CN206700755U - A kind of model of an airplane - Google Patents
A kind of model of an airplane Download PDFInfo
- Publication number
- CN206700755U CN206700755U CN201720350066.2U CN201720350066U CN206700755U CN 206700755 U CN206700755 U CN 206700755U CN 201720350066 U CN201720350066 U CN 201720350066U CN 206700755 U CN206700755 U CN 206700755U
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- CN
- China
- Prior art keywords
- model
- cylindrical sleeve
- cylindrical
- airplane
- 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.)
- Expired - Fee Related
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Abstract
It the utility model is related to a kind of model of an airplane, including model of an airplane body, cylindrical loop bar is installed in model of an airplane body lower end, cylindrical loop bar is slidably mounted in cylindrical sleeve, and the outside of cylindrical sleeve is provided with release handle, the release handle is used to adjust height of the cylindrical loop bar in cylindrical sleeve, cylindrical sleeve is arranged in the cylindrical groove of support base, and interference fit is provided with bearing in support base, cylindrical sleeve passes through the inner ring of bearing, gear-box is provided with outside cylindrical sleeve, driving gear and driven gear are installed in the gear-box, driven gear is arranged on cylindrical sleeve, driving gear and driven gear engaged transmission, and rotary shaft is installed on driving gear, rotary shaft is arranged in rotary electric machine, and rotary electric machine is arranged on the outside of the support base.On the one hand the utility model is capable of the regulation of implementation model aircraft body height, on the other hand allow model of an airplane body to be rotated.
Description
Technical field
It the utility model is related to model aircraft technical field, more particularly to a kind of model of an airplane.
Background technology
Model aircraft is different from the model of an airplane, and model aircraft is normally only used for decorating, shown, it is not possible to fly, be with
The model that aircraft reduces by a certain percentage for image.And the model of an airplane refers to fly and can be realized by modes such as remote controls
A kind of toy of control to aircraft.
Static model aircraft material has a variety of, has metal, plastics, resin, fiberglass etc., is proportionally also classified into more than 10 lis
Rice, more than 20 centimetres, more than 30 centimetres, more than 40 centimetres, until the model more than one meter.Prominent domestic has, destroy -10 model aircrafts, destroy -
15 carrier-borne aircraft models, -20 model aircrafts are destroyed, -11/ is destroyed and destroys -11B model aircrafts etc..
Dynamic airplane model also has a variety of, and main making material is：EPP foam, EPO foams, KT sheet material matter etc..Dynamic flies
Machine model can fly, predominantly telecontrolled aircraft model, by artificially passing through remote control control heading and speed.Flying power
Typically realized by battery or gasoline.
Model aircraft is applied to popularization exhibitions at present, but static model aircraft of the prior art be highly not easy into
Row regulation, can not also realize rotation, can not be adjusted according to different needs.
Utility model content
The purpose of this utility model is for overcome the deficiencies in the prior art, there is provided a kind of model of an airplane.
The utility model is to be achieved through the following technical solutions：
A kind of model of an airplane, including model of an airplane body, cylindrical shroud is installed in described model of an airplane body lower end
Bar, described cylindrical loop bar is slidably mounted in cylindrical sleeve, and the outside of described cylindrical sleeve is provided with tune
Handle is saved, the release handle is used to adjust height of the cylindrical loop bar in cylindrical sleeve, and described cylindrical sleeve is arranged on
In the cylindrical groove of support base, and interference fit is provided with bearing in described support base, and described cylindrical sleeve passes through
The inner ring of bearing, gear-box is provided with outside described cylindrical sleeve, be provided with the gear-box driving gear and
Driven gear, described driven gear are arranged on cylindrical sleeve, driving gear and driven gear engaged transmission, and actively
Rotary shaft is installed, rotary shaft is arranged in rotary electric machine, and described rotary electric machine is arranged on the support base on gear
Outside.
Further, described model of an airplane body includes fuselage, two wings installed in the fuselage both sides, is located at
The head of the front fuselage, the propeller positioned at the head front end, the tail installed in the fuselage tail end.
Further, the modulus ratio of the driving gear and driven gear is 1: 1.
Compared with prior art, the beneficial effects of the utility model are：The utility model when in use, by being provided with
Release handle, it is easy to adjust height of the cylindrical loop bar in cylindrical sleeve, so as to adjust the height of model of an airplane body,
Driving gear is driven to rotate by rotary electric machine, driving gear and driven gear engaged transmission, so as to drive driven gear to rotate,
Driven gear drives cylindrical sleeve to rotate, and can so realize that whole model of an airplane body is rotated.The utility model one
Aspect is capable of the regulation of implementation model aircraft body height, on the other hand allows model of an airplane body to be rotated, is so easy to learn
Life is observed, and improves the enjoyment of student.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, below in conjunction with accompanying drawing and implementation
Example, the utility model is further elaborated.It should be appreciated that specific embodiment described herein is only explaining
The utility model, it is not used to limit the utility model.
Referring to Fig. 1, Fig. 1 is structural representation of the present utility model.
A kind of described model of an airplane, including model of an airplane body 1, described model of an airplane body 1 include fuselage 21, peace
Two wings 22 mounted in the both sides of fuselage 21, the head 23 positioned at the front end of fuselage 21, positioned at the front end of head 23
Propeller 24, the tail 25 installed in the tail end of fuselage 21.
Cylindrical loop bar 2 is installed in the described lower end of model of an airplane body 1, described cylindrical loop bar 2 is slidably installed
In cylindrical sleeve 3, and release handle 4 is provided with the outside of described cylindrical sleeve 3, the release handle 4 is used to adjust
Height of the cylindrical loop bar 2 in cylindrical sleeve 3, described cylindrical sleeve 3 are arranged in the cylindrical groove 6 of support base 5,
And interference fit is provided with bearing 7 in described support base 5, described cylindrical sleeve 3 passes through the inner ring of bearing 7, in institute
Gear-box 8 is provided with outside the cylindrical sleeve 3 stated, driving gear 9 and driven gear 10 are installed in the gear-box 8,
Described driven gear 10 is arranged on cylindrical sleeve 3, driving gear 9 and the engaged transmission of driven gear 10, and in driving tooth
Rotary shaft 11 is installed, rotary shaft 11 is arranged in rotary electric machine 12, and described rotary electric machine 12 is arranged on the branch on wheel 9
Support the outside of seat 5.
In the present embodiment：The modulus ratio of the driving gear 9 and driven gear 10 is 1: 1.
The utility model when in use, by being provided with release handle 4, is easy to adjust cylindrical loop bar 2 in cylindrical sleeve 3
Interior height, so as to adjust the height of model of an airplane body 1, driving gear 9 is driven to rotate by rotary electric machine 12, actively
Gear 9 and the engaged transmission of driven gear 10, so as to drive driven gear 9 to rotate, driven gear 9 drives cylindrical sleeve 3 to rotate,
It can so realize that whole model of an airplane body 1 is rotated.The utility model on the one hand can implementation model aircraft body 1 it is high
The regulation of degree, model of an airplane body 1 is on the other hand allowed to be rotated.
In description of the present utility model, unless otherwise clearly defined and limited, term " installation ", " connected ", " company
Connect " it should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integrally；It can be direct phase
Even, it can also be indirectly connected by intermediary, can be that the connection of two element internals or the interaction of two elements are closed
System.For the ordinary skill in the art, it can understand that above-mentioned term is specific in the utility model with concrete condition
Implication.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
All any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (3)
1. a kind of model of an airplane, including model of an airplane body (1), it is characterised in that：In described model of an airplane body (1) lower end
Cylindrical loop bar (2) is installed, described cylindrical loop bar (2) is slidably mounted in cylindrical sleeve (3), and in described circle
The outside of cylindrical sleeve (3) is provided with release handle (4), and the release handle (4) is used to adjust cylindrical loop bar (2) in cylindrical shroud
Height in cylinder (3), described cylindrical sleeve (3) are arranged in the cylindrical groove (6) of support base (5), and in described branch
Interference fit is provided with bearing (7) in support seat (5), and described cylindrical sleeve (3) passes through the inner ring of bearing (7), described
Gear-box (8) is provided with outside cylindrical sleeve (3), driving gear (9) and driven gear are installed in the gear-box (8)
(10), described driven gear (10) is arranged on cylindrical sleeve (3), and driving gear (9) and driven gear (10) engagement pass
It is dynamic, and rotary shaft (11) is installed on driving gear (9), rotary shaft (11) is arranged in rotary electric machine (12), and described
Rotary electric machine (12) is arranged on the outside of the support base (5).
A kind of 2. model of an airplane according to claim 1, it is characterised in that：Described model of an airplane body (1) includes machine
Body (21), two wings (22) installed in the fuselage (21) both sides, the head (23) positioned at the fuselage (21) front end, position
Propeller (24) in the head (23) front end, the tail (25) installed in the fuselage (21) tail end.
A kind of 3. model of an airplane according to claim 1, it is characterised in that：The driving gear (9) and driven gear
(10) modulus ratio is 1: 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720350066.2U CN206700755U (en) | 2017-04-05 | 2017-04-05 | A kind of model of an airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720350066.2U CN206700755U (en) | 2017-04-05 | 2017-04-05 | A kind of model of an airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206700755U true CN206700755U (en) | 2017-12-05 |
Family
ID=60468965
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720350066.2U Expired - Fee Related CN206700755U (en) | 2017-04-05 | 2017-04-05 | A kind of model of an airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206700755U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110624255A (en) * | 2019-09-26 | 2019-12-31 | 刘沁沁 | Aircraft model rotation display device based on airflow suspension |
-
2017
- 2017-04-05 CN CN201720350066.2U patent/CN206700755U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110624255A (en) * | 2019-09-26 | 2019-12-31 | 刘沁沁 | Aircraft model rotation display device based on airflow suspension |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171205 Termination date: 20190405 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |