CN207085325U - Plate type assembled is adjustable model aircraft - Google Patents
Plate type assembled is adjustable model aircraft Download PDFInfo
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- CN207085325U CN207085325U CN201721001444.2U CN201721001444U CN207085325U CN 207085325 U CN207085325 U CN 207085325U CN 201721001444 U CN201721001444 U CN 201721001444U CN 207085325 U CN207085325 U CN 207085325U
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- fuselage
- wing
- empennage
- plate type
- model aircraft
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Abstract
The utility model provides a kind of adjustable model aircraft of plate type assembled, including board-like wing and fuselage, the wing is provided with fuselage neck, the fuselage is assembled by being carried out through the fuselage neck and the wing, the afterbody of the fuselage is additionally provided with dismountable empennage adjuster, the empennage of the empennage adjuster and wing offsets, for adjusting the angle of the empennage.Also include L-type material and prevent raming.The plate type assembled is adjustable, and model aircraft does wing and fuselage using ABS/PC/ carbon fiber sheets, takes into account crashworthiness and flight stability；Empennage angle is adjusted by empennage adjuster, by adjusting head weight, adjustment of the different flight effects by empennage angle and head weight can be obtained, changeability is stronger, adapts to different playing methods.
Description
Technical field
Model aircraft technical field is the utility model is related to, more particularly to a kind of adjustable model aircraft of plate type assembled.
Background technology
Throwing type model plane, also make hand throw model plane, exactly model plane are dished out as paper helicopter, be allowed to a kind of boat of gliding
Mould.Referring to shown in Figure 1A, 1B and 1C, prior art typically using foam (EVA or EPP) be fuselage 101 and wing 102a,
102b, it is finished product by simple interpolation bonding forming.Existing model plane have the disadvantages that：
(1) because generally use foam is as fuselage wing, it is easily damaged, even with EPP foam, although compared with
It is difficult to damage, but because material is soft, wing is soft to lie prone, poor rigidity, it is impossible to throws energetically, stability is poor；
(2) existing model plane fuselage wing leans on glue sticking, poor reliability；
(3) existing model plane can only adjust flight attitude without any adjustable wing by throwing gimmick.This model plane are unfavorable for
Understanding for flight, also intolerant to object for appreciation.
Utility model content
The purpose of this utility model is to provide a kind of plate type assembled adjustable model aircraft, navigated with solving existing throwing type
Apperance formula is single, playing method is single, stability is poor, the problem of being easily damaged.
To achieve the above object, the utility model provides a kind of adjustable model aircraft of plate type assembled, including board-like machine
The wing and fuselage, the wing are provided with fuselage neck, and the fuselage through the fuselage neck with the wing by being spelled
Dress, the afterbody of the fuselage are additionally provided with dismountable empennage adjuster, and the empennage of the empennage adjuster and wing offsets, is used for
Adjust the angle of the empennage.
It is preferred that the fuselage and wing are attached by the L-type material located at the fuselage both sides and fixed, the L
One vertical plane of section bar is bonded with the fuselage, and another vertical plane is bonded with the wing so that the fuselage and wing
It is mutually perpendicular to.
It is preferred that the fuselage and wing are attached and fixed by screw and the L-type material, or the L-type material with
The fuselage and wing are attached and fixed by gluing.
It is preferred that the empennage adjuster includes empennage adjustment portion and rotary shaft, the empennage adjustment portion is provided with rotation
Axis hole and supporting part, the rotary shaft hole is matched with the rotary shaft to be attached to the afterbody of the fuselage, when the rotary shaft
During rotation, the supporting part offsets in the diverse location of the empennage of the wing and is morphed into difference to apply pressure to empennage
Angle.
It is preferred that the empennage adjuster also includes fastening screw, when the rotary shaft is rotated to diverse location, pass through
The fastening screw fixes the empennage adjustment portion.
It is preferred that the empennage adjustment portion includes two folder faces, two folder face corresponding positions are provided with the rotary shaft hole
And connected by the supporting part, during installation, two folder faces are mounted respectively to the both sides of the afterbody of the fuselage and pass through rotation
Axis connection.
It is preferred that the relative side in two folder faces is provided with antifriction face.
Ramed it is preferred that the head of the wing is additionally provided be detachably connected anti-.
It is preferred that described prevent raming with some models to vary in weight and/or by unlike material, the fastening spiral shell of weight
The head of silk and the wing is assembled.
It is preferred that the material of the wing and fuselage is ABS, PC or carbon fiber.
The utility model has the advantages that：
(1) wing and fuselage are done using ABS/PC/ carbon fiber sheets, existing very strong rigidity also keeps elasticity, taken into account resistance to
Hit and flight stability；
(2) use L-type material as buttress brace, using two planes (by screw or gluing) fixed main body on the outside of it and
Wing：Greatly enhance the rigidity of fuselage and wing, it is ensured that fuselage is vertical with wing, further ensure that fuselage face, wing
The levelness in face；
(3) empennage angle being adjusted by empennage adjuster, empennage adjuster can rotate and fix, and withstand empennage, because
Power suffered by anglec of rotation empennage, power is bigger, and empennage is more past to be upwarped, and due to the elasticity of material itself, empennage is attached to empennage always
On the fulcrum of adjuster；
(4) by the anti-replacing (or changing the fastening screw of unlike material) ramed, adjusting head weight, can obtain not
Same flight effect；
(5) user is allowed to experience DIY enjoyment by the assembling of various spare and accessory parts；
(6) principle and enhancing flown by the adjustment of empennage angle and head weight, the understanding for making user deep can
Object for appreciation property.
Brief description of the drawings
Figure 1A is existing model plane component diagram；
Figure 1B is existing model plane assembling components process schematic；
Fig. 1 C are schematic diagram after existing model plane assembling components；
Fig. 2A is the wing structure schematic diagram of the utility model preferred embodiment；
Fig. 2 B are the airframe structure schematic diagram of the utility model preferred embodiment；
Fig. 2 C are the fuselage of preferred embodiment and schematic diagram after the assembling of empennage adjuster；
Fig. 2 D are overall schematic after the adjustable model aircraft of plate type assembled of preferred embodiment assembles；
Fig. 3 is the L-type material structural representation of preferred embodiment；
Fig. 4 is the empennage controller structure schematic diagram of preferred embodiment；
Fig. 5 A are that the empennage adjuster of preferred embodiment carries out a kind of schematic diagram of angular adjustment；
Fig. 5 B are that the empennage adjuster of preferred embodiment carries out the schematic diagram of another angular adjustment.
Embodiment
Below with reference to accompanying drawing of the present utility model, the technical scheme in the embodiment of the utility model is carried out clear, complete
Whole description and discussion, it is clear that as described herein is only a part of example of the present utility model, is not whole realities
Example, based on the embodiment in the utility model, those of ordinary skill in the art institute on the premise of creative work is not made
The every other embodiment obtained, belongs to the scope of protection of the utility model.
For the ease of the understanding to the utility model embodiment, make below in conjunction with accompanying drawing by taking specific embodiment as an example into one
The explanation of step, and each embodiment does not form the restriction to the utility model embodiment.
As shown in Fig. 2A~2D, a kind of adjustable model aircraft of plate type assembled, including board-like wing are present embodiments provided
21 and fuselage 22, wing 21 is provided with fuselage neck 211, fuselage 22 by carrying out assembly through fuselage neck 211 and wing 21,
In addition, the afterbody of fuselage 22 is additionally provided with dismountable empennage adjuster 24, the phase of empennage 212 of empennage adjuster 24 and wing 21
Support, for adjusting the angle of empennage 212.
Preferably, with reference to shown in figure 3, above-mentioned machine is attached and fixed by the L-type material 23 located at the both sides of fuselage 22
Body 22 and wing 21 are mutually perpendicular to it.During specific installation, the vertical plane and fuselage of the L-type material 23 provided in the present embodiment
Fitting, another vertical plane are bonded with the wing so that fuselage 22 and wing 21 are mutually perpendicular to.The company of not only acting as of L-type material 23
Fixed effect is connect, also acts as the reinforcement beam action as whole model plane, so as to improve the overall structure of spliced model plane
Stability.Fuselage 22 and wing 21 in the present embodiment are respectively equipped with screw hole with 23 corresponding opening position of L-type material, pass through screw
Realize that fuselage 22 and wing 21 are attached and fixed with L-type material 23 respectively through screw hole.In other variant embodiments, L
Section bar also directly can be attached and be fixed by gluing with fuselage and wing, and L-type material is arranged to orthogonal comprising two
Vertical plane, the concrete form of vertical plane refers to Fig. 2 C, other forms also can be deformed into, here to the specific of vertical plane
Form is not specially limited, those skilled in the art can as needed unrestricted choice vertical plane concrete form and its with wing and machine
The mode that is connected of body.
