2017084403A1
WO2017084403A1 PCT/CN2016/096965 CN2016096965W WO2017084403A1 WO 2017084403 A1 WO2017084403 A1 WO 2017084403A1 CN 2016096965 W CN2016096965 W CN 2016096965W WO 2017084403 A1 WO2017084403 A1 WO 2017084403A1
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WO
WIPO (PCT)
Prior art keywords
antenna
positioning
fixing portion
movable portion
guiding
Prior art date
Application number
PCT/CN2016/096965
Other languages
English (en)
Chinese (zh)
Inventor
刘武丰
赵术开
邱进会
Original Assignee
深圳市华讯方舟卫星通信有限公司
华讯方舟科技有限公司
Priority date (The priority date 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 date listed.)
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Publication date
Application filed by 深圳市华讯方舟卫星通信有限公司, 华讯方舟科技有限公司 filed Critical 深圳市华讯方舟卫星通信有限公司
Publication of WO2017084403A1 publication Critical patent/WO2017084403A1/fr

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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
    • H01Q1/20—Resilient mountings
    • 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
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/12—Supports; Mounting means
    • H01Q1/125—Means for positioning
    • H01Q1/1257—Means for positioning using the received signal strength

Definitions

  • the invention relates to a satellite communication antenna, in particular to a portable satellite communication rotary parabolic antenna.
  • the satellite communication rotating parabolic antenna There are two functions of the satellite communication rotating parabolic antenna: the first is to reflect the microwave signal transmitted from the communication satellite to the feed and the high frequency head located at the focus to complete the signal receiving function; the second is to transmit the earth station high power amplifier.
  • the radio frequency signal is electromagnetically transformed into a free-space propagating microwave signal and transmitted to a designated satellite to complete the transmitting function.
  • the main indicators for measuring the performance of satellite communication antennas are transmission and reception gain, transmission and reception efficiency, noise temperature, and radiation characteristics. The accuracy of the antenna directly affects the pros and cons of these indicators.
  • the antenna is divided into a fixed antenna, a portable antenna, a vehicle antenna, and the like according to different usage scenarios.
  • the portable satellite communication antenna in the industry mainly adopts a splicing type, that is, the main surface of the antenna is divided into several pieces, which are spliced before use, and then disassembled and assembled after the communication is completed.
  • the existing portable satellite communication rotating parabolic antenna is convenient for carrying, and the rotating parabolic antenna 1 is usually spliced.
  • the parabolic antenna 1 is constructed by splicing one antenna fixing portion 1-1 and three movable portions 1-2.
  • the parabolic antenna 1 is constructed by splicing one antenna fixing portion 1-1 and five movable portions 1-2.
  • the diameter of the antenna is usually below 1.2 meters. Due to the multiple splicing, it takes more time and is not convenient to install and use, and the accuracy of the antenna reflecting surface will be worse with the increase of the splicing surface, and the mechanical performance will be correspondingly reduced, which directly affects the transmission and reception efficiency of the antenna and the antenna. Radiation performance, as well as wind resistance.
  • the technical problem to be solved by the present invention is to provide a portable satellite communication rotating parabolic antenna, which is not only convenient to carry, but also convenient and quick to install and withdraw, and the production precision of the antenna surface is guaranteed, and the signal of the antenna is ensured. Transceiver performance is good.
  • the present invention provides a portable satellite communication rotating parabolic antenna, comprising a rotating parabolic antenna, the rotating parabolic antenna is formed by splicing and combining an antenna fixing portion and an antenna moving portion, and the antenna fixing portion has one. There is one antenna movable portion, and the antenna movable portion and the antenna fixing portion are fixedly connected by a connecting member.
  • the antenna fixing portion and the antenna movable portion are mirror-symmetrical with respect to the splicing surface, and the splicing surface is a plane where the splicing seam between the antenna fixing portion and the antenna movable portion is located, the rotating paraboloid The axis of the antenna is located within the splice face.
  • a line intersecting the splicing surface with the aperture surface of the rotating parabolic antenna is parallel to the horizontal plane.
  • the connecting member includes a positioning connecting member and/or a fixed connecting member.
