CN209305832U - A kind of integrated stand of integrated installation fire-fighting unmanned plane functional module - Google Patents

Abstract

The utility model relates to unmanned plane fields, specifically, a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module, it is arranged on the fuselage bottom of unmanned plane or two groups of stabilizer blades of unmanned plane, the functional module includes fire monitor cylinder, aims at quiet, holder camera, night vision camera, avoidance component, the integrated stand includes being arranged on fuselage, for fixing the fire monitor bracket of fire-fighting gun barrel, quiet and night vision camera sighting telescope support is aimed at for fixed, for fixing the holder bracket of holder camera, for fixing the avoidance bracket of avoidance component；In the utility model, the bracket for installation function module is integrally disposed in first support and/or second support, and reasonable gravity distribution reduces the use of supporting structure；Functional module is installed around fire-fighting gun barrel radioactivity, keeps functional module structure compact, reduces space required for underbelly, is conducive to unmanned plane and is reduced external dimensions, to mitigate the self weight of unmanned plane.

Description

A kind of integrated stand of integrated installation fire-fighting unmanned plane functional module

Technical field

The utility model relates to unmanned plane fields, are a kind of integrated installation fire-fighting unmanned plane functional modules specifically Integrated stand.

Background technique

With the continuous development of Process of Urbanization Construction, skyscraper is more and more, and consequent is taking place frequently for fire in high buildings, Since high-rise construction is complicated, densely populated place and fire in high buildings have the spy that fire spreading is fast, evacuation is difficult and fighting difficulty is big Point, once catching fire, the intensity of a fire is difficult to control, personnel are difficult to flee from.

In the prior art, common fire-fighting mode be put out a fire by aerial ladder and fire-fighting lance etc., but for Residential housing and more than 24 meters high high-rise fires more than 10 layers, the range of the length and fire-fighting lance of aerial ladder, water cannon As the height of fire occurrence point increases critical constraints, show as aerial ladder be raised to it is aerial after, be affected by the wind, can control and shake Pendulum increases fire fighting difficulty；Secondly, needing to carry out pressurized operation, water to water in such a way that fire-fighting lance, water cannon are put out a fire Pressure also can generate limitation to height.

Unmanned plane has been widely used in various fields as a kind of infant industry technology, with the hair of unmanned air vehicle technique Exhibition makes unmanned plane assign the function of fire-fighting fire extinguishing, it will at a kind of feasible means of high altitude firefighting.Fire-fighting unmanned plane safety work It is to need to be provided simultaneously with fire-fighting function, shooting function, aiming function, night vision function, barrier avoiding function, distance measurement function etc., it is traditional Mode is each position that various function devices are respectively adopted to bracket etc. and are mounted on fire-fighting unmanned plane, and consequent is for nobody The suspension area of machine increases, and suspended weights increase, and the figure that will lead to fire-fighting unmanned plane increases, and self weight increases, in same power Under the action of, the fire-extinguishing apparatus that can be carried can be reduced, and reduce the operating efficiency of fire-fighting unmanned plane, therefore, need a kind of energy collection At the bracket of fire-fighting unmanned plane operation function.

Utility model content

In view of this, the utility model is to solve the above problems, provide a kind of integrated installation fire-fighting unmanned plane functional module Integrated stand, the unmanned machine operation of fire-fighting is needed function integrated installation, be conducive to increase fire-fighting unmanned plane carry fire extinguishing The space of equipment.

The technical solution of the utility model is a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module, setting On the fuselage bottom of unmanned plane or two groups of stabilizer blades of unmanned plane, the functional module includes for emitting disappearing for extinguishment fire suppression bullet The quiet holder camera for shooting unmanned plane during flying real-time pictures of anti-gun barrel, the aiming for assisting fire-fighting gun barrel to aim at is used for Assist gun sight in the night vision camera worked at night, the avoidance group for assisting unmanned plane disturbance in judgement object to get around unmanned plane Part,

The integrated stand includes the fire monitor bracket being arranged on fuselage, for fixing fire-fighting gun barrel, including before being located at The first support of side and second support positioned at rear side；

Further include longitudinal sighting telescope support for being crossed on first support Yu second support top, aims at quiet and night for fixed Depending on camera；Damping device is set between the sighting telescope support and second support；

It further include the holder bracket that first support lower part is set, for fixing holder camera；

It further include that first support top and the avoidance bracket with holder bracket in same vertical region are set, for solid Determine avoidance component.

