CN2566920Y - Improved structure of flying disc - Google Patents

Improved structure of flying disc Download PDF

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Publication number
CN2566920Y
CN2566920Y CN 02237840 CN02237840U CN2566920Y CN 2566920 Y CN2566920 Y CN 2566920Y CN 02237840 CN02237840 CN 02237840 CN 02237840 U CN02237840 U CN 02237840U CN 2566920 Y CN2566920 Y CN 2566920Y
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CN
China
Prior art keywords
seat
luminous
lower cover
luminescence
circuit board
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN 02237840
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Chinese (zh)
Inventor
黄一鏗
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Huang Zhengfu
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN 02237840 priority Critical patent/CN2566920Y/en
Application granted granted Critical
Publication of CN2566920Y publication Critical patent/CN2566920Y/en
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Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to an improvement of a structure of an aerocraft, which comprises a circular disk body, wherein, the position of a shaft center is provided with a nested groove, and the inner side surface of the nested groove is provided with a plurality of circular holes to cause convex blocks of a luminescence seat to be clamped on the circular holes. The luminescence seat is semitransparent, one circumferential surface of the luminescence seat is provided with the convex blocks which are matched with the circular holes of the disk body, the other end of the circumferential surface of the luminescence seat is also provided with a gap which is clamped with a pushing and pulling bevel of a lower cover mutually, and a circuit board is arranged in the luminescence seat. The lower cover is a cover body, which is covered on the luminescence seat, the circumferential surface of the lower cover is provided with a plurality of wheel seats, and the side surface of each wheel seat forms the pushing and pulling bevel which is clamped with the gap of the luminescence seat mutually. A plurality of wheels are pivoted on the wheel seats of the lower cover, the circuit board is arranged in the luminescence seat, and the inner part of the circuit board is provided with a centrifugal switch, a luminescence body, a sounder, etc. Thereby, centrifugal force generated by the whole aerocraft causes the centrifugal switch to be in the state of opening when the aerocraft flies. Thus, the luminescence body and the sounder in the circuit board are actuated, which causes the aerocraft to generate light and sound when the aerocraft flies, and the aerocraft can continue to rotate when the aerocraft falls on the ground. The utility model has multiple variability and rich interest, attracts children's favor, and has the advantages of simple structure and convenient operation and use.

