Airborne satellite communication equipment damping frame device and damping method thereof

Abstract

The invention relates to the technical field of airborne satellite communication, and discloses an airborne satellite communication equipment damping frame device and a damping method thereof.The airborne satellite communication equipment damping frame device comprises a bottom plate, a damping shell is fixedly connected to the top of the bottom plate, and limiting grooves are formed in the two sides of the top of the damping shell correspondingly; the damping protection mechanism comprises fixing rods fixedly connected to the two ends of one side of the inner wall of the damping shell, the outer walls of the fixing rods are sleeved with and slidably connected with sliding sleeves, the two ends of each sliding sleeve are fixedly connected with damping springs correspondingly, and one end of each damping spring is fixedly connected with a square shell. When an aircraft vibrates in the flying process, the satellite communication equipment and the damping frame shake left and right, the damping frame drives the sliding block to move left and right, the sliding block drives the sliding sleeve to move left and right, and the sliding sleeve is elastically deformed by the damping spring in the moving process, so that the frequency of shaking the satellite communication equipment left and right is preliminarily reduced.

Description

Technical Field

[0001] The invention relates to the technical field of airborne satellite communication, in particular to a shock absorbing frame device of airborne satellite communication equipment and a shock absorbing method thereof. Background Art

[0002] Satellite communication, to put it simply, is the communication between radio communication stations on Earth using satellites as relay stations. The satellite communication system consists of two parts: satellites and earth stations. The characteristics of satellite communication are: large communication range, not easily affected by land disasters, can be received at multiple locations at the same time, and can economically realize broadcast and multi-address communication.

[0003] Airborne satellite communication systems have been gradually improved in recent years. Since the existing airborne satellite communication systems are installed at the bottom of the aircraft, the vibrations generated by the aircraft during flight can easily cause vibrations in the satellite communication equipment, affecting the transmission of communication messages and signals. In addition, when the aircraft encounters special circumstances during flight, it may cause severe vibrations in the aircraft, thereby affecting the operation of the satellite communication equipment. Summary of the invention

[0004] The object of the present invention is to provide a shock absorbing frame device and a shock absorbing method for airborne satellite communication equipment to solve the problems raised in the above-mentioned background technology.

[0005] In order to solve the above technical problems, the present invention is achieved through the following technical solutions:

[0006] The present invention relates to a shock-absorbing frame device for airborne satellite communication equipment and a shock-absorbing method thereof, comprising a bottom plate, a shock-absorbing shell being fixedly connected to the top of the bottom plate, limiting grooves being respectively arranged on both sides of the top of the shock-absorbing shell, and a shock-absorbing protection mechanism, the shock-absorbing protection mechanism comprising a fixed rod fixedly connected to both ends of one side of an inner wall of the shock-absorbing shell, a sliding sleeve being sleeved on the outer wall of the fixed rod and slidably connected, shock-absorbing springs being respectively fixedly connected to both ends of the sliding sleeve, one end of the shock-absorbing spring being fixedly connected to a square shell, one side of the outer wall of the square shell being fixedly connected to one side of the inner wall of the shock-absorbing shell, and a shock-absorbing component being arranged on the top of the sliding sleeve.

[0007] Furthermore, the shock absorbing assembly includes a slider fixedly connected to the two ends of the top of the sliding sleeve, the outer wall of the slider is sleeved and slidably connected to the inner wall of the limiting groove, the top of the slider is fixedly connected to a shock absorbing frame, one side of the slider is fixedly connected to a cross bar, one end of the cross bar passes through the square shell and extends to the interior of the square shell, the end of the cross bar away from the slider is fixedly connected to a movable plate, the outer wall of the movable plate is sleeved and slidably connected to the inner wall of the square shell, and the two ends of the top of the square shell are respectively connected to the first elastic tube.

[0008] Furthermore, one end of the first elastic tube passes through the shock-absorbing shell and extends to the outside of the shock-absorbing shell, one end of the first elastic tube away from the square shell is connected to an L-shaped bag, the outer wall of the L-shaped bag is fixedly connected to the inner wall of the shock-absorbing frame, one side of the top end of the L-shaped bag is connected to an air pipe, an adsorption box is connected between the two air pipes, one side of the outer wall of the adsorption box is fixedly connected to the top of the inner wall of the shock-absorbing frame, the outer wall of the adsorption box is connected to a plurality of first suction cups, one side of the inner wall of the adsorption box is fixedly connected to a plurality of first extrusion springs, one end of the first extrusion spring is fixedly connected to a sealing ball, and the outer wall of the sealing ball is in contact with the inner wall of the first suction cup.

[0009] Furthermore, a clamping assembly is provided at the bottom of the shock absorber frame, and the clamping assembly includes a square tube fixedly connected to the bottom of the shock absorber frame, square plates are slidably connected to the inner wall of the square tube at both ends, a first return spring is fixedly connected between the two square plates, and elastic ropes are fixedly connected to the two ends of the square plate on one side close to the first return spring, one end of the elastic rope passes through the square tube and extends to the interior of the square shell, and the end of the elastic rope away from the square plate is fixedly connected to the side wall of the first return spring.

[0010] Furthermore, an L-shaped plate is fixedly connected to one side of the square plate away from the elastic rope, and an end of the L-shaped plate away from the square plate is fixedly connected to a clamping shell, an inner wall of the clamping shell is sleeved and slidably connected with a flexible splint, a second extrusion spring is fixedly connected to the center of one side of the flexible splint, one end of the second extrusion spring is fixedly connected to one side of the inner wall of the clamping shell, two ends of the flexible splint on one side close to the second extrusion spring are respectively fixedly connected to connecting rods, one end of the connecting rod passes through the clamping shell and extends to the outside of the clamping shell, and an end of the connecting rod away from the flexible splint is fixedly connected to an arc-shaped strip.

