CN208839044U - It inserts tail formula hand and throws aircraft - Google Patents
It inserts tail formula hand and throws aircraft Download PDFInfo
- Publication number
- CN208839044U CN208839044U CN201821352125.0U CN201821352125U CN208839044U CN 208839044 U CN208839044 U CN 208839044U CN 201821352125 U CN201821352125 U CN 201821352125U CN 208839044 U CN208839044 U CN 208839044U
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- China
- Prior art keywords
- slot
- wing
- tail
- block
- aircraft
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- 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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- 239000000463 material Substances 0.000 claims description 8
- 230000000694 effects Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229920001328 Polyvinylidene chloride Polymers 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000005033 polyvinylidene chloride Substances 0.000 description 1
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Abstract
The utility model discloses a kind of slotting tail formula hands to throw aircraft, including body, wing, tailplane and vertical tail；Body includes head, fuselage and afterbody, and vertical tail is set to afterbody；Wing card interface is provided on fuselage, wing is removably connected in wing card interface, afterbody is tiltedly installed with the first slot, bottom is equipped with plug division in first slot, plug division two sides are equipped with the second slot, and a slope is equipped in the middle part of tailplane, and slope is equipped with the third slot parallel with the slope, it is provided with convex block on corresponding two inner sidewalls of third slot, convex block matches with the second slot.The utility model uses the first slot, plug division, the second slot, third slot, convex block, convex block can be made to be caught in the second slot when grafting, plug division is caught in third slot, together with plugging together tailplane more with body, it will not fall off multiple impact ground, it is easy to use, it is completely embedded.
Description
Technical field
The utility model relates to a kind of slotting tail formula hands to throw aircraft.
Background technique
Have many model aircrafts in the market, but can not simply disassembly and assembly at any time, and it is raw in model aircraft
Postpartum is sold bought with player after require to store, be unable to disassembly model aircraft, very big placement space can be occupied, and
And wing is easy during placement by backfin, and then is damaged.
A kind of hand throwing aerodone, including body, wing, level are for another example disclosed in Chinese patent literature CN206355596U
Empennage and vertical tail；The body includes head, fuselage and afterbody, and the vertical tail is set to the fuselage tail
Portion；The fuselage is provided with wing card interface, and the afterbody is provided with empennage card interface, and the wing is removably clamped
In the wing card interface, the tailplane is removably connected in the empennage card interface.Though this is inserted tail formula hand and throws aircraft
It is so also able to achieve and circles in the air, but its empennage is plugged on fuselage, depends merely on a protrusion and interface cooperates, when aircraft is fallen
Its rear empennage is detached from fuselage several times on the ground, needs to insert again, very troublesome.
Utility model content
To overcome disadvantages mentioned above, the purpose of this utility model is to provide slotting tail formulas that is a kind of easy to use and being completely embedded
Hand throws aircraft.
In order to reach the goals above, the technical solution adopted in the utility model is: a kind of slotting tail formula hand throwing aircraft, including machine
Body, wing, tailplane and vertical tail；The body includes head, fuselage and afterbody, and the vertical tail is set to
The afterbody；Wing card interface is provided on the fuselage, the wing is removably connected in the wing card interface,
The afterbody is tiltedly installed with the first slot, and bottom is equipped with plug division in first slot, and the plug division two sides are equal
Equipped with the second slot, a slope is equipped in the middle part of the tailplane, the slope is equipped with the third slot parallel with the slope,
It is provided with convex block on corresponding two inner sidewalls of the third slot, the convex block matches with second slot.This
Utility model the utility model has the advantages that using the first slot, plug division, the second slot, third slot, convex block, when grafting, can make convex
Block is caught in the second slot, and plug division is caught in third slot, thus together with plugging together tailplane more with body, even if
Multiple impact ground will not fall off, easy to use, be completely embedded.
Preferably, groove is transversely provided on the opposite face of two convex blocks, the groove inner sidewall is set with a level
The one end for the spring set is connected, and the other end of the spring is connected with block, and the length of the block and spring is greater than described recessed
The depth of slot.Using spring, when being caught in plug division in third slot of block, the spring meeting pushed open by plug division
It is applied to the reversed thrust of block, clamps two blocks by plug division, keeps the grafting effect of tailplane and body more preferable.
