Mounting structure of airborne radiometer

Abstract

The utility model relates to the technical field of mounting structures, and discloses a mounting structure of an airborne radiometer, which comprises a bottom plate, the top of the bottom plate is fixedly connected with a sleeve block, the top of the sleeve block is slidably connected with a sleeve plate, the top of the sleeve plate is fixedly connected with a body, two sides of the sleeve block are provided with a plurality of accommodating grooves, and the top of the sleeve block is symmetrically provided with a plurality of first sliding grooves. A second sliding groove is formed in one side of each first sliding groove, limiting grooves are formed in the bottoms of the first sliding grooves and the bottoms of the second sliding grooves, T-shaped plates are slidably connected into the first sliding grooves, the second sliding grooves and the limiting grooves, and adjusting mechanisms used for adjusting the T-shaped plates are arranged at the tops of the T-shaped plates. Through the arrangement of the T-shaped plate, the body can be connected and fixed, the installation mode is carried out under the pushing of the limiting column, and the limiting column is connected with the bottom plate through the spring, so that when the aircraft vibrates, the limiting column can be adjusted and cached through the spring, and the body can be prevented from loosening.

Description

Technical Field

[0001] This utility model relates to the field of installation structure technology, and in particular to an installation structure for an airborne radiometer. Background Technology

[0002] An airborne radiometer is an instrument used to measure atmospheric radiation. Typically mounted on the surface of an aircraft or drone, its primary function is to monitor and record electromagnetic radiation at various wavelengths. This data is crucial for meteorological research, environmental monitoring, and agricultural management. Airborne radiometers capture radiation signals using photodetectors and convert them into electrical signals for analysis. Depending on the application, radiometers can be designed as multi-band or broadband to obtain more comprehensive radiation information. For example, multispectral radiometers can observe multiple bands, including visible light, near-infrared, and thermal infrared, providing information on vegetation health, soil moisture, and water quality. In agriculture, airborne radiometers enable precision agriculture, guiding crop management with data to improve crop yield and quality.

[0003] When using an airborne radiometer, it needs to be connected to the aircraft first. Most airborne radiometers are connected to the aircraft by bolts. During flight, the operation of the engine, the aerodynamic load on the wings, and the wear of parts can all cause resonance, which in turn generates vibration. As a result, the bolts are prone to loosening over time. Therefore, this problem needs to be solved. Utility Model Content

[0004] The purpose of this invention is to address the shortcomings of existing technologies by proposing an installation structure for an airborne radiometer.

[0005] To achieve the above objectives, the present invention adopts the following technical solution:

[0006] An installation structure for an airborne radiometer includes a base plate. A sleeve block is fixedly connected to the top of the base plate, and a sleeve plate is slidably connected to the top of the sleeve block. A main body is fixedly connected to the top of the sleeve plate. Multiple storage slots are provided on both sides of the sleeve block, and each of the multiple storage slots is provided with a constraint mechanism for constraining the sleeve plate. Multiple first sliding grooves are symmetrically provided on the top of the sleeve block, and a second sliding groove is provided on one side of each of the multiple first sliding grooves. Limiting grooves are provided at the bottom of each of the multiple first sliding grooves, second sliding grooves, and limiting grooves. T-shaped plates are slidably connected inside each of the multiple first sliding grooves, second sliding grooves, and limiting grooves. Adjustment mechanisms are provided on the top of each of the multiple T-shaped plates for adjusting the T-shaped plates. The main body can be connected and fixed by the T-shaped plates.

[0007] As a further embodiment of this utility model, the constraint mechanism includes a limiting post, which is slidably connected to the inside of the storage groove. A limiting rod is fixedly connected to the surface of the limiting post away from the sleeve plate. The limiting rod is slidably connected to one side of the inside of the storage groove. A spring is sleeved on the surface of the limiting rod. One end of the spring is fixedly connected to one side of the inside of the storage groove, and the other end of the spring is fixedly connected to one side of the limiting post. Four mounting holes are opened on the top of the base plate. The four mounting holes are evenly spaced in a square shape. By setting the limiting rod, the sleeve plate can be constrained.

