CN211069018U

CN211069018U - Aircraft model with spraying system

Info

Publication number: CN211069018U
Application number: CN201921127559.5U
Authority: CN
Inventors: 祁先益
Original assignee: Guangzhou Teching Cultural Development Co ltd
Current assignee: Guangzhou Teching Cultural Development Co ltd
Priority date: 2019-07-17
Filing date: 2019-07-17
Publication date: 2020-07-24
Anticipated expiration: 2029-07-17

Abstract

The utility model relates to a toy model technical field, concretely relates to aircraft model with water-spraying system. The utility model discloses an aircraft model with a spraying system, which sends a control signal to the aircraft model, and a control panel of the aircraft model controls the work of a first spraying module; when the first spraying module works, liquid water in the first water storage module flows into the first spraying module from one end of the guide pipe and flows into the first spraying module from the other end of the guide pipe, and the liquid water is atomized by the first spraying module and then is sprayed out of the aircraft model body, so that the smoke effect after the aircraft is ignited is simulated, and the interestingness of the aircraft model is increased; in addition, through at this internal atomizer that sets up of aircraft model, spout aircraft model body behind the liquid water atomization in the module with first retaining, can be used for the teaching scene that actual aircraft rises to the air, have actual teaching meaning.

Description

Aircraft model with spraying system

Technical Field

The utility model relates to a toy model technical field, concretely relates to aircraft model with water-spraying system.

Background

Toys broadly refer to items that can be used to play, and play with toys is often used in human society as a way to teach through lively activities. The toy can also be a natural object, namely, a non-artificial object such as sand, stone, mud, branches and the like, the toy is widely understood, the toy is not limited to a toy for people to play on the street, and all objects which can be played, watched, listened and touched can be called as the toy; an object which forms an expression purpose for objectively describing a morphological structure is a model through subjective consciousness by means of physical or virtual representation. The aircraft model is one of a plurality of toy models, and the current aircraft model only has the effect of watching, is relatively poor in interestingness and has no practical teaching significance.

Disclosure of Invention

In order to overcome the shortcoming and the deficiency that exist among the prior art, the utility model aims at providing an aircraft model with water-spraying system has solved the relatively poor problem of interest of present aircraft model to have actual teaching meaning.

The utility model discloses a realize through following technical scheme:

the utility model provides an aircraft model with a spraying system, which comprises an aircraft model body, a first spraying module and a first water storage module, wherein the first spraying module and the first water storage module are arranged in the aircraft model body; the atomizer is arranged at the bottom end of the aircraft model body, and a spray nozzle of the atomizer is communicated with the outside of the aircraft model body; the atomizer is electrically connected with the control panel.

The first water storage module comprises an upper cover, a cylinder body and a funnel seat which are all arranged in the aircraft model body, the upper cover is detachably connected with the top end of the cylinder body, and the funnel seat is arranged at the bottom end of the cylinder body; one end of the conduit is communicated with the funnel seat.

The middle section of the guide pipe is bent towards the direction of the electronic element far away from the control board; the conduit is attached to the PCB of the control panel.

The aircraft model with the spraying system further comprises a first wireless receiving module or a key switch for controlling the atomizer to start and stop, the wireless receiving module and the key switch are arranged on the aircraft model body, and the wireless receiving module and the key switch are electrically connected with the control panel.

The aircraft model body comprises a base, a primary aircraft body, a secondary aircraft body, an effective load, a fairing and a detachable connecting structure, wherein the first spraying module, the first water storage module and the control panel are all arranged on the first aircraft body, and a spraying port of the atomizer is communicated with the outside of the primary aircraft body; the payload is arranged in the fairing; the primary aircraft body and the base, the primary aircraft body and the secondary aircraft body and the payload are detachably connected through detachable connecting structures; the base is also provided with a wireless transmitting device which is wirelessly connected with the first wireless receiving module; the key switch is arranged on the base.

The detachable connecting structure comprises a first clamping seat and a second clamping seat, wherein a plurality of first clamping pieces are arranged on one end face, close to the second clamping seat, of the first clamping seat, and a plurality of second clamping pieces are arranged on one end face, close to the first clamping seat, of the second clamping seat; the first clamping seat is also provided with a plurality of first clamping grooves respectively corresponding to the second clamping pieces, and the second clamping pieces are arranged in the first clamping grooves; the second clamping seat is also provided with a plurality of second clamping grooves respectively corresponding to the first clamping pieces, and the first clamping pieces are arranged in the second clamping grooves; the other end of the first clamping seat is connected with the primary aircraft body or the secondary aircraft body or the fairing, and the other end of the second clamping seat is connected with the base or the primary aircraft body or the secondary aircraft body.