In the present invention, the back of fire-fighting unmanned plane such as uses multiple battery packs for fixing power-equipment At pure electric power source；Fuselage is the body structure with cavity body structure, and inside is such as used for for various control mould groups to be arranged Control the winged control mould group of unmanned plane during flying, for controlling emitting mould train that whether fire monitor emit, for controlling holder shooting Holder switching model group passes mould group, for controlling electricity for controlling positioning picture, holder shooting picture and aiming at the figure that picture returns Pond exports battery modules, the infrared Ding Gaomo group of height for measuring unmanned plane during flying, for measuring keeping away for obstacle distance Barrier mould group, the work for controlling the fire fighting tank dry powder that dry powder sprays into dry powder injection pipe injection mould group and comprehensively control regulation Mainboard mould group；The side wall of fuselage body structure is arranged in rotor assemblies；Fuselage body structure is arranged in unmanned plane stabilizer blade On bottom plate；Consider from the degree of balance and compactness of unmanned plane, can be installed in the space between unmanned aerial vehicle body lower part and stabilizer blade Functional module.

Since the space size between unmanned aerial vehicle body lower part and stabilizer blade is limited, according to single direct, discrete type installation Fire-fighting gun barrel aims at the functional modules such as quiet, holder camera, night vision camera, avoidance component, required fuselage base areas compared with Horizontal area greatly or between stabilizer blade is larger, necessarily leads to the larger of unmanned plane as a result, so as to cause unmanned plane self weight Increase, therefore, in the technical scheme, by the way that an integrated stand is arranged, by each functional module integrated installation in fuselage bottom, Make it is compact-sized, specifically: first pass through the first support being laterally arranged and second support for fire-fighting gun barrel and be disposed longitudinally on nobody Motor spindle, as center of gravity, divergence expression installs other modules, i.e., will aim at quiet longitudinal direction by longitudinally disposed sighting telescope support and consolidate It is scheduled on the top of fire-fighting gun barrel；Further, quiet for assisting essence of the fire-fighting gun barrel emission port towards conflagration area based on aiming at The effect of degree, by it is described aim at it is quiet be located at same perpendicular with fire-fighting gun barrel axis, even if aim at quiet cross cursor and The center of fire-fighting gun barrel is located on same vertical line, and the vertical interval of gun sight and fire-fighting gun barrel emission port 5mm ~ 50mm it Between；Quiet and fire-fighting gun barrel will be aimed to be fixed by the bracket together, it is ensured that the relative position of the two is constant；To avoid flying Or the vibration of hovering middle fuselage causes the two position to have deviation, solves the problems, such as this by the way that damping device is arranged；To have gun sight Night vision camera is arranged after gun sight and shares a sighting telescope support with gun sight, is conducive to subtract for the function of standby night work The use of limited bracket structure.Secondly, holder camera to be fixed on to the lower part of first support by holder bracket, and it is located at fire monitor Cylinder next door；Finally, avoidance component to be arranged in the top of first support by avoidance bracket, the avoidance component includes using red The avoidance ranging mould group of outer TOF technology, and the avoidance fixed plate for being fixed in first support, the avoidance fixed plate The surface of holder bracket is set, avoidance ranging mould group is made to be located at the top of holder camera, makes full use of the surplus of first support Remaining installation site makes more compact structure, reduces supporting structure；To reduce vibration, between avoidance fixed plate and first horizontal plate Several damping rubber column gel columns are set.

In the present invention, all brackets for installation function module are integrally disposed in first support and/or On two brackets, reasonable gravity distribution reduces the use of supporting structure；Functional module is installed around fire-fighting gun barrel radioactivity, makes function Energy modular structure is compact, reduces space required for underbelly, is conducive to unmanned plane and reduces external dimensions, to mitigate nobody The self weight of machine.