[0008] As a further embodiment of this utility model, the adjustment mechanism includes two constraint plates, which are respectively fixedly connected to both ends of the sleeve plate. The same push plate is slidably connected to the surface of the two constraint plates. The T-shaped plate is fixedly connected to the bottom of the push plate. The top of the push plate near the T-shaped plate is provided with a moving mechanism for moving the push plate. The T-shaped plate can be adjusted by the push plate.

[0009] As a further embodiment of this utility model, the moving mechanism includes a first adjusting arm, which is rotatably connected to one side of the sleeve plate. A pull plate is rotatably connected to the end of the first adjusting arm away from the push plate. A limit hole is provided on the side of the sleeve plate near the limit post. A docking post is fixedly connected to the surface of the pull plate near the limit post. The limit post and the docking post are slidably connected inside the limit hole and cooperate with each other. A second adjusting arm is rotatably connected to the end of the first adjusting arm near the push plate. The other end of the second adjusting arm is rotatably connected to the top of the push plate. By setting the adjusting arm, the push plate can be moved.

[0010] The beneficial effects of this utility model are as follows:

[0011] 1. This utility model employs a technical solution of fixing the main body with limiting posts, thus preventing the main body from becoming loose. This effectively solves the problem that during flight, the operation of the engine, the aerodynamic load on the wings, and the wear of parts can all cause resonance and vibration, leading to loosening of bolts over time. When the push plate is pulled into place, the limiting groove will release the constraint on the T-shaped plate, and the limiting post will also release the constraint on the sleeve plate. When both constraints are released, the main body can be removed. This installation method is carried out by the push of the limiting post, which is connected to the base plate by a spring. Therefore, when the aircraft vibrates, the spring can adjust and buffer the limiting post, thus preventing the main body from becoming loose. Attached Figure Description

[0012] Figure 1 This is a schematic diagram of the overall structure of the installation structure of an airborne radiometer proposed in this utility model;

[0013] Figure 2 This is a schematic diagram of the layered structure of the installation structure of an airborne radiometer proposed in this utility model;

[0014] Figure 3 This is a schematic diagram of the constraint mechanism of the installation structure of an airborne radiometer proposed in this utility model;

[0015] Figure 4 This is a schematic diagram of the adjustment mechanism of the installation structure of an airborne radiometer proposed in this utility model;

[0016] Figure 5 for Figure 4 A magnified structural diagram at point A in the diagram.

[0017] In the diagram: 1. Base plate; 2. Limiting post; 3. Sleeve plate; 4. Pull plate; 5. Body; 101. Mounting hole; 102. Sleeve block; 103. Storage groove; 104. First sliding groove; 105. Second sliding groove; 106. Limiting groove; 201. Limiting rod; 202. Spring; 301. Limiting hole; 302. Constraint plate; 401. Connecting post; 402. First adjusting arm; 403. Second adjusting arm; 404. Push plate; 405. T-shaped plate. Detailed Implementation

[0018] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments.

[0019] Reference Figure 1 - Figure 5 An installation structure for an airborne radiometer includes a base plate 1. A sleeve block 102 is fixedly connected to the top of the base plate 1. A sleeve plate 3 is slidably connected to the top of the sleeve block 102. A body 5 is fixedly connected to the top of the sleeve plate 3. Multiple storage slots 103 are provided on both sides of the sleeve block 102. Each of the multiple storage slots 103 is provided with a constraint mechanism for constraining the sleeve plate 3. Multiple first sliding grooves 104 are symmetrically provided on the top of the sleeve block 102. A second sliding groove 105 is provided on one side of each of the multiple first sliding grooves 104 and the second sliding grooves 105. A limiting groove 106 is provided at the bottom of each of the multiple first sliding grooves 104, the second sliding grooves 105, and the limiting groove 106. A T-shaped plate 405 is slidably connected inside each of the multiple first sliding grooves 104, the second sliding grooves 105, and the limiting groove 106. An adjustment mechanism for adjusting the T-shaped plate 405 is provided on the top of each of the multiple T-shaped plates 405. The body 5 can be connected and fixed by the T-shaped plate 405.