Preferably, the opposite face of two convex blocks is provided with anti-slip layer, increases stiction, enhances connection effect.
Preferably, the convex block and block are trapezoidal, and grafting effect can be made more preferable.
Preferably, the wing card interface is the through-hole being horizontally installed on the fuselage, which is equipped with
Clamping groove on clamping block, the clamping block and the wing is interference fitted, and wing can be made to connect with body stronger.
Preferably, the body front end is equipped with cabin, and the cabin is detachably connected with cabin cover, is arranged in the cabin
There is the box body for placing counterweight.
Preferably, the material of the body, wing, tailplane and vertical tail is EPP, material environmental protection, quality
It is flexible and it is resistance to fall, be able to extend the service life of aircraft.
Detailed description of the invention
Fig. 1 is the main view of the utility model；
Fig. 2 is the structural schematic diagram of the tailplane of the utility model；
Fig. 3 is the main view of the body of the utility model；
Fig. 4 is the partial enlarged view of the utility model.
Specific embodiment
The preferred embodiment of the utility model is described in detail with reference to the accompanying drawing, so that the advantages of the utility model
It can be easier to be readily appreciated by one skilled in the art with feature, to make the protection scope of the utility model apparent clear
Define.
Referring to shown in attached drawing 1, Fig. 2, one of the present embodiment inserts tail formula hand and throws aircraft, including body 1, wing 2, level
Empennage 3 and vertical tail 4；The body 1 includes head 11, fuselage 12 and afterbody 13, and the vertical tail 4 is set to institute
State afterbody 13；Wing card interface 121 is provided on the fuselage 12, the wing 2 is removably connected in the wing
Card interface 121, the afterbody 13 are tiltedly installed with the first slot 131, and bottom is equipped with plug division in first slot 131
132,132 two sides of plug division are equipped with the second slot 133, are equipped with a slope 31, the slope in the middle part of the tailplane 3
31 are equipped with the third slot 32 parallel with the slope 31, are provided on 32 corresponding two inner sidewalls of the third slot
Convex block 33, the convex block 33 match with second slot 133, and 3 both ends of tailplane are equipped with dihedral 34.The slope 31
Range of tilt angles be 25-75 °, preferably 30 °.
In the present embodiment, be transversely provided with groove on the opposite face of two convex blocks 33, the groove inner sidewall with
One end of one horizontally disposed spring is connected, and the other end of the spring is connected with block 331, the block 331 and spring
Length is greater than the depth of the groove.When the plug division of tailplane 3 132 is caught in third slot 32, pushed away by plug division 132
The spring held can be applied to the reversed elastic force of block 331, clamp two blocks 331 by plug division 132, make tailplane and machine
The grafting effect of body is more preferable.
In order to increase stiction, enhance grafting effect, the opposite face of two convex blocks 33 is preferably provided with anti-skidding
Layer, the anti-slip layer can be used the big material of coefficient of friction and be made, it is preferred to use polyvinylidene chloride material.In order to facilitate grafting,
Guiding certain when grafting is given, the convex block 33 and block 331 are trapezoidal.
In the present embodiment, the wing card interface 121 is the through-hole being horizontally installed on the fuselage 12, in the through-hole
Side wall is equipped with clamping block 122, and the clamping groove on the clamping block 122 and the wing 2 is interference fitted.Using 122 He of clamping block
It is stronger that clamping groove can be such that wing connect with body.2 both ends of wing are equipped with dihedral.
In the present embodiment, 1 front end of body is equipped with cabin 14, and the cabin 14 is detachably connected with cabin cover 15,
The box body 16 for placing counterweight is provided in the cabin 14.
In the present embodiment, the material of the body 1, wing 2, tailplane 3 and vertical tail 4 is EPP.EPP material
Material environmental protection, quality it is flexible it is resistance to fall, be able to extend the service life of aircraft.