Further, different high-rise fire situations are different, to guarantee unmanned plane safety work, transmitting firefighting cartridge it Before, it is between 20 to 50 meters that operation fire-fighting unmanned plane, which hovers over the horizontal distance apart from conflagration area, and unmanned plane is located at fire Between 1 to 5 meter of overlying regions；According to the practical relative position of unmanned plane and conflagration area, fire monitor can be adjusted as needed The launch angle of cylinder, guarantees the fire-fighting resilience energy center hot spot of transmitting, therefore most efficient fire extinguishing is arranged described second Frame adjustable angle, the range of the emission port and horizontal elevation angle α that make fire-fighting gun barrel is between 10 ° to 20 °.

Further, the fire monitor drum outer wall is equipped with two groups of buckle structures, bayonet arrangement be clamped by two semicircular rings and At；

The first support forms " Π " type structure by first horizontal plate and two the first vertical plates；

The second support forms " Π " type structure by second horizontal plate and two the second vertical plates；

Two groups of buckle structures are separately fixed between two the first vertical plates and two the second vertical plates.

It is located at the physical location of the first vertical plate and the second vertical plate by adjusting buckle structure to adjust fire-fighting gun barrel Gradient adjusts the angle of departure of fire-fighting gun barrel, simple to operation.

Further, first horizontal plate is connected on the stabilizer blade on front side of fuselage by the first steering engine；Second horizontal plate is logical It crosses on the stabilizer blade that the second steering engine is connected on rear side of fuselage, and the second steering engine is equipped with steering gear electric-machine, drives the by steering gear electric-machine Two level boards move up and down, and make first horizontal plate around the connection electricity rotation with stabilizer blade, so as to adjust the inclination angle of fire-fighting gun barrel Degree adjusts the emission port of fire-fighting gun barrel.

Further, second vertical plate is equipped with arc chute, with the second vertical plate on the outside of fixed buckle structure Equipped with slide bar, the slide bar can slide in arc chute.

In the technical scheme, fixed second horizontal plate also can be used, be located between two the second vertical plates by mobile Fire-fighting gun barrel, achieve the purpose that adjust fire-fighting gun barrel tilt angle, specifically, by blocking between two the second vertical plates The rear end of fire-fighting gun barrel, along movement in a curve, is raised or is reduced in arc chute by the slide bar on buckle structure, changes fire-fighting gun barrel Tilt angle；Preferably, it is equipped with inductor between slide bar and arc chute, (such as remote controler) can be grasped by no-manned machine distant control end Give the realization of inductor signal.In this manner, it can make unmanned plane after hovering, the angle of departure of fire-fighting gun barrel is carried out Fine tuning, makes firefighting cartridge more accurately directive hot spot.

Further, the first support is made of the first C-shaped channel of first horizontal plate and horizontal, the first horizontal plate Lower part is fixed with inverted first U-type groove, and the first C-shaped channel and the first U-type groove form the first sky for holding fastening fire monitor drum outer wall Between；

The second support is made of the second C-shaped channel of second horizontal plate and horizontal, and the first horizontal plate lower part is fixed There is inverted second U-type groove, the second C-shaped channel and the second U-type groove form the second space for holding fastening fire monitor drum outer wall；

By two micro hydraulic cylinder connections between second U-type groove and second horizontal plate, for controlling the second U-type groove The distance between second horizontal plate.

C-shaped channel and U-type groove belong to simple and resulting structure, the two can be used threaded connection and snap connection, in installation or It dismantles convenient and efficient when fire-fighting gun barrel.Second support in the utility model passes through the stretching structure of the second U-type groove, and operator can The fire location described in fire alarm is first passed through, fire height is estimated, the hovering position after conflagration area is reached according to unmanned plane It sets, prejudges the launch angle that fire-fighting gun barrel needs to meet, before unmanned plane takes off, by adjusting the length of the second U-type groove, The preconditioning of the angle of departure is realized so as to adjust the angle of departure of fire-fighting gun barrel in the relative position of adjustment second space and the first space. Further, by two micro hydraulic cylinder connections between second U-type groove and second horizontal plate, for controlling the 2nd U The distance between type groove and second horizontal plate, micro hydraulic cylinder is controlled by remote control end, such as remote controler, to adjust fire-fighting The angle of departure of gun barrel.

