CN206896832U - The dalta wing model of an airplane - Google Patents
The dalta wing model of an airplane Download PDFInfo
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- CN206896832U CN206896832U CN201720286389.XU CN201720286389U CN206896832U CN 206896832 U CN206896832 U CN 206896832U CN 201720286389 U CN201720286389 U CN 201720286389U CN 206896832 U CN206896832 U CN 206896832U
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Abstract
It the utility model is related to a kind of dalta wing model of an airplane, the first cavity volume is provided with the vertical epimere, it is provided with the horizontal wing plate and is arranged on the second cavity volume of the first cavity volume identical, the motor, the propeller and the rudder plate in the receiving space that first cavity volume and the second cavity volume are formed；Two piece of first wing fence is provided with the horizontal wing plate near second cavity volume, first wing fence is vertical with the horizontal wing plate and parallel with the vertical epimere, and two piece of first wing fence is symmetrically distributed in the vertical epimere both sides；The second wing fence is respectively provided with the both ends of the horizontal wing plate, second wing fence is parallel with first wing fence.The dalta wing model of an airplane provided by the utility model, by the way that motor and propeller are installed on into inside, prevention propeller departs from motor and produces accident, and wing fence is fitted with the centre of wing and both ends, serve the effect of further control air-flow so that the flight of the model of an airplane is more steady.
Description
Technical field
Toy airplane field is the utility model is related to, more particularly to a kind of dalta wing model of an airplane.
Background technology
Plate type assembled toy airplane is a kind of simple in construction, and cost is cheap, but have simultaneously can flight function common object for appreciation
Tool, is extensively welcome by children.Wherein the aircraft of delta wing configuration is then one kind most commonly seen in plate type assembled toy airplane,
But the aircraft of this delta wing configuration, its delta wing configuration is relatively simple, poor not only like really spending, and flight performance also compares
Poor, problem mainly has：Take off or start needs by external force, power is thrown if desired for by additional hand, make its have thrust forward and
It can just be taken off after certain height and the elevation angle；Secondly, the existing dalta wing model of an airplane lacks the protection to rudder face, special circumstances
Drag aircraft falls airfoil and rudder face well damage behind ground, influences subsequent flights after repairing, causes utilization rate not high.Specifically
, the structure of existing wing fence aircraft is fallen touch at first behind ground is wing fence, and this kind of model plane are in-flight, the damage of wing fence and
It is relatively small compared with the damage of airfoil rudder face subsequently to repair the influence to caused by flight.In addition, the motor of existing aircraft
It is arranged on often through legs on the model of an airplane, it is directly exposed to be installed on front fuselage or rear end, motor and propeller
It is unprotected, the hidden danger hurted sb.'s feelings after propeller is thrown away be present.
The content of the invention
Based on this, it is necessary to at least one problem mentioned above, there is provided a kind of dalta wing model of an airplane.
A kind of dalta wing model of an airplane, including horizontal wing plate, vertical epimere, motor, propeller and rudder plate, described vertical
Epimere is provided with the first cavity volume, on the horizontal wing plate be provided with the second cavity volume of the first cavity volume identical, the motor,
The propeller and the rudder plate are arranged in the receiving space that first cavity volume and the second cavity volume are formed；Hold described second
Horizontal wing plate near chamber is provided with two piece of first wing fence, and first wing fence is vertical with the horizontal wing plate and is hung down with described
Straight epimere is parallel, and two piece of first wing fence is symmetrically distributed in the vertical epimere both sides；It is each at the both ends of the horizontal wing plate
Provided with the second wing fence, second wing fence is parallel with first wing fence.
In one of the embodiments, the dalta wing model of an airplane also includes some Circular Plates, the Circular Plate installation
In the receiving space that first cavity volume and second cavity volume are formed, the Circular Plate is parallel to each other and center line is mutual
Overlap, the motor and the propeller are arranged in the Circular Plate.
In one of the embodiments, the width phase of the width of the first wing fence afterbody and the vertical epimere afterbody
It is concordant with the trailing edge of the vertical epimere Deng, the trailing edge of first wing fence, the trailing edge of the vertical epimere
Beyond the preset distance of edge first of the horizontal wing plate, the trailing edge of first wing fence and the edge of the rudder plate are apart
Second preset distance.
In one of the embodiments, the horizontal wing plate is two pieces of symmetrical L-squares, the L-square it is non-
Right-angle side is along the first camber line is arranged to, and the one end at the first camber line edge is with a right-angle side of the L-square along by straight
Line connects, and the straight line is vertical with right-angle side edge.
In one of the embodiments, the horizontal wing plate, vertical epimere, the rudder plate, first wing fence, the institute
The second wing fence is stated to connect by fastening structure with the Circular Plate.
The dalta wing model of an airplane provided by the utility model, by the way that motor and propeller are installed on into inside, to propeller
The effect of buffer protection is played with motor, prevention propeller departs from motor and produces accident.And at the centre of wing and both ends all
Wing fence is installed, serves the effect of further control air-flow so that the flight of the model of an airplane is more steady.
Brief description of the drawings
Fig. 1 is the schematic diagram of the dalta wing model of an airplane provided in the embodiment of the utility model one；
Fig. 2 is the floor map of the horizontal wing plate of the dalta wing model of an airplane provided in the embodiment of the utility model one；
Fig. 3 is the floor map of the vertical epimere of the dalta wing model of an airplane provided in the embodiment of the utility model one；
Fig. 4 is the tail structure schematic diagram of the dalta wing model of an airplane provided in the embodiment of the utility model one；
Fig. 5 is the afterbody detail plan schematic diagram of the dalta wing model of an airplane provided in the embodiment of the utility model one.
Embodiment
As shown in figure 1, the utility model provides a kind of dalta wing model of an airplane 10, the aircraft include horizontal wing plate 100,
Vertical epimere 200, motor, propeller and rudder plate 600 etc., certainly, as routine techniques in the art, pacify certainly in aircraft
Equipped with power supply and remote control etc. annex, also there are the details such as the shape for meeting model of an airplane flight function, size certainly, due to
It is not that the utility model wants improved emphasis, therefore does not repeat here.As shown in Figures 2 and 3, it is provided by the utility model
Three Trading Model aircrafts are provided with the first cavity volume 210 on vertical epimere 200, are provided with and the first cavity volume 210 on horizontal wing plate 100
The second cavity volume of identical 110, because vertical epimere 200 and horizontal wing plate 100 intersect vertically connection, so while being provided with first
The cavity volume 110 of cavity volume 210 and second, the two cooperates in shape and size, forms certain receiving space, motor, spiral shell
Revolve oar and the grade of rudder plate 600 part to be just arranged in the receiving space that the first cavity volume 210 and the second cavity volume 110 are formed, due to this
Receiving space both ends are the cross limitation edge that vertical epimere 200 and horizontal wing plate 100 are formed, can be to motor and propeller
Certain restriction effect is formed, even if propeller comes off, can also be stopped by the cross limiting structure, be unlikely to injury.
As shown in figure 1, two piece of first wing fence 300, the first wing fence 300 and water are provided with the horizontal wing plate 100 near the second cavity volume 110
Flat wing plate 100 is vertical and parallel with vertical epimere 200, and two piece of first wing fence 300 is symmetrically distributed in the vertical both sides of epimere 200,
In addition, the second wing fence 400 is also respectively provided with the both ends of horizontal wing plate 100, and the second wing fence 400 is parallel with the first wing fence 300.
Horizontal wing plate 100 near the second cavity volume 110 is considered as airfoil root, and the both ends of horizontal wing plate 100 can be considered machine
The wing tip of the wing, suitable wing fence is respectively equipped with airfoil root and wing tip（It can be considered and determine the wind wing）, you can pass through physics mode
Air-flow is controlled, wing fence is mounted in airfoil root, realizes the control to main stream in flight course middle fuselage, and is mounted in wing tip, gas
Air-flow separation, the unfavorable shadow to flight stability that can prevent tip stall from bringing can just occur after wing fence is touched for stream
Ring.
As a preferable scheme, as shown in figure 1, the dalta wing model of an airplane 10 also includes some Circular Plates 500, annulus
Plate 500 is arranged in the receiving space that the first cavity volume 210 and the second cavity volume 110 are formed, and Circular Plate 500 is parallel to each other and center
Line is overlapped, and motor and propeller are arranged in the Circular Plate 500.On the one hand, Circular Plate 500 can play reinforcing aircraft
The effect of structure, propeller on the other hand can be further limited, prevent from flying out in its space from receiving space.Certainly, annulus
Plate 500 has certain width, and resistance can be produced in aircraft flight, and therefore, the width should be as far as possible small.
As a preferable scheme, as shown in Figure 4 and Figure 5, the width and vertical epimere 200 of the afterbody of the first wing fence 300
The width of afterbody is equal, and the trailing edge of the first wing fence 300 is concordant with the trailing edge of vertical epimere 200, vertical epimere 200
Trailing edge exceeds the preset distance of edge first of horizontal wing plate 100, the trailing edge of the first wing fence 300 and the side of rudder plate 600
Along at a distance of the second preset distance.First preset distance and the second preset distance are set according to the actual requirements.When being arranged on vertical ridge
When the wing fence on the both sides of plate 200 is had with vertical 200 identical width of epimere, certain width identical part does not imply that vertically
Epimere 200 is identical with the shape of the first wing fence 300, but has identical part just to disclosure satisfy that requirement, also can just keep
Aircraft can be horizontal positioned, makes it easy to be placed in ground, realizes the effect taken off on the ground, make its more easy manipulation,
Make without additional force or hand throwing, start motor and can be realized as aircraft to certain speed and taken off from ground.
As a preferable scheme, as shown in Fig. 2 horizontal wing plate 100 is two pieces of symmetrical L-squares, L-square
On-right angle edge be arranged to camber line 120, the one end at the edge of camber line 120 and a right-angle side of L-square by straight line along being connected
Connect, straight line is vertical with right-angle side edge.Horizontal wing plate 100 is arranged to be spliced by two pieces of L-squares, facilitates the spelling of aircraft
Dress.The non-straight arm of angle of L-square is arranged into camber line 120 can reduce the flight resistance of aircraft, simultaneously, it should also to having on aircraft
The place of corner angle carries out radiused processing, to reduce flight resistance.
As a preferable scheme, horizontal wing plate 100, vertical epimere 200, rudder plate 600, the first wing fence 300, second wing
Knife 400 is connected with Circular Plate 500 by fastening structure.
Each technical characteristic of embodiment described above can be combined arbitrarily, to make description succinct, not to above-mentioned reality
Apply all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, the scope that this specification is recorded all is considered to be.
Embodiment described above only expresses several embodiments of the present utility model, and its description is more specific and detailed,
But therefore it can not be interpreted as the limitation to utility model patent scope.It should be pointed out that the common skill for this area
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
The scope of protection of the utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (5)
1. a kind of dalta wing model of an airplane, including horizontal wing plate, vertical epimere, motor, propeller and rudder plate, it is characterised in that
The first cavity volume is provided with the vertical epimere, is provided with the horizontal wing plate and holds with the first cavity volume identical second
Chamber, the motor, the propeller and the rudder plate are arranged in the receiving space that first cavity volume and the second cavity volume are formed；
Two piece of first wing fence is provided with the horizontal wing plate near second cavity volume, first wing fence is vertical with the horizontal wing plate
And parallel with the vertical epimere, two piece of first wing fence is symmetrically distributed in the vertical epimere both sides；In the level
The both ends of wing plate are respectively provided with the second wing fence, and second wing fence is parallel with first wing fence.
2. the dalta wing model of an airplane according to claim 1, it is characterised in that if the dalta wing model of an airplane also includes
Dry Circular Plate, the Circular Plate are arranged in the receiving space that first cavity volume and second cavity volume are formed, the annulus
Plate is parallel to each other and center line overlaps, and the motor and the propeller are arranged in the Circular Plate.
3. the dalta wing model of an airplane according to claim 1, it is characterised in that the width of the first wing fence afterbody and institute
State that the width of vertical epimere afterbody is equal, the trailing edge of first wing fence is concordant with the trailing edge of the vertical epimere,
The trailing edge of the vertical epimere exceeds the preset distance of edge first of the horizontal wing plate, the afterbody side of first wing fence
Along the edge with the rudder plate at a distance of the second preset distance.
4. the dalta wing model of an airplane according to claim 1, it is characterised in that the horizontal wing plate is symmetrical two
Block L-square, the on-right angle edge of the L-square are arranged to the first camber line, the one end at the first camber line edge with it is described straight
For one right-angle side of gusset along being connected by straight line, the straight line is vertical with right-angle side edge.
5. the dalta wing model of an airplane according to claim 2, it is characterised in that the horizontal wing plate, the vertical epimere,
The rudder plate, first wing fence, second wing fence are connected with the Circular Plate by fastening structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720286389.XU CN206896832U (en) | 2017-03-23 | 2017-03-23 | The dalta wing model of an airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720286389.XU CN206896832U (en) | 2017-03-23 | 2017-03-23 | The dalta wing model of an airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206896832U true CN206896832U (en) | 2018-01-19 |
Family
ID=61295073
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720286389.XU Expired - Fee Related CN206896832U (en) | 2017-03-23 | 2017-03-23 | The dalta wing model of an airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206896832U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109018301A (en) * | 2018-08-14 | 2018-12-18 | 晨龙飞机（荆门）有限公司 | A kind of wing avoiding wingtip stall |
-
2017
- 2017-03-23 CN CN201720286389.XU patent/CN206896832U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109018301A (en) * | 2018-08-14 | 2018-12-18 | 晨龙飞机（荆门）有限公司 | A kind of wing avoiding wingtip stall |
| CN109018301B (en) * | 2018-08-14 | 2020-01-24 | 晨龙飞机（荆门）有限公司 | Wing capable of avoiding wing tip stall |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180119 Termination date: 20210323 |