[0020] Reference Figure 3 and Figure 4In a preferred embodiment, the constraint mechanism includes a limiting post 2, which is slidably connected to the inside of the storage groove 103. A limiting rod 201 is fixedly connected to the surface of the limiting post 2 away from the sleeve plate 3. The limiting rod 201 is slidably connected to the inside of the storage groove 103. A spring 202 is sleeved on the surface of the limiting rod 201. One end of the spring 202 is fixedly connected to the inside of the storage groove 103, and the other end of the spring 202 is fixedly connected to the side of the limiting post 2. Four mounting holes 101 are opened on the top of the bottom plate 1. The four mounting holes 101 are evenly spaced in a square shape. The sleeve plate 3 can be constrained by the setting of the limiting rod 201.

[0021] Reference Figure 4 and Figure 5 In a preferred embodiment, the adjustment mechanism includes two constraint plates 302, which are fixedly connected to both ends of the sleeve plate 3. The same push plate 404 is slidably connected to the surface of the two constraint plates 302. A T-shaped plate 405 is fixedly connected to the bottom of the push plate 404. The top of the push plate 404 near the T-shaped plate 405 is provided with a moving mechanism for moving the push plate 404. The T-shaped plate 405 can be adjusted by the push plate 404.

[0022] Reference Figure 4 and Figure 5 In a preferred embodiment, the moving mechanism includes a first adjusting arm 402, which is rotatably connected to one side of the sleeve plate 3. A pull plate 4 is rotatably connected to the end of the first adjusting arm 402 away from the push plate 404. A limiting hole 301 is provided on the side of the sleeve plate 3 near the limiting post 2. A docking post 401 is fixedly connected to the surface of the pull plate 4 near the limiting post 2. The limiting post 2 and the docking post 401 are both slidably connected inside the limiting hole 301 and cooperate with each other. A second adjusting arm 403 is rotatably connected to the end of the first adjusting arm 402 near the push plate 404. The other end of the second adjusting arm 403 is rotatably connected to the top of the push plate 404. By setting the adjusting arm, the push plate 404 can be moved.

[0023] From the above description, it can be seen that the above embodiments of this utility model achieve the following technical effects: When the main body 5 needs to be disassembled, the push plate 404 can be pulled. A T-shaped plate 405 is installed at the bottom of the push plate 404, and the T-shaped plate 405 is initially inside the limiting groove 106. Thus, under the constraint of the limiting groove 106, the main body 5 can be connected and fixed. A first adjusting arm 402 is installed on one side of the push plate 404. Because the push plate 404 is connected to one end of the first adjusting arm 402, when the push plate 404 drives one end of the first adjusting arm 402 to move, the other end of the first adjusting arm 402 will move synchronously. Because the center position of the first adjusting arm 402 is constant, the two ends of the first adjusting arm 402 move in opposite directions. A docking post 401 is installed at the other end of the first adjusting arm 402, and the docking post 401 is initially sliding. Inside the limiting hole 301, when the push plate 404 moves backward, the docking post 401 moves forward. Inside the limiting hole 301, a limiting post 2 is also installed, and the limiting post 2 cooperates with the docking post 401. Thus, when the docking post 401 is pushed, the limiting post 2 will also move synchronously. Through the push of the docking post 401, the limiting post 2 will eventually enter the sleeve block 102. After the push plate 404 is pulled into place, the limiting groove 106 will release the constraint on the T-shaped plate 405, and the limiting post 2 will also release the constraint on the sleeve plate 3. When both constraints are released, the body 5 can be removed. This installation method is carried out under the push of the limiting post 2. The limiting post 2 is connected to the base plate 1 by a spring 202. Thus, when the aircraft vibrates, the spring 202 can adjust and buffer the limiting post 2, thereby preventing the body 5 from becoming loose.

[0024] For ease of description, spatial relative terms such as "above," "on top of," "on the upper surface of," "above," etc., are used herein to describe the spatial positional relationship of a device or feature as shown in the figures to other devices or features. It should be understood that spatial relative terms are intended to encompass different orientations in use or operation beyond the orientation of the device as described in the figures. For example, if the device in the figures were inverted, a device described as "above" or "on top of" other devices or structures would subsequently be positioned as "below" or "under" other devices or structures. Thus, the exemplary term "above" can include both "above" and "below." The device may also be positioned in other different ways (rotated 90 degrees or in other orientations), and the spatial relative descriptions used herein will be interpreted accordingly.