The second-level aircraft body is internally provided with a second spraying module, a second water storage module and a second wireless receiving device which is wirelessly connected with the wireless transmitting device, a water inlet of the second spraying module is communicated with the second water storage module, and a mist outlet of the second spraying module is communicated with the outside of the second aircraft body;

a third spraying module, a third water storage module and a third wireless receiving device which is wirelessly connected with the wireless transmitting device are arranged in the effective load, a water inlet of the third spraying module is communicated with the third water storage module, and a mist outlet of the third spraying module is communicated with the outside of the fairing;

proximity sensors are arranged between the primary aircraft body and the secondary aircraft body and between the secondary aircraft body and the payload.

The fairing comprises a first hood body and a second hood body, wherein one end of the first hood body is provided with a first upper magnet, and one end of the second hood body is provided with a second upper magnet which is mutually adsorbed with the first upper magnet; the other end of the first cover body is provided with a first lower magnet, the other end of the second cover body is provided with a second lower magnet, and the detachable connecting structure close to the fairing is provided with a magnetic attraction piece which is respectively adsorbed with the first lower magnet and the second lower magnet.

The aircraft model with the spraying system further comprises a plurality of boosters and a clamping base arranged on the aircraft model body, clamping blocks are arranged on the side wall of each booster, and a plurality of buckles clamped with the clamping blocks are arranged on the outer side wall of the clamping base.

Wherein, a moving contact and a fourth spraying module or a power supply electrically connected with the moving contact are arranged in the plurality of boosters; and the plurality of buckles are provided with static contacts for contacting with the movable contacts, and the plurality of static contacts are electrically connected with the control panel.

The utility model has the advantages that:

1. the problem of current aircraft model interest relatively poor is solved: the utility model discloses an aircraft model with a spraying system, which sends a control signal to a control panel, and the control panel controls the work of a first spraying module; when first spraying module during operation, the liquid water in the first water storage module flows in from the one end of pipe and flows in first spraying module from the other end of pipe to spout from aircraft model body after being atomized with liquid water by first spraying module, thereby the smog effect after the simulation aircraft is igniteed has increased aircraft model's interest.

2. Has practical teaching significance: because traditional aircraft model only has the viewing effect, the utility model discloses an aircraft model with water spraying system through this internal atomizer that sets up of aircraft model, with the liquid water atomization back of first retaining module from aircraft model body blowout, can be used for the teaching scene that actual aircraft ascended to the air, has actual teaching meaning.

Drawings

The present invention is further explained by using the drawings, but the embodiments in the drawings do not constitute any limitation to the present invention, and for those skilled in the art, other drawings can be obtained according to the following drawings without any inventive work.

Fig. 1 is a schematic perspective view of the present invention.

Fig. 2 is the schematic view of the exploded structure of the aircraft model body of the present invention.

Fig. 3 is a cross-sectional view of the aircraft model body according to the present invention.

Fig. 4 is an exploded schematic view of the fairing of the present invention.

Fig. 5 is a schematic view of the detachable connection structure according to the present invention.

Fig. 6 is an exploded schematic view of the aircraft model body and the booster of the present invention.

Reference numerals

An aircraft model body-1, a base-11, a primary aircraft body-12, a secondary aircraft body-13, a payload-14,

a fairing-15, a first shroud-151, a second shroud-152, a first upper magnet-153, a second upper magnet-154, a first lower magnet-155, a second lower magnet-156, a magnetic attachment-157,

a detachable connecting structure-16, a first clamping seat-161, a second clamping seat-162, a first clamping piece-163, a second clamping piece-164, a first clamping groove-165, a second clamping groove-166,

a booster-17, a clamping block-171, a movable contact-172, a clamping base-18, a clamping buckle-181, a fixed contact-182, a key switch-19,

a first spraying module-2, a control panel-21, a conduit-22, an atomizer-23,

a first water storage module-3, an upper cover-31, a cylinder-32 and a funnel seat-33.

Detailed Description

The following description of the embodiments of the present invention is provided for illustrative purposes, and other advantages and effects of the present invention will be readily apparent to those skilled in the art from the disclosure herein. The present invention can also be implemented or applied through other different specific embodiments, and various details in the present specification can be modified or changed based on different viewpoints and applications without departing from the spirit of the present invention.

It should be noted that the structures shown in the drawings are only used for matching with the contents disclosed in the specification, so as to be understood and read by those skilled in the art, and are not used for limiting the practical limitations of the present invention, so that the modifications or adjustments of any structure do not have the essential meaning in the art, and the technical contents disclosed in the present invention should still fall within the scope that the functions and the achievable objects of the present invention can be achieved without affecting the present invention.

As shown in fig. 1 and 3, an aircraft model with a spraying system comprises an aircraft model body 1, a first spraying module 2 and a first water storage module 3, wherein the first spraying module 2 and the first water storage module 3 are arranged in the aircraft model body 1, the first spraying module 2 comprises a control panel 21, a conduit 22 and an atomizer 23, one end of the conduit 22 is communicated with the first water storage module 3, and the other end of the conduit 22 is communicated with a water inlet of the atomizer 23; the atomizer 23 is arranged at the bottom end of the aircraft model body 1, and a spray nozzle of the atomizer 23 is communicated with the outside of the aircraft model body 1; the atomizer 23 is electrically connected to the control board 21.

In this embodiment, the control board 21 may be externally connected to the key switch 19 of the aircraft model body 1, and the start and stop of the atomizer 23 are controlled by pressing the key switch 19, or the control board 21 may be provided with a first wireless receiving module (not shown in the figure), and the control board 21 may send a wireless signal to the first wireless receiving module through an external wireless sending module or a mobile terminal with a wireless transceiving function, such as a mobile phone, so as to control the atomizer 23 to operate. In this embodiment, the atomizer 23 is a ceramic atomizing plate, which has the characteristics of easy replacement and long service life, and the liquid water molecule structure is broken up by the high-frequency resonance of the ceramic atomizing plate to generate naturally flowing water mist, and the water mist is ejected from the bottom of the aircraft model without heating or adding any chemical reagent, so as to simulate the flying scene of the aircraft. In this embodiment, the aircraft model may be a rocket model or a missile model.

Specifically, the first water storage module 3 comprises an upper cover 31, a cylinder 32 and a funnel seat 33 which are all arranged in the aircraft model body 1, the upper cover 31 is detachably connected with the top end of the cylinder 32, and the funnel seat 33 is arranged at the bottom end of the cylinder 32; one end of the conduit 22 communicates with a funnel seat 33. The cylinder 32 can be used for storing liquid water, and when the liquid water in the cylinder 32 is used up, the upper cover 31 can be detached to supplement the liquid water into the cylinder 32; because the diameter of the cylinder 32 is larger, the funnel seat 33 at the lower end of the cylinder 32 facilitates the water in the cylinder 32 to enter the conduit 22 with smaller diameter, and then the conduit 22 guides the liquid water to the atomizer 23.

Specifically, the middle section of the conduit 22 is bent toward the direction away from the electronic components of the control board 21; the guide pipe 22 is attached to the PCB of the control panel 21, and since the space inside the aircraft model body 1 is limited, the guide pipe 22 is bent, so that the influence of the guide pipe 22 on the electronic components on the control panel 21 can be avoided.

Specifically, the aircraft model body 1 comprises a base 11, a primary aircraft body 12, a secondary aircraft body 13, a payload 14, a fairing 15 and a detachable connecting structure 16, the first spray module 2, the first water storage module 3 and the control panel 21 are all arranged on the first aircraft body, and a spray nozzle of the atomizer 23 is communicated with the outside of the primary aircraft body 12; the effective load 14 is arranged in a fairing 15 and simulates the installation condition of a warhead in a satellite in a real carrier rocket or a real missile; in addition, the payload 4 is a model artificial satellite, and when the fairing 5 is detached from the detachable connecting structure 16, the solar panel of the artificial satellite can be extended out, so as to further simulate the shape of a real artificial satellite.

