CN104383691A - Novel paper plane type model airplane aircraft - Google Patents
Novel paper plane type model airplane aircraft Download PDFInfo
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- CN104383691A CN104383691A CN201410617657.2A CN201410617657A CN104383691A CN 104383691 A CN104383691 A CN 104383691A CN 201410617657 A CN201410617657 A CN 201410617657A CN 104383691 A CN104383691 A CN 104383691A
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- aircraft
- novel paper
- type model
- paper plane
- plane type
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Abstract
The invention discloses a novel paper plane type model airplane aircraft, which is characterized by comprising a V-shaped airframe body, wings arranged on two sides of the airframe body, two screw propellers fixed right ahead of the wings, a cover plate covering a V-shaped slot of the airframe body, and pulleys arranged on the lower part of the airframe body, wherein a flight drive mechanism of the aircraft is arranged in the V-shaped slot of the airframe body. The novel paper plane type model airplane aircraft is novel, simple and light in structure, and stable in flying and landing effects.
Description
Technical field
The present invention relates to model plane technical field, particularly relate to a kind of novel structure, light Novel paper aircraft-type aeromodelling aerocraft.
Background technology
In the modern life, the fan of aeromodelling aerocraft gets more and more, but the moulding of aeromodelling aerocraft is similar on the market at present, fully can not meet the demand of airplane hobbyist, therefore need one not affect flight function, the aeromodelling aerocraft that modern design requires can be met again.
Summary of the invention
For solving the problem, the invention provides a kind of Novel paper aircraft-type aeromodelling aerocraft, its novel structure, simply light, flight and landing effect stability.The technical solution used in the present invention is: a kind of Novel paper aircraft-type aeromodelling aerocraft, it is characterized in that: two screws in the wing dead ahead that comprises V-type fuselage body, is arranged at the wing of fuselage both sides, is fixed on, be covered in fuselage body V-type groove above cover plate and be arranged at the pulley of fuselage body bottom, the flight driving mechanism of aircraft is installed in the V-type groove of described fuselage body.
Preferably, the arranged outside baffle plate of described wing, the edge designs in baffle plate front becomes streamlined.This design accords with full hydrodynamics, is conducive to aircraft stabilized flight.
Owing to have employed technique scheme, the present invention has following technique effect: the present invention is novel in design, structure is ingenious, can meet flight requirement, stop, good stability simultaneously during landing by pulley after sliding a segment distance.
Accompanying drawing explanation
Examples of the present invention will be described by way of reference to the accompanying drawings, wherein:
Fig. 1 is stereogram of the present invention;
Fig. 2 is front view of the present invention.
Detailed description of the invention
All features disclosed in this description, or the step in disclosed all methods or process, except mutually exclusive feature and/or step, all can combine by any way.
Arbitrary feature disclosed in this description, unless specifically stated otherwise, all can be replaced by other equivalences or the alternative features with similar object.That is, unless specifically stated otherwise, each feature is an example in a series of equivalence or similar characteristics.
A kind of Novel paper aircraft-type aeromodelling aerocraft as shown in Figure 1, 2, comprise V-type fuselage body 1, be arranged at the wing 2 of fuselage both sides, be fixed on wing 2 dead ahead two screws 3, be covered in fuselage body 1 V-type groove above cover plate 4 and be arranged at the pulley 5 of fuselage body 1 bottom, wherein, the interior flight driving mechanism installing aircraft of the V-type groove of fuselage body 1.
In the present embodiment, the arranged outside baffle plate 21 of wing 2, the edge designs in baffle plate 21 front becomes streamlined.This design accords with full hydrodynamics, is conducive to aircraft stabilized flight.
The present invention is not limited to aforesaid detailed description of the invention.The present invention expands to any new feature of disclosing in this manual or any combination newly, and the step of the arbitrary new method disclosed or process or any combination newly.
Claims (2)
1. a Novel paper aircraft-type aeromodelling aerocraft, it is characterized in that: two screws (3) in wing (2) dead ahead that comprises V-type fuselage body (1), is arranged at the wing (2) of fuselage both sides, is fixed on, be covered in fuselage body (1) V-type groove above cover plate (4) and be arranged at the pulley (5) of fuselage body (1) bottom, the flight driving mechanism of aircraft is installed in the V-type groove of described fuselage body (1).
2. Novel paper aircraft-type aeromodelling aerocraft according to claim 1, is characterized in that: the arranged outside baffle plate (21) of described wing (2), the edge designs in baffle plate (21) front becomes streamlined.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410617657.2A CN104383691A (en) | 2014-11-06 | 2014-11-06 | Novel paper plane type model airplane aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410617657.2A CN104383691A (en) | 2014-11-06 | 2014-11-06 | Novel paper plane type model airplane aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104383691A true CN104383691A (en) | 2015-03-04 |
Family
ID=52601702
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410617657.2A Pending CN104383691A (en) | 2014-11-06 | 2014-11-06 | Novel paper plane type model airplane aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104383691A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104771913A (en) * | 2015-04-22 | 2015-07-15 | 鹿寨县初级实验中学 | Remote control model airplane |
-
2014
- 2014-11-06 CN CN201410617657.2A patent/CN104383691A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104771913A (en) * | 2015-04-22 | 2015-07-15 | 鹿寨县初级实验中学 | Remote control model airplane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150304 |