CN103316482A - Lantern capable of flying - Google Patents

Lantern capable of flying Download PDF

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Publication number
CN103316482A
CN103316482A CN2012100747275A CN201210074727A CN103316482A CN 103316482 A CN103316482 A CN 103316482A CN 2012100747275 A CN2012100747275 A CN 2012100747275A CN 201210074727 A CN201210074727 A CN 201210074727A CN 103316482 A CN103316482 A CN 103316482A
Authority
CN
China
Prior art keywords
lantern
outer cover
screw
flying
steering gear
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
CN2012100747275A
Other languages
Chinese (zh)
Inventor
尹业宏
蔡志涛
李桂林
江志鹏
田肖祝
王能深
游颖
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.)
Hubei University of Technology
Original Assignee
Hubei University of Technology
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 Hubei University of Technology filed Critical Hubei University of Technology
Priority to CN2012100747275A priority Critical patent/CN103316482A/en
Publication of CN103316482A publication Critical patent/CN103316482A/en
Pending legal-status Critical Current

Links

Abstract

The invention provides a lantern which is capable of flying and is a lantern flying machine. The lantern comprises an outer cover, propellers, a power device, a steering engine system and the like, wherein the outer casing adopts a net structure, and the shape of the outer cover can be designed to be a lantern shape or other geometric bodies; and the screw propellers, the power device and the steering engine system are arranged in the outer cover. The lantern can stably fly and can fly along wall type barriers, and the problems that propellers of propeller type flying toys are broken when touching barriers, and the flying toys fall off and are damaged are solved; and the lantern has an excellent application prospect in practical application fields such as navigation, geological examination, ultimate rescue, cave dwelling exploration and the like.

Description

The lantern that can fly
Affiliated field
The present invention relates to the lantern that a kind of meeting flies, belong to amusement and recreation area of activities.
Background technology
At present, the rotor craft toy has the advantages such as vertical lift, hovering on the market, and is more and more welcome, but because the unstability of the uncertainty of flight environment of vehicle and operation control, the folding oar occurs easily also simultaneously, falls the problem such as machine.As the amusement and recreation toy, high maintenance cost becomes the financial burden that most of airhogs are difficult to bear after damaging.In the practicality application, such as boat fearness, geological exploration, limit rescue, cave dwelling exploration etc., the drawback that rotor craft itself can't evade is restricting its development.
Summary of the invention
For the deficiency of rotor craft, in line with the principle of maximizing favourable factors and minimizing unfavourable ones, design the lantern that a kind of meeting flies, its novel netted outer cover design, outer cover is built-in with screw, power set and steering gear system, has improved its aloft stability and reliability.
The technical problem that the present invention solves can realize by the following technical solutions:
The lantern that a kind of meeting flies mainly is comprised of outer cover, screw, power set and steering gear system, it is characterized in that: described screw, power set and steering gear system all place in the outer cover; Outer cover is network structure, and its profile is the lantern shape, or the basic body such as prismatic, cylindrical, spherical, or the assembly of basic body.
Described screw is two oar coaxial construction, drives the screw rotation by power set.
The angle of inclination of the changeable screw of described steering gear system and horizontal plane, thus realize the flight of lantern front, rear, left and right.
Described power set and steering gear system are controlled by emitter.
The present invention compared with prior art has the following advantages: the lantern that adopts the meeting of above scheme to fly, can be close to the flight of wall kind barrier, solve the common aircraft of screw class touching barrier folding oar and dropped the problem such as damage, guaranteed its aloft stability and unfailing performance.
Description of drawings
Fig. 1, contour structures schematic diagram of the present invention.
The specific embodiment
Below in conjunction with the drawings and the specific embodiments the present invention is described in further detail.
As shown in Figure 1, the lantern that a kind of meeting flies comprises outer cover 1, screw 2, power set 3 and steering gear system 4, and wherein screw 2, power set 3, steering gear system 4 all are installed on the inside of outer cover 1; Outer cover 1 is netted structure, and its profile is the lantern shape; Screw 2 adopts the layout structure of upper and lower twin screw close coupled type, drives upper screw and the positive and negative rotation of lower screw by power set 3, for whole lantern provides necessary lift; The angle of inclination of steering gear system 4 changeable screws 2 and horizontal plane, thus realize the flight of lantern front, rear, left and right.Power set 3 and steering gear system 4 are controlled by emitter.For strengthening the sight at night, can install light-emitting component additional on the outer cover, such as the LED light emitting diode.
Above-mentioned only is the preferred embodiments of the present invention.Without departing from the spirit and scope of the present invention, all members of doing on this structural principle basis substitute or the apparent structural change of described technical field personnel, all surely belong to fall into protection domain of the present invention.

