CN216375032U - Integrated information processing apparatus - Google Patents
Integrated information processing apparatus Download PDFInfo
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- CN216375032U CN216375032U CN202121355003.9U CN202121355003U CN216375032U CN 216375032 U CN216375032 U CN 216375032U CN 202121355003 U CN202121355003 U CN 202121355003U CN 216375032 U CN216375032 U CN 216375032U
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- information processing
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- damping
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Abstract
The utility model relates to the technical field of information processing, and discloses comprehensive information processing equipment which comprises a fixed base, wherein a mounting groove is formed in the fixed base, an information processor is arranged in the mounting groove, heat dissipation boxes are arranged on two sides of the fixed base, a damping mechanism is arranged in the fixed base, and a fixed-point heat dissipation mechanism is arranged in the heat dissipation boxes. This synthesize information processing apparatus, when the aircraft takes off and goes up and down, can produce huge impact force, the shock attenuation upper plate promotes the connecting rod and descends, make the connecting rod promote two sets of sliders I and slide in shock attenuation bottom plate is inside, promote two sets of flexible pieces and slide in the fixed block is inside, further compression spring I, thereby the upper and lower impact force that information processor received has been reduced, when information processor receives the effort of controlling, can make information processor compression spring two that sets up all around, thereby the impact force that information processor received has been slowed down, equipment has been prevented to suffer the striking and has been damaged, the practicality of device has been guaranteed.
Description
Technical Field
The utility model relates to the technical field of information processing, in particular to comprehensive information processing equipment.
Background
The comprehensive information processing equipment is used for warning and prompting to prevent ground collision accidents in flight, providing terrain display pictures such as two-dimensional warning colors, two-dimensional navigation pictures, three-dimensional visual scenes and the like, enhancing the perception of pilots to surrounding terrain, and being applied to the aircrafts such as transporters, fixed wing aircrafts, helicopters and the like.
The existing information processing equipment can generate huge impact force when an airplane takes off or descends, and the existing equipment does not have a damping device, so that the equipment is possibly collided and damaged after being stressed, and the normal operation of the equipment is influenced.
When current information processing equipment dispels the heat, dispel the heat through the vent mostly, can not dispel the heat to equipment inside accurately, the radiating efficiency is low, and the heat radiation equipment passes through electric power and starts, can increase inside heat, is unfavorable for the heat dissipation.
Therefore, a need exists for an integrated information processing device to solve the problems of the device that does not have a shock absorption function, cannot perform accurate heat dissipation, and has low heat dissipation efficiency.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Aiming at the defects of the prior art, the utility model provides the comprehensive information processing equipment which has the advantages of shock absorption and high heat dissipation efficiency, and solves the problems that the equipment in the background art does not have a shock absorption function, can not carry out accurate heat dissipation and has low heat dissipation efficiency.
(II) technical scheme
In order to achieve the purpose, the utility model provides the following technical scheme that the comprehensive information processing equipment comprises a fixed base, wherein a mounting groove is formed in the fixed base, an information processor is arranged in the mounting groove, heat dissipation boxes are arranged on two sides of the fixed base, a damping mechanism is arranged in the fixed base, and a fixed-point heat dissipation mechanism is arranged in the heat dissipation boxes.
Through the technical scheme, through the damper who sets up, can make the integrated information processing equipment take off when the aircraft lands, reduce the impact force that equipment received, prevented that equipment atress striking from taking place to damage, influence the normal use of equipment, the practicality of device has been guaranteed, fixed point heat dissipation mechanism through setting up, it is rotatory to drive rotatory flabellum through natural wind, thereby make radiator fan dispel the heat to information processor, the problem of the long-time high temperature of using of information processor has been reduced, the inside thermal production of equipment has been reduced, the equipment radiating efficiency has been promoted, the practicality of device has been guaranteed.
Preferably, damper includes the inside bottom fixed connection's of unable adjustment base damping bottom plate, damping bottom plate is inside to be provided with two sets of slider one, and is two sets of slider one is close to the flexible piece of damping bottom plate mid point one side fixedly connected with, and is two sets of flexible piece is close to damping bottom plate one side and sets up inside the fixed block, the fixed block sets up inside damping bottom plate, and is two sets of fixedly connected with spring one between the flexible piece, it is two sets of a slider outside is provided with the connecting rod, and is two sets of the connecting rod top sets up in two outsides of slider, and is two sets of slider two sets up in the shock attenuation upper plate, and is two sets of shock attenuation upper plate fixed connection in mounting groove bottom, mounting groove fixedly connected with connecting plate all around, the outside fixedly connected with spring two of connecting plate, two other end fixed connection of spring are in the inside lateral wall of unable adjustment base.
Through the technical scheme, the shock absorption mechanism is arranged, so that when the integrated information processing equipment takes off and lands on an airplane, the impact force received by the equipment is reduced, the equipment is prevented from being damaged due to impact of stress on the equipment, the normal use of the equipment is prevented from being influenced, and the practicability of the device is ensured.
Preferably, the first sliding block is provided with two sets, the two sets of the first sliding block are embedded inside the damping bottom plate and are in sliding connection with the damping bottom plate, and the outer portion of the first sliding block is movably connected with the bottom end of the connecting rod through a bolt.
Preferably, the connecting rods are symmetrically arranged, and the top ends of the two groups of connecting rods are movably connected with the two sliding blocks through bolts.
Preferably, fixed point heat dissipation mechanism includes the swivelling chute that the heat dissipation incasement portion was seted up, the inside bull stick that is provided with of swivelling chute, the outside fixedly connected with multiunit rotating fan leaf of bull stick, bull stick one end extends to the outside fixedly connected with reciprocating screw rod of swivelling chute, the reciprocating screw rod other end is embedded in the heat dissipation incasement portion, the reciprocating screw rod outside is provided with the movable block, the movable block is embedded in inside the spout, spout one side is provided with radiator fan, radiator fan sets up in the inside both sides of unable adjustment base.
Through the fixed point heat dissipation mechanism who sets up, it is rotatory to drive rotatory flabellum through natural wind to make radiator fan dispel the heat to information processor, reduced the long-time high problem of service temperature of information processor, reduced the inside thermal production of equipment, promoted equipment radiating efficiency, guaranteed the practicality of device.
Preferably, the rotating rod is cylindrical, two ends of the rotating rod are embedded in the circle centers of two sides of the rotating groove, and the rotating rod is rotatably connected with the rotating groove.
Preferably, the outer portion of the reciprocating screw rod is in threaded arrangement, the moving block is a cuboid, a threaded groove is formed in the bottom end of the moving block, the reciprocating screw rod is in threaded rotation connection with the moving block, the moving block is embedded in the sliding groove, and the moving block is in sliding connection with the sliding groove.
Compared with the prior art, the utility model provides the comprehensive information processing equipment, which has the following beneficial effects:
1. this synthesize information processing equipment, damper through setting up, when needs the shock attenuation, the aircraft takes off when going up and down, can produce huge impact force, can make the inside information processor who sets up of unable adjustment base take place to rock, make information processor descend, make the shock attenuation upper plate promote the connecting rod and descend, make the connecting rod promote two sets of sliders I and slide in the shock attenuation bottom plate is inside, promote two sets of flexible pieces and slide in the fixed block is inside, further compression spring one, thereby the upper and lower impact force that information processor received has been reduced, when information processor received about the effort, can make information processor compression spring two that set up all around, thereby the impact force that information processor received has been slowed down, equipment has been prevented to suffer the striking and has been damaged, the practicality of device has been guaranteed.
