WO2017084403A1 - Portable satellite communication rotational parabola antenna - Google Patents

Portable satellite communication rotational parabola antenna 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
French (fr)
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.)
Filing date
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/en

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/20Resilient mountings
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10Combinations 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
    • H01Q19/12Combinations 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
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/125Means for positioning
    • H01Q1/1257Means 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.

Abstract

Disclosed is a portable satellite communication rotational parabola antenna, comprising a rotational parabola antenna. The rotational parabola antenna is formed by splicing and combining an antenna fixing portion and an antenna moving portion. There is one antenna fixing portion, and there is one antenna moving portion. The antenna moving portion and the antenna fixing portion are fixedly connected via a connection component. The antenna fixing portion and the antenna moving portion are in mirror symmetry with respect to a splicing plane, wherein the splicing plane is a plane where a splicing seam of the antenna fixing portion mating with the antenna moving portion is located. An axis of the rotational parabola antenna is located in the splicing plane. The connection component comprises a positioning connection component and/or a fixing connection component. The positioning connection component is a rotational positioning component. The present invention is more convenient and able to be rapidly mounted and dismounted, the manufacturing accuracy of an antenna plane is more assured, and the signal transceiving performance of an antenna is better.

Description

一种便携式卫星通信旋转抛物面天线Portable satellite communication rotating parabolic antenna 技术领域Technical field
本发明涉及一种卫星通信天线,特别涉及一种便携式卫星通信旋转抛物面天线。The invention relates to a satellite communication antenna, in particular to a portable satellite communication rotary parabolic antenna.
背景技术Background technique
卫星通信旋转抛物面天线的作用有两项:作用一是将通信卫星传来的微波信号反射到位于焦点处的馈源和高频头内,完成信号接收功能;作用二是将地球站高功放传输的射频信号电磁变换成自由空间传播的微波信号,并向指定卫星发射,完成发射功能。衡量卫星通信天线性能的主要指标有收发增益、收发效率、噪声温度,以及辐射特性,天线的精度直接影响这些指标优劣。天线按使用场景不同划分为固定天线、便携式天线、车载天线等。目前,业内的便携式卫星通信天线主要采取拼接式,即将天线主面分成几块,使用前先拼接,通信完毕后再拆解收装。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. At present, 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.
现有便携式卫星通信旋转抛物天线为便于携带,旋转抛物天线1通常采用拼接方式。如图1所示,旋转抛物天线1由一个天线固定部1-1和三个活动部1-2拼接构成。如图2所示,旋转抛物天线1由一个天线固定部1-1和五个活动部1-2拼接构成。天线的口径通常在1.2米以下。由于多块拼接,在安装使用与撤收时耗时间更多,也不方便,并且随着拼接面增多,天线反射面的精度将变差,机械性能相应下降,直接影响天线的收发效益、天线辐射性能,以及抗风强度。The existing portable satellite communication rotating parabolic antenna is convenient for carrying, and the rotating parabolic antenna 1 is usually spliced. As shown in Fig. 1, the parabolic antenna 1 is constructed by splicing one antenna fixing portion 1-1 and three movable portions 1-2. As shown in FIG. 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.
发明内容Summary of the invention
本发明所要解决的技术问题是提供一种便携式卫星通信旋转抛物面天线,该便携式卫星通信旋转抛物面天线不但便于携带,而且,安装和撤收方便、快捷,天线面的制作精度有保证,天线的信号收发性能好。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.
为解决上述技术问题,本发明提供了一种便携式卫星通信旋转抛物面天线,包括旋转抛物面天线,所述旋转抛物面天线由天线固定部和天线活动部拼接组合而成,所述天线固定部有一个,所述天线活动部有一个,所述天线活动部和所述天线固定部之间通过连接部件固定连接。In order to solve the above technical problem, 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.
所述天线固定部和所述天线活动部相对于拼接面镜像对称,所述拼接面是所述天线固定部和所述天线活动部之间相对接的拼接缝所在的平面,所述旋转抛物面天线的轴线位于所述拼接面内。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.
所述拼接面与所述旋转抛物面天线的口径面相交的直线平行于水平面。A line intersecting the splicing surface with the aperture surface of the rotating parabolic antenna is parallel to the horizontal plane.
所述连接部件包括定位连接部件和/或固定连接部件。The connecting member includes a positioning connecting member and/or a fixed connecting member.
所述定位连接部件是旋转定位部件,所述旋转定位部件包括定位轴座,所述定位轴座的前端通过延伸连接固定部件与所述天线固定部的外底面固定连接,所述定位轴座偏置于所述天线活动部外底面的后 方,所述定位轴座的轴孔内设置有定位转动轴,所述定位转动轴可在所述定位轴座的轴孔内转动,也可沿着轴孔的轴线方向作往复运动,所述定位转动轴平行于所述旋转抛物面天线的轴线,所述定位转动轴的前端与所述天线活动部的外底面固定连接,所述定位转动轴的后端设置有手柄,所述固定连接部件是多个紧固搭扣,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起。The positioning connecting component is a rotating positioning component, and 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.
所述定位轴座的形状呈圆筒状,所述定位轴座的侧壁前部沿着该定位轴座的长度方向设置有导向长豁口,所述导向长豁口的深度大于所述天线活动部底部的厚度,相应地,所述定位转动轴的侧面设置有导向块,当所述天线固定部和天线活动部之间相对接时,所述导向块位于所述导向长豁口的底部;或者,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. Correspondingly, 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
所述定位轴座的侧壁位于同一直径的两端分别设置有轴向凹槽,其中,一个轴向凹槽长,是轴向导向槽,所述轴向导向槽的长度大于所述天线活动部底面的厚度,另一个凹槽短,是固定槽,所述固定槽的长度大于所述导向块的轴向长度,所述轴向导向槽的前端和所述固定槽的前端通过半圆形的周向导向槽连通,所述导向块依次在所述轴向导向槽、周向导向槽、固定槽中往复运动,当所述天线固定部和天线活动部之间相对接时,所述导向块位于所述轴向导向槽的后端。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.
所述导向块的后端面上设置有滚珠。Balls are disposed on the rear end surface of the guide block.
所述导向长豁口内的侧面设置有阻止所述导向块自由运动的弹簧滚珠制动部件,和/或,所述定位转动轴的后部套置有压缩复位弹簧,所述压缩复位弹簧位于所述定位轴座的后端与所述手柄之间。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.
所述定位轴座的侧壁前部沿着该定位轴座的长度方向设置有固定短豁口,所述固定短豁口与所述导向长豁口位于同一直径上,所述固定短豁口的长度大于所述导向块的轴向长度,所述固定短豁口内的侧面设置有阻止所述导向块自由运动的弹簧滚珠制动部件。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.
所述定位连接部件是铰链定位部件,所述铰链定位部件有两个,所述天线活动部的两端分别通过两个所述铰链定位部件与所述天线固定部的两端铰接,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起;或者,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,
所述定位连接部件是卡头定位部件,所述卡头定位部件有多个,多个所述卡头定位部件分为两组,一组所述卡头定位部件分布地设置在所述天线活动部的接缝面上,相应地,所述天线固定部的接缝面上分布地设置有卡口,另一组所述卡头定位部件分布地设置在所述天线活动部的口径半圆周上,相应地,所述天线固定部的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起;或者,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. Correspondingly, 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. Correspondingly, the antenna fixing portion has a bayonet distributed on the half circumference of the aperture, the fixed connecting component is a fastening buckle, and 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
所述定位连接部件是卡头定位部件,所述卡头定位部件有多个,多个所述卡头定位部件分为两组,一组所述卡头定位部件分布地设置在所述天线固定部的接缝面上,相应地,所述天线活动部的接缝面上 分布地设置有卡口,另一组所述卡头定位部件分布地设置在所述天线固定部的口径半圆周上,相应地,所述天线活动部的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起。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. Correspondingly, a bayonet is disposed on the half circumference of the antenna movable portion. The fixed connecting component is a fastening buckle, and 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.
与现有技术相比,本发明的便携式卫星通信旋转抛物面天线具有以下有益效果。The portable satellite communication rotating parabolic antenna of the present invention has the following advantageous effects as compared with the prior art.
1、本技术方案由于采用了所述天线活动部有一个,所述天线活动部和所述天线固定部之间通过连接部件固定连接的技术手段,所以,不但便于携带,而且,安装和撤收方便、快捷,天线面的制作精度有保证,天线的信号收发性能好。1. 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.
2、本技术方案由于采用了所述天线固定部和所述天线活动部相对于拼接面镜像对称,所述拼接面是所述天线固定部和所述天线活动部之间相对接的拼接缝所在的平面,所述旋转抛物面天线的轴线位于所述拼接面内的技术手段,所以,有利于减小便携式卫星通信旋转抛物面天线所占用的空间,更便于携带。2. 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.
3、本技术方案由于采用了所述拼接面与所述旋转抛物面天线的口径面相交的直线平行于水平面的技术手段,所以,可最大限度地降低便携式卫星通信旋转抛物面天线的高度,最便于携带。3. 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. .
4、本技术方案由于采用了所述连接部件包括定位连接部件和/或固定连接部件的技术手段,所以,可通过多种方式将所述天线活动部和所述天线固定部固定在一起。4. In the present technical solution, since 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.
5、本技术方案由于采用了所述定位连接部件是旋转定位部件,所述旋转定位部件包括定位轴座,所述定位轴座的前端通过延伸连接固定部件与所述天线固定部的外底面固定连接,所述定位轴座偏置于所述天线活动部外底面的后方,所述定位轴座的轴孔内设置有定位转动轴,所述定位转动轴可在所述定位轴座的轴孔内转动,也可沿着轴孔的轴线方向作往复运动,所述定位转动轴平行于所述旋转抛物面天线的轴线,所述定位转动轴的前端与所述天线活动部的外底面固定连接,所述定位转动轴的后端设置有手柄,所述固定连接部件是多个紧固搭扣,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段,所以,安装和撤收更方便、快捷,天线面的制作精度更有保证,天线的信号收发性能更好。5. The present invention adopts the positioning connecting component as a rotating positioning component, and 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. Connecting, 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, and the plurality of fastening buckles are distributed along the length direction of the splicing seam to the outside of the antenna fixing portion The surface and the outer surface of the movable portion of the antenna are fixedly connected together, so that the installation and withdrawal are more convenient and quick, the production precision of the antenna surface is more assured, and the signal transmission and reception of the antenna is ensured. Better performance.
6、本技术方案由于采用了所述定位轴座的形状呈圆筒状,所述定位轴座的侧壁前部沿着该定位轴座的长度方向设置有导向长豁口,所述导向长豁口的深度大于所述天线活动部底部的厚度,相应地,所述定位转动轴的侧面设置有导向块,当所述天线固定部和天线活动部之间相对接时,所述导向块位于所述导向长豁口的底部的技术手段,所以,安装和撤收更精准、方便、快捷,天线面的制作精度更有保证,天线的信号收发性能更好。6. 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. Correspondingly, the side of the positioning rotating shaft is provided with a guiding block. When the antenna fixing portion and the antenna movable portion are oppositely connected, the guiding block is located at the The technical means of guiding the bottom of the long gap, therefore, the installation and withdrawal are more precise, convenient and fast, the production precision of the antenna surface is more guaranteed, and the signal transmission and reception performance of the antenna is better.
当采用所述定位轴座的侧壁位于同一直径的两端分别设置有轴向凹槽,其中,一个轴向凹槽长,是轴向导向槽,所述轴向导向槽的长度大于所述天线活动部底面的厚度,另一个凹槽短,是固定槽,所述 固定槽的长度大于所述导向块的轴向长度,所述轴向导向槽的前端和所述固定槽的前端通过半圆形的周向导向槽连通,所述导向块依次在所述轴向导向槽、周向导向槽、固定槽中往复运动,当所述天线固定部和天线活动部之间相对接时,所述导向块位于所述轴向导向槽的后端的技术手段时,则同样,安装和撤收更精准、方便、快捷,天线面的制作精度更有保证,天线的信号收发性能更好。When the sidewalls of the positioning shaft seat are located at two ends of the same diameter, respectively, 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. When the antenna fixing portion and the antenna movable portion are in contact with each other, when the guiding block is located at the rear end of the axial guiding groove, the same is true The installation and withdrawal are more precise, convenient and fast, the production accuracy of the antenna surface is more guaranteed, and the signal transmission and reception performance of the antenna is better.
7、本技术方案由于采用了所述导向块的后端面上设置有滚珠的技术手段,所以,有利于导向块在定位轴座的前端面沿周向运动,也有利于导向块在周向导向槽内运动。7. 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.
8、本技术方案由于采用了所述导向长豁口内的侧面设置有阻止所述导向块自由运动的弹簧滚珠制动部件的技术手段,所以,可以阻止所述导向块沿着定位轴座的长度方向自由运动。当采用所述定位转动轴的后部套置有压缩复位弹簧,所述压缩复位弹簧位于所述定位轴座的后端与所述手柄之间的技术手段时,则同样地,可以阻止所述导向块沿着定位轴座的长度方向自由运动。8. 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. When 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.
9、本技术方案由于采用了所述定位轴座的侧壁前部沿着该定位轴座的长度方向设置有固定短豁口,所述固定短豁口与所述导向长豁口位于同一直径上,所述固定短豁口的长度大于所述导向块的轴向长度,所述固定短豁口内的侧面设置有阻止所述导向块自由运动的弹簧滚珠制动部件的技术手段,所以,可以有效地防止所述导向块沿着定位轴座的周向自由运动。9. In the technical solution, 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.
10、本技术方案由于采用了所述定位连接部件是铰链定位部件,所述铰链定位部件有两个,所述天线活动部的两端分别通过两个所述铰链定位部件与所述天线固定部的两端铰接,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段,所以,有利于保护天线的反射面。10. 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, and 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.
当采用所述定位连接部件是卡头定位部件,所述卡头定位部件有多个,多个所述卡头定位部件分为两组,一组所述卡头定位部件分布地设置在所述天线活动部的接缝面上,相应地,所述天线固定部的接缝面上分布地设置有卡口,另一组所述卡头定位部件分布地设置在所述天线活动部的口径半圆周上,相应地,所述天线固定部的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段时,同样有利于保护天线的反射面。When 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 Correspondingly, 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. Correspondingly, a bayonet is disposed on the half circumference of the antenna fixing portion, and the fixed connecting member is a fastening buckle, and the fastening buckle has a plurality of the fastening portions. When the buckle is distributed along the longitudinal direction of the splicing seam to fix the outer surface of the antenna fixing portion and the outer surface of the movable portion of the antenna together, it is also advantageous to protect the reflecting surface of the antenna.
当采用所述定位连接部件是卡头定位部件,所述卡头定位部件有多个,多个所述卡头定位部件分为两组,一组所述卡头定位部件分布地设置在所述天线固定部的接缝面上,相应地,所述天线活动部的接缝面上分布地设置有卡口,另一组所述卡头定位部件分布地设置在所述天线固定部的口径半圆周上,相应地,所述天线活动部的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段时,同样有利于保护天线的反射面。When 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 Correspondingly, a seam is disposed on the joint surface of the antenna movable portion, and 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. When the buckle is distributed along the longitudinal direction of the splicing seam to fix the outer surface of the antenna fixing portion and the outer surface of the movable portion of the antenna together, it is also advantageous to protect the reflecting surface of the antenna.
附图说明 DRAWINGS
图1为现有技术中第一种便携式卫星通信旋转抛物面天线的结构示意图。1 is a schematic structural view of a first portable satellite communication rotating parabolic antenna in the prior art.
图2为现有技术中第二种便携式卫星通信旋转抛物面天线的结构示意图。2 is a schematic structural view of a second portable satellite communication rotating parabolic antenna in the prior art.
图3为本发明实施例提供的第一种便携式卫星通信旋转抛物面天线处于安装后状态的侧视结构示意图。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.
图4为图3中A向结构示意图。4 is a schematic view showing the structure of the A direction in FIG.
图5是本发明实施例提供的第一种便携式卫星通信旋转抛物面天线处于撤收后状态的侧视结构示意图。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.
图6是图1中另一种定位轴座的展开结构示意图。FIG. 6 is a schematic exploded view of another positioning shaft seat of FIG. 1. FIG.
图7为本发明实施例提供的第二种便携式卫星通信旋转抛物面天线处于安装后状态的侧视结构示意图。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.
图8是本发明实施例提供的第二种便携式卫星通信旋转抛物面天线处于撤收后状态的侧视结构示意图。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.
图9为本发明实施例提供的第三种便携式卫星通信旋转抛物面天线处于安装后状态的侧视结构示意图。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.
图10是本发明实施例提供的第三种便携式卫星通信旋转抛物面天线处于撤收后状态的侧视结构示意图。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.
附图标记说明如下。The reference numerals are explained below.
1~旋转抛物面天线;1 to rotating parabolic antenna;
1-1~天线固定部;1-1 to the antenna fixing portion;
1-2~天线活动部;1-2~ antenna active part;
2~旋转定位部件;2 to rotating positioning components;
2-1~定位轴座;2-1~ positioning shaft seat;
2-1-1~轴向导向槽;2-1-1~ axial guiding groove;
2-1-2~固定槽;2-1-2~ fixing groove;
2-1-3~周向导向槽;2-1-3~week guide groove;
2-2~定位转动轴;2-2~ positioning rotation axis;
2-3~手柄;2-3 ~ handle;
2-4~导向块;2-4~ guiding block;
2-5~滚珠;2-5 to ball;
2-6~弹簧滚珠制动部件;2-6~spring ball brake parts;
2-7~压缩复位弹簧;2-7~ compression return spring;
2-8~弹簧滚珠制动部件;2-8~spring ball brake parts;
2-9~延伸连接固定部件;2-9~ extension connecting fixed parts;
3~紧固搭扣;3~ fastening buckle;
4~底座;4 to the base;
5~铰链定位部件;5~ hinge positioning component;
6~卡头定位部件。6 ~ chuck positioning parts.
具体实施方式 detailed description
如图3至图10所示,本实施方式提供的一种便携式卫星通信旋转抛物面天线,包括旋转抛物面天线1,所述旋转抛物面天线1由天线固定部1-1和天线活动部1-2拼接组合而成,所述天线固定部1-1有一个,所述天线活动部1-2有一个,所述天线活动部1-2和所述天线固定部1-1之间通过连接部件固定连接。从图3中可以看出,所述天线固定部1-1与底座(4)固定连接。所述天线活动部1-2和所述天线固定部1-1选用金属材料进行加工制作(也可采用玻璃纤维制作),要求按照抛物面天线曲率设计加工,以确保两块制作完成后,能够组合成完整的抛物面天线。As shown in FIG. 3 to FIG. 10, 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. . As can be seen from Fig. 3, 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.
本实施方式由于采用了所述天线活动部有一个,所述天线活动部和所述天线固定部之间通过连接部件固定连接的技术手段,所以,不但便于携带,而且,安装和撤收方便、快捷,天线面的制作精度有保证,天线的信号收发性能好。In this embodiment, 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.
作为本实施方式的第一步改进,如图3至图10所示,所述天线固定部1-1和所述天线活动部1-2相对于拼接面镜像对称,所述拼接面是所述天线固定部1-1和所述天线活动部1-2之间相对接的拼接缝所在的平面,所述旋转抛物面天线1的轴线位于所述拼接面内。As a first step improvement of the present embodiment, as shown in FIG. 3 to FIG. 10, 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.
本实施方式由于采用了所述天线固定部和所述天线活动部相对于拼接面镜像对称,所述拼接面是所述天线固定部和所述天线活动部之间相对接的拼接缝所在的平面,所述旋转抛物面天线的轴线位于所述拼接面内的技术手段,所以,有利于减小便携式卫星通信旋转抛物面天线所占用的空间,更便于携带。In this embodiment, 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.
作为本实施方式的第二步改进,如图3至图10所示,所述拼接面与所述旋转抛物面天线1的口径面相交的直线平行于水平面。As a second modification of the present embodiment, as shown in FIGS. 3 to 10, a straight line intersecting the splicing surface with the caliper surface of the rotating parabolic antenna 1 is parallel to the horizontal plane.
本实施方式由于采用了所述拼接面与所述旋转抛物面天线的口径面相交的直线平行于水平面的技术手段,所以,可最大限度地降低便携式卫星通信旋转抛物面天线的高度,最便于携带。In this embodiment, since the straight line intersecting the aperture surface of the rotating parabolic antenna 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.
作为本实施方式的第三步改进,如图3至图10所示,所述连接部件可以是定位连接部件,也可以是固定连接部件。As a third modification of the present embodiment, as shown in FIGS. 3 to 10, the connecting member may be a positioning connecting member or a fixed connecting member.
本实施方式由于采用了所述连接部件包括定位连接部件和/或固定连接部件的技术手段,所以,可通过多种方式将所述天线活动部和所述天线固定部固定在一起。In the present embodiment, since 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.
作为本实施方式的第四步改进,如图3至图5所示,所述定位连接部件是旋转定位部件2,所述旋转定位部件2包括定位轴座2-1,所述定位轴座2-1的前端通过延伸连接固定部件2-9与所述天线固定部1-1的外底面固定连接,所述定位轴座2-1偏置于所述天线活动部1-2外底面的后方,所述定位轴座2-1的轴孔内设置有定位转动轴2-2,所述定位转动轴2-2可在所述定位轴座2-1的轴孔内转动,也可沿着轴孔的轴线方向作往复运动,所述定位转动轴2-2平行于所述旋转抛物面天线1的轴线,所述定位转动轴2-2的前端与所述天线活动部1-2的外底面固定连接,所述定位转动轴2-2的后端设置有手柄2-3。作为一种优选,所述手柄2-3是梅花形手柄。所述固定连接部件是多个紧固搭扣3,多个所述紧固搭扣3沿着拼接缝的长度方向分布将所述天线固定部1-1的外表面和所述天线活动部1-2的外表面固 定连接在一起。As a fourth modification of the present embodiment, as shown in FIGS. 3 to 5, the positioning connecting member is a rotary positioning member 2, and 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. As a preference, 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.
当便携式卫星通信旋转抛物面天线处于撤收状态时(参见图5),先转动手柄2-3半周,再向后拉动手柄2-3,使所述天线活动部1-2和所述天线固定部1-1对接,然后,通过紧固搭扣3将所述天线活动部1-2和所述天线固定部1-1固定在一起,使便携式卫星通信旋转抛物面天线处于使用状态。当便携式卫星通信旋转抛物面天线处于使用状态时,先向前推动手柄2-3,再转动手柄2-3半周,使所述天线活动部1-2和所述天线固定部1-1重合处于撤收状态。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. When 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.
本实施方式由于采用了所述定位连接部件是旋转定位部件,所述旋转定位部件包括定位轴座,所述定位轴座的前端通过延伸连接固定部件与所述天线固定部的外底面固定连接,所述定位轴座偏置于所述天线活动部外底面的后方,所述定位轴座的轴孔内设置有定位转动轴,所述定位转动轴可在所述定位轴座的轴孔内转动,也可沿着轴孔的轴线方向作往复运动,所述定位转动轴平行于所述旋转抛物面天线的轴线,所述定位转动轴的前端与所述天线活动部的外底面固定连接,所述定位转动轴的后端设置有手柄,所述固定连接部件是多个紧固搭扣,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段,所以,安装和撤收更方便、快捷,天线面的制作精度更有保证,天线的信号收发性能更好。In this embodiment, the positioning connecting component is a rotating positioning component, and the rotating positioning component includes a positioning shaft seat, and 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, and 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 movable portion of the antenna is fixedly connected together, so that the installation and withdrawal are more convenient and quick, the production precision of the antenna surface is more guaranteed, and the signal transmission and reception of the antenna is improved. Better.
作为本实施方式的第五步改进,如图3至图5所示,所述定位轴座2-1的形状呈圆筒状,所述定位轴座2-1的侧壁前部沿着该定位轴座2-1的长度方向设置有导向长豁口,所述导向长豁口的深度大于所述天线活动部1-2底部的厚度,相应地,所述定位转动轴2-2的侧面设置有导向块2-4,当所述天线固定部1-1和天线活动部1-2之间相对接时,所述导向块2-4位于所述导向长豁口的底部。As a fifth modification of the embodiment, as shown in FIG. 3 to FIG. 5, 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.
当然,也可以是如图6所示,所述定位轴座2-1的侧壁位于同一直径的两端分别设置有轴向凹槽,其中,一个轴向凹槽长,是轴向导向槽2-1-1,所述轴向导向槽2-1-1的长度大于所述天线活动部1-2底面的厚度,另一个凹槽短,是固定槽2-1-2,所述固定槽2-1-2的长度大于所述导向块2-4的轴向长度,所述轴向导向槽2-1-1的前端和所述固定槽2-1-2的前端通过半圆形的周向导向槽2-1-3连通,所述导向块2-4依次在所述轴向导向槽2-1-1、周向导向槽2-1-3、固定槽2-1-2中往复运动,当所述天线固定部1-1和天线活动部1-2之间相对接时,所述导向块2-4位于所述轴向导向槽2-1-1的后端。Of course, as shown in FIG. 6, 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. 2-1-1, 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. In the reciprocating motion, when the antenna fixing portion 1-1 and the antenna movable portion 1-2 are in contact with each other, the guiding block 2-4 is located at the rear end of the axial guiding groove 2-1-1.
本实施方式由于采用了所述定位轴座的形状呈圆筒状,所述定位轴座的侧壁前部沿着该定位轴座的长度方向设置有导向长豁口,所述导向长豁口的深度大于所述天线活动部底部的厚度,相应地,所述定位转动轴的侧面设置有导向块,当所述天线固定部和天线活动部之间相对接时,所述导向块位于所述导向长豁口的底部的技术手段,所以,安装和撤收更精准、方便、快捷,天线面的制作精度更有保证,天线的信号收发性能更好。In this embodiment, since 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 Correspondingly, the side of the positioning rotating shaft is disposed with a guiding block. When the antenna fixing portion and the antenna movable portion are oppositely connected, the guiding block is located at the guiding length. The technical means at the bottom of the gap, therefore, the installation and withdrawal are more precise, convenient and fast, the production accuracy of the antenna surface is more guaranteed, and the signal transmission and reception performance of the antenna is better.
当采用所述定位轴座的侧壁位于同一直径的两端分别设置有轴向凹槽,其中,一个轴向凹槽长,是轴向导向槽,所述轴向导向槽的长度大于所述天线活动部底面的厚度,另一个凹槽短,是固定槽,所述 固定槽的长度大于所述导向块的轴向长度,所述轴向导向槽的前端和所述固定槽的前端通过半圆形的周向导向槽连通,所述导向块依次在所述轴向导向槽、周向导向槽、固定槽中往复运动,当所述天线固定部和天线活动部之间相对接时,所述导向块位于所述轴向导向槽的后端的技术手段时,则同样,安装和撤收更精准、方便、快捷,天线面的制作精度更有保证,天线的信号收发性能更好。When the sidewalls of the positioning shaft seat are located at two ends of the same diameter, respectively, 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. When the antenna fixing portion and the antenna movable portion are in contact with each other, when the guiding block is located at the rear end of the axial guiding groove, the same is true The installation and withdrawal are more precise, convenient and fast, the production accuracy of the antenna surface is more guaranteed, and the signal transmission and reception performance of the antenna is better.
作为本实施方式的第六步改进,如图3和图5所示,所述导向块2-4的后端面上设置有滚珠2-5。As a sixth modification of the present embodiment, as shown in FIGS. 3 and 5, the rear end faces of the guide blocks 2-4 are provided with balls 2-5.
本实施方式由于采用了所述导向块的后端面上设置有滚珠的技术手段,所以,有利于导向块在定位轴座的前端面沿周向运动,也有利于导向块在周向导向槽内运动。In this embodiment, since the technical means of providing the balls on the rear end surface of the guide block is adopted, 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.
作为本实施方式的第七步改进,如图3和图5所示,所述导向长豁口内的侧面设置有阻止所述导向块2-4自由运动的弹簧滚珠制动部件2-6。当然,也可以是所述定位转动轴2-2的后部套置有压缩复位弹簧2-7,所述压缩复位弹簧2-7位于所述定位轴座2-1的后端与所述手柄2-3之间。As a seventh modification of the present embodiment, as shown in Figs. 3 and 5, 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. Of course, it is also possible that 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.
本实施方式由于采用了所述导向长豁口内的侧面设置有阻止所述导向块自由运动的弹簧滚珠制动部件的技术手段,所以,可以阻止所述导向块沿着定位轴座的长度方向自由运动。当采用所述定位转动轴的后部套置有压缩复位弹簧,所述压缩复位弹簧位于所述定位轴座的后端与所述手柄之间的技术手段时,则同样地,可以阻止所述导向块沿着定位轴座的长度方向自由运动。In this embodiment, since the side surface in the guide long slit is provided with a technical means for preventing the spring ball brake member from freely moving the guide block, the guide block can be prevented from being free along the length direction of the positioning shaft seat. motion. When 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.
作为本实施方式的第八步改进,如图3和图5所示,所述定位轴座2-1的侧壁前部沿着该定位轴座2-1的长度方向设置有固定短豁口,所述固定短豁口与所述导向长豁口位于同一直径上,所述固定短豁口的长度大于所述导向块2-4的轴向长度,所述固定短豁口内的侧面设置有阻止所述导向块2-4自由运动的弹簧滚珠制动部件2-8。作为一种优选,如图3所示,所述导向长豁口远离接缝处,所述固定短豁口靠近接缝处。当然,也可以是所述导向长豁口靠近接缝处,所述固定短豁口远离接缝处。As a modification of the eighth step of the embodiment, as shown in FIG. 3 and FIG. 5, 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. As a preferred, as shown in FIG. 3, the guide long slit is away from the seam, and the fixed short slit is close to the seam. Of course, it is also possible that the guide long slit is close to the seam, and the fixed short slit is away from the seam.
本实施方式由于采用了所述定位轴座的侧壁前部沿着该定位轴座的长度方向设置有固定短豁口,所述固定短豁口与所述导向长豁口位于同一直径上,所述固定短豁口的长度大于所述导向块的轴向长度,所述固定短豁口内的侧面设置有阻止所述导向块自由运动的弹簧滚珠制动部件的技术手段,所以,可以有效地防止所述导向块沿着定位轴座的周向自由运动。In this embodiment, 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.
作为本实施方式的第九步改进,如图7至图8所示,所述定位连接部件是铰链定位部件5,所述铰链定位部件5有两个,所述天线活动部1-2的两端分别通过两个所述铰链定位部件5与所述天线固定部1-1的两端铰接,所述固定连接部件是紧固搭扣3,所述紧固搭扣3有多个,多个所述紧固搭扣3沿着拼接缝的长度方向分布将所述天线固定部1-1的外表面和所述天线活动部1-2的外表面固定连接在一起。As a ninth modification of the present embodiment, as shown in FIGS. 7 to 8, 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, and the fixed connecting member is a fastening buckle 3, and 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.
当然,也可以是如图9至图10所示,所述定位连接部件是卡头定位部件6,所述卡头定位部件6有多个,多个所述卡头定位部件6分为两组,一组所述卡头定位部件6分布地设置在所述天线活动部1-2的接缝面上,相应地,所述天线固定部1-1的接缝面上分布地设置有卡口,另一组所述卡头定位部 件6分布地设置在所述天线活动部1-2的口径半圆周上,相应地,所述天线固定部1-1的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣3,所述紧固搭扣3有多个,多个所述紧固搭扣3沿着拼接缝的长度方向分布将所述天线固定部1-1的外表面和所述天线活动部1-2的外表面固定连接在一起。Of course, as shown in FIG. 9 to FIG. 10, 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. Correspondingly, 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.
还可以是所述定位连接部件是卡头定位部件6,所述卡头定位部件6有多个,多个所述卡头定位部件6分为两组,一组所述卡头定位部件6分布地设置在所述天线固定部1-1的接缝面上,相应地,所述天线活动部1-2的接缝面上分布地设置有卡口,另一组所述卡头定位部件6分布地设置在所述天线固定部1-1的口径半圆周上,相应地,所述天线活动部1-2的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣3,所述紧固搭扣3有多个,多个所述紧固搭扣3沿着拼接缝的长度方向分布将所述天线固定部1-1的外表面和所述天线活动部1-2的外表面固定连接在一起。It is also possible that 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. Positioned on the joint surface of the antenna fixing portion 1-1, correspondingly, the seam surface of the antenna movable portion 1-2 is distributedly provided with a bayonet, and 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, and 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.
本实施方式由于采用了所述定位连接部件是铰链定位部件,所述铰链定位部件有两个,所述天线活动部的两端分别通过两个所述铰链定位部件与所述天线固定部的两端铰接,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段,所以,有利于保护天线的反射面。In this embodiment, since 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. End fastening, 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 technical means of being fixedly connected to the outer surface of the movable portion of the antenna is advantageous for protecting the reflective surface of the antenna.
当采用所述定位连接部件是卡头定位部件,所述卡头定位部件有多个,多个所述卡头定位部件分为两组,一组所述卡头定位部件分布地设置在所述天线活动部的接缝面上,相应地,所述天线固定部的接缝面上分布地设置有卡口,另一组所述卡头定位部件分布地设置在所述天线活动部的口径半圆周上,相应地,所述天线固定部的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段时,同样有利于保护天线的反射面。When 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 Correspondingly, 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. Correspondingly, a bayonet is disposed on the half circumference of the antenna fixing portion, and the fixed connecting member is a fastening buckle, and the fastening buckle has a plurality of the fastening portions. When the buckle is distributed along the longitudinal direction of the splicing seam to fix the outer surface of the antenna fixing portion and the outer surface of the movable portion of the antenna together, it is also advantageous to protect the reflecting surface of the antenna.
当采用所述定位连接部件是卡头定位部件,所述卡头定位部件有多个,多个所述卡头定位部件分为两组,一组所述卡头定位部件分布地设置在所述天线固定部的接缝面上,相应地,所述天线活动部的接缝面上分布地设置有卡口,另一组所述卡头定位部件分布地设置在所述天线固定部的口径半圆周上,相应地,所述天线活动部的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣,所述紧固搭扣有多个,多个所述紧固搭扣沿着拼接缝的长度方向分布将所述天线固定部的外表面和所述天线活动部的外表面固定连接在一起的技术手段时,同样有利于保护天线的反射面。When 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 Correspondingly, a seam is disposed on the joint surface of the antenna movable portion, and 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. When the buckle is distributed along the longitudinal direction of the splicing seam to fix the outer surface of the antenna fixing portion and the outer surface of the movable portion of the antenna together, it is also advantageous to protect the reflecting surface of the antenna.
需要说明的是,以上参照附图所描述的各个实施例仅用以说明本发明而非限制本发明的范围,本领域的普通技术人员应当理解,在不脱离本发明的精神和范围的前提下对本发明进行的修改或者等同替换,均应涵盖在本发明的范围之内。此外,除上下文另有所指外,以单数形式出现的词包括复数形式,反之亦然。另外,除非特别说明,那么任何实施例的全部或一部分可结合任何其它实施例的全部或一部分来使用。 It should be noted that the various embodiments described above with reference to the accompanying drawings are only to illustrate the invention and not to limit the scope of the invention, and those of ordinary skill in the art should understand that without departing from the spirit and scope of the invention Modifications or equivalents to the invention are intended to be included within the scope of the invention. In addition, unless the context indicates otherwise, words in the singular include plural and vice versa. In addition, all or a portion of any embodiment can be used in combination with all or a portion of any other embodiment, unless otherwise stated.

Claims (10)

  1. 一种便携式卫星通信旋转抛物面天线,包括旋转抛物面天线(1),所述旋转抛物面天线(1)由天线固定部(1-1)和天线活动部(1-2)拼接组合而成,所述天线固定部(1-1)有一个,其特征在于:所述天线活动部(1-2)有一个,所述天线活动部(1-2)和所述天线固定部(1-1)之间通过连接部件固定连接。A portable satellite communication rotating parabolic antenna comprising a rotating parabolic antenna (1), the rotating parabolic antenna (1) being spliced and assembled by an antenna fixing portion (1-1) and an antenna moving portion (1-2), There is one antenna fixing portion (1-1), characterized in that: one of the antenna movable portions (1-2), the antenna movable portion (1-2) and the antenna fixing portion (1-1) The connection is fixed by the connecting member.
  2. 根据权利要求1所述的便携式卫星通信抛物面天线,其特征在于:所述天线固定部(1-1)和所述天线活动部(1-2)相对于拼接面镜像对称,所述拼接面是所述天线固定部(1-1)和所述天线活动部(1-2)之间相对接的拼接缝所在的平面,所述旋转抛物面天线(1)的轴线位于所述拼接面内。The portable satellite communication parabolic antenna according to claim 1, wherein said antenna fixing portion (1-1) and said antenna movable portion (1-2) are mirror-symmetrical with respect to a splicing surface, and said splicing surface is A plane in which the splicing seam between the antenna fixing portion (1-1) and the antenna movable portion (1-2) is located, and an axis of the rotating parabolic antenna (1) is located in the splicing plane.
  3. 根据权利要求2所述的便携式卫星通信抛物面天线,其特征在于:所述拼接面与所述旋转抛物面天线(1)的口径面相交的直线平行于水平面。The portable satellite communication parabolic antenna according to claim 2, characterized in that the line of the splicing surface intersecting the aperture surface of the rotating parabolic antenna (1) is parallel to the horizontal plane.
  4. 根据权利要求1所述的便携式卫星通信抛物面天线,其特征在于:所述连接部件包括定位连接部件和/或固定连接部件。The portable satellite communication parabolic antenna according to claim 1, wherein said connecting member comprises a positioning connecting member and/or a fixed connecting member.
  5. 根据权利要求4所述的便携式卫星通信抛物面天线,其特征在于:所述定位连接部件是旋转定位部件(2),所述旋转定位部件(2)包括定位轴座(2-1),所述定位轴座(2-1)的前端通过延伸连接固定部件(2-9)与所述天线固定部(1-1)的外底面固定连接,所述定位轴座(2-1)偏置于所述天线活动部(1-2)外底面的后方,所述定位轴座(2-1)的轴孔内设置有定位转动轴(2-2),所述定位转动轴(2-2)可在所述定位轴座(2-1)的轴孔内转动,也可沿着轴孔的轴线方向作往复运动,所述定位转动轴(2-2)平行于所述旋转抛物面天线(1)的轴线,所述定位转动轴(2-2)的前端与所述天线活动部(1-2)的外底面固定连接,所述定位转动轴(2-2)的后端设置有手柄(2-3),所述固定连接部件是多个紧固搭扣(3),多个所述紧固搭扣(3)沿着拼接缝的长度方向分布将所述天线固定部(1-1)的外表面和所述天线活动部(1-2)的外表面固定连接在一起。A portable satellite communication parabolic antenna according to claim 4, wherein said positioning connecting member is a rotational positioning member (2), said rotational positioning member (2) comprising a positioning shaft seat (2-1), said The front end of the positioning shaft seat (2-1) is fixedly connected to the outer bottom surface of the antenna fixing portion (1-1) by an extension connecting fixing member (2-9), and the positioning shaft seat (2-1) is offset from a rear side of 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) Rotating within the shaft hole of the positioning shaft seat (2-1) or reciprocating along the axial direction of the shaft hole, the positioning rotation shaft (2-2) being parallel to the rotating parabolic antenna (1) An axis of the positioning rotating shaft (2-2) is fixedly coupled to an outer bottom surface of the antenna movable portion (1-2), and a rear end of the positioning rotating shaft (2-2) is provided with a handle ( 2-3) the fixed connecting member is a plurality of fastening buckles (3), and the plurality of fastening buckles (3) are distributed along the length direction of the splicing slit to fix the antenna fixing portion (1) 1) an outer surface and the antenna movable portion (1-2) Fixedly connected to the surface.
  6. 根据权利要求5所述的便携式卫星通信抛物面天线,其特征在于:所述定位轴座(2-1)的形状呈圆筒状,所述定位轴座(2-1)的侧壁前部沿着该定位轴座(2-1)的长度方向设置有导向长豁口,所述导向长豁口的深度大于所述天线活动部(1-2)底部的厚度,相应地,所述定位转动轴(2-2)的侧面设置有导向块(2-4),当所述天线固定部(1-1)和天线活动部(1-2)之间相对接时,所述导向块(2-4)位于所述导向长豁口的底部;或者,The portable satellite communication parabolic antenna according to claim 5, wherein said positioning shaft base (2-1) has a cylindrical shape, and a front side edge of said positioning shaft base (2-1) 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 greater than the thickness of the bottom of the movable portion (1-2) of the antenna, and correspondingly, the positioning rotating shaft ( The side surface of 2-2) is provided with a guiding block (2-4), and when the antenna fixing portion (1-1) and the antenna movable portion (1-2) are in contact with each other, the guiding block (2-4) ) at the bottom of the guiding long slit; or,
    所述定位轴座(2-1)的侧壁位于同一直径的两端分别设置有轴向凹槽,其中,一个轴向凹槽长,是轴向导向槽(2-1-1),所述轴向导向槽(2-1-1)的长度大于所述天线活动部(1-2)底面的厚度,另一个凹槽短,是固定槽(2-1-2),所述固定槽(2-1-2)的长度大于所述导向块(2-4)的轴向长度,所述轴向导向槽(2-1-1)的前端和所述固定槽(2-1-2)的前端通过半圆形的周向导向槽(2-1-3)连通,所述导向块(2-4)依次在所述轴向导向槽(2-1-1)、周向导向槽(2-1-3)、固定槽(2-1-2)中往复运动,当所述天线固定部(1-1)和天线活动部(1-2)之间相对接时,所述导向块(2-4)位于所述轴向导向槽(2-1-1)的后端。 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 (2-1-1). The length of the axial guiding groove (2-1-1) is larger than the thickness of the bottom surface of the movable portion (1-2) of the antenna, and the other groove is short, which is a fixing groove (2-1-2), the fixing groove The length of (2-1-2) is larger than the axial length of the guide block (2-4), the front end of the axial guide groove (2-1-1) and the fixed groove (2-1-2) The front end is communicated by a semicircular circumferential guiding groove (2-1-3), and the guiding block (2-4) is sequentially in the axial guiding groove (2-1-1), the circumferential guiding groove (2-1-3), reciprocating motion in the fixing groove (2-1-2), when the antenna fixing portion (1-1) and the antenna movable portion (1-2) are in contact with each other, the guiding The block (2-4) is located at the rear end of the axial guide groove (2-1-1).
  7. 根据权利要求6所述的便携式卫星通信抛物面天线,其特征在于:所述导向块(2-4)的后端面上设置有滚珠(2-5)。The portable satellite communication parabolic antenna according to claim 6, characterized in that the rear end surface of the guide block (2-4) is provided with balls (2-5).
  8. 根据权利要求6所述的便携式卫星通信抛物面天线,其特征在于:所述导向长豁口内的侧面设置有阻止所述导向块(2-4)自由运动的弹簧滚珠制动部件(2-6),和/或,所述定位转动轴(2-2)的后部套置有压缩复位弹簧(2-7),所述压缩复位弹簧(2-7)位于所述定位轴座(2-1)的后端与所述手柄(2-3)之间。The portable satellite communication parabolic antenna according to claim 6, wherein a side of the guide long slit is provided with a spring ball brake member (2-6) for preventing free movement of the guide block (2-4). And/or, a 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 positioning shaft seat (2-1) Between the back end and the handle (2-3).
  9. 根据权利要求6所述的便携式卫星通信抛物面天线,其特征在于:所述定位轴座(2-1)的侧壁前部沿着该定位轴座(2-1)的长度方向设置有固定短豁口,所述固定短豁口与所述导向长豁口位于同一直径上,所述固定短豁口的长度大于所述导向块(2-4)的轴向长度,所述固定短豁口内的侧面设置有阻止所述导向块(2-4)自由运动的弹簧滚珠制动部件(2-8)。The portable satellite communication parabolic antenna according to claim 6, wherein the front side wall of the positioning shaft base (2-1) is fixed short along the longitudinal direction of the positioning shaft seat (2-1). a gap, 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 surface of the fixed short gap is provided A spring ball brake member (2-8) that prevents the guide block (2-4) from moving freely.
  10. 根据权利要求4所述的便携式卫星通信抛物面天线,其特征在于:所述定位连接部件是铰链定位部件(5),所述铰链定位部件(5)有两个,所述天线活动部(1-2)的两端分别通过两个所述铰链定位部件(5)与所述天线固定部(1-1)的两端铰接,所述固定连接部件是紧固搭扣(3),所述紧固搭扣(3)有多个,多个所述紧固搭扣(3)沿着拼接缝的长度方向分布将所述天线固定部(1-1)的外表面和所述天线活动部(1-2)的外表面固定连接在一起;或者,A portable satellite communication parabolic antenna according to claim 4, wherein said positioning connecting member is a hinge positioning member (5), said hinge positioning member (5) has two, said antenna movable portion (1) Both ends of 2) are respectively hinged to both ends of the antenna fixing portion (1-1) by two hinge positioning members (5), and the fixed connecting member is a fastening buckle (3), the tight There are a plurality of fastening buckles (3), and a 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; or,
    所述定位连接部件是卡头定位部件(6),所述卡头定位部件(6)有多个,多个所述卡头定位部件(6)分为两组,一组所述卡头定位部件(6)分布地设置在所述天线活动部(1-2)的接缝面上,相应地,所述天线固定部(1-1)的接缝面上分布地设置有卡口,另一组所述卡头定位部件(6)分布地设置在所述天线活动部(1-2)的口径半圆周上,相应地,所述天线固定部(1-1)的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣(3),所述紧固搭扣(3)有多个,多个所述紧固搭扣(3)沿着拼接缝的长度方向分布将所述天线固定部(1-1)的外表面和所述天线活动部(1-2)的外表面固定连接在一起;或者,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 one set of the chuck positioning The component (6) is distributedly disposed on the joint surface of the antenna movable portion (1-2), and correspondingly, the joint surface of the antenna fixing portion (1-1) is distributed with a bayonet, and A set of the chuck positioning members (6) are distributedly disposed on a half circumference of the antenna movable portion (1-2), and correspondingly, the antenna fixing portion (1-1) is distributed on a half circumference of the aperture Is provided with a bayonet, the fixed connecting component is a fastening buckle (3), the fastening buckle (3) has a plurality of, the plurality of the fastening buckles (3) along the splicing seam a longitudinal direction distribution fixedly connecting the outer surface of the antenna fixing portion (1-1) and the outer surface of the antenna movable portion (1-2); or
    所述定位连接部件是卡头定位部件(6),所述卡头定位部件(6)有多个,多个所述卡头定位部件(6)分为两组,一组所述卡头定位部件(6)分布地设置在所述天线固定部(1-1)的接缝面上,相应地,所述天线活动部(1-2)的接缝面上分布地设置有卡口,另一组所述卡头定位部件(6)分布地设置在所述天线固定部(1-1)的口径半圆周上,相应地,所述天线活动部(1-2)的口径半圆周上分布地设置有卡口,所述固定连接部件是紧固搭扣(3),所述紧固搭扣(3)有多个,多个所述紧固搭扣(3)沿着拼接缝的长度方向分布将所述天线固定部(1-1)的外表面和所述天线活动部(1-2)的外表面固定连接在一起。 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 one set of the chuck positioning The component (6) is distributedly disposed on the joint surface of the antenna fixing portion (1-1), and correspondingly, the seam surface of the antenna movable portion (1-2) is distributed with a bayonet, and A set of the chuck positioning members (6) are distributedly disposed on a half circumference of the aperture of the antenna fixing portion (1-1), and correspondingly, a half circumference of the antenna movable portion (1-2) is distributed Is provided with a bayonet, the fixed connecting component is a fastening buckle (3), the fastening buckle (3) has a plurality of, the plurality of the fastening buckles (3) along the splicing seam The longitudinal direction distribution securely connects the outer surface of the antenna fixing portion (1-1) and the outer surface of the antenna movable portion (1-2).
PCT/CN2016/096965 2015-11-16 2016-08-26 Portable satellite communication rotational parabola antenna WO2017084403A1 (en)

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