Description

The Flight Vehicle Structure improvement
<one〉technical field:
The utility model provides the improvement of a kind of Flight Vehicle Structure, refer to especially a kind of tool can make aircraft luminous awing, send sound equipment and when dropping down onto ground, can continue turn more voluntarily, belong to the game and body-building utensil.
<two〉background technology:
The flying disc of existing a kind of tool luminous efficacy, assembling type by name flies the light flying disc, includes: the flying disc body, for flying to the disk body of aerial generation orbit by delivery mode; Noctilucence bar rod, interior tool chemical substance is rocked or is destroyed interlayer and can impel chemical substance to mix, and produces luminous plastic strip or rod; It is characterized in that: this flying disc body is provided with the strip Baltimore groove cave that cooperates noctilucence bar rod size design, can be assembled or removal in the mode of plant buckle for noctilucence bar rod, but this structure is after long-time the use, because of the chemical substance in the noctilucence bar rod has certain pot-life, often need to eliminate to renew, use inconvenience, and general user is all the child, easily cause the child to eat by mistake, this i.e. the main disappearance of structure for this reason.
The flying toy of another flying disc by name, it has a disk and thin plate, and has down extended a ring by around this plate, and be primarily characterized in that: this plate is provided with a supporting mechanism in bottom center, this supporting mechanism is definite length extended down, and the length of down extending is enclosed height greater than above-mentioned ring; The design that mat is above-mentioned, flying disc is enclosed when fall supporting ground with ring, supporting of energy this supporting mechanism of mat, and make ring enclose unlikely fully and ground fit, but this kind flying disc stops operating when falling to ground, and is little with the flying disc difference of generally commonly using, and only is the effect of flying disc in the use, on function, more do not have a variability, that is difficult the liking of child that attract.
The purpose of this utility model provides a kind of Flight Vehicle Structure improvement, and this flying toy can produce luminous, sounding when flight, and can continue turn more voluntarily when dropping down onto ground, has various variability and abundant interest, attracts liking of child.Simple in structure, easy for operation.
<three〉summary of the invention:
A kind of Flight Vehicle Structure improvement is made of jointly disk body, luminous seat, lower cover, wheel, circuit board etc.This disk body is circular, is formed with fit slot at shaft core position, and fit slot can close for luminous cover for seat; This luminous seat is translucent, can be linked on the fit slot of disk body, is equipped with circuit board and power supply component in the luminous seat, makes its whole tool luminous efficacy; This lower cover is one to cover the lid on luminous seat, establishes several wheel seats on its periphery, and the number wheels are hubbed on the wheel seat of lower cover; This circuit board is contained in the luminous seat, and basic building blocks such as centrifugal switch, illuminator, acoustical generator are arranged in it, and power supply component promptly provides circuit board required power supply; By this, the centrifugal force that whole aircraft is produced when flight makes centrifugal switch be opening, and so illuminator and the acoustical generator in the circuit board is start, and so disk body has the effect of luminous and sounding when flight;
Wherein, disk body is provided with a plurality of circular holes hole at fit slot inner edge face and engages in it for the projection of luminous seat, and luminous seat is provided with the projection that matches with the circular hole hole of disk body on its periphery, luminous seat can be linked on the fit slot of disk body;
Wherein, also be provided with on the periphery of luminous seat to push away and pull out the breach that the inclined-plane engages mutually, and lower cover is formed with pushing away of engaging mutually of the breach of luminous seat at its limit face and pulls out the inclined-plane, and lower cover can be linked on the luminous seat with lower cover;
Wherein, lower cover can be the structure of no wheel seat, and increases a plurality of wheels that are pivoted on the dish seat, and the dish seat is enclosed within down and covers;
Wherein, can set up an air deflector be installed in luminous seat or under cover, have the plural groups arc shaped blade on the air deflector;
Wherein, place, the bottom of lower cover is provided with ball seat, and this ball seat can rotate freely with respect to lower cover, when aircraft integral body falls to ground, because of ball seat and number wheel tool bracing force, can continue turn voluntarily when landing;
Wherein, dish seat is gone up and is articulated the number foot rest, also establishes several ball seats on the end of number foot rest, and ball seat can be had an effect that rotates freely with respect to foot rest;
Wherein, luminous seat power supply component and circuit board can by on be placed in the luminous seat, bottom like this luminous can be closed, also can omit lower cover;
Wherein, all sides of this luminous seat can be empty thoroughly, and luminous seat can be not a transparence, and the light-emitting component on the circuit board also can be appeared by the saturating vacancy of the luminous all sides of seat;
Wherein, this dish seat directly tool push away and pull out the inclined-plane and directly be fastened on luminous the breach.
A kind of Flight Vehicle Structure improvement of the utility model, its advantage is: simple in structure, easily assembled, safe in utilization, low cost of manufacture is manipulated safe ready.This flying toy can produce luminous, sounding when flight, and can continue turn more voluntarily when dropping down onto ground, has various variability and abundant interest, and the attraction child likes having the market competitiveness.
<four〉description of drawings:
Fig. 1 the utility model Flight Vehicle Structure three-dimensional exploded view.
Fig. 2 the utility model Flight Vehicle Structure three-dimensional combination figure.
Fig. 3 the utility model Flight Vehicle Structure semi-section schematic diagram.
Fig. 4 the utility model Flight Vehicle Structure action schematic diagram.
The second embodiment schematic diagram of Fig. 5 the utility model.
The 3rd embodiment schematic diagram of Fig. 6 the utility model.
The 4th embodiment schematic diagram of Fig. 7 the utility model.
The 5th embodiment schematic diagram of Fig. 8 the utility model.
The 6th embodiment schematic diagram of Fig. 9 the utility model.
Another action schematic diagram of Figure 10 the utility model the 5th embodiment.
The replacing disk body schematic diagram of Figure 11 the utility model.
Figure 12 the utility model the 6th embodiment schematic diagram.Number in the figure is as follows: 10 disk bodies, 11 fit slots, 12 circular hole holes, 20 luminous seat 21 projections 22 breach 30 lower covers 31 wheel seats 32 push away and pull out inclined-plane 33 ball seats, 40 wheels, 50 dish seats, 51 foot rests, 52 ball seats, 60 air deflectors, 70 circuit boards
<five〉specific embodiment:
At first, see also shown in Figure 1, the improvement of a kind of Flight Vehicle Structure of the utility model, it mainly includes: a disk body 10 is the disk body of a circle, form a fit slot 11 at shaft core position, and establish in a plurality of circular holes hole 12 is fastened on for the projection 21 of luminous seat 20 at fit slot 11 inner edge faces;
One luminous seat 20 is one translucent, on periphery, establish the projection 21 that matches with the circular hole hole 12 of disk body 10, and hold also to establish on the periphery at other and pull out the breach 22 that inclined-plane 32 engages mutually with pushing away of lower cover 30, be equipped with a circuit board 50 and a power supply component in the luminous seat 20, make it the effect that whole tool is luminous, send sound equipment;
One lower cover 30 is one to cover the lid on luminous seat 20, and several wheel seats 31 are established in Kaohsiung on periphery, and forms with breach 22 mutual the pushing away of engaging of luminous seat 20 at its limit face and to pull out inclined-plane 32;
Number wheel 40 is hubbed on the wheel seat 31 of lower cover 30;
One circuit board 70 is contained in the luminous seat 20, has basic building blocks such as centrifugal switch, illuminator, acoustical generator in it, and power supply component promptly provides circuit board 70 required power supply;
Promptly as shown in Figure 2, the half-sectional view of assembled state promptly as shown in Figure 3 after the entire combination.
Please continue to consult shown in Figure 4, when start, whole aircraft is penetrated to lose the mode of throwing, have several wheels 40 on the number wheel seat 31 because of lower cover 30, when aircraft drop to ground after flight, because of wheel 40 can be had an effect of rotation, aircraft also can continue rotation voluntarily and can produce the characteristic that moves forward when rotated landing, so promptly solve and commonly use flying disc and land the disappearance that promptly stops, this is the advantage of the utility model maximum when flight.
Real novel another characteristics of written or printed documents are: disk body 10 rotation of aloft flying, so when the flight rotation, produce centrifugal force, because of tool circuit boards 70 and centrifugal switch, illuminator and acoustical generator in the luminous seat 20 thereby the centrifugal force that produced make centrifugal switch be opening, so illuminator and the acoustical generator in the circuit board 70 is start, and luminous seat 20 is that tool is translucent, so make aircraft when flight tool luminous and send the effect of sound equipment, have abundant interest.
