CN210983303U - Military reinforced computer - Google Patents

Military reinforced computer Download PDF

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Publication number
CN210983303U
CN210983303U CN202020021764.XU CN202020021764U CN210983303U CN 210983303 U CN210983303 U CN 210983303U CN 202020021764 U CN202020021764 U CN 202020021764U CN 210983303 U CN210983303 U CN 210983303U
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heat
heat dissipation
block
groove
computer
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CN202020021764.XU
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Chinese (zh)
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杨文杰
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Xi'an Huayu Aviation Technology Co ltd
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Xi'an Huayu Aviation Technology Co ltd
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Abstract

The utility model discloses a for military use ruggedized computer, including display screen, computer housing, heat dissipation installation piece, mounting groove, the upper end of computer housing is connected with the display screen through the pivot, and the lower extreme of computer housing has seted up the mounting groove, the heat dissipation installation piece is installed to the mounting groove notch, and the upper end of heat dissipation installation piece is provided with heat radiation structure, heat radiation structure is connected with the part that generates heat in the computer housing, heat radiation structure includes aluminium base of heat dissipation, heat conduction piece, draw-in groove, filter screen, card frame, heat conduction piece, heat insulating mattress, depressed groove. For military use reinforcement computer, heat dissipation aluminium base piece, heat conduction piece, the conducting strip that heat radiation structure set up mutually support, realize the heat dissipation of the inside part that generates heat of computer casing, reduce the whole power consumption of computer to a certain extent, the heat dissipation aluminium base piece, the heat conduction piece's that heat dissipation installation piece and heat radiation structure set up design can realize the heat dissipation of heat dissipation installation piece department.

