CN107715467A - A kind of UFO aircraft - Google Patents
A kind of UFO aircraft Download PDFInfo
- Publication number
- CN107715467A CN107715467A CN201711211097.0A CN201711211097A CN107715467A CN 107715467 A CN107715467 A CN 107715467A CN 201711211097 A CN201711211097 A CN 201711211097A CN 107715467 A CN107715467 A CN 107715467A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- motor
- ufo
- transmitting module
- radio receiving
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000008859 change Effects 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 6
- 238000013461 design Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 238000011161 development Methods 0.000 description 3
- 240000002836 Ipomoea tricolor Species 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 230000033228 biological regulation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H29/00—Drive mechanisms for toys in general
- A63H29/22—Electric drives
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H30/00—Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
- A63H30/02—Electrical arrangements
- A63H30/04—Electrical arrangements using wireless transmission
Abstract
The present invention relates to toy aircraft technical field, especially a kind of UFO aircraft, including aircraft and remote control, first motor is arranged on the center upper end of mounting bracket, second motor is arranged on the center lower end of mounting bracket, mounting bracket is additionally provided with control board and driving power, first motor and the second motor are all connected with control board, control board sets the first radio receiving transmitting module, the second radio receiving transmitting module is provided with the remote control, the first radio receiving transmitting module is connected with the second radio receiving transmitting module.Beneficial effect of the present invention：The present invention realizes forward-reverse function by servos control baffle plate direction to reach change airflow direction, steering wheel phase reversal controls the turning function that two baffle plates control air-flow to realize aircraft for opposite direction deflection, it is provided with the first blade and the second blade, two layers of oar has bigger lift, more suitable for the low aircraft of motor speed.And motor speed low cost will be lower.
Description
Technical field
The present invention relates to toy aircraft technical field, especially a kind of UFO aircraft.
Background technology
Toy, refer to specialize in the utensil that people plays from the meaning of word, more specific finger specializes in the thing that children play.Play
Tool, since ancient times all by it is believed that be children " playfellow ", with the development in epoch, the material life of people to carrying
Height, toy, which is no longer limited to specialize in children, plays, and toy is adapted to children, is more suitable for young and the elderly.It is to open wisdom
The instrument of skylight, make people's wisdom clever.
Electronic toy be it is a kind of with electronic technology, using electronic component come control action or the various sound and light programs of generation
Action toy.It is caused with the development of electronic technology from electronic toy is the 1950s.Initially simply general
Application electric technology controls the action of toy to claim Electronic Control class with sound, radio wave or light wave on the basis of electronic toy
Toy.
Plus the influence of the Factors on Human such as animation in recent years, film, the development space of toy is really wide.Specifically we
Graduation project main purpose be exactly to design the UFO aircraft of a science fiction, can be with so that meet pursuit of the people to material
Enjoy animation and the enjoyment of toy that film is derived.
UFO shape is plate, therefore is called flying saucer.UFO (body) or flying object unconfirmed (body)
(Unidentified flying object, abbreviation：UFO), not clear origin, uncertain property are referred to, floating and flight are on high
Object.As long as it is that the aerial object that confirmation is not seen or can not recognized in witness's eye is referred to as UFO to mean, Taiwan is referred to as
It is deep and remote floating, such as poly-bag, kite etc.Some believe that it is the spaceship from other celestial bodies, and some people then think that UFO belongs to
Natural phenomena.
The 1940s, U.S. overhead find disk like flying object, and newspaper at that time is referred to as " flying saucer ", and this is
The beginning of the contemporary interest to UFO, later people are conceived to UFO report all over the world, but so far still
Do not find to allow scientific circles are generally accepted to illustrate their evidences from alien civilization.Some UFO photos are through expert
Fraud is accredited as, some is considered as then ball lightning or other natural phenomenas, but has part to find according to existing science all the time
Knowledge is without method interpretation, it may be possible to the following new construable phenomenon of scientific knowledge.
This high-tech flying body, the curious object with research of the mankind always is, UFO moulding is used for aircraft
On, novel in design unique, using soft and graceful circle, existing modern sense, following sense, and can allow people to see that generation is a kind of wrong at a distance
Feel, think and see what genuine UFO occurred.UFO moulding is plus remotely-piloted vehicle this intention, it is believed that can attract many teenagers with
And science fiction fan is liked.
Therefore, it is necessary to propose a kind of UFO aircraft for above mentioned problem.
The content of the invention
The present invention seeks to overcome deficiency of the prior art, there is provided a kind of UFO aircraft.
In order to solve the above-mentioned technical problem, the present invention is to be achieved through the following technical solutions：
A kind of UFO aircraft, including aircraft and remote control, the aircraft include mounting bracket, the first case, second
Case, the first motor and the second motor, the mounting bracket are clamped between the first case and the second case, and described the
One motor is arranged on the center upper end of mounting bracket, and second motor is arranged on the centre bit of mounting bracket
Lower end is put, the mounting bracket is additionally provided with control board and driving power, and the driving power is respectively control board
Power supply is provided with the first motor and the second motor, first motor and the second motor are all connected with controlling
Circuit board, the control board set the first radio receiving transmitting module, the second radio receiving transmitting module are provided with the remote control,
First radio receiving transmitting module is connected with the second radio receiving transmitting module.
Preferably, the centre position of the upper end of first case is provided with the first suction hole, first case it is upper
End ring week, portion was provided with the second suction hole of several annular spreads.
Preferably, the centre position of the lower end of second case is provided with first row stomata.
Preferably, first motor is connected with the first blade by first rotating shaft.
Preferably, second motor is connected with the second blade by the second rotating shaft.
Preferably, the control board is also associated with steering wheel and section board.
Preferably, the steering wheel and section board are arranged in mounting bracket.
Preferably, first radio receiving transmitting module is 2.4GHz6 channel receivers.
Preferably, the remote control is provided with release handle, forward-reverse release handle and left rotation and right rotation release handle up and down.
Beneficial effect of the present invention：After the present invention reaches change airflow direction realization advance by servos control baffle plate direction
Function is moved back, steering wheel phase reversal controls two baffle plates to realize the turning function of aircraft for opposite direction deflection control air-flow, is provided with
First blade and the second blade, two layers of oar has bigger lift, more suitable for the low aircraft of motor speed.And motor speed is low
Cost will be lower.
Design, concrete structure and the caused technique effect of the present invention are described further below with reference to accompanying drawing, with
It is fully understood from the purpose of the present invention, feature and effect.
Brief description of the drawings
Fig. 1 is the structure chart of the present invention；
Fig. 2 is the upward view of the present invention；
Fig. 3 is the first motor and the second motor connection diagram of the present invention.
Embodiment
Embodiments of the invention are described in detail below in conjunction with accompanying drawing, but the present invention can be defined by the claims
Implement with the multitude of different ways of covering.
Such as Fig. 1 and with reference to shown in Fig. 2 and Fig. 3, a kind of UFO aircraft, including aircraft and remote control, the aircraft bag
Include mounting bracket 6, the first case 2, the second case 1, the first motor 7 and the second motor 9, the mounting bracket clamping
Between first case 2 and the second case 1, first motor 7 is arranged on the center upper end of mounting bracket 6, described
Second motor 9 be arranged on mounting bracket 6 center lower end, the mounting bracket 6 be additionally provided with control board and
Driving power, the driving power are respectively that control board and the first motor 7 and the second motor 9 provide power supply,
The motor 9 of first motor 7 and second is all connected with control board, and the control board sets first wirelessly to receive
Module is sent out, the second radio receiving transmitting module, first radio receiving transmitting module and the second wireless receiving and dispatching are provided with the remote control
Module connects.
Further, the centre position of the upper end of first case 2 is provided with the first suction hole 3, first case 2
Top ring week portion be provided with the second suction hole 4 of several annular spreads, the interposition of the lower end of second case 1 installs
It is equipped with first row stomata 5.
Wherein, first motor 7 is connected with the first blade 8 by first rotating shaft, and second motor 9 is logical
Cross the second rotating shaft and be connected with the second blade 10.
In addition, the control board is also associated with steering wheel and section board, the steering wheel and section board are arranged at installation
On support 6.
Wherein, first radio receiving transmitting module is 2.4GHz6 channel receivers, and the remote control is provided with regulation up and down
Handle, forward-reverse release handle and left rotation and right rotation release handle.
LED Color-changing lamps distinguish the direction of head, and coaxial motor disposing way, a pair of positive and negative slurries cause motor driven slurry
Caused torsion is offset, and produces enough lift so that aircraft vertical lifts, while can reach an equalising torque, can
Accomplish hovering, while aircraft will not be caused to produce the phenomenon of spin.
Due to no tail-rotor, close coupled type aircraft eliminates tail rotor failure hidden danger existing for single-rotor helicopter and flown
The potential faults of the middle tail-rotor transmission mechanism caused by tail vibration of beam and deformation, so as to improve the survival rate of aircraft.
Add the winged control with Gyroscopic stabilization so that it eliminates rotation problem caused by the speed discrepancy of two motors, simultaneously
Add and fly control so that operation is more simple, safety.
The present invention is changed airflow direction and realizes forward-reverse function by servos control baffle plate direction to reach, and steering wheel is opposite
Turn the turning function for controlling two baffle plates to realize aircraft for opposite direction deflection control air-flow, be provided with the first blade and the second oar
Leaf, two layers of oar has bigger lift, more suitable for the low aircraft of motor speed.And motor speed low cost will be lower.
Preferred embodiment of the invention described in detail above.It should be appreciated that one of ordinary skill in the art without
Creative work can is needed to make many modifications and variations according to the design of the present invention.Therefore, all technologies in the art
Personnel are available by logical analysis, reasoning, or a limited experiment on the basis of existing technology under this invention's idea
Technical scheme, all should be in the protection domain being defined in the patent claims.
Claims (9)
- A kind of 1. UFO aircraft, it is characterised in that：Including aircraft and remote control, the aircraft includes mounting bracket, first Case, the second case, the first motor and the second motor, the mounting bracket clamp the first case and the second case it Between, first motor is arranged on the center upper end of mounting bracket, and second motor is arranged on installation branch The center lower end of frame, the mounting bracket are additionally provided with control board and driving power, and the driving power is respectively Control board and the first motor and the second motor provide power supply, first motor and the second motor Control board is all connected with, the control board sets the first radio receiving transmitting module, the second nothing is provided with the remote control Line transceiver module, first radio receiving transmitting module are connected with the second radio receiving transmitting module.
- A kind of 2. UFO aircraft as claimed in claim 1, it is characterised in that：The centre position of the upper end of first case The first suction hole is provided with, the top ring week portion of first case is provided with the second suction hole of several annular spreads.
- A kind of 3. UFO aircraft as claimed in claim 1, it is characterised in that：The centre position of the lower end of second case It is provided with first row stomata.
- A kind of 4. UFO aircraft as claimed in claim 1, it is characterised in that：First motor passes through first rotating shaft It is connected with the first blade.
- A kind of 5. UFO aircraft as claimed in claim 1, it is characterised in that：Second motor passes through the second rotating shaft It is connected with the second blade.
- A kind of 6. UFO aircraft as claimed in claim 1, it is characterised in that：The control board be also associated with steering wheel and Section board.
- A kind of 7. UFO aircraft as claimed in claim 6, it is characterised in that：The steering wheel and section board are arranged at installation On support.
- A kind of 8. UFO aircraft as claimed in claim 1, it is characterised in that：First radio receiving transmitting module is 2.4GHz6 Channel receiver.
- A kind of 9. UFO aircraft as claimed in claim 1, it is characterised in that：The remote control is provided with release handle, preceding up and down Enter to retreat release handle and left rotation and right rotation release handle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711211097.0A CN107715467A (en) | 2017-11-28 | 2017-11-28 | A kind of UFO aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711211097.0A CN107715467A (en) | 2017-11-28 | 2017-11-28 | A kind of UFO aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107715467A true CN107715467A (en) | 2018-02-23 |
Family
ID=61218624
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711211097.0A Pending CN107715467A (en) | 2017-11-28 | 2017-11-28 | A kind of UFO aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107715467A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040129827A1 (en) * | 2002-07-26 | 2004-07-08 | C.R.F. Societa Consortile Per Azioni | VTOL aircraft |
| CN2708977Y (en) * | 2004-06-03 | 2005-07-13 | 杨良杰 | Remote controlled flying saucer toy |
| CN201086824Y (en) * | 2007-07-24 | 2008-07-16 | 沈阳航空工业学院 | Dish shaped aircraft |
| CN101708369A (en) * | 2009-12-04 | 2010-05-19 | 许岳煌 | Aircraft toy |
| CN202593856U (en) * | 2012-01-14 | 2012-12-12 | 河南科技大学 | Triphibian saucer-shaped unmanned aircraft |
| CN103072690A (en) * | 2013-01-23 | 2013-05-01 | 中国航空工业空气动力研究院 | Single-ducted coaxial rotor/propeller saucer-shaped aircraft |
| KR20190106444A (en) * | 2018-03-09 | 2019-09-18 | 허동석 | Toy Rocket |
-
2017
- 2017-11-28 CN CN201711211097.0A patent/CN107715467A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040129827A1 (en) * | 2002-07-26 | 2004-07-08 | C.R.F. Societa Consortile Per Azioni | VTOL aircraft |
| CN2708977Y (en) * | 2004-06-03 | 2005-07-13 | 杨良杰 | Remote controlled flying saucer toy |
| CN201086824Y (en) * | 2007-07-24 | 2008-07-16 | 沈阳航空工业学院 | Dish shaped aircraft |
| CN101708369A (en) * | 2009-12-04 | 2010-05-19 | 许岳煌 | Aircraft toy |
| CN202593856U (en) * | 2012-01-14 | 2012-12-12 | 河南科技大学 | Triphibian saucer-shaped unmanned aircraft |
| CN103072690A (en) * | 2013-01-23 | 2013-05-01 | 中国航空工业空气动力研究院 | Single-ducted coaxial rotor/propeller saucer-shaped aircraft |
| KR20190106444A (en) * | 2018-03-09 | 2019-09-18 | 허동석 | Toy Rocket |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180223 |