2. This integrated information processing equipment, through the fixed point heat dissipation mechanism that sets up, when needing the heat dissipation, rotatory flabellum receives blowing of wind-force, it is rotatory to make rotatory flabellum drive the bull stick, it is rotatory to make the bull stick drive reciprocal lead screw, reciprocal lead screw is connected with movable block screw rotation, thereby make the movable block slide inside the spout, make the radiator fan that movable block one side set up dispel the heat to the information processor of the inside setting of unable adjustment base, thereby can realize fixed point radiating effect, the inside thermal production of unable adjustment base has been reduced simultaneously, the practicality of device has been guaranteed to the radiating efficiency.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic top perspective view of the present invention;
FIG. 3 is a schematic top view of the present invention;
FIG. 4 is a schematic view of a mobile heat dissipation device according to the present invention;
fig. 5 is a schematic view of a fixed-point heat dissipation three-dimensional structure according to the present invention.
Wherein: 1. a fixed base; 2. mounting grooves; 3. an information processor; 4. a heat dissipation box; 5. a damping bottom plate; 6. a first sliding block; 7. a telescopic block; 8. a fixed block; 9. a first spring; 10. a connecting rod; 11. a second sliding block; 12. a shock-absorbing upper plate; 13. a connecting plate; 14. a second spring; 15. a rotating tank; 16. a rotating rod; 17. rotating the fan blades; 18. a reciprocating screw rod; 19. a moving block; 20. a chute; 21. a heat dissipation fan.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the integrated information processing apparatus includes a fixing base 1, a mounting groove 2 is disposed inside the fixing base 1, an information processor 3 is disposed inside the mounting groove 2, heat dissipation boxes 4 are disposed on two sides of the fixing base 1, a damping mechanism is disposed inside the fixing base 1, and a fixed point heat dissipation mechanism is disposed inside the heat dissipation boxes 4.
Through the technical scheme, through the damper who sets up, can make the integrated information processing equipment take off when descending at the aircraft, reduce the impact force that equipment received, prevented that equipment atress striking from taking place to damage, influence the normal use of equipment, the practicality of device has been guaranteed, fixed point heat dissipation mechanism through setting up, it is rotatory to drive rotating fan blade 17 through natural wind, thereby make radiator fan 21 dispel the heat to information processor 3, the problem of information processor 3 long-time service temperature is too high has been reduced, the inside thermal production of equipment has been reduced, the equipment radiating efficiency has been promoted, the practicality of device has been guaranteed.
Concretely, damper includes the inside bottom fixed connection's of unable adjustment base 1 shock-absorbing bottom plate 5, the inside two sets of slider 6 that is provided with of shock-absorbing bottom plate 5, two sets of slider 6 are close to the flexible piece 7 of 5 mid points of shock-absorbing bottom plate one side fixedly connected with, two sets of flexible piece 7 are close to shock-absorbing bottom plate 5 one side and set up inside fixed block 8, fixed block 8 sets up inside shock-absorbing bottom plate 5, fixedly connected with spring 9 between two sets of flexible pieces 7, 6 outsides of two sets of slider are provided with connecting rod 10, two sets of connecting rod 10 tops set up in two 11 outsides of slider, two sets of slider 11 set up inside shock-absorbing upper plate 12, two sets of shock-absorbing upper plate 12 fixed connection in mounting groove 2 bottom, mounting groove 2 fixedly connected with connecting plate 13 all around, connecting plate 13 outside fixedly connected with spring two 14, spring two 14 other end fixed connection is in the inside lateral wall of unable adjustment base 1.
Through the technical scheme, when needs the shock attenuation, when the aircraft takes off and goes up and down, can produce huge impact force, can make the information processor 3 of the inside setting of unable adjustment base 1 take place to rock, make information processor 3 descend, make the shock attenuation upper plate 12 promote connecting rod 10 to descend, make connecting rod 10 promote two sets of sliders 6 and slide in damping bottom plate 5 is inside, promote two sets of flexible pieces 7 and slide in fixed block 8 is inside, further compression spring 9, thereby the upper and lower impact force that information processor 3 received has been reduced, when information processor 3 received about the effort, can make information processor 3 compress spring two 14 that set up all around, thereby the impact force that information processor 3 received has been slowed down, equipment has been prevented to suffer the striking and has been damaged, the practicality of device has been guaranteed.
Specifically, a first slider 6 is provided with two sets, a first 6 two sets of sliders are embedded inside the damping bottom plate 5 and are in sliding connection with the damping bottom plate 5, and a first 6 sliders are externally movably connected with the bottom end of the connecting rod 10 through bolts.
