Tandem airborne communication equipment case

Abstract

The utility model discloses a serial airborne communication equipment cabinet, comprising a front panel assembly, a signal processing module, a radio frequency module, a power supply module and a positioning heat dissipation assembly which are arranged in sequence, and the front panel assembly, the signal processing module, the radio frequency module, the power supply module and the positioning heat dissipation assembly are provided with corresponding through holes; the LED lamp further comprises a connecting assembly, the connecting assembly comprises a screw rod, a gasket and a nut, the screw rod penetrates through the through hole, and the gasket and the nut are installed on the lower side of the positioning heat dissipation assembly for locking. The front panel assembly is connected with a positioning mechanism used for positioning the case. The modular computer case has the beneficial effects that the modular arrangement is realized, the whole case is quickly mounted and assembled through the arrangement of the screw rods, the maintenance is convenient, and only a fault module needs to be replaced during maintenance.

Description

Technical Field

[0001] This utility model relates to the field of communication technology, specifically to a serial airborne communication equipment chassis. Background Technology

[0002] Airborne communication equipment refers to electronic devices used for communication on aircraft. It mainly includes aircraft radios and intercoms. Aircraft radios are used for communication between the aircraft and the ground, between the aircraft and ships, and between aircraft; intercoms are used by flight crew to communicate with each other or to connect to the aircraft radio for external communication. Some intercoms also allow communication with ground personnel before takeoff via jacks located on the outside of the aircraft. Compared to ground equipment, airborne communication equipment operates in harsher environments, requiring better shock and vibration resistance; the ability to withstand drastic changes in temperature, humidity, and air pressure; high reliability; small size; and light weight. Aircraft radio antennas must also possess sufficient structural strength and good aerodynamic performance.

[0003] Existing airborne communication equipment has a complex structure, and its internal components need to be installed separately, which greatly increases assembly time and reduces processing efficiency. Furthermore, when used in high-vibration environments, damaged internal components need to be completely disassembled for repair or replacement. Utility Model Content

[0004] To solve the above-mentioned technical problems, this utility model provides a serial airborne communication equipment chassis, which is modular, simple in structure, and convenient to assemble and maintain. During maintenance, only the faulty module needs to be replaced.

[0005] Specifically, this utility model discloses a serial airborne communication equipment chassis, including: a front panel assembly, a signal processing module, a radio frequency module, a power supply module, and a positioning and heat dissipation assembly arranged in sequence, wherein the front panel assembly, the signal processing module, the radio frequency module, the power supply module, and the positioning and heat dissipation assembly are provided with corresponding through holes;

[0006] It also includes a connecting assembly, which includes a screw, a washer, and a nut. The screw passes through the through hole, and the washer and nut are installed on the lower side of the positioning heat dissipation assembly for locking.

[0007] The front panel assembly is connected to a positioning mechanism for positioning the chassis.

[0008] The advantages of adopting the above technical solution are that the modular design allows for quick installation of the entire chassis through the screw mechanism, making assembly and maintenance convenient. During maintenance, only the faulty module needs to be replaced.

[0009] Furthermore, the front panel assembly includes: a panel, a rear housing of the panel, a grounding terminal, and a plurality of interfaces, wherein the grounding terminal and the interfaces are mounted on the panel, and a heat sink is provided on the side of the rear housing of the panel.

[0010] The advantages of adopting the above technical solution are that the panel is designed for installing interfaces and various terminals, and the heat sink facilitates heat dissipation.

[0011] Furthermore, the positioning and heat dissipation component includes a heat dissipation plate, a heat dissipation fin is provided at the bottom of the heat dissipation plate, a positioning hole is provided at the bottom of the heat dissipation plate, a positioning block is installed in the positioning hole, and a circular hole is provided in the positioning block.

[0012] The advantages of adopting the above technical solution are that the heat sink serves to support the power module and also dissipates heat. The positioning holes, together with the positioning components, serve to position the chassis, fix it, and reduce vibration.

[0013] Furthermore, the positioning mechanism includes: a fixing plate, one end of which is equipped with a positioning pin and the other end with a locking device, and the panel is provided with a latch that cooperates with the locking device.

[0014] The advantage of adopting the above technical solution is that the positioning pin and locking device work together to achieve the positioning and locking of the entire chassis, reducing vibration. The positioning pin works with the positioning block at the bottom of the heat sink to achieve the positioning function. The locking device works with the latch to lock the entire chassis, which is fixed and easy to disassemble.

[0015] Furthermore, the fixing plate is provided with a mounting plate, the positioning pin is horizontally locked on the fixing plate, and the positioning pin extends into the circular hole on the positioning block for fixation.

[0016] The advantage of adopting the above technical solution is that the positioning pin is used to cooperate with the heat sink to achieve positioning and fixation.

[0017] Furthermore, the locking device includes a locking rod, a limiting block, and a locking block. One end of the locking rod is hinged to the fixing plate. The limiting block and the locking block are both mounted on the locking rod. The limiting block is provided with a limiting groove, and the limiting groove cooperates with the latch to lock the chassis.

[0018] The advantages of adopting the above technical solution are that the locking function is achieved by setting a limit block and a latch. At the same time, the setting of the locking block can prevent the limit block from loosening in a long-term vibration environment, ensuring a tight fixation. In addition, the locking screw is hinged, which is suitable for different assembly environments.

[0019] Furthermore, the signal processing module, radio frequency module, and power supply module each include a front cover plate, a rear cover plate, and a main body. A heat sink is provided on the outer side of the main body, and sealing ring grooves are provided on the front cover plate and the rear cover plate.

[0020] The advantages of adopting the above technical solution are that the signal processing module, radio frequency module and power supply module are modularized, which facilitates installation and maintenance, and the setting of multiple heat sinks ensures heat dissipation and effectively avoids internal overheating.

[0021] Furthermore, a conductive sealing ring is provided between the front panel assembly, the signal processing module, the radio frequency module, the power module, and the positioning and heat dissipation assembly.

[0022] The advantages of adopting the above technical solution are that the conductive sealing ring ensures electromagnetic compatibility between modules and keeps the internal pressure of each module constant, preventing damage to the internal components of each module due to the decrease in atmospheric pressure at high altitudes.

[0023] Furthermore, the connecting assembly also includes an elastic washer and a cap nut, the cap nut being locked onto the locking rod and located outside the nut.

[0024] The advantages of adopting the above technical solution are that the cap-type nut has the advantages of tightening and aesthetics, and prevents hands from being cut. Attached Figure Description

[0025] To more clearly illustrate the technical solutions in the embodiments of this utility model, the accompanying drawings used in the description of the embodiments or the prior art will be briefly introduced below.

[0026] Figure 1 This is an exploded view of the overall chassis of the serial airborne communication equipment of this utility model.

[0027] Figure 2 This is an overall cross-sectional view of the utility model.

[0028] Figure 3 This is an enlarged view of section A of this utility model.

[0029] Figure 4 This is an installation structure diagram of the chassis and positioning mechanism of this utility model.

[0030] Figure 5 This is a cross-sectional view of the installation of this utility model.

[0031] Figure 6 This is an enlarged view of section B of this utility model.

[0032] Figure 7 This is an enlarged view of section C of this utility model.

[0033] Figure 8 This is a cross-sectional view of the radio frequency module of this utility model.

[0034] The reference numerals used in the attached figures are as follows:

[0035] Front panel assembly 1; panel 11; rear panel housing 12; grounding terminal 13; interface 14; heat sink 15; latch 16; signal processing module 2; radio frequency module 3; front cover 31; rear cover 32; main body 33; power module 4; positioning and heat dissipation assembly 5; heat sink 51; positioning block 52; circular hole 53; through hole 6; screw 7; washer 71; nut 72; elastic washer 73; cap nut 74; positioning mechanism 8; fixing plate 81; positioning pin 82; locking rod 83; limit block 84; locking block 85; conductive sealing ring 9; cover plate 10. Detailed Implementation

[0036] The present invention will now be described in further detail with reference to the accompanying drawings.

[0037] like Figure 1-8 As shown, this utility model discloses a serial airborne communication equipment chassis, including: a front panel assembly 1, a signal processing module 2, a radio frequency module 3, a power supply module 4, and a positioning and heat dissipation assembly 5 arranged in sequence. The front panel assembly 1, the signal processing module 2, the radio frequency module 3, the power supply module 4, and the positioning and heat dissipation assembly 5 are provided with corresponding through holes 6; a cover plate 10 is installed on the side for connecting the above-mentioned components and modules.

[0038] It also includes a connecting assembly, which includes a screw 7, a washer 71 and a nut 72. The screw 7 passes through the through hole 6, and the washer 71 and the nut 72 are installed on the lower side of the positioning heat dissipation assembly 5 for locking.

[0039] The front panel assembly 1 is connected to a positioning mechanism 8 for positioning the chassis.

[0040] The advantages of adopting the above technical solution are that the modular design allows for quick installation of the entire chassis through the screw 7, making assembly and maintenance convenient. During maintenance, only the faulty module needs to be replaced.

[0041] In some implementations, the front panel assembly 1 includes: a panel 11, a rear panel housing 12, a grounding terminal 13, and a plurality of interfaces 14. The grounding terminal 13 and the interfaces 14 are mounted on the panel 11. A heat sink 15 is provided on the side of the rear panel housing 12. The interfaces 14 include a plurality of control interfaces, power interfaces, and radio frequency interfaces. A handle is also provided on the panel 11 to facilitate the transport of the entire chassis.

[0042] In some implementations, the positioning heat dissipation component 5 includes a heat sink 51. The upper surface of the heat sink 51 is provided with a groove, and the lower side of the power supply component is provided with a protrusion. The groove and the protrusion are installed together to provide positioning and reduce gaps. A heat sink is provided at the bottom of the heat sink 51 to provide heat dissipation. The bottom of the heat sink 51 is provided with a positioning hole, and a positioning block 52 is installed in the positioning hole. The positioning block 52 is locked and fixed in the positioning hole. A circular hole 53 is provided in the positioning block 52. The positioning block 52 and the positioning component are arranged together to provide positioning, fix the chassis, and reduce vibration.

[0043] Furthermore, the positioning mechanism 8 includes: a fixing plate 81, with a positioning pin 82 installed at one end and a locking device installed at the other end; and a latch 16 that cooperates with the locking device on the panel 11. The latch 16 is a T-shaped latch, symmetrically fixed to the panel 11 by screws and located on the same side of the panel 11. The positioning pin 82 and the locking device work together to achieve positioning and locking of the entire chassis, reducing vibration. The positioning pin 82 cooperates with the positioning block 52 at the bottom of the heat sink 51 to achieve the positioning function. The locking device cooperates with the latch 16 to lock the entire chassis, making it fixed and easy to disassemble.

[0044] Furthermore, a mounting plate is provided on the fixing plate 81. The fixing plate 81 is horizontally positioned, and a shock absorber is provided on its lower side to support the entire chassis. The mounting plate is vertically positioned, and the positioning pin 82 is horizontally locked onto the fixing plate 81 (e.g., Figure 7 As shown, the locating pin 82 is locked by the nut 72 and the washer 71. The locating pin 82 has a tapered protruding end, which is inserted into the circular hole 53 on the locating block 52 for fixation.

[0045] In some embodiments, the locking device includes: a locking rod 83, a limiting block 84, and a locking block 85 (e.g., Figure 6 As shown, one end of the locking rod 83 is hinged to the fixed plate 81. The locking rod 83 is provided with external threads, and the limiting block 84 and the locking block 85 are provided with internal threads. They are locked onto the locking rod 83 through threaded engagement. The limiting block 84 is provided with a limiting groove, which is an annular groove used to accommodate the protruding end of the latch 16. Then, the limiting groove is locked towards the bottom of the locking rod 83. The locking block 85 is locked in contact with the limiting block 84. The contact surfaces of the locking block 85 and the limiting block 84 are provided with mating convex teeth. The convex teeth increase the friction and ensure the locking force of the locking block 85, effectively preventing the limiting block 84 from loosening and ensuring a tight fixation.

[0046] In some implementations, the signal processing module 2, the radio frequency module 3, and the power supply module 4 all include a front cover plate 31, a rear cover plate 32, and a main body 33. A heat sink is provided on the outer side of the main body 33, and sealing ring grooves are provided on the front cover plate 31 and the rear cover plate 32 (e.g., Figure 8 (As shown).

[0047] The signal processing module 2, RF module 3, and power supply module 4 are modularly designed for easy installation and maintenance. Multiple heat sinks ensure heat dissipation and effectively prevent internal overheating.

[0048] Furthermore, a conductive sealing ring 9 is provided between the front panel assembly 1, the signal processing module 2, the radio frequency module 3, the power module 4, and the positioning and heat dissipation assembly 5.

[0049] The advantages of adopting the above technical solution are that the conductive sealing ring 9 is set to ensure the electromagnetic compatibility between modules and to keep the internal pressure of each module constant, so as to prevent the internal components of each module from being damaged by the decrease in atmospheric pressure at high altitude.

[0050] In some implementations, the connecting assembly also includes a resilient washer 73 and a cap nut 74, which is locked onto the screw 7 and located on the outside of the nut. The advantages of the cap nut 74 are that it provides a tighter tightening and is aesthetically pleasing, preventing hand injuries.

[0051] For those skilled in the art, various modifications and improvements can be made without departing from the inventive concept of this utility model, and these modifications and improvements all fall within the protection scope of this utility model.

Claims

1. A serial airborne communication equipment chassis, characterized in that, include: The front panel assembly (1), signal processing module (2), radio frequency module (3), power supply module (4) and positioning heat dissipation assembly (5) are arranged in sequence, and the front panel assembly (1), signal processing module (2), radio frequency module (3), power supply module (4) and positioning heat dissipation assembly (5) are provided with corresponding through holes (6). It also includes a connecting assembly, which includes a screw (7), a washer (71) and a nut (72), the screw (7) passing through the through hole (6), and the washer (71) and nut (72) being installed and locked on the lower side of the positioning heat dissipation assembly (5); The front panel assembly (1) is connected to a positioning mechanism (8) for positioning the chassis.

2. The serial airborne communication equipment chassis according to claim 1, characterized in that, The front panel assembly (1) includes: a panel (11), a panel rear housing (12), a grounding terminal (13), and a plurality of interfaces (14), wherein the grounding terminal (13) and the interfaces (14) are mounted on the panel (11), and a heat sink (15) is provided on the side of the panel rear housing (12).

3. The serial airborne communication equipment chassis according to claim 1, characterized in that, The positioning heat dissipation component (5) includes a heat dissipation plate (51), a heat dissipation fin is provided at the bottom of the heat dissipation plate (51), a positioning hole is provided at the bottom of the heat dissipation plate (51), a positioning block (52) is installed in the positioning hole, and a circular hole (53) is provided in the positioning block (52).

4. The serial airborne communication equipment chassis according to claim 3, characterized in that, The positioning mechanism (8) includes: a fixing plate (81), one end of which is equipped with a positioning pin (82) and the other end with a locking device, and the panel (11) is provided with a latch (16) that cooperates with the locking device.

5. The serial airborne communication equipment chassis according to claim 4, characterized in that, The fixing plate (81) is provided with an mounting plate, and the positioning pin (82) is horizontally locked on the fixing plate (81). The positioning pin (82) extends into the circular hole (53) on the positioning block (52) for fixation.

6. The serial airborne communication equipment chassis according to claim 4, characterized in that, The locking device includes a locking rod (83), a limiting block (84), and a locking block (85). One end of the locking rod (83) is hinged to the fixing plate (81). The limiting block (84) and the locking block (85) are both mounted on the screw (7). The limiting block (84) is provided with a limiting groove. The limiting groove cooperates with the latch (16) to lock the chassis.

7. The serial airborne communication equipment chassis according to claim 6, characterized in that, The signal processing module (2), radio frequency module (3), and power supply module (4) each include a front cover plate (31), a rear cover plate (32), and a main body (33). The main body (33) is provided with heat sinks on the outside, and the front cover plate (31) and the rear cover plate (32) are provided with sealing ring grooves.

8. The serial airborne communication equipment chassis according to claim 7, characterized in that, A conductive sealing ring (9) is provided between the front panel assembly (1), the signal processing module (2), the radio frequency module (3), the power supply module (4), and the positioning heat dissipation assembly (5).

9. The serial airborne communication equipment chassis according to claim 6, characterized in that, The connecting assembly also includes an elastic washer (73) and a cap nut (74), the cap nut (74) being locked onto the locking rod (83) and located outside the nut.

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