CN208242065U - A kind of protective device of integrated-optic device - Google Patents

Abstract

The utility model discloses a kind of protective devices of integrated-optic device, its structure includes fuselage, display, indicator light, radiator, top cover, motor, derailing switch, operator, baffle, the fuselage front surface and display rear surface are using fitting connection, the fuselage front surface is equipped with derailing switch and first disposes a radiator on equipment left side, then when equipment is run, cooperate rotary shaft and seven flabellums by the blower in radiator, quick 360 ° are carried out together forward to rotate, generate wind-force, cold wind is blowed to equipment inside, the temperature inside equipment is allowed to be able to maintain under a normal temperature, to prevent equipment, internal temperature is stepped up and generates damage to inner body and circuit after longtime running, effectively ensure that equipment can be run for a long time, it is set to extend the service life of equipment with improving Standby working efficiency.

Description

A kind of protective device of integrated-optic device

Technical field

The utility model is a kind of protective device of integrated-optic device, belongs to circuit arrangement field.

Background technique

Electronic device refers in vacuum, gas or solid, utilization and control electron motion rule and manufactured device, point For electron tube, inflation tube device and solid electronic device.

Prior art discloses application No. is a kind of protective device of integrated-optic device of: 201720594374.X, packets Bottom plate is included, plate upper surface is equipped with annular protrusion, and the inside of annular protrusion forms cavity, and bottom plate was provided with bolt hole, ring along one week The upper surface of shape protrusion is equipped with groove, and gasket is embedded in groove, and gasket a part stretches out groove, spiral-lock on annular protrusion There is sealing cover, sealing cover lower surface is equipped with the seal convexity to fit with annular protrusion, and the outer surface of seal convexity was along one week It is equipped with seal groove equipped with seal rubber sleeve, sealing cover lower surface and positioned at gasket corresponding section, sealing cover center is provided with out Air port, the output end of motor are equipped with air draft flabellum, and sealing cover side surface is tangentially equipped with blast pipe, air inlet wind is equipped in blast pipe Machine.The utility model has the beneficial effects that will can directly be integrated in many electronic circuit plates installed, it can be achieved that It is aeration-cooling, and can carry out dust-proof.But disadvantage is that equipment it is scattered hot property it is poor, can be easy to often result in Inner body circuit is burned and causes equipment that can not be run.

Utility model content

In view of the deficienciess of the prior art, the utility model aim is to provide a kind of protection dress of integrated-optic device Set, it is poor to solve the scattered hot property of above equipment, can be easy to often result in inner body circuit be burned and cause equipment without The problem of method is run.

To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of integrated electronic device The protective device of part, structure include fuselage, display, indicator light, radiator, top cover, motor, derailing switch, operator, gear Using being fitting to connection, the fuselage both ends are separately connected two block baffles, described for plate, the fuselage front surface and display rear surface Fuselage front surface is equipped with derailing switch, seven round indicator lights is fixedly connected in the fuselage front surface, and hang down in same plane Straight equidistant arrangement, with operator using being flexibly connected in the fuselage front surface, the fuselage interior is equipped with motor, the fuselage Radiator is fixedly connected on left side, cap base section is welded in the fuselage roof section；The radiator is by radiator master Body, flabellum, nut, rotary shaft, blower, support frame, connector, rear cover composition, the round nut is by threads turn to scattered In hot device main body, the radiator body connects rear cover by connector, and the connector bottom center welding bracing frame is described Support frame bottom and rotary shaft rear surface are using being fitting to connection, and the rotary shaft is used with blower and is flexibly connected, outside the blower Ring is fixedly connected with seven flabellums, and flabellum is arranged in a ring.

Further, the motor connects display by fuselage.

Further, the derailing switch passes through fuselage attended operation device.

Further, the motor connects radiator by fuselage.

Further, top cover is equipped with above the display.

Further, the round indicator light is equipped with seven and equilateral in the same size altogether.

Further, the radiator has heat sinking function.

Beneficial effect

A kind of protective device of integrated-optic device of the utility model is equipped with radiator, first disposes on equipment left side One radiator cooperates rotary shaft and seven flabellums by blower in radiator then when equipment is run, together into Quick 360 ° of row forward rotates, and generates wind-force, blows cold wind to equipment inside, the temperature inside equipment is allowed to be able to maintain at one Under normal temperature, to prevent equipment, internal temperature is stepped up and generates damage to inner body and circuit after longtime running, effectively Ensure that equipment can be run for a long time, the service life of equipment and improve the working efficiency of equipment to extend.

Detailed description of the invention

Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model Sign, objects and advantages will become more apparent upon:

Fig. 1 is a kind of structural schematic diagram of the protective device of integrated-optic device of the utility model；

Fig. 2 is the heat spreader structures schematic diagram of the utility model.

In figure: fuselage -1, display -2, indicator light -3, radiator -4, radiator body -401, flabellum -402, nut - 403, rotary shaft -404, blower -405, support frame -406, connector -407, rear cover -408, top cover -5, motor -6, derailing switch - 7, operator -8, baffle -9.

Specific embodiment

To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below In conjunction with specific embodiment, the utility model is further described.

Fig. 1-Fig. 2 is please referred to, the utility model provides a kind of technical solution: a kind of protective device of integrated-optic device, Its structure includes fuselage 1, display 2, indicator light 3, radiator 4, top cover 5, motor 6, derailing switch 7, operator 8, baffle 9, institute 1 front surface of fuselage and 2 rear surface of display are stated using being fitting to connection, 1 both ends of fuselage are separately connected two block baffles 9, described 1 front surface of fuselage is equipped with derailing switch 7, seven round indicator lights 3 is fixedly connected in 1 front surface of fuselage, and in same flat The vertical equidistant arrangement in face, with operator 8 using being flexibly connected in 1 front surface of fuselage, equipped with motor inside the fuselage 1 6, radiator 4 is fixedly connected on 1 left side of fuselage, 1 top cross-section of fuselage welds 5 bottom section of top cover；It is described to dissipate Hot device 4 by radiator body 401, flabellum 402, nut 403, rotary shaft 404, blower 405, support frame 406, connector 407, after Lid 408 forms, and the round nut 403 is by the way that in threads turn to radiator body 401, the radiator body 401 passes through Connector 407 connects rear cover 408, the 407 bottom center welding bracing frame 406 of connector, 406 bottom of support frame as described above and rotation 404 rear surface of shaft is using being fitting to connection, and the rotary shaft 404 is used with blower 405 and is flexibly connected, 405 outer ring of blower Seven flabellums 402 are fixedly connected with, and flabellum 402 is arranged in a ring.

Flabellum 402 described in this patent cooperates blower 405 to have heat sinking function, and the rotary shaft 404 has 360 ° of rotations Function.

It is carrying out in use, connecting radiator 4, first one radiator of placement on equipment left side using fuselage 1 first 1, then when equipment is run, rotary shaft and seven flabellums 402 are cooperated by the blower 105 in radiator 1, carried out together Quick 360 ° forward rotate, and generate wind-force, blow cold wind to equipment inside, the temperature inside equipment is allowed to be able to maintain at one just Under normal temperature, to prevent equipment, internal temperature is stepped up and generates damage to inner body and circuit after longtime running, effectively Ensure that equipment can be run for a long time, to extend the service life of equipment and improve the working efficiency of equipment.

The utility model solves the problems, such as that the scattered hot property of the problem of being to be solved equipment is poor, can be easy to often result in interior Portion's part circuit is burned and causes equipment that can not be run, and the utility model is combined with each other by above-mentioned component, is equipped with Radiator first disposes a radiator to pass through the blower in radiator then when equipment is run on equipment left side Cooperate rotary shaft and seven flabellums, carry out quick 360 ° together and forward rotate, generates wind-force, cold wind is blowed to equipment inside, The temperature inside equipment is allowed to be able to maintain under a normal temperature, internal temperature is stepped up pair after longtime running to prevent equipment Inner body and circuit generate damage, effectively ensure that equipment can be run for a long time, to extend the use of equipment Service life and the working efficiency for improving equipment.It is described in detail below:

The round nut 403 is by the way that in threads turn to radiator body 401, the radiator body 401 passes through company Fitting 407 connects rear cover 408, the 407 bottom center welding bracing frame 406 of connector, 406 bottom of support frame as described above and rotation 404 rear surface of axis is using being fitting to connection, and for the rotary shaft 404 with blower 405 using being flexibly connected, 405 outer ring of blower is solid Surely seven flabellums 402 are connected, and flabellum 402 is arranged in a ring.

The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims All changes are embraced therein.It should not treat any reference in the claims as limiting related right It is required that.

In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiments being understood that.

Claims (6)

1. a kind of protective device of integrated-optic device, structure includes fuselage (1), display (2), indicator light (3), radiator (4), top cover (5), motor (6), derailing switch (7), operator (8), baffle (9), fuselage (1) front surface and display (2) Rear surface is using being fitting to connection, and fuselage (1) both ends are separately connected two block baffles (9), and fuselage (1) front surface is equipped with Derailing switch (7), it is characterised in that:

It is fixedly connected with seven round indicator lights (3) in fuselage (1) front surface, and is in the vertical equidistant arrangement of same plane, institute It states in fuselage (1) front surface with operator (8) using being flexibly connected, is equipped with motor (6) inside the fuselage (1), the fuselage (1) it is fixedly connected on left side radiator (4), fuselage (1) top cross-section welds top cover (5) bottom section；

The radiator (4) by radiator body (401), flabellum (402), nut (403), rotary shaft (404), blower (405), Support frame (406), connector (407), rear cover (408) composition, the round nut (403) pass through threads turn to radiator master In body (401), the radiator body (401) passes through connector (407) connection rear cover (408), connector (407) bottom Center weldment support frame (406), support frame as described above (406) bottom and rotary shaft (404) rear surface are using fitting connection, the rotation For shaft (404) with blower (405) using being flexibly connected, blower (405) outer ring is fixedly connected with seven flabellums (402), and fans Leaf (402) is arranged in a ring.

2. a kind of protective device of integrated-optic device according to claim 1, it is characterised in that: the motor (6) is logical Cross fuselage (1) connection display (2).

3. a kind of protective device of integrated-optic device according to claim 1, it is characterised in that: the derailing switch (7) Pass through fuselage (1) attended operation device (8).

4. a kind of protective device of integrated-optic device according to claim 1, it is characterised in that: the motor (6) is logical Cross fuselage (1) connection radiator (4).

5. a kind of protective device of integrated-optic device according to claim 1, it is characterised in that: the display (2) Top is equipped with top cover (5).

6. a kind of protective device of integrated-optic device according to claim 1, it is characterised in that: the circle indicator light (3) altogether equipped with seven and equilateral in the same size.