When in use, by wing 2 be inserted into wing card interface 121 in, clamping block 122 be caught in clamping block 122 make wing 2 with
Body 1 is connected firmly, and the third slot 32 of tailplane 3 is mutually plugged together by diagram direction with plug division 132, convex block 33 is blocked
Enter in the second slot 133, tailplane 3 can be made to be connected firmly with body 1, so that aircraft is flown nonstop to, even if multiple impact
Face will not cause to loosen.To make aircraft circle round, the overturning of tailplane 3 is inserted into afterbody for 180 ° according to the method described above
13。
Embodiment of above is only to illustrate the technical ideas and features of the present invention, and its object is to allow be familiar with this skill
The people of art understands the content of the utility model and is implemented, and does not limit the protection scope of the present invention, and all
According to the equivalent change or modification that the spirit of the present invention is substantially done, should all cover within the protection scope of the present utility model.
Claims (7)
1. a kind of slotting tail formula hand throws aircraft, including body (1), wing (2), tailplane (3) and vertical tail (4)；The machine
Body (1) includes head (11), fuselage (12) and afterbody (13), and the vertical tail (4) is set to the afterbody
(13)；It is provided with wing card interface (121) on the fuselage (12), the wing (2) is removably connected in the wing card
Interface (121), it is characterised in that: the afterbody (13) is tiltedly installed with the first slot (131), first slot
(131) interior bottom is equipped with plug division (132), and plug division (132) two sides are equipped with the second slot (133), the horizontal tail
A slope (31) are equipped in the middle part of the wing (3), the slope (31) is equipped with the third slot (32) parallel with slope (31), described
It is provided with convex block (33) on corresponding two inner sidewalls of third slot (32), the convex block (33) and second slot
(133) match.
2. slotting tail formula hand according to claim 1 throws aircraft, it is characterised in that: on the opposite face of two convex blocks (33)
Be transversely provided with groove, the groove inner sidewall is connected with one end of a horizontally disposed spring, the other end of the spring with
Block (331) is connected, and the length of the block (331) and spring is greater than the depth of the groove.
3. slotting tail formula hand according to claim 2 throws aircraft, it is characterised in that: the opposite face of two convex blocks (33) is equal
It is provided with anti-slip layer.
4. slotting tail formula hand described in any one of according to claim 1 or 2 or 3 throws aircraft, it is characterised in that: the convex block
(33) and block (331) is trapezoidal.
5. slotting tail formula hand according to claim 1 throws aircraft, it is characterised in that: the wing card interface (121) is laterally
Through-hole on the fuselage (12) is set, which is equipped with clamping block (122), the clamping block (122) with it is described
Clamping groove interference fit on wing (2).
6. slotting tail formula hand according to claim 1 throws aircraft, it is characterised in that: body (1) front end is equipped with cabin
(14), the cabin (14) is detachably connected with cabin cover (15), and the box for placing counterweight is provided on the cabin (14)
Body (16).
7. slotting tail formula hand according to claim 1 throws aircraft, it is characterised in that: the body (1), wing (2), horizontal tail
The material of the wing (3) and vertical tail (4) is EPP.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821352125.0U CN208839044U (en) | 2018-08-21 | 2018-08-21 | It inserts tail formula hand and throws aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821352125.0U CN208839044U (en) | 2018-08-21 | 2018-08-21 | It inserts tail formula hand and throws aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208839044U true CN208839044U (en) | 2019-05-10 |
Family
ID=66357171
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821352125.0U Expired - Fee Related CN208839044U (en) | 2018-08-21 | 2018-08-21 | It inserts tail formula hand and throws aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208839044U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114475072A (en) * | 2021-12-30 | 2022-05-13 | 浙江旭日工贸有限公司 | Clamping decoration and production process thereof |
-
2018
- 2018-08-21 CN CN201821352125.0U patent/CN208839044U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114475072A (en) * | 2021-12-30 | 2022-05-13 | 浙江旭日工贸有限公司 | Clamping decoration and production process thereof |
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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: 20190510 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |