Remote sensing satellite ground receiving terminal

Abstract

The utility model relates to the technical field of satellite communication, and provides a remote sensing satellite ground receiving terminal, which comprises a remote sensing satellite receiving terminal, a ground terminal support frame arranged below the remote sensing satellite receiving terminal, a support seat fixedly connected to the bottom end of the ground terminal support frame, and a moving groove arranged inside the support seat. A fixed cone plate is arranged in the moving groove, a first sliding groove is formed in the side edge of the fixed cone plate, a sliding rod is slidably connected into the first sliding groove, one end of the sliding rod is fixedly connected with the fixed cone plate, and the other end of the sliding rod is fixedly connected with a pulling block. Through cooperation of a supporting seat, a moving groove, a second limiting groove, a limiting rod and an outer supporting block, when the remote sensing satellite receiving terminal is located on a soft land for signal receiving, a fixed cone plate can move in the moving groove, so that the fixed cone plate extends outwards, at the moment, after the fixed cone plate is inserted into the soil ground, the stability of the equipment is enhanced, and the stability of the equipment is improved. And the equipment signal receiving efficiency is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of satellite communications, in particular to a remote sensing satellite ground receiving terminal. Background Art

[0002] Remote sensing satellite ground receiving terminals are primarily used to receive signals from remote sensing satellites, including images, meteorological data, and geographic information. These signals are typically installed on the ground and capture satellite signals using antennas and other receiving devices. However, current technology exhibits limitations in some scenarios, particularly when operating on soil surfaces, where stability and signal reception efficiency may be compromised.

[0003] Remote sensing satellite ground receiving terminals may need to be used in various environments, including soft soil. Soil is prone to deformation and sinking, especially after rain or in humid conditions. This unstable ground condition can lead to unstable installation of the receiving terminal, causing it to wobble or tilt, which in turn affects antenna alignment and signal reception stability. Therefore, a remote sensing satellite ground receiving terminal is proposed to address this issue. Utility Model Content

[0004] The utility model provides a remote sensing satellite ground receiving terminal, which solves the problems in the related art that the remote sensing satellite ground receiving terminal is unstable when working on soil ground and has low signal receiving efficiency.

[0005] The technical solution of the utility model is as follows: a remote sensing satellite ground receiving terminal, including a remote sensing satellite receiving terminal, a ground terminal support frame is arranged under the remote sensing satellite receiving terminal, the bottom end of the ground terminal support frame is fixedly connected to a support seat, a movable groove is opened inside the support seat, a fixed cone plate is arranged inside the movable groove, a first slide groove is arranged on the side of the fixed cone plate, a slide rod is slidably connected inside the first slide groove, one end of the slide rod is connected to the fixed cone plate in a fixed state, and the other end of the slide rod is fixedly connected to a pulling block.

[0006] Optionally, the bottom end of the fixed cone plate is arranged in a cone shape in the longitudinal direction, and groups of external support blocks are arranged on both sides of the fixed cone plate, and each group of external support blocks is arranged in a transverse cone shape.

[0007] Optionally, the first sliding groove is symmetrically arranged on the support seat, sliding rods are symmetrically arranged on both sides of the fixed cone plate, and the outer walls of the sliding rods are arranged in a fit shape with the first sliding groove.

[0008] Optionally, a second sliding groove is provided inside the pulling block, a moving rod is slidably connected inside the second sliding groove, a spring is wrapped around the outer wall of the moving rod, the moving rod passes through the second sliding groove and is fixedly connected to an auxiliary handle, and limiting rods are fixedly connected on both sides of the auxiliary handle, a first limiting groove is provided on the side of the support seat, a second limiting groove is provided at the lower end of the first limiting groove, and the limiting rod is inserted inside the first limiting groove.

[0009] Optionally, one end of the spring is fixedly connected to the moving rod, and the other end of the spring is fixedly connected to the second sliding groove.

[0010] Optionally, the first limiting groove and the second limiting groove are symmetrically arranged on both sides of the first sliding groove, and the limiting rods are symmetrically arranged on both sides of the pulling block.

[0011] Optionally, the first limiting groove and the second limiting groove have the same opening diameter, and the outer wall of the limiting rod fits with the inner wall of the first limiting groove.

[0012] Optionally, a pulling ring is fixedly connected to the outer end of the auxiliary handle, the pulling ring is arranged in a ring shape, and the outer wall of the pulling ring is provided with anti-slip lines.

[0013] The working principle and beneficial effects of the utility model are as follows: through the cooperation of the support seat, the movable groove, the first slide groove, the fixed cone plate, the slide rod, the pulling block, the second slide groove, the spring, the movable rod, the auxiliary handle, the pulling ring, the first limit groove, the second limit groove, the limit rod and the outer support block, when the remote sensing satellite receiving terminal is on relatively soft land for signal reception, it can be moved in the movable groove through the fixed cone plate, so that the fixed cone plate is extended outward. At this time, after the fixed cone plate is inserted into the soil ground, the stability of the equipment is enhanced, and the efficiency of the equipment in receiving signals is improved. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The preferred implementation scheme will be described below in a clear and understandable manner with reference to the accompanying drawings to further illustrate the above-mentioned characteristics, technical features, advantages and implementation methods of the present invention.