Specifically, the detachable connection between the primary aircraft body 12 and the base 11, between the primary aircraft body 12 and the secondary aircraft body 13, and between the secondary aircraft body 13 and the payload 14 is realized through detachable connection structures 16 respectively; the base 11 is further provided with a wireless transmitting device (not shown in the figure) wirelessly connected with the first wireless receiving module; the key switch 19 is disposed on the base 11. The wireless transmitting device is controlled by a switch on the base 11 to communicate with the first wireless receiving device of the control panel 21, so that the first spraying module 2 is controlled to work in a wireless control mode; the aircraft model of this embodiment, when in-service use and watch, aircraft model body 1 then simulates the multistage formula structure of real aircraft, between one-level aircraft body 12 and base 11, between one-level aircraft body 12 and second grade aircraft body 13 and between second grade aircraft body 13 and payload 14 all realize dismantling the connection through dismantling connection structure 16 for the aircraft model of this embodiment possesses the authenticity in the teaching meaning.

Specifically, the fairing 15 includes a first shroud 151 and a second shroud 152, one end of the first shroud 151 is provided with a first upper magnet 153, and one end of the second shroud 152 is provided with a second upper magnet 154 which is mutually adsorbed with the first upper magnet 153; the other end of the first cover 151 is provided with a first lower magnet 155, the other end of the second cover 152 is provided with a second lower magnet 156, and the detachable connecting structure 16 close to the fairing 15 is provided with a magnetic attraction piece 157 which is respectively attracted to the first lower magnet 155 and the second lower magnet 156. When the first cover 151 is covered on the second cover 152, the first upper magnet 153 and the second upper magnet 154 are adsorbed, so that the difficulty in assembling and disassembling the whole fairing 15 is simplified; meanwhile, the lower ends of the first cover 151 and the second cover 152 are respectively installed in a way of being attracted to the magnetic attraction piece 157 by the first lower magnet 155 and the second lower magnet 156, so that the installation stability of the first cover 151 and the second cover 152 is improved; meanwhile, in this embodiment, the magnetic element 157 is assembled with a plurality of magnets therein, i.e. the outer sidewall of the magnetic element 157 is distributed with a plurality of magnets, so the installation directions of the first cover 151 and the second cover 152 are not limited.

Specifically, as shown in fig. 5, the detachable connecting structure 16 includes a first engaging seat 161 and a second engaging seat 162, wherein a plurality of first engaging pieces 163 are disposed on an end surface of the first engaging seat 161 close to the second engaging seat 162, and a plurality of second engaging pieces 164 are disposed on an end surface of the second engaging seat 162 close to the first engaging seat 161; the first clamping seat 161 is further provided with a plurality of first clamping grooves 165 respectively corresponding to the second clamping pieces 164, and the second clamping pieces 164 are arranged in the first clamping grooves 165; the second clamping seat 162 is further provided with a plurality of second clamping grooves 166 respectively corresponding to the first clamping pieces 163, and the first clamping pieces 163 are arranged in the second clamping grooves 166; the other end of the first clamping seat 161 is connected with the primary aircraft body 12 or the secondary aircraft body 13 or the fairing 15, and the other end of the second clamping seat 162 is connected with the base 11 or the primary aircraft body 12 or the secondary aircraft body 13. The first snap-fit seat 161 and the second snap-fit seat 162 are snap-fit, so that the arrangement of the segmented structure is realized between the base 11 and the primary aircraft body 12, between the primary aircraft body 12 and the secondary aircraft body 13, and between the secondary aircraft body 13 and the payload 14.

Specifically, a second spraying module (not shown in the figure), a second water storage module (not shown in the figure) and a second wireless receiving device (not shown in the figure) which is wirelessly connected with the wireless transmitting device are arranged in the secondary aircraft body 13, a water inlet of the second spraying module is communicated with the second water storage module, and a mist outlet of the second spraying module is communicated with the outside of the second aircraft body; a third spraying module (not shown in the figure), a third water storage module (not shown in the figure) and a third wireless receiving device (not shown in the figure) which is wirelessly connected with the wireless sending device are arranged in the payload 14, a water inlet of the third spraying module is communicated with the third water storage module, and a mist outlet of the third spraying module is communicated with the outside of the fairing 15; proximity sensors (not shown) are arranged between the primary aircraft body 12 and the secondary aircraft body 13 and between the secondary aircraft body 13 and the payload 14. In the embodiment, the working principle of the second spraying module and the third spraying module is the same as that of the first spraying module; in addition, except that the bottom of the primary aircraft body 12 can spray fog, the bottom of the secondary aircraft body 13 and the bottom of the payload 14 can spray fog, so that a sectional type lift-off scene of a carrier aircraft is simulated; proximity sensors are respectively arranged between the primary aircraft body 12 and the secondary aircraft body 13 and between the secondary aircraft body 13 and the payload 14, so that whether the bottom end of the secondary aircraft body 13 is connected with the primary aircraft body 12 through the detachable connecting structure 16 or not and whether the bottom end of the payload 14 is connected with the secondary aircraft body 13 through the detachable connecting structure 16 or not can be judged; if the bottom end of the secondary aircraft body 13 is not connected with the primary aircraft body 12 through the detachable connection structure 16, the first spray module 2 of the primary aircraft body 12 does not spray mist but the second spray module of the secondary aircraft body 13 sprays mist when the switch of the base 11 is pressed; similarly, if the bottom end of the payload 14 is not connected to the secondary aircraft body 13 by the detachable connection structure 16, the second spray module of the secondary aircraft body 13 does not spray mist when the switch of the base 11 is pressed, but the third spray module of the payload 14 sprays mist.