[0011] Furthermore, an auxiliary component is provided on the top of the base plate, and the auxiliary component includes vertical plates fixedly connected to both sides of the top of the base plate, and a number of vertical bars are fixedly connected to the top of the shock-absorbing shell. A rotating shell is rotatably connected to the center of one side of the vertical bar, and an air pressure plate is sleeved on the inner wall of the rotating shell and slidably connected. A sliding rod is fixedly connected to one side of the air pressure plate, and one end of the sliding rod passes through the rotating shell and extends to the outside of the rotating shell.

[0012] Furthermore, a spring is fixedly connected to one side of the air pressure plate close to the sliding rod, one end of the spring is fixedly connected to one side of the inner wall of the rotating shell, a rotating main block is rotatably connected between the two sliding rods, an arc-shaped clamping block is fixedly connected to one side of the rotating main block, a vertical pipe is connected to the top of the inner wall of the arc-shaped clamping block, a curved pipe is connected to one side of the outer wall of the rotating shell, one end of the curved pipe is connected to one side of the outer wall of the vertical pipe, and one side of the vertical pipe is connected to a second suction cup.

[0013] Furthermore, a heat dissipation assembly is provided on one side of the rotating main block, and the heat dissipation assembly includes an extrusion rod fixedly connected to the side of the rotating main block away from the arc clamping block, a second return spring is fixedly connected to the side of the rotating main block close to the extrusion rod, one end of the second return spring is fixedly connected to one side of the vertical plate, one end of the extrusion rod penetrates the vertical plate and extends to the outside of the vertical plate, and the end of the extrusion rod away from the rotating main block is fixedly connected to the extrusion plate.

[0014] Furthermore, a circular shell is sleeved on and slidably connected to the outer wall of the extrusion plate, one end of the circular shell is fixedly connected to the side wall of the vertical plate, a second elastic tube is connected to the top of the outer wall of the circular shell, a top shell is connected between the two second elastic tubes, the bottom of the top shell is fixedly connected to the top of the shock-absorbing frame, a condensation block is fixedly connected to the bottom of the inner wall of the top shell, and a number of air holes are respectively opened on both sides of the bottom of the inner wall of the top shell.

[0015] A shock absorbing frame device for airborne satellite communication equipment and a shock absorbing method thereof, and a shock absorbing method for a shock absorbing frame for airborne satellite communication equipment, comprising the following steps:

[0016] Step 1: This device is installed on the bottom plate of the aircraft, and the satellite communication device is placed inside the shock-absorbing frame. When the aircraft vibrates during flight, the satellite communication device and the shock-absorbing frame will shake left and right, and the shock-absorbing frame drives the slider to move left and right, and the slider drives the sliding sleeve to move left and right. During the movement of the sliding sleeve, it is elastically deformed by the shock-absorbing spring. When the slider moves left and right, the slider drives the cross bar to move, and the cross bar drives the moving plate to move. The moving plate moves inside the square shell, and air pressure is generated inside the square shell. The air pressure enters the inside of the L-shaped bag through the first elastic tube, so that the L-shaped bag expands, and the other cross bar drives the moving plate to move in the opposite direction. During the movement of the moving plate, negative pressure is generated in the area inside the square shell, and the negative pressure enters the inside of the L-shaped bag through the first elastic tube, and the negative pressure enters the trachea through the L-shaped bag, and the negative pressure enters the inside of the adsorption box through the trachea, and the negative pressure enters the inside of the first suction cup through the adsorption box;

[0017] Step 2: When the moving plate moves, the moving plate drives the elastic rope to move, so that the elastic rope is stretched. During the stretching process of the elastic rope, the two square plates are driven to move closer to each other. The square plate drives the L-shaped plate to move. The L-shaped plate drives the clamping shell to move. The clamping shell drives the flexible splint to move. The two flexible splints move closer to each other and are subjected to the reaction force of the satellite communication equipment. The flexible splint drives the connecting rod to move in the opposite direction. The connecting rod drives the arc-shaped bar to move in the opposite direction. The arc-shaped bar squeezes the middle end of the L-shaped bag, so that the air pressure inside the L-shaped bag moves to the upper and lower ends.

[0018] Step 3: When the aircraft vibrates violently during flight, the shock absorber will also drive the satellite communication device to move violently left and right. The satellite communication device squeezes the arc clamp block, which drives the rotating main block to move, and the rotating main block drives the sliding rod to rotate. The sliding rod drives the air pressure plate to slide inside the rotating shell. During the movement of the air pressure plate inside the rotating shell, negative pressure is generated in the area of ​​the rotating shell away from the spring. The negative pressure enters the interior of the vertical pipe through the bent pipe, and the negative pressure enters the interior of the second suction cup through the vertical pipe, and the satellite communication device is adsorbed by the second suction cup.

[0019] Step 4: When the rotating main block is pushed, the rotating main block drives the extrusion rod to move, and the extrusion rod drives the extrusion plate to move. The extrusion plate moves inside the round shell, thereby generating air pressure. The air pressure enters the interior of the top shell through the second elastic tube, and is affected by the cold air emitted by the condensation block. The air pressure discharges the cold air inside the top shell through the air holes to the top of the outer wall of the satellite communication equipment, and the cold air reacts with the hot air emitted when the satellite communication equipment is working, which can generate water vapor at the outer wall of the first suction cup.

