CN207286685U - A kind of remote control glider with anti-tampering signal head - Google Patents

A kind of remote control glider with anti-tampering signal head Download PDF

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Publication number
CN207286685U
CN207286685U CN201721235115.4U CN201721235115U CN207286685U CN 207286685 U CN207286685 U CN 207286685U CN 201721235115 U CN201721235115 U CN 201721235115U CN 207286685 U CN207286685 U CN 207286685U
Authority
CN
China
Prior art keywords
fuselage
tailplane
head
remote control
wing
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
CN201721235115.4U
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Chinese (zh)
Inventor
刘峻宏
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.)
Henan Tun Lan Technology Co Ltd
Original Assignee
Henan Tun Lan Technology Co Ltd
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 Henan Tun Lan Technology Co Ltd filed Critical Henan Tun Lan Technology Co Ltd
Priority to CN201721235115.4U priority Critical patent/CN207286685U/en
Application granted granted Critical
Publication of CN207286685U publication Critical patent/CN207286685U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

It the utility model is related to aerodone field, more particularly, to a kind of remote control glider with anti-tampering signal head, including, head, fuselage, wing, tail pipe, tailplane and vertical tail, wherein, the head is arranged at fore-body position and is connected with fuselage, and the tail pipe is arranged at fuselage afterbody position and is connected with fuselage, and the vertical tail is arranged on tailplane and is vertically connected with tailplane and connect;The vertical tail is arranged on tailplane and is vertically connected with tailplane and connect;The head top is provided with Kafra fiber layer and CW carbon cloths, the Kafra fiber layer is mutually 45° angle setting with CW carbon cloths, the utility model solves the problems, such as that conventional remote controls aerodone is existing easy to be out of control so as to causing larger cost allowance in play, requirement of the contestant to remote control glider during contest is met, has ensured the normal performance of contestant.

Description

A kind of remote control glider with anti-tampering signal head
Technical field
Aerodone field is the utility model is related to, is glided more particularly, to a kind of remote control with anti-tampering signal head Machine.
Background technology
Model plane have many uses general on the living conditions, and the instrument that we can be using it as amusement and recreation, can also be carried out with it Aerial photography, such as model plane achieve certain effect to building, landscape planning Aerial photography.Navigate due to the use of model airplane machine The a series of advantages such as bat has the cost that shooting condition is unrestricted, very low, convenient and reliable, effect is good, have been used in city road Circuit planning is shot, then by computer composograph, to plan and building offer important evidence.Remote control glider is model plane One kind, is the aerodone being remotely controlled using remote control equipment.Size length can be made with design requirement, currently on the market institute Existing most of remote control gliders are used by people as the instrument of amusement and recreation, such as gliding sports, however, most of The head material of remote control glider is mostly glass fibre or ABS engineering plastics, and this design exists to ensure receiver Signal stabilization and have ignored the contest intensity required by contest and easily during sports it is out of control cause more to be lost ask Topic, can not meet competition competitor to its requirement.
The content of the invention
It is mostly glass fibre or ABS engineering plastics to solve the head material of current most of remote control gliders, is Ensure the signal stabilization of receiver and have ignored the contest intensity required by contest, thus cause more losses, meet The problem of people are not to its requirement, the utility model provides a kind of remote control with anti-tampering signal head and glides Machine, its technical solution are as follows:A kind of remote control glider with anti-tampering signal head, including, head, fuselage, wing, tail Pipe, tailplane and vertical tail, wherein, the head is arranged at fore-body position and is connected with fuselage, described Tail pipe is arranged at fuselage afterbody position and is connected with fuselage, and the wing is arranged at back position and is connected with fuselage Connect.The tailplane is arranged at tail pipe rear positions and is connected with tail pipe, and the vertical tail is arranged at horizontal tail It is vertically connected on the wing and with tailplane and connects;The head top is provided with Kafra fiber layer and CW carbon cloths, and described is triumphant Husband draws fibrous layer to be mutually 45° angle setting with CW carbon cloths;
LV carbon cloths and unidirectional carbon filament are provided with the fuselage, the unidirectional carbon filament is arranged on LV carbon cloths and and LV Carbon cloth is connected to a fixed;
Unidirectional carbon filament is provided with the wing, the unidirectional carbon filament is connected to a fixed with wing, the wing LV carbon cloths are provided with outside circumference, the LV carbon cloths are connected with wing.
The beneficial effects of the utility model are:The utility model scientific structure design, production and processing technology is simple and convenient, profit Head intensity in the presence of solving common remote control glider with technical solutions of the utility model is insufficient for contest needs So as to influence the problem of normally performance of competitor of taking in competition, moreover, the utility model also solves conventional remote controls aerodone at the same time It is existing easy to be out of control so as to the problem of causing larger cost allowance in play, contestant is met to remote control glider Requirement during contest, has ensured the normal performance of contestant.
Brief description of the drawings
Fig. 1 is the structure diagram of the utility model;
Fig. 2 is the utility model handpiece structure schematic diagram;
Figure label is:1- fuselages, 2- heads, 3- tail pipes, 4- wings, 5- tailplanes, 6- vertical tails, 7-LV carbon The unidirectional carbon filament of cloth, 8-, 9-CW carbon cloths, 10- Kafra fiber layers.
Embodiment
Below in conjunction with the accompanying drawings 1 and attached drawing 2 the utility model is further described:
It is mostly glass fibre or ABS engineering plastics to solve the head material of current most of remote control gliders, is Ensure the signal stabilization of receiver and have ignored the contest intensity required by contest, thus cause more losses, meet The problem of people are not to its requirement, the utility model provides a kind of remote control with anti-tampering signal head and glides Machine, its technical solution are as follows:A kind of remote control glider with anti-tampering signal head, including, head 2, fuselage 1, wing 4, Tail pipe 3, tailplane 5 and vertical tail 6, wherein, the head 2 is arranged at 1 forward position of fuselage and is connected with fuselage 1 Connect, the tail pipe 3 is arranged at 1 rear positions of fuselage and is connected with fuselage 1, and the wing 4 is arranged at 1 upper bit of fuselage Put and be connected with fuselage 1.The tailplane 5 is arranged at 3 rear positions of tail pipe and is connected with tail pipe 3, and described hangs down Straight tail 6 is arranged on tailplane 5 and is vertically connected with tailplane 5 and connect;2 top of head is provided with Kev and tows Dimension layer 10 and CW carbon cloths 9, the Kafra fiber layer 10 are mutually 45° angle with CW carbon cloths 9 and are superimposed setting;On the fuselage 1 Be provided with LV carbon cloths 7 and unidirectional carbon filament 8, the unidirectional carbon filament 8 on the fuselage 1 stacked with 7 bilayer of LV carbon cloths on fuselage plus One is pressed on, and is connected with the Kafra fiber layer 10 being arranged on head 2, unidirectional carbon filament is provided with the wing 4 8, the unidirectional carbon filament 8 is connected to a fixed with wing 4, and LV carbon cloths 7 are provided with 4 outside circumference of wing, described LV carbon cloths 7 are connected with wing 4, and the design of said structure makes the utility model not only solve common remote control in use Head intensity in the presence of aerodone, which is insufficient for contest, to be needed so as to influence to take in competition normal the problem of playing of competitor, It is existing easy to be out of control so as to causing larger cost in play that the utility model also solves conventional remote controls aerodone at the same time The problem of loss, meet requirement of the contestant to remote control glider during contest, ensured contestant's It is normal to play, moreover, the structure design of head can ensure that remote control glider receives letter in use in the utility model Number stability, meet competition competitor's control requirement to remote control glider in use.