Specifically, as shown in fig. 6, the aircraft model with the spraying system further includes a plurality of boosters 17 and a clamping base 18 disposed on the aircraft model body 1, a clamping block 171 is disposed on a side wall of each booster 17, a plurality of buckles 181 clamped with the clamping block 171 are disposed on an outer side wall of the clamping base 18, and the boosters 17 and the aircraft model body 1 are detachable through cooperation of the clamping block 171 and the buckles 181; meanwhile, a movable contact 172 and a fourth spraying module or a power supply electrically connected with the movable contact 172 are arranged in each of the plurality of boosters 17; the plurality of buckles 181 are provided with the fixed contacts 182 for contacting the movable contacts 172, the plurality of fixed contacts 182 are electrically connected with the control panel 21, and after the booster 17 is assembled with the aircraft model body 1, if a power supply is installed in the booster 17, the booster 17 supplies power to the control panel 21, each spray module, each proximity sensor and each wireless receiving module in the aircraft model body 1 through the contact of the movable contacts 172 and the fixed contacts 182, so that the extensibility of the aircraft model of the embodiment is increased.

In summary, the aircraft model with the spraying system of the embodiment has the following effects

1. The problem of current aircraft model interest relatively poor is solved: the utility model discloses an aircraft model with a spraying system, through sending control signal to control panel 21, control panel 21 controls the work of first spraying module 2; when the first spraying module 2 works, the liquid water in the first water storage module 3 flows in from one end of the guide pipe 22 and flows in the first spraying module 2 from the other end of the guide pipe 22, and the liquid water is atomized by the first spraying module 2 and then sprayed out from the aircraft model body 1, so that the smoke effect after the ignition of the aircraft is simulated, and the interestingness of the aircraft model is increased.

2. Has practical teaching significance: because traditional aircraft model only has the viewing effect, the utility model discloses an aircraft model with water-spraying system through set up atomizer 23 in aircraft model body 1, with the liquid water atomization back of first retaining module 3 from aircraft model body 1 blowout, can be used for the teaching scene that actual aircraft ascended to the air, has actual teaching meaning.

It should be finally noted that the above embodiments are only intended to illustrate the technical solutions of the present invention, and not to limit the scope of the present invention, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solutions of the present invention can be modified or replaced with equivalents without departing from the spirit and scope of the technical solutions of the present invention.

Claims

1. An aircraft model with a spraying system, comprising an aircraft model body (1), characterized in that: also comprises a first spraying module (2) and a first water storage module (3) which are arranged in the aircraft model body (1),

the first spraying module (2) comprises a control panel (21), a conduit (22) and an atomizer (23), one end of the conduit (22) is communicated with the first water storage module (3), and the other end of the conduit (22) is communicated with a water inlet of the atomizer (23); the atomizer (23) is arranged at the bottom end of the aircraft model body (1), and a spray nozzle of the atomizer (23) is communicated with the outside of the aircraft model body (1); the atomizer (23) is electrically connected with the control board (21).

2. An aircraft model with a spraying system according to claim 1, wherein: the first water storage module (3) comprises an upper cover (31), a cylinder body (32) and a funnel seat (33) which are all arranged in the aircraft model body (1), the upper cover (31) is detachably connected with the top end of the cylinder body (32), and the funnel seat (33) is arranged at the bottom end of the cylinder body (32); one end of the guide pipe (22) is communicated with the hopper seat (33).

3. An aircraft model with a spraying system according to claim 1, wherein: the middle section of the guide pipe (22) is bent towards the direction of the electronic element far away from the control board (21); the conduit (22) is attached to the PCB of the control panel (21).