[0020] The present invention has the following beneficial effects:

[0021] (1) In the present invention, the device is mounted on the bottom plate of the aircraft, and the satellite communication device is placed inside the shock-absorbing frame. When the aircraft vibrates during flight, the satellite communication device and the shock-absorbing frame will shake left and right, and the shock-absorbing frame drives the slider to move left and right, and the slider drives the sliding sleeve to move left and right. During the movement of the sliding sleeve, the sliding sleeve is elastically deformed by the shock-absorbing spring, thereby preliminarily reducing the frequency of the satellite communication device being shaken left and right. When the slider moves left and right, the slider drives the cross bar to move, and the cross bar drives the moving plate to move. The moving plate moves inside the square shell, and air pressure is generated inside the square shell. The air pressure enters the inside of the L-shaped bag through the first elastic tube, from The L-shaped bag is expanded, and the satellite communication equipment is squeezed during the expansion process, which can further reduce the vibration of the satellite communication equipment and enhance the protection effect of the satellite communication equipment. Another cross bar will drive the movable plate to move in the opposite direction. During the movement of the movable plate, negative pressure is generated in the area inside the square shell. The negative pressure enters the interior of the L-shaped bag through the first elastic tube, and the negative pressure enters the trachea through the L-shaped bag. The negative pressure enters the interior of the adsorption box through the trachea, and the negative pressure enters the interior of the first suction cup through the adsorption box. The satellite communication equipment is adsorbed by the first suction cup to prevent the satellite communication equipment from being hit during the shaking process, thereby enhancing the protection effect of the satellite communication equipment.

[0022] (2) According to the present invention, when the movable plate moves, the movable plate drives the elastic rope to move, so that the elastic rope is stretched. During the stretching process, the elastic rope drives the two square plates to approach each other. The square plate drives the L-shaped plate to move. The L-shaped plate drives the clamping shell to move. The clamping shell drives the flexible clamping plate to move. The two flexible clamping plates approach each other, thereby clamping the satellite communication equipment to prevent the satellite communication equipment from shaking up and down. Under the reaction force of the satellite communication equipment, the flexible clamping plate drives the connecting rod to move in the opposite direction. The connecting rod drives the arc-shaped bar to move in the opposite direction. The arc-shaped bar squeezes the middle end of the L-shaped bag, so that the air pressure inside the L-shaped bag moves to the upper and lower ends, thereby enhancing the expansion and squeezing effect of the L-shaped bag, and further enhancing the shock-absorbing protection effect of the satellite communication equipment.

[0023] (3) In the present invention, when the aircraft vibrates violently during flight, the shock absorbing frame will also drive the satellite communication equipment to move violently left and right. The satellite communication equipment squeezes the arc clamp block, and the arc clamp block drives the rotating main block to move. The rotating main block drives the sliding rod to rotate, and the sliding rod drives the air pressure plate to slide inside the rotating shell, thereby reducing the shock of the satellite communication equipment, further enhancing the protection effect of the satellite communication equipment. In the process of the air pressure plate moving inside the rotating shell, negative pressure will be generated in the area of ​​the rotating shell away from the spring. The negative pressure enters the interior of the vertical pipe through the bent pipe, and the negative pressure enters the interior of the second suction cup through the vertical pipe. The satellite communication equipment is adsorbed by the second suction cup to prevent the satellite communication equipment from moving to the left and then continuing to move to the right, further reducing the shaking force generated by the satellite communication equipment and enhancing the protection effect of the satellite communication equipment.

[0024] (4) In the present invention, when the rotating main block is pushed, the rotating main block drives the extrusion rod to move, and the extrusion rod drives the extrusion plate to move. The extrusion plate moves inside the circular shell, thereby generating air pressure. The air pressure enters the interior of the top shell through the second elastic tube, and is affected by the cold air emitted by the condensation block. The air pressure discharges the cold air inside the top shell through the air holes to the top of the outer wall of the satellite communication equipment, thereby preventing the body surface temperature from being too high during the operation of the satellite communication equipment, thereby enhancing the protection effect of the satellite communication equipment. The cold air reacts with the hot air emitted by the satellite communication equipment during operation, thereby generating water vapor at the outer wall of the first suction cup, further enhancing the adsorption effect of the first suction cup, thereby indirectly improving the protection effect of the satellite communication equipment.

[0025] Of course, any product implementing the present invention does not necessarily need to achieve all of the advantages described above at the same time. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the accompanying drawings required for describing the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other accompanying drawings can be obtained based on these accompanying drawings without paying creative work.

[0027] Figure 1 It is a schematic diagram of the overall top view structure of the present invention;

[0028] Figure 2 It is a schematic diagram of the overall side half-section structure of the present invention;

[0029] Figure 3 It is a schematic diagram of the internal top view structure of the present invention;

[0030] Figure 4 This is a schematic diagram of the explosion structure of the shock absorbing assembly of the present invention;

[0031] Figure 5 This is a schematic diagram of the exploded structure of the heat dissipation assembly of the present invention;

[0032] Figure 6 This is a schematic diagram of the exploded structure of the clamping assembly of the present invention;

[0033] Figure 7 It is a schematic diagram of the top view of the auxiliary component of the present invention;

[0034] Figure 8 This is a schematic diagram of a half-section structure of an auxiliary component of the present invention;

[0035] Fig. 9 For the present invention Figure 2 A magnified view of middle;

[0036] Fig.10 For the present invention Figure 5 Enlarged view of middle B;

[0037] Fig.11 It is a schematic flow chart of the vibration reduction method of the present invention.