Claims (3)

1. a kind of remote control glider with anti-tampering signal head, including, head, fuselage, wing, tail pipe, tailplane and Vertical tail, it is characterised in that:The head is arranged at fore-body position and is connected with fuselage, and the tail pipe is set It is connected in fuselage afterbody position and with fuselage, the wing is arranged at back position and is connected with fuselage, described Tailplane be arranged at tail pipe rear positions and be connected with tail pipe, the vertical tail be arranged on tailplane and with Tailplane, which is vertically connected, to be connect;The head top is provided with Kafra fiber layer and CW carbon cloths, the Kafra fiber Layer is mutually 45° angle setting with CW carbon cloths.
A kind of 2. remote control glider with anti-tampering signal head according to claim 1, it is characterised in that:Described LV carbon cloths and unidirectional carbon filament are provided with fuselage, the unidirectional carbon filament is arranged on LV carbon cloths and is fixedly linked with LV carbon cloths Connect.
A kind of 3. remote control glider with anti-tampering signal head according to claim 1, it is characterised in that:Described Unidirectional carbon filament is provided with wing, the unidirectional carbon filament is connected to a fixed with wing, is set in the wing outside circumference There are LV carbon cloths, the LV carbon cloths are connected with wing.
CN201721235115.4U 2017-09-25 2017-09-25 A kind of remote control glider with anti-tampering signal head Expired - Fee Related CN207286685U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721235115.4U CN207286685U (en) 2017-09-25 2017-09-25 A kind of remote control glider with anti-tampering signal head

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721235115.4U CN207286685U (en) 2017-09-25 2017-09-25 A kind of remote control glider with anti-tampering signal head

Publications (1)

Publication Number Publication Date
CN207286685U true CN207286685U (en) 2018-05-01

Family

ID=62439700

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721235115.4U Expired - Fee Related CN207286685U (en) 2017-09-25 2017-09-25 A kind of remote control glider with anti-tampering signal head

Country Status (1)

Country Link
CN (1) CN207286685U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180501

Termination date: 20190925

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