CN205287614U - Stationary vane model aeroplane and model ship - Google Patents
Stationary vane model aeroplane and model ship Download PDFInfo
- Publication number
- CN205287614U CN205287614U CN201620022477.4U CN201620022477U CN205287614U CN 205287614 U CN205287614 U CN 205287614U CN 201620022477 U CN201620022477 U CN 201620022477U CN 205287614 U CN205287614 U CN 205287614U
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- model
- fuselage
- utility
- fins
- empennages
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Abstract
The utility model discloses a stationary vane model aeroplane and model ship, including fuselage, aircraft nose and two fins, the long 68.5cm of fuselage, span 50cm, two fins install in the rear of fuselage, the external diameter distance of being close to between two fins of tail one end be 11.53cm, the external diameter distance of being close to between two fins of aircraft nose one end is 12.27cm, fin width 1cm, fuselage and aircraft nose between install the connecting plate, the angle of connecting plate and fuselage bottom be 8 degrees. The utility model discloses an optimize the width of fuselage and abdominal streamline, the two vertical tail front and back installations of adjustment, improved the lift when model aeroplane and model ship take off, reduced relative energy consumption to make the ability reinforcing that aircraft automatic correction flight gesture is unusual, flight performance is more stable.
Description
Technical field
This utility model relates to a kind of model, particularly relates to a kind of fixed-wing model plane.
Background technology
Common fixed-wing model plane have that flying quality is not good, energy consumption is big, easy stall, and these are all exaggerated model plane manipulation difficulty and the probability that causes model plane surprisingly to be damaged increases.
The utility model discloses a kind of low energy consumption, the model plane that flying quality is stable.
Utility model content
The fixed-wing model plane that the technical problems to be solved in the utility model is to provide a kind of low energy consumption, flying quality is stable.
In order to solve above-mentioned technical problem, the technical solution adopted in the utility model is, a kind of fixed-wing model plane, including fuselage, head and two empennages, it is characterised in that, the long 68.5cm of described fuselage, span 50cm, two described empennages are installed on the rear of fuselage, and the external diameter distance between two empennages of tail one end is 11.53cm, external diameter distance between two empennages of head one end is 12.27cm, empennage width 1cm; The angle being provided with connecting plate, described connecting plate and fuselage bottom between described fuselage and head is 8 degree.
Above-described fixed-wing model plane, described fuselage, head and two empennages are using polypropylene expanded plate as installation material.
This utility model has the advantage that
This utility model, by optimizing the streamline of fuselage and abdominal part, adjusting the width installed before and after double; two vertical tail, improves lift when model plane take off, and reduces relative energy consumption, and makes aircraft automatically revise the ability enhancing that flight attitude is abnormal, and flying quality is more stable.
Accompanying drawing explanation
Below in conjunction with the drawings and specific embodiments, the utility model is described in more detail.
Fig. 1 is front view of the present utility model.
Fig. 2 is top view of the present utility model.
Detailed description of the invention
This utility model embodiment, the structure of a kind of fixed-wing model plane is as depicted in figs. 1 and 2, including fuselage and two empennages, it is characterized in that, the described long 68.5cm of fuselage 1, span 50cm, two described empennages 2 are installed on the rear of fuselage, external diameter distance between two empennages 2 of tail one end is 11.53cm, and the external diameter distance between two empennages 2 of head one end is 12.27cm, the wide 1cm of empennage 2; The angle being provided with connecting plate 4, described connecting plate and fuselage bottom between described fuselage 1 and head 3 is 8 degree.
Above-described fixed-wing model plane, described fuselage 1 and empennage 2 using polypropylene expanded plate as installation material.
The above; it is only this utility model preferably detailed description of the invention; but protection domain of the present utility model is not limited thereto; any those familiar with the art is in the technical scope that this utility model discloses; it is equal to replacement according to the technical solution of the utility model and inventive concept thereof or is changed, all should be encompassed within protection domain of the present utility model.
Claims (2)
1. fixed-wing model plane, including fuselage, head and two empennages, it is characterized in that, the long 68.5cm of described fuselage, span 50cm, two described empennages are installed on the rear of fuselage, and the external diameter distance between two empennages of tail one end is 11.53cm, external diameter distance between two empennages of head one end is 12.27cm, empennage width 1cm; The angle being provided with connecting plate, described connecting plate and fuselage bottom between described fuselage and head is 8 degree.
2. fixed-wing model plane according to claim 1, it is characterised in that described fuselage, head and two empennages are using polypropylene expanded plate as installation material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620022477.4U CN205287614U (en) | 2016-01-12 | 2016-01-12 | Stationary vane model aeroplane and model ship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620022477.4U CN205287614U (en) | 2016-01-12 | 2016-01-12 | Stationary vane model aeroplane and model ship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205287614U true CN205287614U (en) | 2016-06-08 |
Family
ID=56475633
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620022477.4U Expired - Fee Related CN205287614U (en) | 2016-01-12 | 2016-01-12 | Stationary vane model aeroplane and model ship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205287614U (en) |
-
2016
- 2016-01-12 CN CN201620022477.4U patent/CN205287614U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160608 Termination date: 20180112 |