A miniaturized radio frequency microwave transceiver channel device

Abstract

The present invention relates to the field of communication transmission technology, and discloses a miniaturized radio frequency microwave transceiver channel device, comprising a fuselage, wherein the outer wall of the fuselage is provided with heat dissipation holes, the outer wall of the fuselage is provided with an assembly groove, and further comprising: an adjustment mechanism, wherein the adjustment mechanism is arranged inside the assembly groove, the adjustment mechanism comprises a support plate 1, the outer wall of the support plate 1 is fixedly connected to a limit block, the inner wall of the support plate 1 is fixedly connected to a guide sleeve 1, the outer wall of the support plate 1 is connected to a support plate 2 via a rotating shaft hinge, the top of the support plate 2 is provided with an adjustment component, and the guide sleeve 1 is used to adjust the signal transmission direction of a transmitting rod through a spherical sleeve. The present invention supports the transmitting rod through the adjustment mechanism and uniformly adjusts the angle of the transmitting rod, thereby increasing the adjustment efficiency of the transmitting rod and preventing the transmitting rod from becoming loose and unable to be adjusted, thereby increasing the service life of the miniaturized radio frequency microwave transceiver channel device.

Description

Technical Field

[0001] The present invention relates to the field of communication transmission technology, and in particular to a miniaturized radio frequency microwave transceiver channel device. Background Art

[0002] With the development of modern science and technology, products have increasingly higher requirements for the size and performance of internal components. Traditional RF microwave transceiver channel devices are large in size and difficult to operate efficiently in limited spaces. They cannot meet the current trend of miniaturization and integration. Miniaturized RF microwave transceiver channel devices are designed to achieve efficient signal transmission, reception and processing in a small space, help upgrade technological products, and provide new possibilities for meeting product space and functional requirements.

[0003] The patent application with application number CN201320707640.7 discloses a miniaturized microwave transceiver channel device, which relates to a medium-capacity small microwave communication channel device in the communication field. It consists of a crystal oscillator reference source, a frequency synthesizer, a local oscillator switching switch, a power management unit, a differential filter, a radio frequency modulator, a digitally controlled attenuator, a transmit filter amplifier unit, a power amplifier, a coupler, a transmitter detector, a radio frequency transceiver switch, a radio frequency filter, a low-noise amplifier, a receive filter amplifier unit, a first-stage mixer unit, an automatic gain control amplifier and other components.

[0004] However, when existing miniaturized RF microwave transceiver channel devices receive RF signals, part of the signal propagation direction is parallel to the receiving device, resulting in the signal being unable to be received, affecting the integrity of information transmission. When transmitting signals, some angles around the device output signals as useless areas, resulting in a waste of spectrum resources and reducing the overall efficiency of the device. Conventional RF microwave transceiver channel devices require manual adjustment of the antenna transmission direction, making it difficult to control the transmission accuracy. At the same time, long-term use will cause the antenna to become loose, making it impossible to adjust the antenna. Summary of the Invention

[0005] The object of the present invention is to provide a miniaturized radio frequency microwave transceiver channel device to solve the problems raised in the above background technology.

[0006] To achieve the above-mentioned object, the present invention provides the following technical solution: a miniaturized radio frequency microwave transceiver channel device, comprising a body, an outer wall of which is provided with heat dissipation holes, an outer wall of which is provided with an assembly groove, and further comprising:

[0007] An adjustment mechanism is arranged inside the assembly groove, and the adjustment mechanism includes a support plate 1, the outer wall of the support plate 1 is fixedly connected to a limit block, the inner wall of the support plate 1 is fixedly connected to a guide sleeve 1, the inner wall of the guide sleeve 1 is covered with a spherical sleeve, the inner wall of the spherical sleeve is fixedly connected to a transmitting rod, the outer wall of the support plate 1 is connected to the support plate 2 through a rotating shaft hinge, an adjustment component is provided on the top of the support plate 2, and the guide sleeve 1 is used to adjust the signal transmission direction of the transmitting rod through the spherical sleeve.