Through the technical scheme, the first sliding block 6 can slide in the damping bottom plate 5 through the arrangement, and the two groups of connecting rods 10 for pushing rotate, so that the impact force received by the information processor 3 is reduced, and the practicability of the device is guaranteed.
Specifically, the connecting rods 10 are arranged in two groups, the two groups of connecting rods 10 are symmetrically arranged, and the top ends of the two groups of connecting rods 10 are movably connected with the second sliding blocks 11 through bolts.
Specifically, fixed point heat dissipation mechanism includes the inside swivelling chute 15 of seting up of heat dissipation case 4, the inside bull stick 16 that is provided with of swivelling chute 15, the outside fixedly connected with multiunit rotating fan 17 of bull stick 16, 16 one end of bull stick extends to the outside fixedly connected with reciprocal lead screw 18 of swivelling chute 15, the reciprocal lead screw 18 other end is embedded inside heat dissipation case 4, reciprocal lead screw 18 outside is provided with movable block 19, movable block 19 is embedded inside spout 20, spout 20 one side is provided with radiator fan 21, radiator fan 21 sets up in the inside both sides of unable adjustment base 1.
Through the technical scheme, when the heat dissipation is needed, rotating fan 17 receives the blowing of wind power, make rotating fan 17 drive bull stick 16 rotatory, make bull stick 16 drive reciprocal lead screw 18 rotatory, reciprocal lead screw 18 and movable block 19 threaded connection, thereby make movable block 19 slide in spout 20 is inside, make radiator fan 21 that movable block 19 one side set up dispel the heat to the information processor 3 of the inside setting of unable adjustment base 1, thereby can realize the radiating effect of fixed point, the inside thermal production of unable adjustment base 1 has been reduced simultaneously, the practicality of device has been guaranteed to the radiating efficiency.
Specifically, the rotating rod 16 is cylindrical, two ends of the rotating rod 16 are embedded in the circle centers of two sides of the rotating groove 15, and the rotating rod 16 is rotatably connected with the rotating groove 15.
Specifically, the outside of the reciprocating screw rod 18 is provided with threads, the moving block 19 is a cuboid, a thread groove is formed in the bottom end of the moving block 19, the reciprocating screw rod 18 is in threaded rotation connection with the moving block 19, the moving block 19 is embedded in the sliding groove 20, and the moving block 19 is in sliding connection with the sliding groove 20.
When needs the shock attenuation, when the aircraft takes off and goes up and down, can produce huge impact force, can make the information processor 3 of the inside setting of unable adjustment base 1 take place to rock, make information processor 3 descend, make shock attenuation upper plate 12 promote connecting rod 10 to descend, make connecting rod 10 promote two sets of sliders 6 and slide in 5 insides of shock attenuation bottom plate, promote two sets of flexible pieces 7 and slide inside fixed block 8, further compression spring one 9, thereby the upper and lower impact force that information processor 3 received has been reduced, when information processor 3 received about the effort, can make information processor 3 compress spring two 14 that set up all around, thereby the impact force that information processor 3 received has been slowed down, the equipment has been prevented to suffer the striking and has been damaged, the practicality of device has been guaranteed.
When needing to dispel the heat, rotatory flabellum 17 receives blowing of wind-force, make rotatory flabellum 17 drive bull stick 16 rotatory, make bull stick 16 drive reciprocal lead screw 18 rotatory, reciprocal lead screw 18 and movable block 19 threaded connection, thereby make movable block 19 slide in spout 20 is inside, make radiator fan 21 that movable block 19 one side set up dispel the heat to the information processor 3 of the inside setting of unable adjustment base 1, thereby can realize the radiating effect of fixed point, the inside thermal production of unable adjustment base 1 has been reduced simultaneously, the practicality of device has been guaranteed to the radiating efficiency.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. Synthesize information processing apparatus, including unable adjustment base (1), its characterized in that: the fixing base is characterized in that a mounting groove (2) is formed in the fixing base (1), an information processor (3) is arranged in the mounting groove (2), heat dissipation boxes (4) are arranged on two sides of the fixing base (1), a damping mechanism is arranged in the fixing base (1), and a fixed-point heat dissipation mechanism is arranged in the heat dissipation boxes (4).