[0025] It should be noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the exemplary embodiments according to this application. As used herein, the singular form is intended to include the plural form as well, unless the context clearly indicates otherwise. Furthermore, it should be understood that when the terms "comprising" and / or "including" are used in this specification, they indicate the presence of features, steps, operations, devices, components, and / or combinations thereof.

[0026] It should be noted that the terms "first," "second," etc., in the specification, claims, and accompanying drawings of this application are used to distinguish similar objects and are not necessarily used to describe a specific order or sequence. It should be understood that such data can be interchanged where appropriate so that the embodiments of this application described herein can be implemented, for example, in orders other than those illustrated or described herein. Furthermore, the terms "comprising" and "having," and any variations thereof, are intended to cover non-exclusive inclusion; for example, a process, method, system, product, or apparatus that comprises a series of steps or units is not necessarily limited to those steps or units explicitly listed, but may include other steps or units not explicitly listed or inherent to such processes, methods, products, or apparatus.

[0027] The above description is merely a preferred embodiment of this utility model and is not intended to limit the utility model. Various modifications and variations can be made to this utility model by those skilled in the art. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. An installation structure for an airborne radiometer, comprising a base plate (1), characterized in that, The top of the base plate (1) is fixedly connected to a sleeve block (102), the top of the sleeve block (102) is slidably connected to a sleeve plate (3), the top of the sleeve plate (3) is fixedly connected to a body (5), the sleeve block (102) has multiple storage slots (103) on both sides, the multiple storage slots (103) are provided with a constraint mechanism for constraining the sleeve plate (3), the top of the sleeve block (102) is symmetrically provided with multiple first sliding grooves (104), the multiple first sliding grooves (104) are provided with a second sliding groove (105) on one side, the multiple first sliding grooves (104) and the second sliding grooves (105) are provided with a limit groove (106) at the bottom, the multiple first sliding grooves (104), the second sliding grooves (105) and the limit grooves (106) are slidably connected with T-shaped plates (405), the top of the multiple T-shaped plates (405) are provided with an adjustment mechanism for adjusting the T-shaped plates (405).

2. The mounting structure of the airborne radiometer according to claim 1, characterized in that, The constraint mechanism includes a limiting post (2), which is slidably connected to the inside of the storage groove (103). A limiting rod (201) is fixedly connected to the surface of the limiting post (2) away from the sleeve plate (3), and the limiting rod (201) is slidably connected to the inside of the storage groove (103).

3. The mounting structure of the airborne radiometer according to claim 2, characterized in that, A spring (202) is fitted on the surface of the limiting rod (201). One end of the spring (202) is fixedly connected to one side of the inside of the storage groove (103), and the other end of the spring (202) is fixedly connected to one side of the limiting post (2). Four mounting holes (101) are opened on the top of the base plate (1), and the four mounting holes (101) are evenly opened in a square shape.

4. The mounting structure of the airborne radiometer according to claim 1, characterized in that, The adjustment mechanism includes two constraint plates (302), which are fixedly connected to both ends of the sleeve plate (3). The same push plate (404) is slidably connected to the surface of the two constraint plates (302). The T-shaped plate (405) is fixedly connected to the bottom of the push plate (404). The top of the push plate (404) near the T-shaped plate (405) is provided with a moving mechanism for moving the push plate (404).

5. The mounting structure of the airborne radiometer according to claim 4, characterized in that, The moving mechanism includes a first adjusting arm (402), which is rotatably connected to one side of the sleeve plate (3). A pull plate (4) is rotatably connected to the end of the first adjusting arm (402) away from the push plate (404). A limit hole (301) is opened on the side of the sleeve plate (3) near the limit post (2). A docking post (401) is fixedly connected to the surface of the pull plate (4) near the limit post (2).

6. The mounting structure of the airborne radiometer according to claim 5, characterized in that, The limiting post (2) and the docking post (401) are slidably connected inside the limiting hole (301), and the limiting post (2) and the docking post (401) cooperate with each other. The first adjusting arm (402) is rotatably connected to the end near the push plate (404) with a second adjusting arm (403), and the other end of the second adjusting arm (403) is rotatably connected to the top of the push plate (404).

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