The novel directly firmly rotation on the ground of fit slot 11 of hand-holdable disk body 10 when playing of this reality in addition, because of disk body 10 bottom tools are counted wheel 40, whole aircraft like this also can change gyro into to be used, and promptly has various variability in the use.
The projection 21 of in addition luminous seat 20 is fastened in the circular hole hole 12 of fit slot 11 of disk body 10, therefore luminous seat 20 can take off rapidly, and after taking off luminous seat 20, disk body 10 also can independently use, disk body 10 is promptly identical with the effect of commonly using flying disc, and this also is another advantage of the utility model.
Please continue to consult shown in Figure 5, be the utility model second embodiment, the structure of lower cover 30 no wheel seats 31, and a plurality of wheels 40 that on a dish seat 50, are pivoted, dish seat 50 is enclosed within on the lower cover 30 again, whole when implementing the also identical effect of tool.
Please continue to consult shown in Figure 6, be the utility model the 3rd embodiment, system sets up an air deflector 60 and is installed on luminous seat 20 or the lower cover 30, because of having the blade of plural groups arc on the air deflector 60, when turn, produce the rising shape during airflow passes air deflector 60, with disk body 10 whole ejections upwards, arc shaped blade design on the air deflector 60 makes disk body 10 because of air deflector 60 events, has and can fly the time higher and more of a specified duration when flight.
Please continue to consult shown in Figure 7, be the utility model the 4th embodiment, the place, bottom that ties up to lower cover 30 establishes a ball seat 33, this ball seat 33 can rotate freely with respect to lower cover 30, when aircraft integral body falls to ground, because of ball seat 33 and number wheel 40 tool bracing forces, make the aircraft whole machine balancing better, and when landing, can continue turn voluntarily.
Please continue to consult shown in Figure 8, be the utility model the 5th embodiment, can on dish seat 50, articulate number foot rest 51, also establish several ball seats 52 on the end of number foot rest 51, ball seat 52 can be had an effect that rotates freely with respect to foot rest 51, and when adding elastomer in start on each pivoting point the tool elastic acting force.
Please continue to consult shown in Figure 9, when aircraft aloft flies, centrifugal force because of disk body 10 rotation generations, foot rest 51 on the dish seat 50 is opened with ball seat 52, when slowly down landing,, make the foot rest 51 and ball seat 52 thereby decline gradually of dish seat 50 because of weakening of centrifugal force, cause is at the elastomeric elastic acting force of each pivoting point, when unlikely foot rest 51 and ball seat 52 integral body of making when descending hang down.
Please continue to consult shown in Figure 10, when disk body 10 falls to ground, because of the foot rest 51 of dish seat 50 is tool support forces with ball seat 52, make the disk body 10 unlikely ground that are fitted in, also can rotate voluntarily because of ball seat 52 after landing, after landing, can rotate by aircraft and operation forward the identical effect of equal tool when implementing again.
Please continue to consult shown in Figure 11, the projection 21 of luminous seat 20 is to be fastened in the circular hole hole l2 of fit slot 11 of disk body 10, therefore disk body 10 can separate rapidly with 20 of luminous seats, so be that replaceable another disk body 13 makes it to have more variability, disk body 10 can be had different colours or a pattern, when recreation, have more rich and the entertaining sense, in addition after luminous seat 20 takes off, the also replaceable circuit board 70 that different illuminators and acoustical generator or tool difference in functionality are housed of circuit board 70 is contained in the luminous seat 20 again, make it the different luminous and sounding effect of tool, have more different interesting, and the adjusting device of can having in its circuit board 70 also can be equipped with thumb-acting switch can manually adjust light-emitting component or acoustical generator start simultaneously or start one only, make it to meet different occasions and use this aircraft, make whole aircraft richer variability in recreation.
Please continue to consult shown in Figure 12, the power supply component of luminous seat 20 and circuit board 70 can by on insert in luminous 20, the bottom of luminous seat 20 like this can be closed, also can omit lower cover 30, and luminous seat 20 all sides can be empty thoroughly, luminous seat 20 can be a transparence, and the light-emitting component on the circuit board 70 also can be appeared by the saturating vacancy of luminous seat 20 all sides, and dish seat 50 or air deflector 60 directly tool push away and pull out the inclined-plane and directly be fastened in luminous 20 the breach 22.
Other what deserves to be mentioned is, the luminous seat 20 and the lower cover 30 that are fastened on the disk body 10 are pulled down, promptly as the flying disc commonly used, can use separately.

Claims (10)

1. a Flight Vehicle Structure improvement is made of jointly disk body, luminous seat, lower cover, wheel, circuit board, it is characterized in that: this disk body is formed with the fit slot that can supply luminous cover for seat to close for circular at shaft core position; The luminous seat of this shape that is translucent can be linked on the fit slot of disk body, is equipped with in the luminous seat to make its integral body have the circuit board and the power supply component of luminous efficacy; This lower cover is one to cover the lid on luminous seat, is provided with wheel seat on its periphery, and this wheel is hubbed on the wheel seat of lower cover; This circuit board is contained in the luminous seat, basic building blocks such as centrifugal switch, illuminator, acoustical generator are arranged in it, and power supply component provides promptly circuit board required power supply.
2. a kind of Flight Vehicle Structure improvement according to claim 1, it is characterized in that: wherein, this disk body is provided with the luminous seat of a plurality of confessions projection at fit slot inner edge face and engages circular hole hole in it, luminous seat is provided with the projection that matches with the circular hole hole of disk body on its periphery, luminous seat can be linked on the fit slot of disk body.
3. a kind of Flight Vehicle Structure improvement according to claim 1, it is characterized in that: wherein, also be provided with on periphery of this luminous seat to push away and pull out the breach that the inclined-plane engages mutually with lower cover, and lower cover is formed with pushing away of engaging mutually of the breach of luminous seat at its limit face and pulls out the inclined-plane, and this lower cover can be linked on the luminous seat.
4. a kind of Flight Vehicle Structure improvement according to claim 1 is characterized in that: wherein, this lower cover is the structure of no wheel seat, and is pivoted with a plurality of wheels on the dish seat, and the dish seat is enclosed within down and covers.
5. a kind of Flight Vehicle Structure improvement according to claim 1 is characterized in that: wherein, can set up an air deflector be installed in luminous seat or under cover, and have the plural groups arc shaped blade on the air deflector.
6. a kind of Flight Vehicle Structure improvement according to claim 1 is characterized in that: wherein, place, the bottom of lower cover is provided with the ball seat that can rotate freely with respect to lower cover.
7. according to claim 1 or 4 described a kind of Flight Vehicle Structure improvement, it is characterized in that: wherein, be articulated with foot rest on this dish seat, also be provided with ball seat on the end of foot rest.
8. a kind of Flight Vehicle Structure improvement according to claim 1 is characterized in that: wherein, luminous seat power supply component and circuit board can by on be placed in the luminous seat, luminous bottom can be closed.
9. a kind of Flight Vehicle Structure improvement according to claim 1 is characterized in that: wherein, all sides of this luminous seat can be empty thoroughly.
10. according to claim 1 or 4 described a kind of Flight Vehicle Structures improvement, it is characterized in that: wherein, this dish seat directly tool pushes away and pulls out the inclined-plane and directly be fastened on luminous the breach.
CN 02237840 2002-06-10 2002-06-10 Improved structure of flying disc Expired - Fee Related CN2566920Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 02237840 CN2566920Y (en) 2002-06-10 2002-06-10 Improved structure of flying disc

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 02237840 CN2566920Y (en) 2002-06-10 2002-06-10 Improved structure of flying disc

Publications (1)

Publication Number Publication Date
CN2566920Y true CN2566920Y (en) 2003-08-20

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Application Number Title Priority Date Filing Date
CN 02237840 Expired - Fee Related CN2566920Y (en) 2002-06-10 2002-06-10 Improved structure of flying disc

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106474750A (en) * 2016-11-30 2017-03-08 威立达数码科技(深圳)有限公司 Flying disc
CN109432724A (en) * 2018-12-13 2019-03-08 福州大学 Novel body building aircraft and its control method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106474750A (en) * 2016-11-30 2017-03-08 威立达数码科技(深圳)有限公司 Flying disc
CN109432724A (en) * 2018-12-13 2019-03-08 福州大学 Novel body building aircraft and its control method

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: HUANG ZHENGFU

Free format text: FORMER OWNER: HUANG YI

Effective date: 20040114

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20040114

Address after: Taichung City in Taiwan Province Road 40 Lane 16 Lane 1

Patentee after: Huang Zhengfu

Address before: Taiwan, China

Patentee before: Huang Yikeng

C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee