CN209351603U - A kind of unmanned plane battery fixing structure - Google Patents

Abstract

The utility model discloses a kind of unmanned plane battery fixing structures, including pedestal, the upper surface of the pedestal is equipped with rectangular recess, there are four support tubes for the bottom side array distribution of the rectangular recess, bottom side array distribution between four support tubes in rectangular recess has heat release hole, blower is equipped in the bottom side of rectangular recess above heat release hole, the inside of four support tubes is equipped with spring, the top of four springs is equipped with support column, the inner side of four support columns and four support tubes is slidably connected, the top of four support columns is equipped with battery and places block, the upper surface that the battery places block is from left to right successively arranged U-shaped lower platen, battery placing groove and L-type through slot, the unmanned plane battery fixing structure, structure is simple and firm, it can fly, buffer function is played in damping during transport etc., battery is avoided to loosen, together When, it can cool down to battery, prevent battery temperature excessively high, not influence the service life of battery.

Description

A kind of unmanned plane battery fixing structure

Technical field

The utility model relates to battery fixing structure technical field, specially a kind of unmanned plane battery fixing structure.

Background technique

UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft, unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target Machine, civilian aspect, unmanned plane are taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, are observing wild move The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making etc. field, is greatly expanded The purposes of unmanned plane itself, unmanned plane mainly include the offer electric power such as fuel cell, solar battery, lithium battery, therefore at it It needs to carry battery on fuselage, unmanned plane there is no unified battery mount scheme at present, all be unmanned plane manufacturer according to certainly Body design installation, and or structure is complicated, lead to install that trouble is inconvenient or structure is too simple, it is fixed built on the sand, lead Pond is sent a telegraph to loosen during flight, transport etc., meanwhile, battery long-time output power flies, and battery itself is certainly Strip resistance is also easy to produce heat, influences the service life of battery.

Utility model content

The technical problems to be solved in the utility model is to overcome existing defect, provides a kind of unmanned machine battery fixed knot Structure, structure is simple and firm, damping can play buffer function during flight, transport etc., battery is avoided to loosen, meanwhile, It can cool down to battery, prevent battery temperature excessively high, not influence the service life of battery, can effectively solve background technique The problems in.

To achieve the above object, the utility model provides the following technical solutions: a kind of unmanned plane battery fixing structure, including Pedestal, the upper surface of the pedestal are equipped with rectangular recess, and there are four support tubes for the bottom side array distribution of the rectangular recess, are located at Bottom side array distribution between four support tubes in rectangular recess has heat release hole, in the bottom side of rectangular recess above heat release hole Equipped with blower, the inside of four support tubes is equipped with spring, and the top of four springs is equipped with support column, four support columns and four The inner side of a support tube is slidably connected, and the top of four support columns is equipped with battery and places block, and the battery places block Upper surface is from left to right successively arranged U-shaped lower platen, battery placing groove and L-type through slot, and the right side bottom side of the U-shaped lower platen is set There is triangular form fixture block, and the right end of U-shaped lower platen and triangular form fixture block and L-type through slot are clamped, the rear side of the battery placing groove Equipped with elastic plate, the front side of the battery placing groove is equipped with electrode connecting hole, and the bottom side of battery placing groove is equipped with rectangular straight slot.

As a kind of optimal technical scheme of the utility model, the side top of the rectangular recess is equipped with baffle, described Baffle is corresponding with convex block, and the convex block is located at the side bottom side that battery places block.

As a kind of optimal technical scheme of the utility model, the bottom side of the pedestal sets that there are four installations by threaded hole Column, four mounting post array distributions are in the bottom side of pedestal.

As a kind of optimal technical scheme of the utility model, the inner top side of the U-shaped lower platen is bonded by viscose glue There is rubber thermal grease.

As a kind of optimal technical scheme of the utility model, the bottom side of the spring is socketed with positioning column, and positioning column Bottom end and rectangular recess bottom side connect.

Compared with prior art, the utility model has the beneficial effects that this unmanned plane battery fixing structure, elastic plate is pushed Battery makes extremely being connected to inside electrode connecting hole for battery, and is fixed by U-shaped lower platen, and structure is simple and firm, In flight, transportational process, support column squeezes spring, damping can play buffer function during flight, transport etc., avoid electricity Pond loosens, and opens blower, can accelerate internal gas flow communication, cool down to battery, prevent battery temperature excessively high, do not influence electricity The service life in pond.

Detailed description of the invention

FIG. 1 is a schematic structural view of the utility model；

Fig. 2 is that the utility model structure faces schematic cross-sectional view；

Fig. 3 is the utility model structure backsight schematic cross-sectional view.

In figure: 1 pedestal, 2 mounting posts, 3 U-shaped lower platens, 4 rectangular straight slot, 5 battery placing grooves, 6 batteries place block, 7 gears Plate, 8 convex blocks, 9 support columns, 10 support tubes, 11 heat release holes, 12 rectangular recess, 13 blowers, 14 triangular form fixture blocks, 15 L-type through slots, 16 elastic plates, 17 rubber thermal greases, 18 electrode connecting holes, 19 springs, 20 positioning columns.

Specific embodiment

The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.

Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of unmanned plane battery fixing structure, including bottom Seat 1, the bottom side of pedestal 1 by threaded hole set there are four mounting post 2, four 2 array distributions of mounting post are in the bottom side of pedestal 1, just It is fixed in the installation of the structure, the upper surface of pedestal 1 is equipped with rectangular recess 12, and the side top of rectangular recess 12 is equipped with baffle 7, Baffle 7 is corresponding with convex block 8, and convex block 8 is located at the side bottom side that battery places block 6, prevents battery from placing block 6 de- from rectangular recess 12 It falls, there are four support tubes 10 for the bottom side array distribution of rectangular recess 12, in rectangular recess 12 between four support tubes 10 Bottom side array distribution has heat release hole 11, is equipped with blower 13, four supports in the bottom side of rectangular recess 12 above heat release hole 11 The inside of cylinder 10 is equipped with spring 19, and the top of four springs 19 is equipped with support column 9, and the bottom side of spring 19 is socketed with positioning column 20, and the bottom end of positioning column 20 is connect with the bottom side of rectangular recess 12, can be positioned to spring 19, be prevented to deviate Damping effect is influenced, the inner side of four support columns 9 and four support tubes 10 is slidably connected, the top of four support columns 9 Block 6 is placed equipped with battery, battery places block 6 and support column 9 is pushed to squeeze spring 19, can the damping during flight, transport etc. Buffer function is played, battery is avoided to loosen, the upper surface that battery places block 6 is from left to right successively arranged U-shaped lower platen 3, battery The inner top side of placing groove 5 and L-type through slot 15, U-shaped lower platen 3 is bonded with rubber thermal grease 17 by viscose glue, and battery is avoided to produce Raw heat transfer gives U-shaped lower platen 3, does not influence U-shaped lower platen 3 and pushes fixed effect, the right side of U-shaped lower platen 3 to battery Side bottom side is equipped with triangular form fixture block 14, and the right end of U-shaped lower platen 3 and triangular form fixture block 14 and L-type through slot 15 are clamped, can be right U-shaped lower platen 3 is clamped, and U-shaped lower platen 3 pushes battery, and battery is fixed, and structure is simple and firm, and battery is put The rear side for setting slot 5 is equipped with elastic plate 16, and the front side of battery placing groove 5 is equipped with electrode connecting hole 18, and the bottom side of battery placing groove 5 is set There is rectangular straight slot 4, open blower 13, internal gas flow communication can be accelerated, the heat that battery generates passes through rectangular straight slot 4 and heat dissipation Outside is discharged in hole 11, cools down to battery, prevents battery temperature excessively high, does not influence the service life of battery.

When in use: battery being put into inside battery placing groove 5, the extreme card of battery is made by the promotion battery of elastic plate 16 It connecing inside electrode connecting hole 18, and is fixed by U-shaped lower platen 3, structure is simple and firm, in flight, transportational process, Support column 9 squeezes spring 19, damping can play buffer function during flight, transport etc., avoid battery from loosening, open wind Machine 13 can accelerate internal gas flow communication, cool down to battery, prevent battery temperature excessively high, and do not influence battery uses the longevity Life.

The utility model structure is simple and firm, damping can play buffer function during flight, transport etc., avoid Battery loosens, meanwhile, it can cool down to battery, prevent battery temperature excessively high, not influence the service life of battery.

While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art, It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.

Claims (5)

1. a kind of unmanned plane battery fixing structure, including pedestal (1), it is characterised in that: the upper surface of the pedestal (1) is equipped with square Connected in star (12), there are four support tube (10) for the bottom side array distribution of the rectangular recess (12), are located at four support tubes (10) Between in the bottom side array distribution of rectangular recess (12) have heat release hole (11), be located above heat release hole (11) in rectangular recess (12) Bottom side be equipped with blower (13), the inside of four support tubes (10) is equipped with spring (19), and the top of four springs (19) is all provided with Have support column (9), the inner side of four support columns (9) and four support tubes (10) is slidably connected, four support columns (9) Top is equipped with battery and places block (6), the upper surface that the battery places block (6) be from left to right successively arranged U-shaped lower platen (3), The right side bottom side of battery placing groove (5) and L-type through slot (15), the U-shaped lower platen (3) is equipped with triangular form fixture block (14), and U-shaped The right end and triangular form fixture block (14) of lower platen (3) and L-type through slot (15) are clamped, and the rear side of the battery placing groove (5) is equipped with The front side of elastic plate (16), the battery placing groove (5) is equipped with electrode connecting hole (18), and the bottom side of battery placing groove (5) is equipped with Rectangular straight slot (4).

2. a kind of unmanned plane battery fixing structure according to claim 1, it is characterised in that: the rectangular recess (12) Side top is equipped with baffle (7), and the baffle (7) is corresponding with convex block (8), and the convex block (8) is located at the side that battery places block (6) Face bottom side.

3. a kind of unmanned plane battery fixing structure according to claim 1, it is characterised in that: the bottom side of the pedestal (1) It is set by threaded hole there are four mounting post (2), bottom side of four mounting post (2) array distributions in pedestal (1).

4. a kind of unmanned plane battery fixing structure according to claim 1, it is characterised in that: the U-shaped lower platen (3) Inner top side is bonded with rubber thermal grease (17) by viscose glue.

5. a kind of unmanned plane battery fixing structure according to claim 1, it is characterised in that: the bottom side of the spring (19) It is socketed with positioning column (20), and the bottom end of positioning column (20) is connect with the bottom side of rectangular recess (12).