Further, the sighting telescope support includes bracket upper plate, bracket lower plate and at least two gun sight fixing pieces；Institute It states by 4 to 8 positioning column supports between bracket upper plate and bracket lower plate, gun sight fixing piece is consolidated by upper stationary part and lower part Determine part to be clamped, gun sight is arranged on bracket between upper stationary part and lower fixture by lower fixture On plate.The damping device is between gun sight fixing piece and bracket upper plate.Preferably, damping device is to be arranged on bracket Damping spring between plate, bracket lower plate avoids unmanned plane during hovering aiming, and vibration is excessive to lead to aim bias mistake Greatly, fire-fighting precision is improved.

Secondly, night vision camera is arranged by camera fixing piece in bracket upper plate, guarantee central point and the aiming of night vision camera The central point of mirror is on same vertical equity line.

When the relative position of first support and/or second support changes, it is longitudinally crossed on aiming between the two Mirror support also will drive the position synchronous change of gun sight and night vision camera, and the relative position of itself and the angle of departure of fire-fighting gun barrel It remains unchanged, the precision of aiming will not be changed.

Further, the holder bracket includes the first holder bracket for connecting with holder camera and is fixed on first The second holder bracket below bracket；Holder damping device is equipped between the first holder bracket and the second holder bracket.

Using double holder supporting structures, double shield is provided for the fixation of holder camera, and can between two layers of cradle head structure For holder damping device to be arranged, it is preferable that the middle part of the holder damping device is annular rotary table plate, annular rotary table plate court Outer radioactivity is set there are four short slab, and short slab lower part is fixed with shock-absorbing ball, in the flight course of unmanned plane, the vibration transmitted from fuselage It moves when through double holder brackets, is eliminated or reduced by shock-absorbing ball and vibrate, guarantee the steady of holder camera shooting picture.

Further, the holder bracket further includes horizontal shell and two horizontal struts；The horizontal shell is set in On holder camera, the both lateral sides of horizontal shell pass through horizontal strut respectively and are connected on two groups of stabilizer blades.

Further, the damping device is by being arranged in several dampings of sighting telescope support Yu first support contact area Ball is constituted；The middle part of the holder damping device is annular rotary table plate, and radioactivity sets that there are four short slabs to annular rotary table plate outwardly, short Plate lower part is fixed with shock-absorbing ball.

The good damping effect since its is small in size using shock-absorbing ball as damping device, and can array be distributed in contact It between face, can effectively extend lanyard, due to not being associated with mutually between shock-absorbing ball, be convenient for local replacing.

Compared with prior art, the utility model is integrally disposed in first support for the bracket of installation function module And/or in second support, reasonable gravity distribution reduces the use of supporting structure；Functional module is pacified around fire-fighting gun barrel radioactivity Dress, keeps functional module structure compact, reduces space required for underbelly, is conducive to unmanned plane and reduces external dimensions, thus Mitigate the self weight of unmanned plane；By preconditioning the angle of departure of fire-fighting gun barrel before unmanned plane takes off or after hovering to fire-fighting gun barrel The angle of departure be finely adjusted, all advantageously ensure that fire-fighting gun barrel accurately reaches hot spot, improve fire-fighting efficiency.

Detailed description of the invention

Fig. 1 is the structure chart of the utility model fire-fighting unmanned plane.

Fig. 2 is the left view of the utility model fire-fighting unmanned plane.

Fig. 3 is the front view of the utility model fire-fighting unmanned plane.

Fig. 4 is fire monitor rack assumption diagram in embodiment 1.

Fig. 5 is integrated stand structure chart in embodiment 2.

Fig. 6 is sighting telescope support structure chart in the utility model.

Fig. 7 is holder bracket and avoidance rack assumption diagram in the utility model.