[0008] According to the above technical solution, a sliding groove is provided on the outer wall of the fuselage, and a guide groove 1 is provided on the outer wall of the fuselage, and the guide groove 1 is used to guide the limit block.

[0009] According to the above technical solution, a notch is provided on the outer wall of the guide sleeve 1, the inner wall of the support plate 2 is fixedly connected to the guide sleeve 2, and the inner wall of the support plate 2 is connected to the adjustment block through a rotating shaft hinge, and the notch is used to increase the adjustment limit of the firing rod.

[0010] According to the above technical solution, the adjustment assembly includes a support sleeve, the outer wall of the support sleeve is fixedly connected to support rod 1, the outer wall of support rod 1 is hingedly connected to a limit rod through a rotating shaft, the outer wall of the limit rod is fixedly connected to guide plate 1, the bottom of guide plate 1 is fixedly connected to guide sleeve 3, the inner wall of guide sleeve 3 is covered and connected with the ball head set on the outer wall of support rod 4, the outer wall of support rod 4 is fixedly connected to an adjustment sleeve, and the support rod 4 adjusts the angle of guide plate 1 by rotating the ball head on the inner wall of guide sleeve 3.

[0011] According to the above technical solution, the outer wall of the support sleeve is fixedly connected to the support rod 2, the outer wall of the support rod 2 is provided with a guide groove 2, the groove wall of the guide groove 2 is slidably connected to the support rod 3, the inner wall of the support rod 3 is covered with the ball head provided on the outer wall of the adjustment rod, the outer wall of the adjustment rod is fixedly connected to the guide plate 2, and the guide plate 2 is used to adjust the covering angle of the launching rod.

[0012] According to the above technical solution, the outer wall of the support plate 1 is slidably connected to the inner wall of the assembly groove, the outer wall of the limit block slides along the groove wall of the guide groove 1, and the limit block is used to limit the support plate 1.

[0013] According to the above technical solution, there are two groups of sliding grooves, and the two groups of sliding grooves are symmetrically opened on the outer wall of the fuselage with the center line of the fuselage as the symmetry axis. The sliding grooves pass through the outer wall of the fuselage and are connected to the inner wall of the assembly groove. The sliding grooves are used to guide the adjustment block.

[0014] According to the above technical solution, the outer wall of the adjustment block passes through the inner wall of the assembly groove through a slider and slides in the sliding groove wall. The slot size matches the diameter of the launching rod. The outer wall of the adjustment block and the outer wall of the fuselage limit the support plate 2 through friction.

[0015] According to the above technical solution, the inner wall of the support sleeve is rotatably connected to the outer wall of the launching rod through a bearing, the inner wall of the adjustment sleeve is slidably connected to the outer wall of the launching rod, the support rod 1 is elastic and is used to compensate for the displacement caused by the angle adjustment of the guide plate 1, the inner wall of the adjustment sleeve and the outer wall of the launching rod limit the support rod 4 through friction, and the guide plate 1 is in the shape of a conical surface and is used to reflect the microwaves emitted by the launching rod.

[0016] According to the above technical solution, the outer wall of the second guide plate is hingedly connected to the outer wall of the first guide plate through a rotating shaft. The second guide plate is in the shape of a conical surface and is made of aluminum plate, which is used to reflect the microwaves emitted by the transmitting rod. The bottom of the outer wall of the support sleeve is a conical surface, which is used to increase the adjustment limit of the transmitting rod.

[0017] Compared with the prior art, the present invention has the following beneficial effects:

[0018] 1. This miniaturized RF microwave transceiver channel device supports the transmitting rod through an adjustment mechanism and uniformly adjusts the angle of the transmitting rod, thereby increasing the adjustment efficiency and accuracy of the transmitting rod, while preventing the transmitting rod from loosening and becoming unable to be adjusted, thereby extending the service life of the miniaturized RF microwave transceiver channel device.

[0019] 2. This miniaturized RF microwave transceiver channel device increases the adjustment range of the transmitting rod through the slots opened on the outer wall of the spherical sleeve, making the angle adjustment of the transmitting rod more flexible, increasing the coverage range of the RF microwave transceiver channel device's transmitted signals, and at the same time preventing the received signal from being parallel to the transmitting rod, which would affect the reception of the received signal.

[0020] 3. This miniaturized RF microwave transceiver channel device covers the transmitting rod with adjustable angle guide plates 1 and 2, reflecting the microwave signals emitted by the transmitting rod, reducing the ineffective coverage area of ​​the transmitting rod and increasing signal strength. At the same time, it reflects the received signal back to the transmitting rod, improving signal reception efficiency.

[0021] 4. This miniaturized RF microwave transceiver channel device uses a spherical sleeve provided on the outer wall of the transmitting rod to allow manual fine-tuning after the entire transmitting rod is adjusted in angle. This increases the coverage range of the RF microwave transceiver channel device while preventing the transmitting rod from becoming loose due to frequent adjustments, which would affect the coverage range of the RF microwave transceiver channel device. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 The structure of the present invention is schematically shown Figure 1 ;

[0023] Figure 2 The structure of the present invention is schematically shown Figure 2 ;

[0024] Figure 3 The structure of the present invention is schematically shown Figure 3 ;

[0025] Figure 4 Schematic diagram of the structure of the adjustment mechanism of the present invention Figure 1 ;

[0026] Figure 5 The structural diagram of the adjustment mechanism of the present invention is as follows Figure 2 ;

[0027] Figure 6 Schematic diagram of the structure of the adjustment mechanism of the present invention Figure 3 ;

[0028] Figure 7 Schematic diagram of the structure of the adjustment component of the present invention Figure 1 ;

[0029] Figure 8 Schematic diagram of the structure of the adjustment component of the present invention Figure 2 ;

[0030] Figure 9 A cross-sectional view of an adjustment assembly according to the present invention.

[0031] In the figure: 1. Body; 101. Heat dissipation hole; 102. Sliding groove; 103. Guide groove 1; 104. Assembly groove; 2. Adjustment mechanism; 201. Support plate 1; 202. Guide sleeve 1; 203. Notch; 204. Spherical sleeve; 205. Launch rod; 206. Support plate 2; 207. Guide sleeve 2; 208. Adjustment block; 209. Limit block; 3. Adjustment assembly; 301. Support sleeve; 302. Support rod 1; 303. Limit rod; 304. Guide plate 1; 305. Support rod 2; 306. Adjustment rod; 307. Support rod 3; 308. Guide plate 2; 309. Guide sleeve 3; 310. Support rod 4; 311. Adjustment sleeve; 312. Guide groove 2. DETAILED DESCRIPTION

[0032] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0033] For example 1, please refer to Figures 1-6 The present invention provides a technical solution: a miniaturized radio frequency microwave transceiver channel device, comprising a body 1, a heat dissipation hole 101 formed on the outer wall of the body 1, an assembly groove 104 formed on the outer wall of the body 1, and further comprising:

[0034] Adjustment mechanism 2, adjustment mechanism 2 is arranged inside the assembly groove 104, adjustment mechanism 2 includes support plate 1 201, the outer wall of support plate 1 201 is fixedly connected to the limit block 209, the inner wall of support plate 1 201 is fixedly connected to the guide sleeve 1 202, the inner wall of guide sleeve 1 202 is covered with a spherical sleeve 204, the inner wall of spherical sleeve 204 is fixedly connected to the firing rod 205, the outer wall of support plate 1 201 is connected to support plate 2 206 through a rotating shaft hinge, and the top of support plate 206 is provided with an adjustment component 3, guide sleeve 1 202 is used to adjust the signal transmission direction of the transmitting rod 205 through the spherical sleeve 204. When the miniaturized radio frequency microwave transceiver channel device is put into use, the device is placed in a suitable position and the device is started. When the transmission angle of the transmitting rod 205 needs to be adjusted, the adjustment block 208 is toggled to make the adjustment block 208 slide in the sliding groove 102, driving the support plate 206 to slide in the assembly groove 104. The support plate 206 is connected to the support plate 1 201 through a hinge, so that the support plate 1 201 drives the limit block 209 in the guide groove. The support plate 101 slides in the assembly groove 104 and protrudes from the top of the fuselage 1, driving the launch rod 205 to rise. At the same time, after the support plate 101 rises, the support plate 206 is used to adjust the block 208 so that the support plate 206 drives the launch rod 205 to adjust the angle, thereby increasing the coverage range of the device and preventing the launch rod 205 from being at the same angle in the same plane, causing part of the received signal to be parallel to the launch rod 205, thereby reducing the signal reception efficiency. After the angle of the launch rod 205 is adjusted, the support plate 206 is used to adjust the block 208 so that the support plate 206 drives the launch rod 205 to adjust the angle. After that, the firing rod 205 is toggled so that the firing rod 205 rotates on the inner wall of the guide sleeve 1 202 or the guide sleeve 2 207 through the spherical sleeve 204 provided on the outer wall, and the firing angle of the firing rod 205 is finely adjusted so that the firing rod 205 is at a suitable signal transmitting angle and signal receiving angle. The firing rod 205 drives the spherical sleeve 204 to rotate in the guide sleeve 1 202, and the notch 203 provided on the outer wall of the spherical sleeve 204 increases the adjustment angle of the firing rod 205, making the angle adjustment of the firing rod 205 more flexible.

[0035] A sliding groove 102 is provided on the outer wall of the fuselage 1, and a guide groove 103 is provided on the outer wall of the fuselage 1. The guide groove 103 is used to guide the limit block 209. When the firing angle of the firing rod 205 needs to be adjusted, the adjustment block 208 is toggled to slide the adjustment block 208 in the sliding groove 102, driving the second support plate 206 to slide in the assembly groove 104. The second support plate 206 is hinged to the first support plate 201, so that the first support plate 201 drives the limit block 209 to slide in the guide groove 103, so that the first support plate 201 slides in the assembly groove 104 and protrudes from the top of the fuselage 1, driving the firing rod 205 to rise. At the same time, after the first support plate 201 is raised, the second support plate 206 is used to limit the adjustment block 208, so that the second support plate 206 drives the firing rod 205 to adjust the angle;

[0036] A notch 203 is provided on the outer wall of the guide sleeve 1 202, and a guide sleeve 207 is fixedly connected to the inner wall of the support plate 206. The inner wall of the support plate 206 is hinged with an adjustment block 208 via a rotating shaft. The notch 203 is used to increase the adjustment limit of the firing rod 205. After the angle of the firing rod 205 is adjusted, the firing rod 205 is toggled so that the firing rod 205 rotates on the inner wall of the guide sleeve 1 202 or the guide sleeve 2 207 through the spherical sleeve 204 provided on the outer wall, and the firing angle of the firing rod 205 is fine-tuned so that the firing rod 205 is at a suitable signal transmission angle and signal reception angle. The firing rod 205 drives the spherical sleeve 204 to rotate in the guide sleeve 1 202, and the adjustment angle of the firing rod 205 is increased through the notch 203 provided on the outer wall of the spherical sleeve 204, so that the angle adjustment of the firing rod 205 is more flexible.

[0037] The outer wall of the support plate 101 is slidably connected to the inner wall of the assembly groove 104, and the outer wall of the limit block 209 slides along the wall of the guide groove 103. The limit block 209 is used to limit the support plate 1 201. After the adjustment block 208 is toggled to slide in the sliding groove 102, the adjustment block 208 drives the support plate 206 to slide in the assembly groove 104. The support plate 206 is hinged to the support plate 1 201, so that the support plate 1 201 drives the limit block 209 to slide in the guide groove 103, so that the support plate 1 201 slides in the assembly groove 104 and protrudes from the top of the fuselage 1, driving the firing rod 205 to rise;

[0038] There are two groups of sliding grooves 102, which are symmetrically arranged on the outer wall of the fuselage 1 with the center line of the fuselage 1 as the symmetry axis. The sliding grooves 102 pass through the outer wall of the fuselage 1 and are connected to the inner wall of the assembly groove 104. The sliding grooves 102 are used to guide the adjustment block 208. After the adjustment block 208 is moved to slide in the sliding grooves 102, the adjustment block 208 drives the second support plate 206 to slide in the assembly groove 104. The second support plate 206 is connected to the first support plate 201 through a hinge, and the adjustment block 208 is limited by the sliding grooves 102, so that the second support plate 206 is tilted, driving the firing rod 205 to adjust the angle;

[0039] The outer wall of the adjustment block 208 passes through the inner wall of the assembly groove 104 through the slider and slides on the wall of the sliding groove 102. The size of the slot 203 matches the diameter of the firing rod 205. The outer wall of the adjustment block 208 and the outer wall of the fuselage 1 limit the support plate 206 through friction. After the adjustment block 208 is moved to slide in the sliding groove 102, the support plate 206 is driven to tilt, so that the support plate 206 drives the firing rod 205 to adjust the angle. After the adjustment is completed, the inclination angle of the support plate 206 is locked by the friction between the outer wall of the adjustment block 208 and the fuselage 1.

[0040] Example 2, based on Example 1, please refer to Figure 7-Figure 9 The present invention provides a technical solution: the adjustment component 3 includes a support sleeve 301, the outer wall of the support sleeve 301 is fixedly connected to the support rod 1 302, the outer wall of the support rod 1 302 is hingedly connected to the limit rod 303 through a rotating shaft, the outer wall of the limit rod 303 is fixedly connected to the guide plate 1 304, the bottom of the guide plate 1 304 is fixedly connected to the guide sleeve 309, the inner wall of the guide sleeve 309 is covered and connected with the ball head set on the outer wall of the support rod 4 310, and the outer wall of the support rod 4 310 is fixedly connected with the adjustment sleeve 311. The support rod 4 310 adjusts the angle of the guide plate 1 304 by rotating the ball head on the inner wall of the guide sleeve 309. After the angle adjustment of the transmitting rod 205 is completed, the guide plate 1 304 is driven to rotate horizontally with the transmitting rod 205 as the center by rotating the support sleeve 301, and the reflection direction of the transmitted signal is adjusted so that the guide plate 1 304 reflects the part of the transmitted signal that does not need to be covered, thereby increasing the strength of the signal in the use range, and at the same time receiving the signal through After the reflection on the inner wall of the conical surface of the guide plate 1 304 is completed, the efficiency of receiving the signal and the signal receiving of the transmitting rod 205 is increased. After the horizontal angle adjustment of the guide plate 1 304 is completed, the adjustment sleeve 311 is toggled so that the guide plate 1 304 is supported by the support rod 1 302, and the vertical angle adjustment is performed with the center line of the limit rod 303 as the rotation axis. During the vertical angle adjustment of the guide plate 1 304, the bottom of the guide plate 1 304 is supported by the support rod 4 310 and the guide sleeve 309. The support rod 1 302 compensates for the displacement caused by the vertical angle adjustment of the guide plate 1 304 through elasticity. At the same time, during the vertical adjustment of the guide plate 1 304, after the guide plate 2 308 limits the adjustment rod 306 through the support rod 2 305 and the support rod 3 307, the guide plate 2 308 swings on the outer wall of the guide plate 1 304 to adjust the covering angle of the transmitting rod 205, so that the coverage of the device over the use range is more accurate.