4. An aircraft model with a spraying system according to claim 1, wherein: the aircraft model with the spraying system further comprises a first wireless receiving module or a key switch (19) for controlling the starting and stopping of the atomizer (23), the wireless receiving module and the key switch (19) are arranged on the aircraft model body (1), and the wireless receiving module and the key switch (19) are electrically connected with the control panel (21).

5. An aircraft model with a spraying system according to claim 4, wherein: the aircraft model body (1) comprises a base (11), a primary aircraft body (12), a secondary aircraft body (13), a payload (14), a fairing (15) and a detachable connecting structure (16), wherein the first spraying module (2), the first water storage module (3) and the control panel (21) are all arranged on the first aircraft body, and a spraying port of the atomizer (23) is communicated with the outside of the primary aircraft body (12); the payload (14) is disposed within a fairing (15); the detachable connection between the primary aircraft body (12) and the base (11), between the primary aircraft body (12) and the secondary aircraft body (13) and between the secondary aircraft body (13) and the payload (14) is realized through detachable connection structures (16); the base (11) is also provided with a wireless transmitting device which is in wireless connection with the first wireless receiving module; the key switch (19) is arranged on the base (11).

6. An aircraft model with a spraying system according to claim 5, wherein: the detachable connecting structure (16) comprises a first clamping seat (161) and a second clamping seat (162), a plurality of first clamping pieces (163) are arranged on one end face, close to the second clamping seat (162), of the first clamping seat (161), and a plurality of second clamping pieces (164) are arranged on one end face, close to the first clamping seat (161), of the second clamping seat (162); the first clamping seat (161) is also provided with a plurality of first clamping grooves (165) which respectively correspond to the second clamping pieces (164), and the second clamping pieces (164) are arranged in the first clamping grooves (165); the second clamping seat (162) is also provided with a plurality of second clamping grooves (166) which respectively correspond to the first clamping pieces (163), and the first clamping pieces (163) are arranged in the second clamping grooves (166); the other end of first joint seat (161) is connected with one-level aircraft body (12) or second grade aircraft body (13) or radome fairing (15), the other end of second joint seat (162) is connected with base (11) or one-level aircraft body (12) or second grade aircraft body (13).

7. An aircraft model with a spraying system according to claim 5, wherein: a second spraying module, a second water storage module and a second wireless receiving device which is wirelessly connected with the wireless transmitting device are arranged in the secondary aircraft body (13), a water inlet of the second spraying module is communicated with the second water storage module, and a mist outlet of the second spraying module is communicated with the outside of the second aircraft body;

a third spraying module, a third water storage module and a third wireless receiving device which is wirelessly connected with the wireless transmitting device are arranged in the payload (14), a water inlet of the third spraying module is communicated with the third water storage module, and a mist outlet of the third spraying module is communicated with the outside of the fairing (15);

proximity sensors are arranged between the primary aircraft body (12) and the secondary aircraft body (13) and between the secondary aircraft body (13) and the payload (14).

8. An aircraft model with a spraying system according to claim 5, wherein: the fairing (15) comprises a first hood body (151) and a second hood body (152), a first upper magnet (153) is arranged at one end of the first hood body (151), and a second upper magnet (154) which is mutually adsorbed with the first upper magnet (153) is arranged at one end of the second hood body (152); the other end of the first cover body (151) is provided with a first lower magnet (155), the other end of the second cover body (152) is provided with a second lower magnet (156), and the detachable connecting structure (16) close to the fairing (15) is provided with a magnetic attraction piece (157) which is respectively adsorbed to the first lower magnet (155) and the second lower magnet (156).

9. An aircraft model with a spraying system according to claim 1, wherein: aircraft model with spraying system still includes a plurality of boosters (17) and locates joint base (18) of aircraft model body (1), the lateral wall of booster (17) is equipped with fixture block (171), the lateral wall of joint base (18) is equipped with buckle (181) of a plurality of and fixture block (171) joint.

10. An aircraft model with a misting system as defined in claim 9 wherein: a movable contact (172) and a fourth spraying module or a power supply electrically connected with the movable contact (172) are arranged in the plurality of boosters (17); the plurality of buckles (181) are provided with static contacts (182) used for being in contact with the movable contacts (172), and the plurality of static contacts (182) are electrically connected with the control panel (21).