[0038] In the accompanying drawings, the components represented by the reference numerals are listed as follows:

[0039] In the figure: 1, bottom plate; 2, shock-absorbing shell; 3, limit groove; 4, shock-absorbing protection mechanism; 41, fixed rod; 42, sliding sleeve; 43, shock-absorbing spring; 44, square shell; 45, shock-absorbing assembly; 46, clamping assembly; 47, auxiliary assembly; 48, heat dissipation assembly; 451, slider; 452, shock-absorbing frame; 453, cross bar; 454, moving plate; 455, first elastic tube; 456, L-shaped bag; 457, air pipe; 458, adsorption box; 459, first suction cup; 4510, first extrusion spring; 4511, sealing ball; 461, elastic rope; 462, square tube; 463, square plate; 464, first complex Position spring; 465, L-shaped plate; 466, clamping shell; 467, flexible clamping plate; 468, second extrusion spring; 469, connecting rod; 4610, arc-shaped strip; 471, vertical plate; 472, vertical strip; 473, rotating shell; 474, air pressure plate; 475, sliding rod; 476, rotating main block; 477, arc-shaped clamping block; 478, vertical tube; 479, second suction cup; 4710, bent tube; 481, extrusion rod; 483, extrusion plate; 482, second return spring; 484, round shell; 485, second elastic tube; 486, top shell; 487, condensation block; 488, air hole; 4711, spring. DETAILED DESCRIPTION

[0040] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. 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 creative work are within the scope of protection of the present invention.

[0041] Example 1, please refer to Figure 1-Figure 11 As shown, the present invention is a shock-absorbing frame device for airborne satellite communication equipment and a shock-absorbing method thereof, comprising a bottom plate 1, a shock-absorbing shell 2 is fixedly connected to the top of the bottom plate 1, and limiting grooves 3 are respectively provided on both sides of the top of the shock-absorbing shell 2, the purpose of such a setting is to limit the moving distance, and also includes;

[0042] The shock-absorbing protection mechanism 4 includes a fixing rod 41 fixedly connected to both ends of one side of the inner wall of the shock-absorbing shell 2. The purpose of this arrangement is to prevent the sliding sleeve 42 from falling off. The outer wall of the fixing rod 41 is sleeved and slidably connected with the sliding sleeve 42. The two ends of the sliding sleeve 42 are respectively fixedly connected with shock-absorbing springs 43. One end of the shock-absorbing spring 43 is fixedly connected with a square shell 44. One side of the outer wall of the square shell 44 is fixedly connected to one side of the inner wall of the shock-absorbing shell 2. A shock-absorbing assembly 45 is arranged on the top of the sliding sleeve 42.

[0043] The shock absorbing assembly 45 includes a slider 451 fixedly connected to the two ends of the top of the sliding sleeve 42, the outer wall of the slider 451 is sleeved and slidably connected to the inner wall of the limiting groove 3, the top of the slider 451 is fixedly connected to a shock absorbing frame 452, one side of the slider 451 is fixedly connected to a cross bar 453, one end of the cross bar 453 passes through the square shell 44 and extends to the inside of the square shell 44, the end of the cross bar 453 away from the slider 451 is fixedly connected to a moving plate 454, the outer wall of the moving plate 454 is sleeved and slidably connected to the inner wall of the square shell 44, and the two ends of the top of the square shell 44 are respectively connected to the first elastic tube 455, the purpose of this arrangement is to enable elastic stretching.

[0044] One end of the first elastic tube 455 passes through the shock absorbing shell 2 and extends to the outside of the shock absorbing shell 2, and the end of the first elastic tube 455 away from the square shell 44 is connected to an L-shaped bag 456, the outer wall of the L-shaped bag 456 is fixedly connected to the inner wall of the shock absorbing frame 452, and the top side of the L-shaped bag 456 is connected to an air pipe 457, and an adsorption box 458 is connected between the two air pipes 457, and the outer wall of the adsorption box 458 is fixedly connected to the top of the inner wall of the shock absorbing frame 452. The outer wall of the adsorption box 458 is connected to a plurality of first suction cups 459, and the inner wall of the adsorption box 458 is fixedly connected to a plurality of first extrusion springs 4510, and one end of the first extrusion spring 4510 is fixedly connected to a sealing ball 4511, the purpose of this arrangement is to seal the first suction cup 459 to prevent the gas inside the adsorption box 458 from being discharged outward, and the outer wall of the sealing ball 4511 is contacted with the inner wall of the first suction cup 459.

[0045] A clamping assembly 46 is provided at the bottom of the shock absorbing frame 452, and the clamping assembly 46 includes a square tube 462 fixedly connected to the bottom of the shock absorbing frame 452, and square plates 463 are respectively slidably connected to the inner wall of the square tube 462 at both ends, and a first return spring 464 is fixedly connected between the two square plates 463, and elastic ropes 461 are respectively fixedly connected to the two ends of the square plate 463 on one side close to the first return spring 464. The purpose of this arrangement is to enable tensile deformation, one end of the elastic rope 461 passes through the square tube 462 and extends to the inside of the square shell 44, and the end of the elastic rope 461 away from the square plate 463 is fixedly connected to the side wall of the first return spring 464.

[0046] An L-shaped plate 465 is fixedly connected to one side of the square plate 463 away from the elastic rope 461, and one end of the L-shaped plate 465 away from the square plate 463 is fixedly connected to a clamping shell 466, and a flexible splint 467 is sleeved on the inner wall of the clamping shell 466 and slidably connected. The purpose of this arrangement is to provide friction on the outer surface to enhance the clamping effect, and a second extrusion spring 468 is fixedly connected to the center of one side of the flexible splint 467, and one end of the second extrusion spring 468 is fixedly connected to one side of the inner wall of the clamping shell 466, and two ends of the side of the flexible splint 467 close to the second extrusion spring 468 are respectively fixedly connected to connecting rods 469, one end of the connecting rod 469 passes through the clamping shell 466 and extends to the outside of the clamping shell 466, and one end of the connecting rod 469 away from the flexible splint 467 is fixedly connected to an arc-shaped strip 4610.

[0047] This device is installed on the bottom plate of the aircraft, and the satellite communication device is placed inside the shock-absorbing frame 452. When the aircraft vibrates during flight, the satellite communication device and the shock-absorbing frame 452 will shake left and right, and the shock-absorbing frame 452 drives the slider 451 to move left and right, and the slider 451 drives the sliding sleeve 42 to move left and right. During the movement of the sliding sleeve 42, it is elastically deformed by the shock-absorbing spring 43, thereby preliminarily reducing the frequency of the satellite communication device being shaken left and right. When the slider 451 moves left and right, the slider 451 drives the cross bar 453 to move, and the cross bar 453 drives the moving plate 454 to move. The moving plate 454 moves inside the square shell 44, and air pressure is generated inside the square shell 44. The air pressure enters the inside of the L-shaped bag 456 through the first elastic tube 455, thereby The L-shaped bag 456 is expanded, and the satellite communication equipment is squeezed during the expansion process of the L-shaped bag 456, which can further reduce the vibration of the satellite communication equipment and enhance the protection effect of the satellite communication equipment. The other cross bar 453 will drive the movable plate 454 to move in the opposite direction. During the movement of the movable plate 454, negative pressure is generated in the area inside the square shell 44, and the negative pressure enters the interior of the L-shaped bag 456 through the first elastic tube 455. The negative pressure enters the air pipe 457 through the L-shaped bag 456, and the negative pressure enters the interior of the adsorption box 458 through the air pipe 457. The negative pressure enters the interior of the first suction cup 459 through the adsorption box 458, and the satellite communication equipment is adsorbed by the first suction cup 459 to prevent the satellite communication equipment from being hit during the shaking process, thereby enhancing the protection effect of the satellite communication equipment.

[0048] When the movable plate 454 moves, the movable plate 454 drives the elastic rope 461 to move, so that the elastic rope 461 is stretched. During the stretching process of the elastic rope 461, the two square plates 463 are driven to approach each other, and the square plate 463 drives the L-shaped plate 465 to move. The L-shaped plate 465 drives the clamping shell 466 to move, and the clamping shell 466 drives the flexible splint 467 to move. The two flexible splints 467 approach each other, thereby clamping the satellite communication equipment to prevent the satellite communication equipment from shaking up and down. Under the reaction force of the satellite communication equipment, the flexible splint 467 drives the connecting rod 469 to move in the opposite direction, and the connecting rod 469 drives the arc-shaped bar 4610 to move in the opposite direction. The arc-shaped bar 4610 squeezes the middle end of the L-shaped bag 456, so that the air pressure inside the L-shaped bag 456 moves to the upper and lower ends, thereby enhancing the expansion and squeezing effect of the L-shaped bag 456, and further enhancing the shock absorption protection effect of the satellite communication equipment.

[0049] In embodiment 2, an auxiliary component 47 is provided on the top of the base plate 1, and the auxiliary component 47 includes vertical plates 471 fixedly connected to both sides of the top of the base plate 1, and a plurality of vertical bars 472 are fixedly connected to the top of the shock-absorbing shell 2. A rotating shell 473 is rotatably connected to the center of one side of the vertical bar 472, and an air pressure plate 474 is sleeved on the inner wall of the rotating shell 473 and slidably connected. A sliding rod 475 is fixedly connected to one side of the air pressure plate 474, and one end of the sliding rod 475 passes through the rotating shell 473 and extends to the outside of the rotating shell 473.

[0050] A spring 4711 is fixedly connected to one side of the air pressure plate 474 close to the sliding rod 475. The purpose of this arrangement is to enable reset. One end of the spring 4711 is fixedly connected to one side of the inner wall of the rotating shell 473. A rotating main block 476 is rotatably connected between the two sliding rods 475. One side of the rotating main block 476 is fixedly connected to an arc-shaped clamping block 477. The top of the inner wall of the arc-shaped clamping block 477 is connected to a vertical pipe 478. One side of the outer wall of the rotating shell 473 is connected to a bent pipe 4710. One end of the bent pipe 4710 is connected to one side of the outer wall of the vertical pipe 478. One side of the vertical pipe 478 is connected to a second suction cup 479. The purpose of this arrangement is to produce an adsorption effect.

[0051] A heat dissipation assembly 48 is provided on one side of the rotating main block 476, and the heat dissipation assembly 48 includes an extrusion rod 481 fixedly connected to the side of the rotating main block 476 away from the arc clamping block 477, and a second return spring 482 is fixedly connected to the side of the rotating main block 476 close to the extrusion rod 481, one end of the second return spring 482 is fixedly connected to one side of the vertical plate 471, one end of the extrusion rod 481 penetrates the vertical plate 471 and extends to the outside of the vertical plate 471, and the end of the extrusion rod 481 away from the rotating main block 476 is fixedly connected to the extrusion plate 483.

[0052] A circular shell 484 is sleeved on and slidably connected to the outer wall of the extrusion plate 483, one end of the circular shell 484 is fixedly connected to the side wall of the vertical plate 471, a second elastic tube 485 is connected to the top of the outer wall of the circular shell 484, a top shell 486 is connected between the two second elastic tubes 485, the bottom of the top shell 486 is fixedly connected to the top of the shock absorbing frame 452, a condensation block 487 is fixedly connected to the bottom of the inner wall of the top shell 486, the purpose of this arrangement is to be able to emit cold air, and a number of air holes 488 are respectively provided on both sides of the bottom of the inner wall of the top shell 486.

[0053] A shock absorbing frame device for airborne satellite communication equipment and a shock absorbing method thereof, and a shock absorbing method for a shock absorbing frame for airborne satellite communication equipment, comprising the following steps:

[0054] Step 1: This device is installed on the bottom plate of the aircraft, and the satellite communication device is placed inside the shock-absorbing frame 452. When the aircraft vibrates during flight, the satellite communication device and the shock-absorbing frame 452 will shake left and right, and the shock-absorbing frame 452 drives the slider 451 to move left and right, and the slider 451 drives the sliding sleeve 42 to move left and right. During the movement of the sliding sleeve 42, it is elastically deformed by the shock-absorbing spring 43. When the slider 451 moves left and right, the slider 451 drives the cross bar 453 to move, and the cross bar 453 drives the moving plate 454 to move. The moving plate 454 is inside the square shell 44. When the first elastic tube 455 moves, air pressure is generated inside the square shell 44, and the air pressure enters the L-shaped bag 456 through the first elastic tube 455, so that the L-shaped bag 456 expands, and the other cross bar 453 drives the moving plate 454 to move in the opposite direction. During the movement of the moving plate 454, negative pressure is generated in the area inside the square shell 44, and the negative pressure enters the L-shaped bag 456 through the first elastic tube 455, and the negative pressure enters the air pipe 457 through the L-shaped bag 456, and the negative pressure enters the interior of the adsorption box 458 through the air pipe 457, and the negative pressure enters the interior of the first suction cup 459 through the adsorption box 458;

[0055] Step 2: When the moving plate 454 moves, the moving plate 454 drives the elastic rope 461 to move, so that the elastic rope 461 is stretched. During the stretching process of the elastic rope 461, the two square plates 463 are driven to approach each other. The square plate 463 drives the L-shaped plate 465 to move. The L-shaped plate 465 drives the clamping shell 466 to move. The clamping shell 466 drives the flexible clamping plate 467 to move. The two flexible clamping plates 467 approach each other and are subjected to the reaction force of the satellite communication equipment. The flexible clamping plate 467 drives the connecting rod 469 to move in the opposite direction. The connecting rod 469 drives the arc-shaped bar 4610 to move in the opposite direction. The arc-shaped bar 4610 squeezes the middle end of the L-shaped bag 456, so that the air pressure inside the L-shaped bag 456 moves to the upper and lower ends.

[0056] Step 3: When the aircraft vibrates violently during flight, the shock absorber 452 will also drive the satellite communication device to move violently left and right. The satellite communication device squeezes the arc clamp 477, and the arc clamp 477 drives the rotating main block 476 to move. The rotating main block 476 drives the sliding rod 475 to rotate, and the sliding rod 475 drives the air pressure plate 474 to slide inside the rotating shell 473. During the movement of the air pressure plate 474 inside the rotating shell 473, negative pressure will be generated in the area of ​​the rotating shell 473 away from the spring 4711. The negative pressure enters the interior of the vertical pipe 478 through the curved pipe 4710, and the negative pressure enters the interior of the second suction cup 479 through the vertical pipe 478, and the satellite communication device is adsorbed by the second suction cup 479;

[0057] Step 4: When the rotating main block 476 is pushed, the rotating main block 476 drives the extrusion rod 481 to move, and the extrusion rod 481 drives the extrusion plate 483 to move. The extrusion plate 483 moves inside the round shell 484, thereby generating air pressure. The air pressure enters the interior of the top shell 486 through the second elastic tube 485, and is affected by the cold air emitted by the condensation block 487. The air pressure discharges the cold air inside the top shell 486 through the air hole 488 to the top of the outer wall of the satellite communication equipment, and the cold air reacts with the hot air emitted when the satellite communication equipment is working, which can cause water vapor to be generated on the outer wall of the first suction cup 459.

[0058] During use, when the aircraft vibrates violently during flight, the shock absorbing frame 452 will also drive the satellite communication equipment to move violently left and right. The satellite communication equipment squeezes the arc clamping block 477, and the arc clamping block 477 drives the rotating main block 476 to move. The rotating main block 476 drives the sliding rod 475 to rotate, and the sliding rod 475 drives the air pressure plate 474 to slide inside the rotating shell 473, thereby reducing the shock of the satellite communication equipment, further enhancing the protection effect of the satellite communication equipment, and when the air pressure plate 474 moves inside the rotating shell 473, negative pressure will be generated in the area of ​​the rotating shell 473 away from the spring 4711, and the negative pressure enters the interior of the vertical pipe 478 through the curved pipe 4710, and the negative pressure enters the interior of the second suction cup 479 through the vertical pipe 478, and the satellite communication equipment is adsorbed by the second suction cup 479 to prevent the satellite communication equipment from moving to the left and then continuing to move to the right, further reducing the shaking force generated by the satellite communication equipment and enhancing the protection effect of the satellite communication equipment.

[0059] When the rotating main block 476 is pushed, the rotating main block 476 drives the extrusion rod 481 to move, and the extrusion rod 481 drives the extrusion plate 483 to move. The extrusion plate 483 moves inside the round shell 484, thereby generating air pressure. The air pressure enters the interior of the top shell 486 through the second elastic tube 485, and is affected by the cold air emitted by the condensation block 487. The air pressure discharges the cold air inside the top shell 486 through the air hole 488 to the top of the outer wall of the satellite communication equipment, preventing the body surface temperature from being too high during the operation of the satellite communication equipment, thereby enhancing the protection effect of the satellite communication equipment. The cold air reacts with the hot air emitted by the satellite communication equipment during operation, which can generate water vapor at the outer wall of the first suction cup 459, further enhancing the adsorption effect of the first suction cup 459, thereby indirectly improving the protection effect of the satellite communication equipment.

[0060] The preferred embodiments of the present invention disclosed above are only used to help illustrate the present invention. The preferred embodiments do not describe all the details in detail, nor do they limit the invention to the specific implementation methods described. Obviously, many modifications and changes can be made according to the content of this specification. This specification selects and specifically describes these embodiments in order to better explain the principles and practical applications of the present invention, so that those skilled in the art can understand and use the present invention well. The present invention is limited only by the claims and their full scope and equivalents.

Claims

1. A shock-absorbing bracket device for airborne satellite communication equipment, characterized in that: It comprises a bottom plate (1), the top of the bottom plate (1) is fixedly connected to a shock absorbing shell (2), and limiting grooves (3) are respectively provided on both sides of the top of the shock absorbing shell (2), and further comprises: A shock absorbing protection mechanism (4), the shock absorbing protection mechanism (4) comprising a fixed rod (41) fixedly connected to both ends of one side of the inner wall of the shock absorbing shell (2), the outer wall of the fixed rod (41) being sleeved and slidably connected with a sliding sleeve (42), the two ends of the sliding sleeve (42) being respectively fixedly connected with shock absorbing springs (43), one end of the shock absorbing spring (43) being fixedly connected with a square shell (44), one side of the outer wall of the square shell (44) being fixedly connected to one side of the inner wall of the shock absorbing shell (2), and a shock absorbing component (45) being arranged at the top of the sliding sleeve (42).

2. The shock mount device for airborne satellite communication equipment according to claim 1, characterized in that: The shock absorbing assembly (45) comprises a slider (451) fixedly connected to the two ends of the top of the sliding sleeve (42); the outer wall of the slider (451) is sleeved and slidably connected to the inner wall of the limiting groove (3); the top of the slider (451) is fixedly connected to a shock absorbing frame (452); one side of the slider (451) is fixedly connected to a cross bar (453); one end of the cross bar (453) passes through the square shell (44) and extends to the inside of the square shell (44); one end of the cross bar (453) away from the slider (451) is fixedly connected to a moving plate (454); the outer wall of the moving plate (454) is sleeved and slidably connected to the inner wall of the square shell (44); and the two ends of the top of the square shell (44) are respectively connected to the first elastic tube (455).

3. The shock mount device for airborne satellite communication equipment according to claim 2, characterized in that: One end of the first elastic tube (455) passes through the shock absorbing shell (2) and extends to the outside of the shock absorbing shell (2); one end of the first elastic tube (455) away from the square shell (44) is connected to an L-shaped bag (456); the outer wall of the L-shaped bag (456) is fixedly connected to the inner wall of the shock absorbing frame (452); one side of the top end of the L-shaped bag (456) is connected to an air pipe (457); an adsorption box (458) is connected between the two air pipes (457); the adsorption box (458) One side of the outer wall of the box (458) is fixedly connected to the top of the inner wall of the shock-absorbing frame (452), and the outer wall of the adsorption box (458) is connected to a plurality of first suction cups (459), and one side of the inner wall of the adsorption box (458) is fixedly connected to a plurality of first extrusion springs (4510), and one end of the first extrusion spring (4510) is fixedly connected to a sealing ball (4511), and the outer wall of the sealing ball (4511) is in contact with the inner wall of the first suction cup (459).

4. The shock mount device for airborne satellite communication equipment according to claim 3, characterized in that: A clamping assembly (46) is provided at the bottom of the shock absorbing frame (452), and the clamping assembly (46) comprises a square tube (462) fixedly connected to the bottom of the shock absorbing frame (452), square plates (463) are slidably connected to the inner walls of the square tube (462) at both ends, a first return spring (464) is fixedly connected between the two square plates (463), and elastic ropes (461) are fixedly connected to the two ends of one side of the square plate (463) close to the first return spring (464), one end of the elastic rope (461) passes through the square tube (462) and extends to the inside of the square shell (44), and one end of the elastic rope (461) away from the square plate (463) is fixedly connected to the side wall of the first return spring (464).

5. The shock mount device for airborne satellite communication equipment according to claim 4, characterized in that: The side of the square plate (463) away from the elastic rope (461) is fixedly connected to an L-shaped plate (465), and the end of the L-shaped plate (465) away from the square plate (463) is fixedly connected to a clamping shell (466). The inner wall of the clamping shell (466) is sleeved and slidably connected with a flexible clamp (467). A second extrusion spring (468) is fixedly connected at the center of one side of the flexible clamp (467). One end of the second extrusion spring (468) is fixedly connected to one side of the inner wall of the clamping shell (466). Both ends of the side of the flexible clamp (467) close to the second extrusion spring (468) are respectively fixedly connected to connecting rods (469). One end of the connecting rod (469) passes through the clamping shell (466) and extends to the outside of the clamping shell (466). The end of the connecting rod (469) away from the flexible clamp (467) is fixedly connected to an arc-shaped strip (4610).

6. The shock mount device for airborne satellite communication equipment according to claim 5, characterized in that: An auxiliary component (47) is arranged on the top of the bottom plate (1), and the auxiliary component (47) comprises vertical plates (471) fixedly connected to both sides of the top of the bottom plate (1); a plurality of vertical bars (472) are fixedly connected to the top of the shock-absorbing shell (2) on all sides; a rotating shell (473) is rotatably connected to the center of one side of the vertical bar (472); an air pressure plate (474) is sleeved on the inner wall of the rotating shell (473) and slidably connected; a sliding rod (475) is fixedly connected to one side of the air pressure plate (474); one end of the sliding rod (475) passes through the rotating shell (473) and extends to the outside of the rotating shell (473).