  • the positioning connecting component is a rotating positioning component
  • the rotating positioning component includes a positioning shaft seat, and a front end of the positioning shaft seat is fixedly connected to an outer bottom surface of the antenna fixing portion by an extension connecting fixing component, and the positioning shaft seat is biased Placed behind the outer bottom surface of the antenna movable portion a positioning rotating shaft is disposed in the shaft hole of the positioning shaft seat, and the positioning rotating shaft can rotate in the shaft hole of the positioning shaft seat or reciprocate along the axial direction of the shaft hole, Positioning the rotating shaft parallel to the axis of the rotating parabolic antenna, the front end of the positioning rotating shaft is fixedly connected with the outer bottom surface of the movable portion of the antenna, the rear end of the positioning rotating shaft is provided with a handle, and the fixed connecting component is And a plurality of the fastening buckles, wherein the plurality of the fastening buckles are fixedly connected along the longitudinal direction of the splicing seam to fix the outer surface of the antenna fixing portion and the outer surface of the antenna movable portion.
  • the positioning shaft seat has a cylindrical shape, and a front side wall of the positioning shaft seat is provided with a guiding long gap along a length direction of the positioning shaft seat, and the guiding long gap has a depth greater than the antenna movable portion.
  • the side surface of the positioning rotating shaft is provided with a guiding block, and when the antenna fixing portion and the antenna movable portion are oppositely connected, the guiding block is located at the bottom of the guiding long slit; or
  • the sidewalls of the positioning shaft seat are respectively provided with axial grooves at two ends of the same diameter, wherein one axial groove is long and is an axial guiding groove, and the length of the axial guiding groove is greater than the antenna activity
  • the thickness of the bottom surface of the portion, the other groove is short, is a fixing groove, the length of the fixing groove is larger than the axial length of the guiding block, and the front end of the axial guiding groove and the front end of the fixing groove pass a semicircle
  • the circumferential guide is connected to the slot, and the guiding block reciprocates in the axial guiding groove, the circumferential guiding groove and the fixing groove in sequence, and when the antenna fixing portion and the antenna movable portion are in contact with each other, the guiding The block is located at the rear end of the axial guide groove.
  • Balls are disposed on the rear end surface of the guide block.
  • a side of the guiding long slit is provided with a spring ball braking member for preventing free movement of the guiding block, and/or a rear portion of the positioning rotating shaft is sleeved with a compression return spring, and the compression return spring is located at the Between the rear end of the positioning shaft seat and the handle.
  • the front side wall of the positioning shaft seat is provided with a fixed short gap along the length direction of the positioning shaft seat, and the fixed short gap is located on the same diameter as the guiding long gap, and the length of the fixed short gap is larger than
  • the axial length of the guide block, the side surface in the fixed short gap is provided with a spring ball brake member that prevents the guide block from freely moving.
  • the positioning connecting component is a hinge positioning component, and the hinge positioning component has two ends, and two ends of the antenna movable portion are respectively hinged with two ends of the antenna fixing portion by two hinge positioning components, the fixing
  • the connecting member is a fastening buckle, and the fastening buckle has a plurality of the fastening buckles distributed along the length direction of the splicing slit to the outer surface of the antenna fixing portion and the antenna movable portion The outer surfaces are fixedly connected together; or,
  • the positioning connecting component is a chuck positioning component, the chuck positioning component has a plurality of, and the plurality of chuck positioning components are divided into two groups, and a set of the chuck positioning components are distributedly disposed in the antenna activity.
  • a seam is disposed on the joint surface of the antenna fixing portion, and another set of the chuck positioning members are disposed on the half circumference of the movable portion of the antenna.
  • the antenna fixing portion has a bayonet distributed on the half circumference of the aperture
  • the fixed connecting component is a fastening buckle
  • the fastening buckle has a plurality of the fastening buckles. Fixing the outer surface of the antenna fixing portion and the outer surface of the antenna movable portion together along the length direction of the splicing seam; or
  • the positioning connecting component is a chuck positioning component, the chuck positioning component has a plurality of, and the plurality of chuck positioning components are divided into two groups, and a set of the chuck positioning components are distributedly disposed on the antenna.
  • a joint surface of the portion correspondingly, a joint surface of the movable portion of the antenna
  • a bayonet is disposed in a distributed manner, and another set of the chuck positioning members is disposed on the half circumference of the aperture of the antenna fixing portion.
  • a bayonet is disposed on the half circumference of the antenna movable portion.
