CN215900930U

CN215900930U - Linkage type flight device

Info

Publication number: CN215900930U
Application number: CN202121056158.2U
Authority: CN
Inventors: 陶丽君
Original assignee: Coco Tongman Technology Shenzhen Co ltd
Current assignee: Coco Tongman Technology Shenzhen Co ltd
Priority date: 2021-05-17
Filing date: 2021-05-17
Publication date: 2022-02-25
Anticipated expiration: 2031-05-17

Abstract

The utility model relates to the technical field of flying devices, and discloses a linkage type flying device which comprises an aircraft, a cover body, a fixing piece and a lamp strip, wherein the fixing piece and the aircraft are respectively arranged in the cover body; the aircraft generates airflow to realize flight, and the synchronous driving cover body is rotationally arranged to drive the lamp strip to be rotationally arranged. During the use, the aircraft starts, throws out the flying device, and the flying device is in aerial according to the angle of throwing out from steady flight, not only realizes holistic flight, moreover, impels the cover body rotatory, drives the lamp area rotatory, and at this moment, the lamp area is the circular telegram and starts the arrangement, throws the light source outwards, and the user watches the light source that the lamp area throws, and based on the vision inertia, the projection light source that the user saw forms pattern or characters, strengthens flying device's interest, has more striking nature and attractiveness simultaneously, improves the experience sense that the user used.

Description

Linkage type flight device

Technical Field

The utility model relates to the technical field of flight devices, in particular to a linkage type flight device.

Background

The flying device is a toy which is loved by children and extensive model airplane enthusiasts.

At present, with the increasing attention of people to intelligent life, various related technologies of the aerodynamic aircraft are widely applied to flight devices, and various types of flight devices are created.

When the flying device product is used, the flying device is thrown out, the flying device flies in the air in a self-stabilizing mode according to the thrown angle, the flying angle of the flying device is kept unchanged under the action of the gyro effect of the rotation of the built-in paddle, and the flying ball can continuously fly along the direction of the angle.

In the prior art, the flying device is only used for flying, is lack of projection of patterns, characters and the like, and has low interest and insufficient attraction.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a linkage type flight device, and aims to solve the problem that the flight device does not have a projection function in the prior art.

The utility model is realized in this way, the coordinated type flight device, including aircraft, cover body, fixed part and lamp area, the said fixed part and said aircraft are placed in the said cover body separately, the said aircraft presents and links the arrangement with the said cover body through the said fixed part, the said lamp area installs the said cover body, the said lamp area projects the light source, the light source forms the pattern or characters on the basis of the visual inertia; the aircraft generates airflow to realize flight, and synchronously drives the cover body to be in rotary arrangement to drive the lamp strip to be in rotary arrangement.

Furthermore, the cover body is arranged in a spherical shape and comprises a first cover piece and a second cover piece, the first cover piece and the second cover piece are arranged in a buckling mode, a cover cavity is formed by the first cover piece and the second cover piece, and the fixing piece and the aircraft are respectively arranged in the cover cavity; the aircraft is the level and arranges, the cover body includes the cover frame, follows to deviate from the aircraft direction, the cover frame is to arch up the arc and arranges, the upper portion of cover frame extends to the top of first cover spare, the lower part of cover frame extends to the bottom of second cover spare, the lamp area is installed the cover frame.

Furthermore, the first cover piece comprises a first middle frame which is annularly arranged, the second cover piece comprises a second middle frame which is annularly arranged, and the first middle frame and the second middle frame are arranged in an abutting and overlapping mode to form a buckling part; the mounting with the aircraft is the connection and arranges, just the mounting respectively with first center with the second center is the connection and arranges.

Further, the mounting includes two fixed groups, two fixed group is the crisscross arrangement of cross, fixed group includes two dead levers, two the dead lever is the interval along the level and corresponds the arrangement, the inner of dead lever with the aircraft is the connection and arranges, the outer end of dead lever with buckling part is the connection and arranges.

Further, the aircraft comprises at least one blade, a main motor, a power supply part and a device shell, wherein the blade, the main motor and the power supply part are respectively arranged on the device shell, the power supply part is used for providing power, the blade is started to generate airflow to realize flight, and the main motor is used for driving the blade to rotate to generate airflow.

Further, the aircraft comprises four main motors and four blades, each main motor and each blade are arranged in a one-to-one correspondence manner, and the main motors are used for driving the blades to rotate; the four main motors are respectively installed on the device shell, the four main motors are arranged in four corners, and the four blades are arranged in four corners.

Further, the fixing piece comprises a fixing frame, the fixing frame comprises four fixing sleeves, each fixing sleeve and each main motor are arranged in a one-to-one correspondence mode, the fixing sleeves surround and are arranged on the main motors, and the four fixing sleeves are arranged in four corners; the inner end of the fixed rod is connected with the fixed sleeve.

Further, the linkage type flying device comprises a conductive piece, the conductive piece is installed on the cover body, the conductive piece is in conductive arrangement, the lamp strip is in electrical connection arrangement with the conductive piece, and the conductive piece is in electrical connection arrangement with the power supply piece; the power supply part supplies power to the lamp strip through the conductive part.

Furthermore, the linkage type flying device comprises a plurality of lamp belts, and the clusters or characters projected by the lamp belts are uniformly arranged; and the lamp strips are correspondingly arranged at intervals along the circumferential direction of the cover body.

Furthermore, the linkage type flying device comprises a middle shaft, the middle shaft is longitudinally arranged, two ends of the middle shaft are respectively connected with the cover body, and the middle shaft penetrates through the aircraft; the aircraft comprises at least one flying paddle, and the flying paddle rotates to generate airflow to realize the flight of the aircraft; the middle shaft penetrates through the middle part of the flying paddle.

Compared with the prior art, when the linkage type flying device is used, the aircraft is started to throw the flying device out, the flying device flies in the air stably according to the throwing angle under the action of the aircraft, and the cover body is connected with the aircraft through the fixing piece, so that the aircraft generates air flow, the integral flying is realized, the cover body is prompted to rotate to drive the lamp strip to rotate, at the moment, the lamp strip is in power-on starting arrangement, the light source is projected outwards, a user watches the light source projected by the lamp strip, and the projected light source seen by the user forms patterns or characters based on visual inertia, so that the interest of the flying device is enhanced, the striking performance and the attractiveness are achieved, and the use experience of the user is improved.

Drawings

FIG. 1 is an exploded view of a linkage type flying device provided by the present invention;

FIG. 2 is a schematic perspective view of a linkage type flying device provided by the present invention;

FIG. 3 is a schematic perspective view of the linkage type flying device according to the present invention, showing the engagement between the aircraft and the fixed member;

FIG. 4 is an exploded view of the aircraft and the fixed member of the coupled flying device of the present invention;

FIG. 5 is a schematic bottom view of the aircraft and the fixed member of the coupled flying device provided in the present invention;

FIG. 6 is a schematic perspective view of a fixed member of the coupled flying device provided by the present invention;

FIG. 7 is a schematic perspective view of a first cover member of the linked flying device provided by the present invention;

FIG. 8 is a schematic perspective view of another embodiment of a linked flying device provided by the present invention;

FIG. 9 is a partial perspective view of another embodiment of the linked flying device provided by the utility model.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the utility model and are not intended to limit the utility model.

The following describes the implementation of the present invention in detail with reference to specific embodiments.

The same or similar reference numerals in the drawings of the present embodiment correspond to the same or similar components; in the description of the present invention, it should be understood that if there is an orientation or positional relationship indicated by the terms "upper", "lower", "left", "right", etc. based on the orientation or positional relationship shown in the drawings, it is only for convenience of describing the present invention and simplifying the description, but it is not intended to indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and therefore, the terms describing the positional relationship in the drawings are only used for illustrative purposes and are not to be construed as limiting the present patent, and the specific meaning of the terms may be understood by those skilled in the art according to specific circumstances.

Referring to fig. 1-9, preferred embodiments of the present invention are provided.

The linkage type flight device comprises an aircraft 2, a cover body 1, a fixing part 3 and a lamp strip 4, wherein the fixing part 3 and the aircraft 2 are respectively arranged in the cover body 1, the aircraft 2 is connected with the cover body 1 through the fixing part 3 and is arranged in a linkage manner, the lamp strip 4 is arranged on the cover body 1, and the lamp strip 4 projects a light source which forms patterns or characters based on visual inertia; the aircraft 2 generates airflow to realize flight, and the synchronous driving cover body 1 is rotationally arranged to drive the lamp strip 4 to be rotationally arranged.

Foretell coordinated type flight device, during the use, aircraft 2 starts, throw the flight device out, under the effect of aircraft 2, the flight device is in aerial according to the angle of throwing flight from steady, because the cover body 1 is connected the arrangement through mounting 3 and aircraft 2, consequently, aircraft 2 produces the air current, not only realize holistic flight, and, make the cover body 1 rotatory, it is rotatory to drive lamp area 4, at this moment, lamp area 4 is the circular telegram and starts the arrangement, throw the light source outwards, the user watches the light source that lamp area 4 throws, based on the vision inertia, the projection light source that the user saw forms pattern or characters, the interest of reinforcing flight device, it is striking and attractive to have more simultaneously, improve the experience sense that the user used.

Based on the rotation frequency of the flying device, this frequency may be preset; because the different lamp strips 4 rotate the projection light source, the light source is formed on the retina based on visual inertia and maintains a limited time, and the plurality of lamp strips 4 are matched to realize that the projection light source seen by a user forms patterns or characters.

Linkage type flight device includes the control panel, and the control panel has preset control program, and the control panel is electric connection with aircraft 2 and arranges, realizes that the control panel controls aircraft 2.

The aircraft 2 is coincided with the center of the cover body 1, so that the eccentric effect is avoided, the interference on the self-stability of the flying ball is avoided, and the judgment of the flying track of the whole flying ball is ensured.

The aircraft 2 comprises an acceleration sensor, the acceleration sensor is electrically connected with the control board, the acceleration sensor feeds back signals to the control board, and the control board controls the main motor 23 to start so as to realize the flight control of the flight device.

The flying device comprises a plurality of infrared sensors, and the infrared sensors can be arranged on the cover body 1 and also can be arranged on the aircraft 2 and used for avoiding obstacles or following.

The infrared sensor is arranged in an up-down left-right front-back mode, and different positions are arranged respectively, so that the accuracy of avoiding obstacles or following is improved.

Torsion generated by relative rotation between the cover body 1 and the blades is offset, and downward wind power is generated at the same time, so that the flying device generates lift force to realize flying.

The lamp strip 4 comprises a plurality of lamp beads, each lamp bead is combined to form a pattern or characters, and the patterns or the characters are projected outwards through each lamp bead, so that the projection of the patterns or the characters is realized.

The aircraft protective cover comprises a cover body 1, a fixing piece 3 and an aircraft 2, wherein the cover body 1 is arranged in a spherical shape, the cover body 1 comprises a first cover piece 11 and a second cover piece 12, the first cover piece 11 and the second cover piece 12 are arranged in a buckling mode, the first cover piece 11 and the second cover piece 12 form a cover cavity, and the fixing piece 3 and the aircraft 2 are respectively arranged in the cover cavity; the arrangement of the fixing element 3 and the aircraft 2 is effected.

The aircraft 2 is horizontally arranged, the cover body 1 comprises a cover frame, the cover frame is arranged in an arched arc shape along the direction departing from the aircraft 2, the upper part of the cover frame extends to the top of the first cover piece 11, the lower part of the cover frame extends to the bottom of the second cover piece 12, and the lamp strip 4 is provided with the cover frame; the projection scope in increase lamp area 4 improves and throws the effect, and simultaneously, the projection angle in increase lamp area 4 reduces the limitation of throwing, satisfies multiple projection demand.

The first cover piece 11 comprises a first middle frame which is annularly arranged, the second cover piece 12 comprises a second middle frame which is annularly arranged, and the first middle frame and the second middle frame are arranged in an abutting and overlapping mode to form a buckling part; the fixing piece 3 is connected with the aircraft 2, and the fixing piece 3 is respectively connected with the first middle frame and the second middle frame; the setting of the mounting 3 of being convenient for, simultaneously, under the effect of mounting 3, the lock steadiness of first cover 11 and second cover 12 is strengthened.

The fixing piece 3 comprises two fixing groups which are arranged in a crisscross manner, each fixing group comprises two fixing rods 31, the two fixing rods 31 are horizontally arranged at intervals in a corresponding manner, the inner ends of the fixing rods 31 are connected with the aircraft 2, and the outer ends of the fixing rods 31 are connected with the buckling parts; like this, under the effect of two fixed groups, the fixed effect of the loudness of reinforcing cover body 1 and aircraft 2, when the aircraft 2 of being convenient for flies, the synchronous drive cover body 1 is rotatory.

The dead lever 31 is the horizontal arrangement, and is in the middle part of the cover body 1, like this, when the drive cover body 1 is rotatory, makes the cover body 1 atress more even, improves the rotation stationarity of the cover body 1, and then improves flight device's flight stationarity.

The first cover piece 11 is provided with a first lamp groove which is arranged in a long strip shape, the second cover piece 12 is provided with a second lamp groove which is arranged in a long strip shape, the first lamp groove and the second lamp groove are in butt joint and communicated arrangement, and the lamp strip 4 is tiled to install the first lamp groove and the second lamp groove; like this, the setting in the lamp area 4 of being convenient for, and when the cover body 1 was rotatory, avoid lamp area 4 to cause the skew, improve the setting steadiness in lamp area 4.