[0041] The outer wall of the support sleeve 301 is fixedly connected to the support rod 2 305, and the outer wall of the support rod 2 305 is provided with a guide groove 2 312. The groove wall of the guide groove 2 312 is slidably connected to the support rod 307. The inner wall of the support rod 307 is covered with the ball head provided on the outer wall of the adjustment rod 306. The outer wall of the adjustment rod 306 is fixedly connected to the guide plate 2 308. The guide plate 2 308 is used to adjust the covering angle of the firing rod 205. During the vertical adjustment process of the guide plate 1 304, after the guide plate 2 308 limits the adjusting rod 306 through the support rod 2 305 and the support rod 3 307, the guide plate 2 308 swings on the outer wall of the guide plate 1 304 to adjust the covering angle of the firing rod 205, so that the coverage of the device over the use range is more accurate.

[0042] The inner wall of the support sleeve 301 is rotatably connected to the outer wall of the launching rod 205 through a bearing, and the inner wall of the adjustment sleeve 311 is slidably connected to the outer wall of the launching rod 205. The support rod 1 302 is elastic and is used to compensate for the displacement caused by the angle adjustment of the guide plate 1 304. The inner wall of the adjustment sleeve 311 and the outer wall of the launching rod 205 limit the support rod 4 310 through friction. The guide plate 1 304 is in the shape of a conical surface and is used to reflect the microwaves emitted by the launching rod 205. After the horizontal angle adjustment of the guide plate 1 304 is completed, the adjustment sleeve 311 is toggled so that the guide plate 1 304 is supported by the support rod 1 302, and the vertical angle is adjusted with the center line of the limit rod 303 as the rotation axis. During the vertical angle adjustment of the guide plate 1 304, the bottom of the guide plate 1 304 is supported by the support rod 4 310 and the guide sleeve 309. The support rod 1 302 compensates for the displacement caused by the vertical angle adjustment of the guide plate 1 304 through elasticity;

[0043] The outer wall of guide plate 2 308 is hingedly connected to the outer wall of guide plate 1 304 via a rotating shaft. Guide plate 2 308 has a conical curved surface and is made of aluminum plate. It is used to reflect microwaves emitted by the transmitting rod 205. The bottom of the outer wall of the support sleeve 301 is a conical surface, which is used to increase the adjustment limit of the transmitting rod 205. After the angle of the transmitting rod 205 is adjusted, the support sleeve 301 is rotated to drive guide plate 1 304 to rotate horizontally about the transmitting rod 205, adjusting the reflection direction of the transmitted signal. Guide plate 1 304 reflects the portion of the transmitted signal that does not need to be covered, thereby increasing the signal strength within the usable range. At the same time, the received signal is reflected by the inner wall of guide plate 1 304 with a conical curved surface, thereby increasing the efficiency of receiving the received signal and the signal from the transmitting rod 205.

[0044] While embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions, and variations may be made to these embodiments without departing from the principles and spirit of the invention, and that the scope of the invention is defined by the appended claims and their equivalents.

Claims

1. A miniaturized radio frequency microwave transceiver channel device, comprising a body (1), wherein the outer wall of the body (1) is provided with heat dissipation holes (101), characterized in that: The outer wall of the fuselage (1) is provided with an assembly groove (104), and further comprises: An adjustment mechanism (2), the adjustment mechanism (2) being arranged inside the assembly groove (104), the adjustment mechanism (2) comprising a support plate (201), the outer wall of the support plate (201) being fixedly connected to a limit block (209), the inner wall of the support plate (201) being fixedly connected to a guide sleeve (202), the inner wall of the guide sleeve (202) being covered and connected to a spherical sleeve (204), the inner wall of the spherical sleeve (204) being fixedly connected to a transmitting rod (205), the outer wall of the support plate (201) being connected to the support plate (206) via a rotating shaft hinge, the top of the support plate (206) being provided with an adjustment component (3), the guide sleeve (202) being used to adjust the signal transmitting direction of the transmitting rod (205) via the spherical sleeve (204); The adjustment assembly (3) includes a support sleeve (301), the outer wall of the support sleeve (301) is fixedly connected to a support rod (302), the outer wall of the support rod (302) is hingedly connected to a limit rod (303) via a rotating shaft, the outer wall of the limit rod (303) is fixedly connected to a guide plate (304), the bottom of the guide plate (304) is fixedly connected to a guide sleeve (309), the inner wall of the guide sleeve (309) is covered and connected with a ball head provided on the outer wall of the support rod (310), the outer wall of the support rod (310) is fixedly connected to an adjustment sleeve (311), and the support rod (310) adjusts the angle of the guide plate (304) by rotating the ball head on the inner wall of the guide sleeve (309).