  • the fixed connecting component is a fastening buckle
  • the fastening buckle has a plurality of the fastening buckles distributed along the length direction of the splicing seam to the outer surface of the antenna fixing portion and the The outer surfaces of the movable parts of the antenna are fixedly connected together.
  • the portable satellite communication rotating parabolic antenna of the present invention has the following advantageous effects as compared with the prior art.
  • the technical solution adopts the technical means that the movable part of the antenna and the fixed part of the antenna are fixedly connected by a connecting component, so that it is not only convenient to carry, but also installed and removed. Convenient and fast, the production accuracy of the antenna surface is guaranteed, and the signal transmission and reception performance of the antenna is good.
  • the present invention adopts the antenna fixing portion and the antenna movable portion to be mirror-symmetrical with respect to the splicing surface, and the splicing surface is a splicing seam between the antenna fixing portion and the antenna movable portion.
  • the plane in which the rotating parabolic antenna is located is located in the splicing plane, so that it is advantageous to reduce the space occupied by the portable satellite communication rotating parabolic antenna, and is more convenient to carry.
  • the technical solution adopts the technical method that the straight line intersecting the aperture surface of the rotating parabolic antenna is parallel to the horizontal plane, so that the height of the portable satellite communication rotating parabolic antenna can be minimized, and the most convenient to carry. .
  • the connecting member includes a technical means for positioning the connecting member and/or fixing the connecting member, the antenna movable portion and the antenna fixing portion can be fixed together in various ways.
  • the present invention adopts the positioning connecting component as a rotating positioning component
  • the rotating positioning component includes a positioning shaft seat, and the front end of the positioning axle seat is fixed to the outer bottom surface of the antenna fixing portion by extending the connecting fixing component.
  • the positioning shaft seat is offset behind the outer bottom surface of the movable portion of the antenna, and a positioning rotating shaft is disposed in the shaft hole of the positioning shaft seat, and the positioning rotating shaft can be in the shaft hole of the positioning shaft seat
  • the inner rotation can also reciprocate along the axial direction of the shaft hole, the positioning rotation axis is parallel to the axis of the rotating parabolic antenna, and the front end of the positioning rotation shaft is fixedly connected with the outer bottom surface of the antenna movable portion.
  • a rear end of the positioning rotating shaft is provided with a handle
  • the fixed connecting component is a plurality of fastening buckles
  • the plurality of fastening buckles are distributed along the length direction of the splicing seam to the outside of the antenna fixing portion
  • the technical solution adopts the shape of the positioning shaft seat to be cylindrical, and the front side of the side wall of the positioning shaft seat is provided with a guiding long gap along the length direction of the positioning shaft seat, and the guiding long gap
  • the depth of the antenna is greater than the thickness of the bottom of the movable portion of the antenna.
  • the side of the positioning rotating shaft is provided with a guiding block.
  • axial grooves are provided, wherein one axial groove is long, which is an axial guiding groove, and the length of the axial guiding groove is greater than the length
  • the thickness of the bottom surface of the antenna movable portion, and the other groove is short, which is a fixing groove
  • the length of the fixing groove is larger than the axial length of the guiding block, and the front end of the axial guiding groove and the front end of the fixing groove are communicated by a semicircular circumferential guiding groove, and the guiding block is sequentially in the axial direction Reciprocating movement in the guiding groove, the circumferential guiding groove, and the fixing groove.
  • the technical solution adopts the technical means that the ball is disposed on the rear end surface of the guiding block, so that the guiding block moves in the circumferential direction on the front end surface of the positioning shaft seat, and the guide block is also guided in the circumferential direction. Movement in the tank.
  • the technical solution adopts the technical means that the side of the guiding long gap is provided with a spring ball brake component for preventing the free movement of the guiding block, so that the length of the guiding block along the positioning shaft seat can be prevented. Free movement in direction.
  • the rear portion of the positioning rotating shaft is sleeved with a compression return spring, and the compression return spring is located between the rear end of the positioning shaft seat and the handle, the same can be prevented.
  • the guide block is free to move along the length of the positioning shaft seat.
  • the front side wall of the positioning shaft seat is provided with a fixed short gap along the length direction of the positioning shaft seat, and the fixed short gap is located on the same diameter as the guiding long gap.