Specifically when being spliced, referring again to fuselage shown in Fig. 2A~2D, is prepared first, then L is installed on fuselage
Section bar is as buttress brace, then installs empennage adjuster 24, finally, fuselage neck fuselage being attached on wing on fuselage again
Place, while fixed wing and L-type material.Assembled process is simple, and spliced overall structure is very firm.
Preferably, with reference to figure 4, the empennage adjuster 24 in the present embodiment includes empennage adjustment portion 241 and rotary shaft, empennage
Adjustment portion is provided with rotary shaft hole 242 and supporting part 243, and rotary shaft hole 242 is used to match with above-mentioned rotary shaft to be attached to
The afterbody of fuselage 22, certainly, the corresponding position of fuselage also are provided with axis hole so that rotary shaft passes through fuselage axis hole and rotary shaft hole
Realize being rotatably connected for empennage adjuster and fuselage.When adjusting so that rotary shaft rotates, then supporting part will be with wing 21
The diverse location of empennage 212 offset and be morphed into different angles to apply different pressure to empennage 212.Referring specifically to
Shown in Fig. 5 A and Fig. 5 B, gradually rotated by rotating rotary shaft supporting part so as to apply different pressure to empennage, make it
It is in different angle to be deformed into wing-body, so as to realize the regulation of empennage angle.Here empennage adjuster can rotate, and
Empennage is withstood, changes the power suffered by empennage because of the change of the anglec of rotation, power is bigger, and empennage is more past to be upwarped.Due to material itself
Elasticity, empennage is attached on the fulcrum of empennage adjuster always.
Specifically, above-mentioned empennage adjuster also includes fastening screw, when the rotary shaft for adjusting above-mentioned is rotated to different positions
When putting, fastened by fastening screw, so as to fixed empennage adjustment portion, and then realize that the angle after empennage angular adjustment is consolidated
Fixed, adjustment process is simple, and locking and fastening means are easily operated, and locking effect is preferable.
Preferably, referring again to Fig. 4, the empennage adjustment portion in the present embodiment includes two folder faces, and two folder faces correspond to position
Place is put provided with rotary shaft hole and is connected by above-mentioned supporting part, during installation, two folder faces are mounted respectively to the afterbody of fuselage
Both sides and by rotating axis connection.That is, fuselage is clipped in the middle by two folder faces, and it is used for by the supporting part of connection and wing
Offset, it is simple in construction, and be easily assembled to.
In further preferred embodiment, the relative side in above-mentioned two folder faces is provided with antifriction face.Antifriction face can
Made using quality of rubber materials, with prevent folder face relative to fuselage rotate when abrasion of the friction to sheet material between the two.
In another preferred embodiment, referring again to shown in Fig. 2 D, be additionally provided with the head of wing be detachably connected it is anti-
Ram 25.It is installed after fuselage inserts wing, and it can further improve steady when model plane use after assembly after installation
Solidity, and can effectively prevent use when head it is bad by damage.
In a further preferred embodiment, prevent raming with some models to vary in weight and/or by unlike material,
The fastening screw of weight and the head of wing are assembled.What is varied in weight anti-rams or by the anti-institute that rams of fastening screw adjustment
In the weight of head, and then head weight can be adjusted by the replacing (or changing fastening screw of unlike material) to preventing raming,
Different flight effects can be obtained.
The material of wing and fuselage in above-described embodiment can be set to ABS, PC or carbon fiber as needed, by ABS, PC or
Carbon fiber sheet carries out making wing and fuselage.The existing very strong rigidity of board-like wing and fuselage of this different materials also keeps bullet
Property, take into account crashworthiness and flight stability.Wing rigidity and impact resistance are protected simultaneously.
The fuselage wing of the adjustable model aircraft of plate type assembled provided herein is formed by plate cutting；The empennage of wing is adjustable
Section part can adjust certain angle up and down by joint-cutting and material its own resilient；Fuselage is clamped with the lateral surface of 2 L-type materials, so
This is integrally inserted into wing locating groove afterwards, then the another side of L-type material is bonded fixation with wing.Empennage adjuster is fixed on
Afterbody, withstands empennage variable partition, rotatable locking, and the different anglecs of rotation causes the level angle of empennage different；
And fixed in head and prevent raming, prevent that raming or change the anti-fixed screw ramed changes the center of gravity of airplane by changing.This flies
The change of machine model is various, simple in construction, is easy to assembled.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to
In this, any those skilled in the art is in the technical scope that the utility model discloses, the deformation done to the utility model
Or replace, it should all cover within the scope of protection of the utility model.Therefore, the scope of protection of the utility model should be with described
Scope of the claims is defined.
Claims (10)
1. a kind of adjustable model aircraft of plate type assembled, it is characterised in that including board-like wing and fuselage, the wing is provided with
Fuselage neck, the fuselage is assembled by being carried out through the fuselage neck and the wing, and the afterbody of the fuselage is additionally provided with
Dismountable empennage adjuster, the empennage of the empennage adjuster and wing offsets, for adjusting the angle of the empennage.
2. the adjustable model aircraft of plate type assembled according to claim 1, it is characterised in that the fuselage and wing are by setting
L-type material in the fuselage both sides is attached and fixed, and a vertical plane of the L-type material is bonded with the fuselage, another
Individual vertical plane is bonded with the wing so that the fuselage and wing are mutually perpendicular to.
3. the adjustable model aircraft of plate type assembled according to claim 2, it is characterised in that the fuselage and wing pass through spiral shell
Silk is attached and fixed with the L-type material, or the L-type material and the fuselage and wing are attached and solid by gluing
It is fixed.
4. the adjustable model aircraft of plate type assembled according to claim 1, it is characterised in that the empennage adjuster includes tail
Wing adjustment portion and rotary shaft, the empennage adjustment portion are provided with rotary shaft hole and supporting part, the rotary shaft hole and the rotation
Axle is matched to be attached to the afterbody of the fuselage, and when the rotary shaft rotates, the supporting part is in the empennage of the wing
Diverse location offsets is morphed into different angles to apply pressure to empennage.
5. the adjustable model aircraft of plate type assembled according to claim 4, it is characterised in that the empennage adjuster also includes
Fastening screw, when the rotary shaft is rotated to diverse location, the empennage adjustment portion is fixed by the fastening screw.
6. the adjustable model aircraft of plate type assembled according to claim 4, it is characterised in that the empennage adjustment portion includes two
Individual folder face, two folder face corresponding positions are provided with and the rotary shaft hole and connected by the supporting part, during installation, two folder faces
It is mounted respectively to the both sides of the afterbody of the fuselage and by rotating axis connection.
7. the adjustable model aircraft of plate type assembled according to claim 6, it is characterised in that the relative side in two folder faces is set
There is antifriction face.
8. the adjustable model aircraft of plate type assembled according to claim 1, it is characterised in that the head of the wing is additionally provided with
What is be detachably connected anti-rams.
9. the adjustable model aircraft of plate type assembled according to claim 8, it is characterised in that if anti-ram has dry weight
Measure different models and/or assembled by unlike material, the fastening screw of weight and the head of the wing.
10. the adjustable model aircraft of plate type assembled according to claim 1, it is characterised in that the material of the wing and fuselage
Expect for ABS, PC or carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721001444.2U CN207085325U (en) | 2017-08-11 | 2017-08-11 | Plate type assembled is adjustable model aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721001444.2U CN207085325U (en) | 2017-08-11 | 2017-08-11 | Plate type assembled is adjustable model aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207085325U true CN207085325U (en) | 2018-03-13 |
Family
ID=61540850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721001444.2U Active CN207085325U (en) | 2017-08-11 | 2017-08-11 | Plate type assembled is adjustable model aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207085325U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109331479A (en) * | 2018-11-28 | 2019-02-15 | 佛山科学技术学院 | A kind of adjustable model aircraft of plate type assembled |
| CN112810794A (en) * | 2021-02-10 | 2021-05-18 | 汉王科技股份有限公司 | Aircraft, aircraft holster and method for replacing aircraft holster |
-
2017
- 2017-08-11 CN CN201721001444.2U patent/CN207085325U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109331479A (en) * | 2018-11-28 | 2019-02-15 | 佛山科学技术学院 | A kind of adjustable model aircraft of plate type assembled |
| CN112810794A (en) * | 2021-02-10 | 2021-05-18 | 汉王科技股份有限公司 | Aircraft, aircraft holster and method for replacing aircraft holster |
| CN112810794B (en) * | 2021-02-10 | 2023-09-05 | 汉王科技股份有限公司 | Aircraft, aircraft holster and method for exchanging aircraft holsters |
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