2. The miniaturized radio frequency microwave transceiver channel device according to claim 1, characterized in that: The outer wall of the fuselage (1) is provided with a sliding groove (102), and the outer wall of the fuselage (1) is provided with a guide groove (103), and the guide groove (103) is used to guide the limit block (209).

3. The miniaturized radio frequency microwave transceiver channel device according to claim 1, characterized in that: The outer wall of the guide sleeve 1 (202) is provided with a notch (203), the inner wall of the support plate 2 (206) is fixedly connected to the guide sleeve 2 (207), and the inner wall of the support plate 2 (206) is connected to the adjustment block (208) via a rotating shaft hinge, and the notch (203) is used to increase the adjustment limit of the firing rod (205).

4. The miniaturized radio frequency microwave transceiver channel device according to claim 3, characterized in that: The outer wall of the support sleeve (301) is fixedly connected to the second support rod (305), the outer wall of the second support rod (305) is provided with a second guide groove (312), the groove wall of the second guide groove (312) is slidably connected to the third support rod (307), the inner wall of the third support rod (307) is covered with a ball head provided on the outer wall of the adjustment rod (306), the outer wall of the adjustment rod (306) is fixedly connected to the second guide plate (308), and the second guide plate (308) is used to adjust the covering angle of the firing rod (205).

5. The miniaturized radio frequency microwave transceiver channel device according to claim 1, characterized in that: The outer wall of the support plate 1 (201) is slidably connected to the inner wall of the assembly groove (104), and the outer wall of the limit block (209) slides along the groove wall of the guide groove 1 (103). The limit block (209) is used to limit the support plate 1 (201).

6. The miniaturized radio frequency microwave transceiver channel device according to claim 2, characterized in that: The number of the sliding grooves (102) is two groups, and the two groups of sliding grooves (102) are symmetrically opened on the outer wall of the fuselage (1) with the center line of the fuselage (1) as the symmetry axis. The sliding grooves (102) pass through the outer wall of the fuselage (1) and are connected to the inner wall of the assembly groove (104). The sliding grooves (102) are used to guide the adjustment block (208).

7. The miniaturized radio frequency microwave transceiver channel device according to claim 3, characterized in that: The outer wall of the adjustment block (208) passes through the inner wall of the assembly groove (104) through a slider and slides on the groove wall of the sliding groove (102). The size of the groove (203) matches the diameter of the firing rod (205). The outer wall of the adjustment block (208) and the outer wall of the fuselage (1) limit the support plate 2 (206) through friction.

8. The miniaturized radio frequency microwave transceiver channel device according to claim 1, characterized in that: The inner wall of the support sleeve (301) is rotatably connected to the outer wall of the launch rod (205) through a bearing, and the inner wall of the adjustment sleeve (311) is slidably connected to the outer wall of the launch rod (205). The support rod 1 (302) is elastic and is used to compensate for the displacement generated by the angle adjustment of the guide plate 1 (304). The inner wall of the adjustment sleeve (311) and the outer wall of the launch rod (205) limit the support rod 4 (310) through friction. The guide plate 1 (304) is in the shape of a conical surface and is used to reflect the microwaves emitted by the launch rod (205).

9. The miniaturized radio frequency microwave transceiver channel device according to claim 4, characterized in that: The outer wall of the second guide plate (308) is hingedly connected to the outer wall of the first guide plate (304) via a rotating shaft. The second guide plate (308) is in the shape of a conical surface and is made of an aluminum plate, and is used to reflect the microwaves emitted by the transmitting rod (205). The bottom of the outer wall of the support sleeve (301) is a conical surface, which is used to increase the adjustment limit of the transmitting rod (205).

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