[0015] The present invention will be further described in detail below with reference to the accompanying drawings and specific implementation methods.

[0016] Figure 1 This is a schematic diagram of the three-dimensional structure of the remote sensing satellite receiving terminal of the utility model;

[0017] Figure 2 For this utility model Figure 1 A magnified view of the structure at point A;

[0018] Figure 3 This is a schematic diagram of a three-dimensional partial cross-sectional structure of the ground terminal support frame of the utility model;

[0019] Figure 4 For this utility model Figure 3 A magnified view of the structure at point B.

[0020] Figure 5 It is a schematic diagram of the three-dimensional local structure of the fixed cone plate of the utility model.

[0021] In the figure: 1. Remote sensing satellite receiving terminal; 2. Ground terminal support frame; 3. Support seat; 4. Moving groove; 5. First slide groove; 6. Fixed cone plate; 7. Slide rod; 8. Pulling block; 9. Second slide groove; 10. Spring; 11. Moving rod; 12. Auxiliary handle; 13. Pulling ring; 14. First limiting groove; 15. Second limiting groove; 16. Limiting rod; 17. External support block. DETAILED DESCRIPTION

[0022] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the specific implementation methods of the present invention will be described below with reference to the accompanying drawings. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings and other implementation methods can be obtained based on these drawings without inventive work.

[0023] To simplify the drawings, only the parts relevant to the utility model are schematically shown in each figure; they do not represent the actual structure of the product. Furthermore, to simplify the drawings and facilitate understanding, in some figures, only one of the components with the same structure or function is schematically shown or labeled. In this document, "one" not only means "only one" but also "more than one," and "several" includes "two" and "more than two."

[0024] It should be noted that, unless otherwise specified or limited, the terms "mounted," "connected," and "connected" should be understood broadly. For example, they can refer to fixed, detachable, or integral connections; mechanical or electrical connections; direct or indirect connections through an intermediary; and internal communication between two components. Those skilled in the art will understand the specific meanings of these terms in this utility model based on the specific circumstances.

[0025] In addition, in the description of the present application, the terms "first", "second", etc. are only used to distinguish the description and cannot be understood as indicating or implying relative importance.

[0026] Refer to the instruction manual Figure 1-5The support frame 3 is fixed on the support frame 3 and the support frame 3 is provided with a movable groove 4. The movable groove 4 is provided inside the support frame 3. The side of the movable groove 4 is provided with a fixed cone plate 6. The first slide groove 5 is provided on the side of the fixed cone plate 6. The first slide groove 5 is slidably connected with a slide rod 7. One end of the slide rod 7 is connected to the fixed cone plate 6 in a fixed state, and the other end of the slide rod 7 is fixedly connected to a pulling block 8. When the remote sensing satellite receiving terminal 1 is on a relatively soft soil ground, the sliding effect of the slide rod 7 and the first slide groove 5 can drive the fixed cone plate 6 to slide in the movable groove 4 and slide out. At this time, the fixed cone plate 6 will be inserted into the soil ground, which can effectively provide a stable effect for the remote sensing satellite receiving terminal 1, so that the remote sensing satellite receiving terminal 1 can receive signals in a stable state, thereby improving the use efficiency of the remote sensing satellite receiving terminal 1.

[0027] Then, the bottom end of the fixed cone plate 6 is set in a longitudinal conical shape, and a group of external support blocks 17 are set on both sides of the fixed cone plate 6. Each group of external support blocks 17 is set in a transverse conical shape. The outward expansion shape of the external support blocks 17 can increase the support area of ​​the fixed cone plate 6 inside the soil, thereby making the fixed cone plate 6 more stably fixed inside the soil, thereby improving the stability of the remote sensing satellite receiving terminal 1.

[0028] Then, the first slide groove 5 is symmetrically arranged on the support seat 3, and the sliding rods 7 are symmetrically arranged on both sides of the fixed cone plate 6, and the outer wall of the sliding rod 7 is fitted with the first slide groove 5; through the sliding of the two groups of sliding rods 7 and the first slide groove 5, the sliding out effect of the fixed cone plate 6 in the movable groove 4 is more stable.

[0029] Next, a second slide groove 9 is opened inside the pulling block 8, and a moving rod 11 is slidably connected inside the second slide groove 9. A spring 10 is wrapped around the outer wall of the moving rod 11, and the moving rod 11 passes through the second slide groove 9 and is fixedly connected to an auxiliary handle 12. The auxiliary handle 12 is fixedly connected to a limiting rod 16 on both sides. A first limiting groove 14 is opened on the side of the support seat 3, and a second limiting groove 15 is opened at the lower end of the first limiting groove 14. The limiting rod 16 is inserted into the first limiting groove 14; the sliding of the moving rod 11 inside the second slide groove 9 releases the fixed limit of the insertion of the first limiting groove 14. When the fixed cone plate 6 is extended outward, the second limiting groove 15 is fixedly limited by the limiting rod 16, so that the support seat 3 no longer plays a normal supporting and stabilizing role in the soil ground studio, so that the extended insertion of the fixed cone plate 6 into the soil becomes controllable.

[0030] At this time, one end of the spring 10 is fixedly connected to the moving rod 11, and the other end of the spring 10 is fixedly connected to the second slide groove 9; the elastic performance of the spring 10 drives the moving rod 11 to reset, so that the limit rod 16 can be reset without being affected by external force and inserted into the first limit groove 14 or the second limit groove 15 to ensure the normal operation of the equipment.

[0031] Next, the first limiting groove 14 and the second limiting groove 15 are symmetrically arranged on both sides of the first slide groove 5, and the limiting rod 16 is symmetrically arranged on both sides of the pulling block 8; through this structure, the fixed cone plate 6 is in a fixed state, and the two groups of limiting rods 16 are inserted into the first limiting groove 14 or the second limiting groove 15, further improving the fixing effect.

[0032] Secondly, the first limiting groove 14 and the second limiting groove 15 have the same diameter, and the outer wall of the limiting rod 16 fits with the inner wall of the first limiting groove 14; through this structure, the limiting rod 16 is more stable when inserted in the first limiting groove 14 or the second limiting groove 15, reducing the gap, increasing the friction, and improving the stability effect.

[0033] Finally, a pulling ring 13 is fixedly connected to the outer end of the auxiliary handle 12. The pulling ring 13 is arranged in a ring shape, and the outer wall of the pulling ring 13 is provided with anti-slip grooves. By pulling the pulling ring 13 outward, the moving rod 11 is driven to move and then the insertion limit of the limiting rod 16 on the first limiting groove 14 or the second limiting groove 15 is released, so that the convenience of equipment operation is improved to a certain extent.

[0034] It should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit the present invention. Although the present invention has been described in detail with reference to the preferred embodiments, those skilled in the art should understand that the technical solutions of the present invention may be modified or replaced by equivalents without departing from the spirit and scope of the technical solutions of the present invention, and all of these should be included in the scope of the claims of the present invention.

Claims

1. A remote sensing satellite ground receiving terminal, characterized in that: The invention comprises a remote sensing satellite receiving terminal (1), wherein a ground terminal support frame (2) is provided below the remote sensing satellite receiving terminal (1), a support seat (3) is fixedly connected to the bottom end of the ground terminal support frame (2), a movable groove (4) is provided inside the support seat (3), a fixed cone plate (6) is provided inside the movable groove (4), a first slide groove (5) is provided on the side of the fixed cone plate (6), a slide rod (7) is slidably connected inside the first slide groove (5), one end of the slide rod (7) is fixedly connected to the fixed cone plate (6), and the other end of the slide rod (7) is fixedly connected to the pulling block (8).

2. A remote sensing satellite ground receiving terminal according to claim 1, characterized in that: The bottom end of the fixed cone plate (6) is arranged in a conical shape in the longitudinal direction, and two groups of external support blocks (17) are arranged on both sides of the fixed cone plate (6), and each group of external support blocks (17) is arranged in a transverse conical shape.

3. A remote sensing satellite ground receiving terminal according to claim 1, characterized in that: The first slide groove (5) is symmetrically arranged on the support seat (3), and slide rods (7) are symmetrically arranged on both sides of the fixed cone plate (6), and the outer wall of the slide rod (7) is arranged in a fitting state with the first slide groove (5).

4. A remote sensing satellite ground receiving terminal according to claim 1, characterized in that: A second sliding groove (9) is provided inside the pulling block (8), a moving rod (11) is slidably connected inside the second sliding groove (9), a spring (10) is wound around the outer wall of the moving rod (11), the moving rod (11) passes through the second sliding groove (9) and is fixedly connected to an auxiliary handle (12), and limiting rods (16) are fixedly connected to both sides of the auxiliary handle (12), a first limiting groove (14) is provided on the side of the support seat (3), a second limiting groove (15) is provided at the lower end of the first limiting groove (14), and the limiting rod (16) is inserted into the first limiting groove (14).

5. A remote sensing satellite ground receiving terminal according to claim 4, characterized in that: One end of the spring (10) is fixedly connected to the moving rod (11), and the other end of the spring (10) is fixedly connected to the second sliding groove (9).

6. A remote sensing satellite ground receiving terminal according to claim 4, characterized in that: The first limiting groove (14) and the second limiting groove (15) are symmetrically arranged on both sides of the first sliding groove (5), and the limiting rod (16) is symmetrically arranged on both sides of the pulling block (8).

7. A remote sensing satellite ground receiving terminal according to claim 6, characterized in that: The first limiting groove (14) and the second limiting groove (15) have the same opening diameter, and the outer wall of the limiting rod (16) and the inner wall of the first limiting groove (14) are in contact with each other.

8. A remote sensing satellite ground receiving terminal according to claim 4, characterized in that: The outer end of the auxiliary handle (12) is fixedly connected to a pulling ring (13), the pulling ring (13) is arranged in a ring shape, and the outer wall of the pulling ring (13) is provided with anti-slip patterns.

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