7. The shock mount device for airborne satellite communication equipment according to claim 6, characterized in that: A spring (4711) is fixedly connected to one side of the air pressure plate (474) close to the sliding rod (475), one end of the spring (4711) is fixedly connected to one side of the inner wall of the rotating shell (473), a rotating main block (476) is rotatably connected between the two sliding rods (475), an arc-shaped clamping block (477) is fixedly connected to one side of the rotating main block (476), a vertical pipe (478) is connected to the top of the inner wall of the arc-shaped clamping block (477), a curved pipe (4710) is connected to one side of the outer wall of the rotating shell (473), one end of the curved pipe (4710) is connected to one side of the outer wall of the vertical pipe (478), and a second suction cup (479) is connected to one side of the vertical pipe (478).

8. The shock-absorbing bracket device for airborne satellite communication equipment according to claim 7, characterized in that: A heat dissipation assembly (48) is provided on one side of the rotating main block (476), and the heat dissipation assembly (48) includes an extrusion rod (481) fixedly connected to a side of the rotating main block (476) away from the arc-shaped clamping block (477); a second return spring (482) is fixedly connected to a side of the rotating main block (476) close to the extrusion rod (481); one end of the second return spring (482) is fixedly connected to one side of the vertical plate (471); one end of the extrusion rod (481) passes through the vertical plate (471) and extends to the outside of the vertical plate (471); and one end of the extrusion rod (481) away from the rotating main block (476) is fixedly connected to an extrusion plate (483).

9. The shock mount device for airborne satellite communication equipment according to claim 8, characterized in that: A circular shell (484) is sleeved on and slidably connected to the outer wall of the extrusion plate (483); one end of the circular shell (484) is fixedly connected to the side wall of the vertical plate (471); a second elastic tube (485) is connected to the top of the outer wall of the circular shell (484); a top shell (486) is connected between the two second elastic tubes (485); the bottom of the top shell (486) is fixedly connected to the top of the shock absorbing frame (452); a condensation block (487) is fixedly connected to the bottom of the inner wall of the top shell (486); and a plurality of air holes (488) are respectively provided on both sides of the bottom of the inner wall of the top shell (486).

10. According to any one of claims 1 to 9, a shock absorbing method for a shock absorbing frame of an airborne satellite communication device, comprising the following steps, characterized in that: Step 1: This device is installed on the bottom plate of the aircraft, and the satellite communication device is placed inside the shock-absorbing frame (452). When the aircraft vibrates during flight, the satellite communication device and the shock-absorbing frame (452) will shake left and right, and the shock-absorbing frame (452) drives the slider (451) to move left and right, and the slider (451) drives the sliding sleeve (42) to move left and right. During the movement of the sliding sleeve (42), the elastic deformation of the shock-absorbing spring (43) is received. When the slider (451) moves left and right, the slider (451) drives the cross bar (453) to move, and the cross bar (453) drives the moving plate (454) to move. The moving plate (454) is inside the square shell (44). When the square shell (44) moves, air pressure is generated inside the square shell (44), and the air pressure enters the inside of the L-shaped bag (456) through the first elastic tube (455), so that the L-shaped bag (456) expands, and the other cross bar (453) drives the moving plate (454) to move in the opposite direction. During the movement of the moving plate (454), negative pressure is generated in the area inside the square shell (44), and the negative pressure enters the inside of the L-shaped bag (456) through the first elastic tube (455), and the negative pressure enters the air pipe (457) through the L-shaped bag (456), and the negative pressure enters the inside of the adsorption box (458) through the air pipe (457), and the negative pressure enters the inside of the first suction cup (459) through the adsorption box (458); Step 2: When the moving plate (454) moves, the moving plate (454) drives the elastic rope (461) to move, so that the elastic rope (461) is stretched. During the stretching process of the elastic rope (461), the two square plates (463) are driven to move closer to each other. The square plate (463) drives the L-shaped plate (465) to move. The L-shaped plate (465) drives the clamping shell (466) to move. The clamping shell (466) drives the flexible clamping plate (467) to move. The two flexible clamping plates (467) move closer to each other and are subjected to the reaction force of the satellite communication equipment. The flexible clamping plate (467) drives the connecting rod (469) to move in the opposite direction. The connecting rod (469) drives the arc-shaped bar (4610) to move in the opposite direction. The arc-shaped bar (4610) squeezes the middle end of the L-shaped bag (456), so that the air pressure inside the L-shaped bag (456) moves to the upper and lower ends. Step 3: When the aircraft vibrates violently during flight, the shock absorber (452) will also drive the satellite communication device to move violently left and right. The satellite communication device squeezes the arc clamp (477), and the arc clamp (477) drives the rotating main block (476) to move. The rotating main block (476) drives the sliding rod (475) to rotate, and the sliding rod (475) drives the air pressure plate (474) to slide inside the rotating shell (473). During the movement of the air pressure plate (474) inside the rotating shell (473), negative pressure is generated in the area of ​​the rotating shell (473) away from the spring (4711). The negative pressure enters the interior of the vertical pipe (478) through the curved pipe (4710), and the negative pressure enters the interior of the second suction cup (479) through the vertical pipe (478), and the satellite communication device is adsorbed by the second suction cup (479); Step 4: When the rotating main block (476) is pushed, the rotating main block (476) drives the extrusion rod (481) to move, and the extrusion rod (481) drives the extrusion plate (483) to move. The extrusion plate (483) moves inside the round shell (484), thereby generating air pressure. The air pressure enters the interior of the top shell (486) through the second elastic tube (485), and is affected by the cold air emitted by the condensation block (487). The air pressure discharges the cold air inside the top shell (486) through the air hole (488) to the top of the outer wall of the satellite communication equipment, and the cold air reacts with the hot air emitted when the satellite communication equipment is working, which can cause water vapor to be generated on the outer wall of the first suction cup (459).

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