  • the length of the fixed short slit is larger than the axial length of the guide block, and the side surface of the fixed short gap is provided with a technical means for preventing the spring ball brake member from freely moving the guide block, so that the effective prevention can be effectively prevented.
  • the guide block is free to move along the circumferential direction of the positioning shaft seat.
  • the technical solution adopts the positioning connecting component as a hinge positioning component, and the hinge positioning component has two, and two ends of the movable portion of the antenna pass through the two hinge positioning components and the antenna fixing portion respectively.
  • the two ends are hinged
  • the fixed connecting component is a fastening buckle
  • the fastening buckle has a plurality of the fastening buckles distributed along the length direction of the splicing seam to fix the antenna fixing portion
  • the technical means of the outer surface and the outer surface of the movable portion of the antenna are fixedly connected, so that it is advantageous to protect the reflecting surface of the antenna.
  • the positioning connecting component is a chuck positioning component
  • the chuck positioning component is plural, and the plurality of chuck positioning components are divided into two groups, and a set of the chuck positioning components are distributedly disposed in the
  • a seam is disposed on the joint surface of the antenna fixing portion, and another set of the chuck positioning members are disposed at a semicircle of the antenna movable portion.
  • a bayonet is disposed on the half circumference of the antenna fixing portion
  • the fixed connecting member is a fastening buckle
  • the fastening buckle has a plurality of the fastening portions.
  • the positioning connecting component is a chuck positioning component
  • the chuck positioning component is plural, and the plurality of chuck positioning components are divided into two groups, and a set of the chuck positioning components are distributedly disposed in the
  • a seam is disposed on the joint surface of the antenna movable portion
  • another set of the chuck positioning members are disposed at a semicircle of the antenna fixing portion.
  • a bayonet is disposed on the semicircle of the antenna movable portion.
  • the fixed connecting member is a fastening buckle, and the fastening buckle has a plurality of the fastening.
  • FIG. 1 is a schematic structural view of a first portable satellite communication rotating parabolic antenna in the prior art.
  • FIG. 2 is a schematic structural view of a second portable satellite communication rotating parabolic antenna in the prior art.
  • FIG. 3 is a schematic side view showing the structure of a first portable satellite communication rotating parabolic antenna in an installed state according to an embodiment of the present invention.
  • FIG. 4 is a schematic view showing the structure of the A direction in FIG.
  • FIG. 5 is a schematic side view showing the structure of the first portable satellite communication rotating parabolic antenna in the state after the withdrawal according to the embodiment of the present invention.
  • FIG. 6 is a schematic exploded view of another positioning shaft seat of FIG. 1.
  • FIG. 6 is a schematic exploded view of another positioning shaft seat of FIG. 1.
  • FIG. 7 is a side view showing a second portable satellite communication rotating parabolic antenna in a state after installation according to an embodiment of the present invention.
  • FIG. 8 is a side view showing a second portable satellite communication rotating parabolic antenna in a state after being retracted according to an embodiment of the present invention.
  • FIG. 9 is a schematic side view showing the structure of a third portable satellite communication rotating parabolic antenna in an installed state according to an embodiment of the present invention.
  • FIG. 10 is a schematic side view showing the structure of a third portable satellite communication rotating parabolic antenna according to an embodiment of the present invention.
  • a portable satellite communication rotating parabolic antenna provided by the present embodiment includes a rotating parabolic antenna 1 which is spliced by an antenna fixing portion 1-1 and an antenna movable portion 1-2.
  • the antenna fixing portion 1-1 has one, and the antenna movable portion 1-2 has one.
  • the antenna movable portion 1-2 and the antenna fixing portion 1-1 are fixedly connected by a connecting member. .
  • the antenna fixing portion 1-1 is fixedly connected to the base (4).
  • the antenna movable portion 1-2 and the antenna fixing portion 1-1 are made of a metal material (which can also be made of glass fiber), and are required to be designed according to the curvature of the parabolic antenna to ensure that after the two pieces are completed, they can be combined. Become a complete parabolic antenna.
  • the antenna movable portion since the antenna movable portion is used, the antenna movable portion and the antenna fixing portion are fixedly connected by a connecting member, so that it is not only convenient to carry, but also convenient for installation and withdrawal. Fast, the production accuracy of the antenna surface is guaranteed, and the signal transmission and reception performance of the antenna is good.
