CN105561599A - Aviation toy precise positioning system - Google Patents

Aviation toy precise positioning system Download PDF

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Publication number
CN105561599A
CN105561599A CN201410546391.7A CN201410546391A CN105561599A CN 105561599 A CN105561599 A CN 105561599A CN 201410546391 A CN201410546391 A CN 201410546391A CN 105561599 A CN105561599 A CN 105561599A
Authority
CN
China
Prior art keywords
remote control
toy
precise position
position system
aviation
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
Application number
CN201410546391.7A
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Chinese (zh)
Inventor
许美兰
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.)
Individual
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 CN201410546391.7A priority Critical patent/CN105561599A/en
Publication of CN105561599A publication Critical patent/CN105561599A/en
Pending legal-status Critical Current

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Abstract

The invention discloses an aviation toy precise positioning system, which comprises a remote control device and sensing equipment connected with the remote control device, wherein an operation panel is arranged on the remote control device; a liquid crystal display screen is arranged on the operation panel; and a plurality of press buttons are also arranged under the liquid crystal display screen arranged on the operation panel. Various parameters required for controlling a toy aircraft can be set and changed at any time through the plurality of press buttons arranged on the aviation toy precise positioning system; and the parameter change is displayed in real time through the liquid crystal display screen, so that an operator can precisely set self desired parameters. The size of the used sensing equipment is small, so that the shock-resistant performance of the aviation toy precise positioning system is improved.

Description

Aerial toy Precise Position System
Technical field
The present invention relates to a kind of mould aircraft, particularly a kind of positioning control system be arranged in toy aircraft.
Background technology
When toy aircraft is in hover state aloft, be subject to blowing of crosswind sometimes, now the tail vane of toy aircraft will produce the phenomenon offset in the horizontal direction.In order to correct this shift phenomenon, usually the aerial toy Precise Position System that can regulate direction can be installed on the tail vane of toy aircraft.When skew occurs the tail vane of toy aircraft, aerial toy Precise Position System will send corresponding control signal to the tail vane steering wheel in toy aircraft, makes tail vane make the action contrary with offset direction by tail vane steering wheel, thus resists the skew of tail vane.
In prior art, toy aircraft azimuth device be provided with guidance panel, what have does not then have.The operator of toy aircraft cannot the various parameters of setup control toy aircraft flight on the toy aircraft azimuth device not having guidance panel.In addition, the volume of the sensing apparatus that aerial toy Precise Position System is all is also larger, causes the anti-vibration ability of aerial toy Precise Position System to reduce, and also makes its neutral dot characteristics be deteriorated.
Need a kind of aerial toy Precise Position System of improvement to overcome above-mentioned defect for this reason.
Summary of the invention
An object of the present invention is just to provide one can either change various flight parameter as required at any time, the aerial toy Precise Position System that the parameter of setting intuitively can be shown again, provides a kind of aerial toy Precise Position System with good anti-seismic performance simultaneously.
To achieve these goals, aerial toy Precise Position System of the present invention have employed following technical scheme; The sensing apparatus comprising remote control and be connected with remote control, remote control is provided with guidance panel, and guidance panel is provided with a LCDs, and on guidance panel, the below of LCDs is also provided with multiple button.
Beneficial effect of the present invention is just: can be set and change the various flight parameters controlled required for toy aircraft at any time by the multiple buttons on aerial toy Precise Position System, the change of institute's setting parameter is again by real-time the showing of LCDs, and such operator just can accurately set out the parameter oneself wanted; The sensing apparatus volume adopted is very little, thus improves the anti-seismic performance of aerial toy Precise Position System.
Multiple buttons on guidance panel comprise patten transformation button and numerical value change button.Remote control is provided with error amendment interface and afterbody rudder control interface, and aerial toy Precise Position System is connected with the receiving system of toy aircraft with afterbody rudder control interface by error amendment interface.Sensing apparatus is fixed in toy aircraft by double faced adhesive tape.
In another embodiment of the present invention, remote control and sensing apparatus all have employed light metal housing.
Accompanying drawing explanation
Fig. 1 is the planar structure schematic diagram of aerial toy Precise Position System of the present invention.
Detailed description of the invention
Now by reference to the accompanying drawings embodiments of the invention are described.
See Fig. 1, aerial toy Precise Position System of the present invention, for toy aircraft, and be connected with the receiving system in toy aircraft and tail vane steering wheel, the sensing apparatus 33 comprising remote control 22 and be connected with remote control 22, remote control 22 is provided with guidance panel 23, and guidance panel 23 is provided with a LCDs 231, and on guidance panel 23, the below of LCDs 231 is also provided with multiple button 232 and 233.In conjunction with multiple button 232 and 233 and LCDs 231, the operator of toy aircraft can parameter accurately needed for the flight of setup control toy aircraft.
The maximum gauge of sensing apparatus 33 is no more than 30 millimeters, and maximum gauge is no more than 18 millimeters.Such sensing apparatus volume is very little, therefore effectively can improve the anti-seismic performance of aerial toy Precise Position System.
As a preferred embodiment of aerial toy Precise Position System of the present invention, still with reference to figure 1, the LCDs 231 on guidance panel 23 is liquid crystal mesogens display screen.Multiple button 232 and 233 is respectively patten transformation button and numerical value change button.Press patten transformation button 232, LCDs 231 just has the corresponding content of display, the operator of toy aircraft according to the displaying contents on LCDs 231, can select the parameter kind needing setting.After choosing the parameter kind that will set, then press numerical value adjustment strong 233, regulate the size of set parameter values, same, the numerical value change of institute's setting parameter also can be shown by LCDs 231.
In the above embodiment of the present invention, remote control 22 is provided with error amendment interface 222 and afterbody rudder control interface 221, and aerial toy Precise Position System is linked together with the receiving system of toy aircraft by error amendment interface 222 and afterbody rudder control interface 221.Remote control 22 is also established an interface, the tail vane steering wheel of toy aircraft is then provided with the joint that can insert this interface, such remote control 22 just can link together with tail vane steering wheel.
In addition, sensing apparatus 33 is also provided with a joint, remote control 22 is then provided with the interface coordinated with this joint, the joint on sensing apparatus 33 is inserted in the interface on remote control 22, thus makes both be connected.By double faced adhesive tape, sensing apparatus 33 dividend is fixed in toy aircraft, can alleviate the impact of vibration on sensing apparatus of toy aircraft fuselage like this.
In another embodiment of the present invention, the remote control of aerial toy Precise Position System and sensing apparatus all have employed metallic shell, the interference of electromagnetic wave to aerial toy Precise Position System can be reduced like this, to improve the adjusting function of aerial toy Precise Position System.
Above disclosedly be only preferred embodiment of the present invention, certainly can not limit the interest field of the present invention with this, therefore according to the equivalent variations that the present patent application the scope of the claims is done, still belong to the scope that the present invention is contained.

Claims (4)

1. an aerial toy Precise Position System, it is characterized in that: the sensing apparatus comprising remote control and be connected with remote control, described remote control is provided with guidance panel, guidance panel is provided with a LCDs, and on guidance panel, the below of LCDs is also provided with multiple button.
2. according to aerial toy Precise Position System according to claim 1, it is characterized in that: the multiple buttons on described guidance panel comprise patten transformation button and numerical value change button.
3. according to aerial toy Precise Position System according to claim 1, it is characterized in that: described remote control is provided with error amendment interface and afterbody rudder control interface, described aerial toy Precise Position System is connected with the receiving system of toy aircraft with afterbody rudder control interface by error amendment interface.
4. according to aerial toy Precise Position System according to claim 1, it is characterized in that: described remote control and sensing apparatus all have employed light metal housing.
CN201410546391.7A 2014-10-15 2014-10-15 Aviation toy precise positioning system Pending CN105561599A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410546391.7A CN105561599A (en) 2014-10-15 2014-10-15 Aviation toy precise positioning system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410546391.7A CN105561599A (en) 2014-10-15 2014-10-15 Aviation toy precise positioning system

Publications (1)

Publication Number Publication Date
CN105561599A true CN105561599A (en) 2016-05-11

Family

ID=55872568

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410546391.7A Pending CN105561599A (en) 2014-10-15 2014-10-15 Aviation toy precise positioning system

Country Status (1)

Country Link
CN (1) CN105561599A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105771266A (en) * 2014-12-25 2016-07-20 许美兰 Toy plane position accurate control device
CN105797400A (en) * 2014-12-31 2016-07-27 马铿杰 Aviation flight system with strong shake resistance
CN106621384A (en) * 2015-11-04 2017-05-10 许美兰 Aerial toy precise positioning system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105771266A (en) * 2014-12-25 2016-07-20 许美兰 Toy plane position accurate control device
CN105797400A (en) * 2014-12-31 2016-07-27 马铿杰 Aviation flight system with strong shake resistance
CN106621384A (en) * 2015-11-04 2017-05-10 许美兰 Aerial toy precise positioning system

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C06 Publication
PB01 Publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160511

WD01 Invention patent application deemed withdrawn after publication