Specific embodiment

The utility model is further described With reference to embodiment.Wherein, the utility model embodiment The same or similar label correspond to the same or similar components in attached drawing, only for illustration, should not be understood as to this reality With novel limitation；In order to better illustrate the utility model embodiment, the certain components of attached drawing have omission, amplification or contracting It is small, do not represent the size of actual product；The side of the instructions such as embodiment term " on ", "lower", "left", "right" in the utility model Position or positional relationship are to be based on the orientation or positional relationship shown in the drawings, rather than the device or element of indication or suggestion meaning must There must be specific orientation or be constructed with specific orientation, it for the ordinary skill in the art, can be according to specific Situation understands the concrete meaning of above-mentioned term.

Embodiment 1

As shown in Figure 1, a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module, is arranged in the fuselage of unmanned plane On two groups of stabilizer blades 4 of 1 bottom or unmanned plane, the functional module includes fire monitor cylinder 51, aims at quiet 71, holder camera 72, night Depending on camera 73, avoidance component 74,

The integrated stand includes the fire monitor bracket being arranged on fuselage, for fixing fire-fighting gun barrel, including before being located at The first support 52 of side and second support 53 positioned at rear side；

Further include longitudinal sighting telescope support 711 for being crossed on first support 52 Yu 53 top of second support, is taken aim at for fixation Quasi- quiet and night vision camera；Damping device 7114 is set between the sighting telescope support 711 and second support 53；

It further include the holder bracket 721 that 52 lower part of first support is set, for fixing holder camera 72；

It further include that 52 top of first support and the avoidance bracket with holder bracket 721 in same vertical region are set 741, for fixing avoidance component.

As shown in Fig. 2, different high-rise fire situations are different, to guarantee unmanned plane safety work, transmitting firefighting cartridge it Before, it is between 20 to 50 meters that operation fire-fighting unmanned plane, which hovers over the horizontal distance apart from conflagration area, and unmanned plane is located at fire Between 1 to 5 meter of overlying regions；According to the practical relative position of unmanned plane and conflagration area, fire monitor can be adjusted as needed The launch angle of cylinder, guarantees the fire-fighting resilience energy center hot spot of transmitting, therefore most efficient fire extinguishing is arranged described second 53 adjustable angle of frame, the range of the emission port and horizontal elevation angle α that make fire-fighting gun barrel 51 is between 10 ° to 20 °；It is preferred that Ground, α=13 ° ~ 14 °.

As shown in figure 3, based on aiming at quiet 71 for assisting 51 emission port of fire-fighting gun barrel towards the work of the precision of conflagration area With, aim at quiet 71 by described and be located at same perpendicular with the axis of fire-fighting gun barrel 51, even if aim at quiet 71 cross cursor and The center of fire-fighting gun barrel 51 is located on same vertical line, and the vertical interval of gun sight 71 and 51 emission port of fire-fighting gun barrel 5mm ~ Between 50mm.

As shown in figure 4,51 outer wall of fire-fighting gun barrel is equipped with two groups of buckle structures, bayonet arrangement is by two semicircular rings 511 It is clamped；The first support 52 forms " Π " type structure by first horizontal plate 521 and two the first vertical plates 522；It is described Second support 53 forms " Π " type structure by second horizontal plate 531 and two the second vertical plates 532；Two groups of buckle structures point It is not fixed between two the first vertical plates 522 and two the second vertical plates 532.

The first horizontal plate 521 is connected on the stabilizer blade 4 of 1 front side of fuselage by the first steering engine；Second horizontal plate 531 is logical It crosses the second steering engine to be connected on the stabilizer blade 4 of 1 rear side of fuselage, and the second steering engine is equipped with steering gear electric-machine, drives by steering gear electric-machine Second horizontal plate 531 moves up and down, and makes first horizontal plate 521 around the connection electricity rotation with stabilizer blade 4, so as to adjust fire-fighting gun barrel 51 tilt angle adjusts the emission port of fire-fighting gun barrel 51.

Second vertical plate 532 is equipped with arc chute 533, with the second vertical plate 532 on the outside of fixed buckle structure Equipped with slide bar 534, the slide bar 534 can slide in arc chute 533.Preferably, between slide bar 534 and arc chute 533 Equipped with inductor, remote controler such as can be grasped by no-manned machine distant control end and gives the realization of inductor signal.It in this manner, can be with Make unmanned plane after hovering, the angle of departure of fire-fighting gun barrel 51 is finely adjusted, makes firefighting cartridge more accurately directive hot spot.

As shown in fig. 6, the sighting telescope support 711 is taken aim at including bracket upper plate 7111, bracket lower plate 7112 and at least two Quasi- mirror fixing piece 712；It is supported, is aimed at by 4 to 8 positioning columns 7113 between the bracket upper plate 7111 and bracket lower plate 7112 Mirror fixing piece 712 is clamped by upper stationary part 7121 and lower fixture 7122, and gun sight 71 is located at upper stationary part Between 7121 and lower fixture 7122, it is arranged on bracket upper plate 7111 by lower fixture 7122.The damping device 7114 between gun sight fixing piece 712 and bracket upper plate 7111.Preferably, damping device 7114 is to be arranged in bracket upper plate 7111, the damping spring between bracket lower plate 7112 avoids unmanned plane during hovering aiming, and vibration is excessive to be caused to aim at partially Difference is excessive, improves fire-fighting precision.

Secondly, night vision camera 73 is arranged by camera fixing piece in bracket upper plate 7111, guarantee the center of night vision camera 73 The central point with gun sight 71 is put on same vertical equity line.

As shown in fig. 7, the holder bracket 721 include the first holder bracket 722 for being connect with holder camera 72 and It is fixed on the second holder bracket 723 of 52 lower section of first support；Between the first holder bracket 722 and the second holder bracket 723 Equipped with holder damping device 724.The holder bracket 721 further includes horizontal shell 725 and two horizontal struts 726；The water Flat housing 725 is set on holder camera 72, and the both lateral sides of horizontal shell 725 pass through horizontal strut 726 respectively and are connected to two On group stabilizer blade 4.

The damping device 7114 is by being arranged in several dampings of sighting telescope support 711 Yu 52 contact area of first support Ball is constituted；The middle part of the holder damping device 724 is annular rotary table plate, and radioactivity sets that there are four short to annular rotary table plate outwardly Plate, short slab lower part are fixed with shock-absorbing ball.

The avoidance component 74 includes the avoidance ranging mould group 741 using infrared distance measurement principle, and for being fixed in Avoidance fixed plate 742 in first support 52, the avoidance fixed plate 742 are arranged in the surface of holder bracket 721, make avoidance Ranging mould group 741 is located at the top of holder camera 72, makes full use of the remaining installation site of first support 52, keeps structure tighter It gathers, reduces supporting structure；To reduce vibration, several damping rubbers are set between avoidance fixed plate 742 and first horizontal plate 521 Column 743.

Embodiment 2

The present embodiment the difference is that only with embodiment 1, as shown in figure 5, the first support 52 is by first level First C-shaped channel 512 of plate 521 and horizontal is constituted, and 521 lower part of first horizontal plate is fixed with inverted first U-type groove 513, First C-shaped channel 512 and the first U-type groove 513 form the first space for holding fastening 51 outer wall of fire-fighting gun barrel；

The second support 53 is made of the second C-shaped channel 514 of second horizontal plate 531 and horizontal, the first horizontal plate 521 lower parts are fixed with inverted second U-type groove 515, and the second C-shaped channel 514 and the second U-type groove 515, which are formed, holds fastening fire-fighting gun barrel The second space of 51 outer walls；

By the connection of two micro hydraulic cylinders between second U-type groove 515 and second horizontal plate 531, for controlling the The distance between two U-type grooves 515 and second horizontal plate 531.

Further, it is connected between second U-type groove 515 and second horizontal plate 531 by two micro hydraulic cylinders, For control the distance between the second U-type groove 515 and second horizontal plate 531, micro hydraulic cylinder by be remotely controlled end, such as remote controler into Row control, to adjust the angle of departure of fire-fighting gun barrel 51.

It obviously, is not the restriction to the utility model although the utility model is disclosed with above-described embodiment.Any The those of ordinary skill in field without departing from the spirit and scope of the utility model, can do on the basis of the above description Possible change and modification out.Therefore, the protection scope of the utility model should be with claims institute circle of the utility model Subject to fixed range.

Claims (10)

1. fuselage (1) bottom or the nothing of unmanned plane is arranged in a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module On two groups of man-machine stabilizer blades (4), the functional module includes fire monitor cylinder (51), aims at quiet (71), holder camera (72), night vision Camera (73), avoidance component (74), which is characterized in that

The integrated stand includes the fire monitor bracket being arranged on fuselage, for fixing fire-fighting gun barrel, including being located at front side First support (52) and second support (53) positioned at rear side；

It further include longitudinal sighting telescope support (711) for being crossed on first support (52) Yu second support (53) top, for fixing Aim at quiet and night vision camera；Damping device (7114) are set between the sighting telescope support (711) and second support (53)；

It further include holder bracket (721) of the setting in first support (52) lower part, for fixing holder camera (72)；

It further include the avoidance bracket being arranged on first support (52) top and with holder bracket (721) in same vertical region (741), for fixing avoidance component.

2. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 1, which is characterized in that Second support (53) adjustable angle, the range of the emission port for making fire-fighting gun barrel (51) and horizontal elevation angle α at 10 ° extremely Between 20 °.

3. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 1 or 2, feature exist In fire-fighting gun barrel (51) outer wall is equipped with two groups of buckle structures, and bayonet arrangement is clamped by two semicircular rings (511)；

The first support (52) forms " Π " type structure by first horizontal plate (521) and two the first vertical plates (522)；

The second support (53) forms " Π " type structure by second horizontal plate (531) and two the second vertical plates (532)；

Two groups of buckle structures are separately fixed between two the first vertical plates (522) and two the second vertical plates (532).

4. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 3, which is characterized in that Second vertical plate (532) is equipped with arc chute (533), sets on the outside of fixed buckle structure with the second vertical plate (532) Have slide bar (534), the slide bar (534) can the sliding in arc chute (533).

5. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 1 or 2 or 4, special Sign is that the first support (52) is made of the first C-shaped channel (512) of first horizontal plate (521) and horizontal, first water Plate (521) lower part is fixed with inverted first U-type groove (513), and the first C-shaped channel (512) and the first U-type groove (513), which are formed, to hold Fasten first space of fire-fighting gun barrel (51) outer wall；

The second support (53) is made of the second C-shaped channel (514) of second horizontal plate (531) and horizontal, the first level Plate (521) lower part is fixed with inverted second U-type groove (515), and the second C-shaped channel (514) and the second U-type groove (515), which are formed, to hold tightly The second space of fire-fighting gun barrel Gu (51) outer wall；

It is connect between second U-type groove (515) and second horizontal plate (531) by two micro hydraulic cylinders, for controlling the The distance between two U-type grooves (515) and second horizontal plate (531).

6. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 1 or 2 or 4, special Sign is that the sighting telescope support (711) includes that bracket upper plate (7111), bracket lower plate (7112) and at least two gun sights are solid Determine part (712)；Pass through 4 to 8 positioning column (7113) supports, institute between the bracket upper plate (7111) and bracket lower plate (7112) Damping device (7114) is stated to be located between gun sight fixing piece (712) and bracket upper plate (7111).

7. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 1, which is characterized in that The holder bracket (721) includes the first holder bracket (722) for connecting with holder camera (72) and is fixed on first The second holder bracket (723) below frame (52)；It is equipped between the first holder bracket (722) and the second holder bracket (723) Holder damping device (724).

8. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 7, which is characterized in that The holder bracket (721) further includes horizontal shell (725) and two horizontal struts (726)；The horizontal shell (725) is arranged On holder camera (72), the both lateral sides of horizontal shell (725) pass through horizontal strut (726) respectively and are connected to two groups of stabilizer blades (4) on.

9. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 7 or 8, feature exist In,

The damping device (7114) by sighting telescope support (711) and first support (52) contact area be set several subtract Ball is shaken to constitute；

The middle part of the holder damping device (724) is annular rotary table plate, and radioactivity is set there are four short slab annular rotary table plate outwardly, Short slab lower part is fixed with shock-absorbing ball.

10. a kind of integrated stand of integrated installation fire-fighting unmanned plane functional module according to claim 1, feature exist In the axis for aiming at quiet (71) and fire-fighting gun barrel (51) is located at same perpendicular.