Claims (4)

1. lantern that can fly, be comprised of outer cover (1), screw (2), power set (3) and steering gear system (4) etc., it is characterized in that: described screw (2), power set (3) and steering gear system (4) all place in the outer cover (1);
Described outer cover (1) reticulates structure, and profile is the lantern shape, or the basic body such as prismatic, cylindrical, spherical, or the assembly of basic body.
2. the lantern that meeting according to claim 1 flies is characterized in that: described screw (2) is two oar coaxial construction, drives screw (2) rotation by power set (3).
3. the lantern that meeting according to claim 1 flies is characterized in that: the angle of inclination of the changeable screw of described steering gear system (4) (2) and horizontal plane, thus realize the flight of lantern front, rear, left and right.
4. the lantern that meeting according to claim 1 flies is characterized in that: described power set (3) and steering gear system (4) are controlled by emitter.
CN2012100747275A 2012-03-21 2012-03-21 Lantern capable of flying Pending CN103316482A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012100747275A CN103316482A (en) 2012-03-21 2012-03-21 Lantern capable of flying

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012100747275A CN103316482A (en) 2012-03-21 2012-03-21 Lantern capable of flying

Publications (1)

Publication Number Publication Date
CN103316482A true CN103316482A (en) 2013-09-25

Family

ID=49185699

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2012100747275A Pending CN103316482A (en) 2012-03-21 2012-03-21 Lantern capable of flying

Country Status (1)

Country Link
CN (1) CN103316482A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106005392A (en) * 2016-06-29 2016-10-12 汇星海科技(天津)有限公司 Spherical aerial vehicle
CN107340782A (en) * 2017-07-03 2017-11-10 深圳市中微信息技术有限公司 A kind of intelligence follows unmanned vehicle and its control method

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1887398A (en) * 2006-07-20 2007-01-03 罗之洪 Steering mechanism assembly of model airplane
DE202008003847U1 (en) * 2008-01-25 2008-07-31 Surkamp, Sven Protective cover for aircraft propellers
CN201151485Y (en) * 2007-12-07 2008-11-19 王学威 Coaxial counter-rotating flying saucer
CN201223729Y (en) * 2008-05-21 2009-04-22 上海市宝山区青少年科学技术指导站 Security protection cover of model helicopter
CN201524420U (en) * 2009-05-26 2010-07-14 罗之洪 Model airplane fully covered with shell
CN101912688A (en) * 2010-08-13 2010-12-15 倪康汉 Linkage for remote control coaxial twin-screw reversal helicopter model
CN202637974U (en) * 2012-03-21 2013-01-02 湖北工业大学 Flying lantern

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1887398A (en) * 2006-07-20 2007-01-03 罗之洪 Steering mechanism assembly of model airplane
CN201151485Y (en) * 2007-12-07 2008-11-19 王学威 Coaxial counter-rotating flying saucer
DE202008003847U1 (en) * 2008-01-25 2008-07-31 Surkamp, Sven Protective cover for aircraft propellers
CN201223729Y (en) * 2008-05-21 2009-04-22 上海市宝山区青少年科学技术指导站 Security protection cover of model helicopter
CN201524420U (en) * 2009-05-26 2010-07-14 罗之洪 Model airplane fully covered with shell
CN101912688A (en) * 2010-08-13 2010-12-15 倪康汉 Linkage for remote control coaxial twin-screw reversal helicopter model
CN202637974U (en) * 2012-03-21 2013-01-02 湖北工业大学 Flying lantern

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106005392A (en) * 2016-06-29 2016-10-12 汇星海科技(天津)有限公司 Spherical aerial vehicle
CN107340782A (en) * 2017-07-03 2017-11-10 深圳市中微信息技术有限公司 A kind of intelligence follows unmanned vehicle and its control method

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Legal Events

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20130925