The first cover piece 11 is arranged in a hemispherical shape, and the first cover piece 11 is provided with a plurality of hollow openings, so that the airflow can flow conveniently, and the flying device can fly conveniently.

The second cover member 12 is arranged in a hemispherical shape, and the first cover member 11 is provided with a plurality of hollow openings, so that the air flow can flow conveniently, and the flying device can fly conveniently.

The cover body 1 is arranged in a spherical shape, so that the whole stress is more uniform, and the flight stability of the flight device is improved.

The aircraft 2 is positioned in the middle of the cover body 1, so that the overall stress is more uniform, and the flight stability of the flight device is improved.

The aircraft 2 comprises at least one blade 22, a main motor 23, a power supply element and an aircraft shell 21, wherein the blade 22, the main motor 23 and the power supply element are respectively arranged on the aircraft shell 21, the power supply element is used for supplying power, the blade 22 is started to generate airflow to realize flight, and the main motor 23 is used for driving the blade 22 to rotate to generate airflow; in this way, the air flow is generated by the blades 22, and the flight of the flying device is realized.

The aircraft 2 comprises four main motors 23 and four blades 22, wherein each main motor 23 is arranged corresponding to each blade 22 one by one, and the main motors 23 are used for driving the blades 22 to rotate; the four main motors 23 are respectively arranged on the device shell 21, the four main motors 23 are arranged in four corners, and the four blades 22 are arranged in four corners; the advantage of this arrangement is that the flight smoothness of the flying device is improved.

The fixing piece 3 comprises a fixing frame, the fixing frame comprises four fixing sleeves 32, each fixing sleeve 32 is arranged corresponding to each main motor 23 one by one, the fixing sleeves 32 are arranged in a manner of surrounding and sleeving the main motors 23, and the four fixing sleeves 32 are arranged in four corners; the inner end of the fixed rod 31 is connected with the fixed sleeve 32; under the cooperation of the fixed sleeve 32 and the fixed rod 31, the relative fixing effect of the cover body 1 and the aircraft 2 is enhanced, and the aircraft 2 is ensured to drive the cover body 1 to rotate.

The fixing part 3 comprises two reinforcing rods 33, the two reinforcing rods 33 are arranged in a crisscross manner, and two ends of each reinforcing rod 33 are respectively connected with two oppositely arranged fixing sleeves 32; this enhances the stability of the overall structure under the action of the two reinforcing bars 33.

Reinforcing rod 33 is about conflicting and connection arrangement with aircraft 2, the installation of aircraft 2 of realization, and reinforcing aircraft 2's setting steadiness.

Two reinforcing rods 33 are crisscross reinforcing portions that form, and reinforcing portions are corresponding with the middle part of aircraft 2 and arrange, improve flight device's flight stationarity.

The linkage type flying device comprises a conductive piece 5, wherein the conductive piece 5 is provided with a cover body 1, the conductive piece 5 is in conductive arrangement, a lamp strip 4 is in electrical connection arrangement with the conductive piece 5, and the conductive piece 5 is in electrical connection arrangement with a power supply piece; the power supply part supplies power to the lamp strip 4 through the conductive part 5; thus, the lamp strip 4 is powered.

The conductive member 5 includes a conductive sheet having a plurality of guide portions, each of which is circumferentially arranged at intervals; the lamp belts 4 are arranged in one-to-one correspondence with the conductive cloths, and the lamp belts 4 are electrically connected with the conductive cloths; the synchronous power supply to a plurality of lamp belts 4 is realized.

The conductive piece 5 and the aircraft 2 are coaxially arranged, so that the whole stress is more uniform, and the flight stability of the flight device is improved.

The conductive piece 5 comprises a positive guide plate and a negative guide plate, the positive guide plate is arranged at the top of the cover body 1, the positive electrode of the lamp strip 4 is electrically connected with the positive guide plate, the negative guide plate is arranged at the bottom of the cover body 1, and the negative electrode of the lamp strip 4 is electrically connected with the negative guide plate; the circuit layout of the lamp strip 4 is realized.

The positive guide plate and the negative guide plate are coaxially arranged, so that the integral stress is more uniform, and the flight stability of the flight device is improved.

The linkage type flying device comprises a plurality of lamp belts 4, and the balls or characters projected by the lamp belts 4 are arranged in a consistent manner; the lamp belts 4 are correspondingly arranged at intervals along the circumferential direction of the cover body 1; like this, when the cover body 1 is rotatory, drive each lamp area 4 rotatory, improve lamp area 4's the effect of throwing.

The linkage type flying device comprises a middle shaft 6, the middle shaft 6 is longitudinally arranged, two ends of the middle shaft 6 are respectively connected with the cover body 1, and the middle shaft 6 penetrates through the aircraft 2; the aircraft 2 comprises at least one flying paddle 24, and the flying paddle 24 rotates to generate airflow to realize the flying of the aircraft 2; the middle shaft 6 penetrates through the middle part of the flying paddle 24, so that the whole stress is more uniform, and the flying stability of the flying device is improved.

The aircraft 2 comprises two flying paddles 24, the two flying paddles 24 are correspondingly arranged at intervals along the top-down direction, the middle shaft 6 sequentially penetrates through the two flying paddles 24, and the aircraft 2 has enough flying force under the action of the two flying paddles 24.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the utility model, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.

Claims

1. The linkage type flying device is characterized by comprising an aircraft, a cover body, a fixing piece and a lamp strip, wherein the fixing piece and the aircraft are respectively arranged in the cover body; the aircraft generates airflow to realize flight, and synchronously drives the cover body to be in rotary arrangement to drive the lamp strip to be in rotary arrangement.

2. The linked flying device of claim 1, wherein the cover is spherically arranged and comprises a first cover and a second cover, the first cover and the second cover are arranged in a buckling manner, the first cover and the second cover form a cover cavity, and the fixing member and the aircraft are respectively arranged in the cover cavity; the aircraft is the level and arranges, the cover body includes the cover frame, follows to deviate from the aircraft direction, the cover frame is to arch up the arc and arranges, the upper portion of cover frame extends to the top of first cover spare, the lower part of cover frame extends to the bottom of second cover spare, the lamp area is installed the cover frame.

3. The linked flying device of claim 2, wherein the first cover piece comprises a first middle frame, the first middle frame is annularly arranged, the second cover piece comprises a second middle frame, the second middle frame is annularly arranged, and the first middle frame and the second middle frame are arranged in an abutting and overlapping manner to form a buckling part; the mounting with the aircraft is the connection and arranges, just the mounting respectively with first center with the second center is the connection and arranges.

4. The linked flying device of claim 3, wherein said fixed member comprises two fixed groups, said two fixed groups are arranged in a crisscross manner, said fixed group comprises two fixed rods, said two fixed rods are arranged along the horizontal in a spaced-apart correspondence, the inner ends of said fixed rods are arranged in connection with said aircraft, and the outer ends of said fixed rods are arranged in connection with said buckling parts.

5. The linked flying device according to claim 4, wherein the aircraft comprises at least one blade, a main motor, a power supply unit and a device shell, the blade, the main motor and the power supply unit are respectively arranged on the device shell, the power supply unit is used for providing power supply, the blade generates airflow to realize flying, and the main motor is used for driving the blade to rotate to generate airflow.

6. The linked flying device according to claim 5, wherein said aircraft comprises four said main motors and four said blades, each said main motor being arranged in one-to-one correspondence with each said blade, said main motors being adapted to drive said blades to rotate; the four main motors are respectively installed on the device shell, the four main motors are arranged in four corners, and the four blades are arranged in four corners.

7. The linked flying device according to claim 6, wherein said fixed member comprises a fixed frame, said fixed frame comprises four fixed sleeves, each of said fixed sleeves is arranged in one-to-one correspondence with each of said main motors, said fixed sleeves surround and are arranged for sleeving said main motors, and four of said fixed sleeves are arranged in four corners; the inner end of the fixed rod is connected with the fixed sleeve.

8. The linked flying device of claim 7, wherein said linked flying device comprises an electrically conductive member, said electrically conductive member being attached to said cover, said electrically conductive member being in an electrically conductive arrangement, said light strip being in an electrically connected arrangement with said electrically conductive member, said electrically conductive member being in an electrically connected arrangement with said power supply; the power supply part supplies power to the lamp strip through the conductive part.

9. The coupled flying device of any one of claims 1 to 8, wherein said coupled flying device comprises a plurality of light strips, each of said light strips projecting a blob or text in a uniform arrangement; and the lamp strips are correspondingly arranged at intervals along the circumferential direction of the cover body.

10. The linked flying device according to any one of claims 1 to 8, wherein the linked flying device comprises a middle shaft, the middle shaft is arranged longitudinally, two ends of the middle shaft are respectively connected with the cover body, and the middle shaft penetrates through the aircraft; the aircraft comprises at least one flying paddle, and the flying paddle rotates to generate airflow to realize the flight of the aircraft; the middle shaft penetrates through the middle part of the flying paddle.