  • the antenna fixing portion 1-1 and the antenna movable portion 1-2 are mirror-symmetrical with respect to a splicing surface, and the splicing surface is the A plane in which the splicing seams between the antenna fixing portion 1-1 and the antenna movable portion 1-2 are located, and an axis of the rotating parabolic antenna 1 is located in the splicing plane.
  • the antenna fixing portion and the antenna moving portion are mirror-symmetrical with respect to the splicing surface, and the splicing surface is a splicing seam between the antenna fixing portion and the antenna moving portion.
  • the plane, the axis of the rotating parabolic antenna is located in the splicing plane, so that it is advantageous to reduce the space occupied by the portable satellite communication rotating parabolic antenna, and is more convenient to carry.
  • a straight line intersecting the splicing surface with the caliper surface of the rotating parabolic antenna 1 is parallel to the horizontal plane.
  • the height of the portable satellite communication rotating parabolic antenna can be minimized, and the most convenient for carrying.
  • the connecting member may be a positioning connecting member or a fixed connecting member.
  • the connecting means includes a technique of positioning the connecting member and/or fixing the connecting member, the antenna movable portion and the antenna fixing portion can be fixed together in various ways.
  • the positioning connecting member is a rotary positioning member 2
  • the rotary positioning member 2 includes a positioning shaft seat 2-1, and the positioning shaft seat 2
  • the front end of the -1 is fixedly connected to the outer bottom surface of the antenna fixing portion 1-1 by the extension connecting fixing member 2-9, and the positioning shaft base 2-1 is offset from the outer bottom surface of the antenna movable portion 1-2.
  • a positioning rotating shaft 2-2 is disposed in the shaft hole of the positioning shaft seat 2-1, and the positioning rotating shaft 2-2 can rotate in the shaft hole of the positioning shaft seat 2-1, and can also be along The axial direction of the shaft hole reciprocates, the positioning rotating shaft 2-2 is parallel to the axis of the rotating parabolic antenna 1, the front end of the positioning rotating shaft 2-2 and the outer bottom surface of the antenna movable portion 1-2 A fixed connection is provided, and a rear end of the positioning rotary shaft 2-2 is provided with a handle 2-3.
  • the handle 2-3 is a plum-shaped handle.
  • the fixed connecting member is a plurality of fastening buckles 3, and the plurality of the fastening buckles 3 are distributed along the length direction of the splicing slit to the outer surface of the antenna fixing portion 1-1 and the antenna movable portion 1-2 outer surface solid Be sure to connect together.
  • the handle When the portable satellite communication rotating parabolic antenna is in the retracted state (see FIG. 5), the handle is first rotated for 2-3 weeks, and then the handle 2-3 is pulled back to make the antenna movable portion 1-2 and the antenna fixing portion. The 1-1 is butted, and then the antenna movable portion 1-2 and the antenna fixing portion 1-1 are fixed together by the fastening buckle 3, so that the portable satellite communication rotating parabolic antenna is in use.
  • the handle 2-3 is pushed forward, and then the handle is turned 2-3 for a half cycle, so that the antenna movable portion 1-2 and the antenna fixing portion 1-1 are overlapped. Receive status.
  • the positioning connecting component is a rotating positioning component
  • the rotating positioning component includes a positioning shaft seat
  • the front end of the positioning shaft seat is fixedly connected to the outer bottom surface of the antenna fixing portion by extending the connecting fixing component.
  • the positioning shaft seat is offset from the outer bottom surface of the movable portion of the antenna, and a positioning rotating shaft is disposed in the shaft hole of the positioning shaft seat, and the positioning rotating shaft can rotate in the shaft hole of the positioning shaft seat
  • Reciprocating motion may also be performed along an axial direction of the shaft hole, the positioning rotation axis being parallel to an axis of the rotating parabolic antenna, and a front end of the positioning rotation shaft being fixedly connected to an outer bottom surface of the antenna movable portion, a rear end of the positioning rotating shaft is provided with a handle
  • the fixed connecting component is a plurality of fastening buckles
  • the plurality of fastening buckles are distributed along the length direction of the splicing seam to the outer surface of the antenna fixing portion and The outer surface of the mov
  • the positioning shaft seat 2-1 has a cylindrical shape, and the front side wall of the positioning shaft seat 2-1 is along the The longitudinal direction of the positioning shaft seat 2-1 is provided with a guiding long slit, and the depth of the guiding long slit is larger than the thickness of the bottom of the antenna movable portion 1-2, and correspondingly, the side surface of the positioning rotating shaft 2-2 is disposed
  • the guiding block 2-4 is located at the bottom of the guiding long slit when the antenna fixing portion 1-1 and the antenna movable portion 1-2 are in contact with each other.
  • the sidewalls of the positioning shaft seat 2-1 are respectively provided with axial grooves at both ends of the same diameter, wherein one axial groove is long and is an axial guiding groove.
  • the length of the axial guiding groove 2-1-1 is greater than the thickness of the bottom surface of the antenna movable portion 1-2, and the other groove is short, which is a fixing groove 2-1-2, the fixing
  • the length of the groove 2-1-2 is larger than the axial length of the guiding block 2-4, and the front end of the axial guiding groove 2-1-1 and the front end of the fixing groove 2-1-2 pass through a semicircle
  • the circumferential guide is connected to the slot 2-1-3, and the guide block 2-4 is sequentially in the axial guiding groove 2-1-1, the circumferential guiding groove 2-1-3, and the fixing groove 2-1-2.
  • the guiding block 2-4 is located at the rear end of the axial guiding grooves at both ends of the same diameter, wherein one axial groove is long and is an axial guiding groove.
  • the shape of the positioning shaft seat is cylindrical
  • the front side wall of the positioning shaft seat is provided with a guiding long gap along the length direction of the positioning shaft seat, and the depth of the guiding long gap is
  • the side of the positioning rotating shaft is disposed with a guiding block.
  • axial grooves are provided, wherein one axial groove is long, which is an axial guiding groove, and the length of the axial guiding groove is greater than the length
  • the thickness of the bottom surface of the antenna movable portion, and the other groove is short, which is a fixing groove
  • the length of the fixing groove is larger than the axial length of the guiding block, and the front end of the axial guiding groove and the front end of the fixing groove are communicated by a semicircular circumferential guiding groove, and the guiding block is sequentially in the axial direction Reciprocating movement in the guiding groove, the circumferential guiding groove, and the fixing groove.
  • the rear end faces of the guide blocks 2-4 are provided with balls 2-5.
  • the guide block is advantageously moved in the circumferential direction on the front end surface of the positioning shaft seat, and the guide block is also facilitated in the circumferential guide groove. motion.
  • the side surface in the guide long slit is provided with a spring ball brake member 2-6 for preventing the guide block 2-4 from freely moving.
  • a spring ball brake member 2-6 for preventing the guide block 2-4 from freely moving.
  • the rear portion of the positioning rotating shaft 2-2 is sleeved with a compression return spring 2-7, and the compression return spring 2-7 is located at the rear end of the positioning shaft seat 2-1 and the handle. Between 2-3.
  • the guide block can be prevented from being free along the length direction of the positioning shaft seat. motion.
  • the rear portion of the positioning rotating shaft is sleeved with a compression return spring, and the compression return spring is located between the rear end of the positioning shaft seat and the handle, the same can be prevented.
  • the guide block is free to move along the length of the positioning shaft seat.
  • the front side wall of the positioning shaft seat 2-1 is provided with a fixed short gap along the longitudinal direction of the positioning shaft seat 2-1.
  • the fixed short slit is located on the same diameter as the guiding long slit, the length of the fixed short slit is larger than the axial length of the guiding block 2-4, and the side in the fixed short gap is provided to block the guiding Blocks 2-4 freely moving spring ball brake components 2-8.
  • the guide long slit is away from the seam, and the fixed short slit is close to the seam.
  • the guide long slit is close to the seam, and the fixed short slit is away from the seam.
  • the front side wall of the positioning shaft seat is provided with a fixed short gap along the longitudinal direction of the positioning shaft seat, and the fixed short gap is located on the same diameter as the guiding long opening, and the fixing is fixed.
  • the length of the short gap is greater than the axial length of the guide block, and the side surface of the fixed short gap is provided with a technical means for preventing the spring ball brake member from freely moving the guide block, so that the guide can be effectively prevented.
  • the block is free to move in the circumferential direction of the positioning shaft seat.
  • the positioning connecting member is a hinge positioning member 5
  • the hinge positioning member 5 has two, and two of the antenna movable portions 1-2
  • the two ends are hinged to the two ends of the antenna fixing portion 1-1 by the two hinge positioning members 5
  • the fixed connecting member is a fastening buckle 3
  • the fastening buckle 3 has a plurality of The fastening buckle 3 is fixedly coupled to the outer surface of the antenna fixing portion 1-2 and the outer surface of the antenna movable portion 1-2 along the longitudinal direction of the splicing slit.
  • the positioning connecting component is a chuck positioning component 6, and the chuck positioning component 6 has a plurality of, and the plurality of the chuck positioning components 6 are divided into two groups.
  • a set of the chuck positioning members 6 are disposed on the joint surface of the antenna movable portion 1-2, and correspondingly, the seam surface of the antenna fixing portion 1-1 is disposed with a bayonet
  • Another set of said chuck positioning portion A member 6 is disposed on the half circumference of the aperture of the antenna movable portion 1-2.
  • the antenna fixing portion 1-1 is disposed with a bayonet distributed on the half circumference of the aperture, and the fixed connecting member is tight.
  • a fastening buckle 3 having a plurality of fastening buckles 3, a plurality of the fastening buckles 3 being distributed along the length direction of the splicing slit to the outer surface of the antenna fixing portion 1-1 and the antenna
  • the outer surfaces of the movable portions 1-2 are fixedly coupled together.
  • the positioning connecting component is a chuck positioning component 6, the chuck positioning component 6 has a plurality of, and the plurality of the chuck positioning components 6 are divided into two groups, and the set of the chuck positioning components 6 are distributed.
  • the seam surface of the antenna movable portion 1-2 is distributedly provided with a bayonet
  • the other group of the chuck positioning member 6 Distributedly disposed on the half-circle of the diameter of the antenna fixing portion 1-1, correspondingly, the antenna movable portion 1-2 is disposed with a bayonet distributed on the half circumference of the aperture
  • the fixed connecting member is a fastening
  • the buckle 3 has a plurality of the fastening buckles 3, and the plurality of the fastening buckles 3 are distributed along the length direction of the splicing slit to the outer surface of the antenna fixing portion 1-1 and the antenna movable portion.
  • the outer surfaces of 1-2 are fixedly connected together.
  • the positioning connecting component is a hinge positioning component
  • the hinge positioning component has two, and two ends of the antenna movable portion respectively pass through two of the hinge positioning component and the antenna fixing component.
  • the fixed connection component is a fastening buckle
  • the fastening buckle has a plurality of
  • the plurality of fastening buckles are distributed along the length direction of the splicing seam to the outer surface of the antenna fixing portion
  • the positioning connecting component is a chuck positioning component
  • the chuck positioning component is plural, and the plurality of chuck positioning components are divided into two groups, and a set of the chuck positioning components are distributedly disposed in the
  • a seam is disposed on the joint surface of the antenna fixing portion, and another set of the chuck positioning members are disposed at a semicircle of the antenna movable portion.
  • a bayonet is disposed on the half circumference of the antenna fixing portion
  • the fixed connecting member is a fastening buckle
  • the fastening buckle has a plurality of the fastening portions.
  • the positioning connecting component is a chuck positioning component
  • the chuck positioning component is plural, and the plurality of chuck positioning components are divided into two groups, and a set of the chuck positioning components are distributedly disposed in the
  • a seam is disposed on the joint surface of the antenna movable portion
  • another set of the chuck positioning members are disposed at a semicircle of the antenna fixing portion.
  • a bayonet is disposed on the semicircle of the antenna movable portion.
  • the fixed connecting member is a fastening buckle, and the fastening buckle has a plurality of the fastening.

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Abstract

L'invention concerne une antenne parabolique rotative de communication par satellite portable, comprenant une antenne parabolique rotative. L'antenne parabolique rotative est formée par raccordement et combinaison d'une partie de fixation d'antenne et d'une partie de déplacement d'antenne. Il existe une seule partie de fixation d'antenne, et il existe une seule partie de déplacement d'antenne. La partie de déplacement d'antenne et la partie de fixation d'antenne sont reliées de manière fixe par l'intermédiaire d'un composant de liaison. La partie de fixation d'antenne et la partie de déplacement d'antenne sont en symétrie miroir par rapport à un plan de raccordement, le plan de raccordement étant un plan dans lequel se trouve un joint de raccordement de la partie de fixation d'antenne appariée avec la partie de déplacement d'antenne. Un axe de l'antenne parabolique rotative est situé dans le plan de raccordement. Le composant de liaison comprend un premier composant de liaison de positionnement et/ou un composant de liaison de fixation. Le composant de liaison de positionnement est un composant de positionnement rotatif. La présente invention est plus pratique et permet un montage et un démontage rapides, la précision de fabrication d'un plan d'antenne est davantage assurée, et les performances d'émission-réception de signal d'une antenne sont meilleures.
PCT/CN2016/096965 2015-11-16 2016-08-26 Antenne parabolique rotative de communication par satellite portable WO2017084403A1 (fr)

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CN201510783042.1A CN105390792B (zh) 2015-11-16 2015-11-16 一种便携式卫星通信旋转抛物面天线

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109103565A (zh) * 2018-10-18 2018-12-28 燕山大学 可拆卸便携式并联天线
CN110034995A (zh) * 2019-02-27 2019-07-19 浙江胜百信息科技有限公司 一种户外天线网桥

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105390792B (zh) * 2015-11-16 2018-06-01 深圳市华讯方舟卫星通信有限公司 一种便携式卫星通信旋转抛物面天线
CN106324735A (zh) * 2016-10-26 2017-01-11 深圳大学 一种电磁波准直元件及组件

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2178000Y (zh) * 1993-10-12 1994-09-21 张建民 折合式卫星接收天线
WO1998038695A1 (fr) * 1997-02-27 1998-09-03 Sakimura Corporation Reflecteur pliable facile a manier
CN201238077Y (zh) * 2008-08-06 2009-05-13 四川九洲电器集团有限责任公司 便携式卫星接收天线
CN201838704U (zh) * 2010-11-05 2011-05-18 重庆金美通信有限责任公司 可收折式抛物面天线
CN105390792A (zh) * 2015-11-16 2016-03-09 深圳市华讯方舟卫星通信有限公司 一种便携式卫星通信旋转抛物面天线

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3971023A (en) * 1974-12-30 1976-07-20 Taggart Robert B Parabolic reflector assembled from triangular shaped petals
US4458251A (en) * 1981-05-19 1984-07-03 Prodelin, Inc. Concave reflector for radio antenna use
US4766443A (en) * 1984-06-15 1988-08-23 Winegard Company Satellite dish antenna apparatus
JP3837399B2 (ja) * 2003-06-03 2006-10-25 三洋電機株式会社 折り畳み可能なアンテナ装置
CN201266668Y (zh) * 2008-09-01 2009-07-01 李红梅 移动通信天线快速锁扣装置
CN102983383B (zh) * 2012-12-12 2015-02-04 上海航天测控通信研究所 一种新型展开到位锁定装置
CN203826562U (zh) * 2014-05-06 2014-09-10 贵州振华天通设备有限公司 一种互换式抛物面天线
CN203859231U (zh) * 2014-05-06 2014-10-01 西安普天天线有限公司 一种分瓣结构的微波抛物面天线反射器
CN204257798U (zh) * 2014-12-23 2015-04-08 中国电子科技集团公司第五十四研究所 一种具有自动展开功能的大型馈源天线

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2178000Y (zh) * 1993-10-12 1994-09-21 张建民 折合式卫星接收天线
WO1998038695A1 (fr) * 1997-02-27 1998-09-03 Sakimura Corporation Reflecteur pliable facile a manier
CN201238077Y (zh) * 2008-08-06 2009-05-13 四川九洲电器集团有限责任公司 便携式卫星接收天线
CN201838704U (zh) * 2010-11-05 2011-05-18 重庆金美通信有限责任公司 可收折式抛物面天线
CN105390792A (zh) * 2015-11-16 2016-03-09 深圳市华讯方舟卫星通信有限公司 一种便携式卫星通信旋转抛物面天线

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109103565A (zh) * 2018-10-18 2018-12-28 燕山大学 可拆卸便携式并联天线
CN110034995A (zh) * 2019-02-27 2019-07-19 浙江胜百信息科技有限公司 一种户外天线网桥

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