Description

Military reinforced computer
Technical Field
The utility model relates to a computer field, in particular to for military use ruggedized computer.
Background
The computer is commonly called computer, and is a modern electronic computing machine for high-speed computation, which can perform numerical computation, logic computation and memory function. The PCI bus specification of the PCI SIG is used in an industrial control Computer system (1995, 11.8. the PCI bus Manufacturer's Association (PICMG) issues a CPCI specification of 1.0 edition, and then the PCI-PCI Bridge specification, the Computer Telephony TDM specification and a User-defined finished I/O pin specification are successively introduced;
Patent number is 201721054765.9's patent discloses an open-air military notebook of CPCI type, including host computer casing 1 and display 2, host computer casing 1 links to each other with display 2, host computer casing 1 is equipped with recess 3, be equipped with a fan 4 in the recess 3, 4 one side of fan is equipped with a heat radiation fins 5, the 3 lower extreme of recess is equipped with a cover plate 6, be equipped with the first ventilation hole 7 of a plurality of and a plurality of second ventilation hole 8 on the cover plate 6, the first ventilation hole 7 of a plurality of is located fan 4 below, a plurality of second ventilation hole 8 is located 5 one side of heat radiation fins and is located the another side of cover plate 6. Most of the existing field military notebooks adopt a CPCI type bus interface standard, and the CPCI type bus interface standard has Hot plug (Hot Swap), high openness and high reliability, and also needs the notebooks to have good heat dissipation performance. Referring to fig. 1 and 2, and the arrows on fig. 2 are pointed to that, when the fan is activated, the heat in the main housing 1 can be quickly dissipated due to the convection of air.
The above patent documents have some problems: because the fan and the radiating fins are matched for radiating, the fan consumes serious energy, and the cover plate is generally easy to block with a contact object.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides for military use reinforcement computer, can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
For military use ruggedized computer, including display screen, computer housing, heat dissipation installation piece, mounting groove, the upper end of computer housing is connected with the display screen through the pivot, and the lower extreme of computer housing has seted up the mounting groove, the heat dissipation installation piece is installed to the mounting groove notch, and the upper end of heat dissipation installation piece is provided with heat radiation structure, heat radiation structure is connected with the part that generates heat in the computer housing.
Preferably, the heat radiation structure includes heat dissipation aluminum substrate, heat conduction piece, draw-in groove, filter screen, card frame, conducting strip, heat insulating mattress, depressed groove, and the lateral wall of heat dissipation aluminum substrate is provided with the heat conduction piece, the draw-in groove has been seted up to the lateral wall of heat conduction piece, and the draw-in groove inslot is provided with the card frame, be provided with the filter screen in the frame of card frame, the upper end of heat conduction piece is connected with the heat conduction piece, and the upper end cover of heat conduction piece has the heat insulating mattress, the depressed groove has been seted up to the lower extreme of heat insulating mattress, and the heat insulating mattress lower extreme contacts with heat dissipation.
Preferably, the heat dissipation mounting block is matched with the heat dissipation aluminum base block and the heat conduction block arranged in the heat dissipation structure.
Preferably, the lower end of the heat dissipation mounting block is provided with a heat dissipation small hole and a through groove, the through groove formed in the heat dissipation mounting block is internally provided with a heat dissipation aluminum substrate, the heat dissipation small hole formed in the heat dissipation mounting block is provided with a heat conduction block, and the clamping groove is matched with the clamping frame.
Preferably, the conducting strip is located the depressed trench that the heat insulating mattress seted up, and the screw hole that the conducting strip was seted up and the screwed hole that the conducting block upper end was seted up set up in alignment, the coating has the heat-conducting glue between conducting strip and heat dissipation aluminum substrate, the conducting block.
Compared with the prior art, the utility model discloses following beneficial effect has:
The utility model discloses in, heat dissipation aluminum base piece, heat conduction piece, the conducting strip that heat radiation structure set up mutually support, realize the heat dissipation of the inside part that generates heat of computer casing, reduce the whole power consumption of computer to a certain extent, and the heat dissipation aluminum base piece, the heat conduction piece's that heat dissipation installation piece and heat radiation structure set up design can realize the heat dissipation of heat dissipation installation piece department.
Drawings
FIG. 1 is a schematic view of the overall structure of the military ruggedized computer of the present invention;
FIG. 2 is a schematic view of the military ruggedized computer of the present invention, shown disassembled in its overall configuration;
FIG. 3 is a schematic view of the military computer with a detachable heat dissipation structure;
Fig. 4 is the heat conduction block schematic diagram of the military reinforcement computer of the utility model.
In the figure: 1. a display screen; 2. a computer housing; 3. a heat dissipation structure; 301. a heat-dissipating aluminum substrate; 302. a heat conducting block; 303. a card slot; 304. a filter screen; 305. clamping a frame; 306. a heat conductive sheet; 307. a heat insulating pad; 308. A recessed groove; 4. a heat dissipation mounting block; 5. and (4) mounting the groove.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1-4, the military reinforced computer comprises a display screen 1, a computer case 2, a heat dissipation mounting block 4 and a mounting groove 5, wherein the upper end of the computer case 2 is connected with the display screen 1 through a rotating shaft, the lower end of the computer case 2 is provided with the mounting groove 5, the heat dissipation mounting block 4 is mounted at the notch of the mounting groove 5, the upper end of the heat dissipation mounting block 4 is provided with a heat dissipation structure 3, and the heat dissipation structure 3 is connected with a heating component in the computer case 2.
The heat dissipation structure 3 includes a heat dissipation aluminum substrate 301, a heat conduction block 302, a clamping groove 303, a filter screen 304, a clamping frame 305, a heat conduction sheet 306, a heat insulation pad 307, and a recessed groove 308, wherein the heat conduction block 302 is disposed on a side wall of the heat dissipation aluminum substrate 301, the clamping groove 303 is disposed on a side wall of the heat conduction block 302, the clamping frame 305 is disposed in the clamping groove 303, the filter screen 304 is disposed in a frame of the clamping frame 305, the heat conduction sheet 306 is connected to an upper end of the heat conduction block 302, the heat insulation pad 307 covers an upper end of the heat conduction sheet 306, the recessed groove 308 is disposed at a lower end of the heat insulation pad 307, and a lower end of the heat insulation pad 307; the heat dissipation aluminum substrate 301, the heat conduction block 302 and the heat conduction sheet 306 of the heat dissipation structure 3 are mutually matched to realize the heat dissipation of the heating component inside the computer case 2, thereby reducing the overall energy consumption of the computer to a certain extent.
Wherein, the heat dissipation mounting block 4 is matched with the heat dissipation aluminum base 301 and the heat conduction block 302 arranged on the heat dissipation structure 3; the heat dissipation mounting block 4 and the heat dissipation aluminum base 301 and the heat conduction block 302 arranged on the heat dissipation structure 3 can realize heat dissipation at the heat dissipation mounting block 4.
The lower end of the heat dissipation mounting block 4 is provided with a small heat dissipation hole and a through groove, the through groove formed in the heat dissipation mounting block 4 is provided with a heat dissipation aluminum substrate 301, the small heat dissipation hole formed in the heat dissipation mounting block 4 is provided with a heat conduction block 302, and the clamping groove 303 is matched with the clamping frame 305.
The heat conducting plate 306 is located in a groove 308 formed in the heat insulating pad 307, a threaded hole formed in the heat conducting plate 306 is aligned with a threaded hole formed in the upper end of the heat conducting block 302, and heat conducting glue is coated between the heat conducting plate 306 and the heat dissipating aluminum substrate 301 and between the heat conducting block 302.
It should be noted that, when assembling the computer case 2, the heat dissipation structure 3, and the heat dissipation mounting block 4, the present invention is a military computer, wherein the lower end of the heat dissipation aluminum base 301 of the heat dissipation structure 3 is inserted into the through groove formed at the upper end of the heat dissipation mounting block 4, the protruding strip of the sidewall of the heat dissipation aluminum base 301 is located at the upper end surface of the heat dissipation mounting block 4, the heat-resistant adhesive is used to fixedly connect the heat dissipation aluminum base 301 and the heat dissipation mounting block 4, the filter screen 304 is placed in the frame of the clamping frame 305, the filter screen 304 is fixedly connected with the clamping frame 305, the clamping frame 305 is aligned with the clamping groove 303 formed at the sidewall of the heat conduction block 302, the clamping frame 305 is pushed into the groove 303, thereby realizing the movable arrangement between the filter screen 304 and the heat conduction block 302, the lower end of the heat conduction block 302 contacts the upper end of the heat dissipation mounting block 4, the, one end of the heat conducting block 302 contacts with the heat radiating aluminum base 301, the contact end between the heat conducting block 302 and the heat radiating aluminum base 301 is coated with heat conducting glue, the side wall of the heat conducting block 302 contacts with the upper end of the heat radiating installation block 4, heat-resisting glue is coated between the heat conducting block 302 and the heat radiating installation block 4, the heat conducting block 302 and the heat radiating installation block 4 are fixedly installed, because the filter screen 304 and the clamping frame 305 can be pulled out from the groove 303 of the clamping groove, the end surface of the heat conducting block 302, which is provided with the clamping groove 303, is not tightly attached to the heat radiating aluminum base 301, the filter screen 304 is convenient to take out for replacement and cleaning, the lower end of the heat conducting sheet 306 is coated with heat conducting glue, the screw hole formed in the heat conducting sheet 306 aligns with the screw hole formed in the upper end surface of the heat conducting block 302, the upper end of the heat conducting block 302 contacts, the edge of the lower end of the heat insulation pad 307 is coated with heat-resistant colloid, the lower end of the heat insulation pad 307 is tightly attached to the upper ends of the heat dissipation aluminum base block 301 and the heat conduction block 302, the concave groove 308 formed in the heat insulation pad 307 is matched with the heat conduction sheet 306, the heat insulation pad 307, the heat dissipation aluminum base block 301 and the heat conduction block 302 are installed, the heat dissipation installation block 4 and the heat dissipation structure 3 are placed into the groove of the installation groove 5, bolts are inserted into threaded holes formed in the four corners of the heat dissipation installation block 4, the heat dissipation installation block 4 is connected with the computer case 2, when the heat dissipation installation block 4 is connected, the heat conduction sheet 306 is connected with a heating part inside the computer case 2, and the notebook can be fully reinforced by expanding 3UCPCI slots inside the computer case 2.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (4)

1. For military use reinforcement computer, its characterized in that: comprises a display screen (1), a computer case (2), a heat dissipation installation block (4) and a mounting groove (5), wherein the upper end of the computer case (2) is connected with the display screen (1) through a rotating shaft, the lower end of the computer case (2) is provided with the mounting groove (5), the notch of the mounting groove (5) is provided with the heat dissipation installation block (4), the upper end of the heat dissipation installation block (4) is provided with a heat dissipation structure (3), the heat dissipation structure (3) is connected with a heating component in the computer case (2), the heat dissipation structure (3) comprises a heat dissipation aluminum block (301), a heat conduction block (302), a clamping groove (303), a filter screen (304), a clamping frame (305), a heat conduction sheet (306), a heat insulation pad (307) and a concave groove (308), the side wall of the heat dissipation aluminum block (301) is provided with the heat conduction block (302), the side wall of the heat, and draw-in groove (303) inslot is provided with card frame (305), be provided with filter screen (304) in the frame of card frame (305), the upper end of heat conduction piece (302) is connected with conducting strip (306), and the upper end of conducting strip (306) covers has heat insulating mattress (307), depressed groove (308) have been seted up to the lower extreme of heat insulating mattress (307), and heat insulating mattress (307) lower extreme and heat dissipation aluminum substrate (301) and heat conduction piece (302) up end contact.
2. The military reinforcement computer of claim 1, wherein: the heat dissipation mounting block (4) is matched with a heat dissipation aluminum base block (301) and a heat conduction block (302) which are arranged on the heat dissipation structure (3).
3. The military reinforcement computer of claim 2, wherein: the lower extreme of heat dissipation installation piece (4) has been seted up heat dissipation aperture and has been led to the groove, and the logical inslot that heat dissipation installation piece (4) were seted up is provided with heat dissipation aluminum substrate (301), the heat dissipation aperture department that heat dissipation installation piece (4) were seted up is provided with heat conduction piece (302), draw-in groove (303) and card frame (305) match the setting.
4. The military reinforcement computer of claim 3, wherein: the heat conducting sheet (306) is positioned in a groove of a concave groove (308) formed in a heat insulation pad (307), a threaded hole formed in the heat conducting sheet (306) is aligned with a threaded hole formed in the upper end of the heat conducting block (302), and heat conducting glue is coated between the heat conducting sheet (306) and the heat dissipation aluminum base block (301) and between the heat conducting block (302).
CN202020021764.XU 2020-01-07 2020-01-07 Military reinforced computer Active CN210983303U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020021764.XU CN210983303U (en) 2020-01-07 2020-01-07 Military reinforced computer

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Application Number Priority Date Filing Date Title
CN202020021764.XU CN210983303U (en) 2020-01-07 2020-01-07 Military reinforced computer

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CN210983303U true CN210983303U (en) 2020-07-10

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112629866A (en) * 2020-12-22 2021-04-09 中国人民解放军海军航空大学青岛校区 Aeroengine detector

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112629866A (en) * 2020-12-22 2021-04-09 中国人民解放军海军航空大学青岛校区 Aeroengine detector

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