2. The integrated information processing apparatus according to claim 1, characterized in that: the damping mechanism comprises a damping bottom plate (5) fixedly connected with the bottom end inside a fixed base (1), two groups of first sliding blocks (6) are arranged inside the damping bottom plate (5), two groups of first sliding blocks (6) are fixedly connected with a telescopic block (7) on one side close to the midpoint of the damping bottom plate (5), two groups of telescopic blocks (7) are arranged inside a fixed block (8) on one side close to the damping bottom plate (5), the fixed block (8) is arranged inside the damping bottom plate (5), two groups of first telescopic blocks (7) are fixedly connected with a spring (9), two groups of first sliding blocks (6) are externally provided with connecting rods (10), the top ends of the two groups of connecting rods (10) are arranged outside second sliding blocks (11), two groups of second sliding blocks (11) are arranged inside a damping upper plate (12), and two groups of damping upper plates (12) are fixedly connected to the bottom of a mounting groove (2), the mounting groove (2) is fixedly connected with connecting plates (13) all around, the outside fixedly connected with spring two (14) of connecting plates (13), spring two (14) other end fixed connection is in unable adjustment base (1) inside lateral wall.
3. The integrated information processing apparatus according to claim 2, characterized in that: the first sliding blocks (6) are arranged in two groups, the first sliding blocks (6) are embedded inside the damping bottom plate (5) and are in sliding connection with the damping bottom plate (5), and the outer portions of the first sliding blocks (6) are movably connected with the bottom ends of the connecting rods (10) through bolts.
4. The integrated information processing apparatus according to claim 2, characterized in that: the connecting rods (10) are arranged in two groups, the connecting rods (10) are symmetrically arranged, and the top ends of the connecting rods (10) are movably connected with the second sliding blocks (11) through bolts.
5. The integrated information processing apparatus according to claim 1, characterized in that: fixed point heat dissipation mechanism includes inside swivelling chute (15) of seting up of heat dissipation case (4), swivelling chute (15) inside is provided with bull stick (16), bull stick (16) outside fixedly connected with multiunit rotating fan blade (17), bull stick (16) one end extends to the reciprocal lead screw (18) of swivelling chute (15) outside fixedly connected with, the reciprocal lead screw (18) other end is embedded inside heat dissipation case (4), reciprocal lead screw (18) outside is provided with movable block (19), movable block (19) are embedded inside spout (20), spout (20) one side is provided with radiator fan (21), radiator fan (21) set up in unable adjustment base (1) inside both sides.
6. The integrated information processing apparatus according to claim 5, wherein: the rotating rod (16) is cylindrical, the two ends of the rotating rod (16) are embedded in the circle centers of the two sides of the rotating groove (15), and the rotating rod (16) is rotatably connected with the rotating groove (15).
7. The integrated information processing apparatus according to claim 5, wherein: the external portion of the reciprocating screw rod (18) is in threaded arrangement, the moving block (19) is a cuboid, a threaded groove is formed in the bottom end of the moving block (19), the reciprocating screw rod (18) is in threaded rotation connection with the moving block (19), the moving block (19) is embedded in the sliding groove (20), and the moving block (19) is in sliding connection with the sliding groove (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121355003.9U CN216375032U (en) | 2021-06-17 | 2021-06-17 | Integrated information processing apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121355003.9U CN216375032U (en) | 2021-06-17 | 2021-06-17 | Integrated information processing apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216375032U true CN216375032U (en) | 2022-04-26 |
Family
ID=81217100
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121355003.9U Active CN216375032U (en) | 2021-06-17 | 2021-06-17 | Integrated information processing apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216375032U (en) |
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2021
- 2021-06-17 CN CN202121355003.9U patent/CN216375032U/en active Active
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