CN206424575U - A kind of model plane wing - Google Patents
A kind of model plane wing Download PDFInfo
- Publication number
- CN206424575U CN206424575U CN201621464833.4U CN201621464833U CN206424575U CN 206424575 U CN206424575 U CN 206424575U CN 201621464833 U CN201621464833 U CN 201621464833U CN 206424575 U CN206424575 U CN 206424575U
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- CN
- China
- Prior art keywords
- floor
- wing
- model
- model plane
- utility
- Prior art date
- 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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Abstract
The utility model discloses a kind of model plane wing; including floor; it is characterized in that; described floor is the sheet material of strip; some floors are crisscross to be spliced into gap on the upside of gap on the downside of frame structure, one of floor of floor intersection, another floor; it is connected together above and below two floors, while the side of the framework constituted in floor is provided with engaging lug.The light-duty weight of model plane wing structure described in the utility model is low, reduces the physical burden of junction, ensures the connective stability of wing, it is to avoid wing self-deformation, it is to avoid sagging or even breaking releasing situation occurs in wing, improves security.
Description
Technical field
The utility model is related to model plane technical field, more particularly to a kind of model plane wing.
Background technology
Model refers to a kind of reconstruction physically in kind to jobbie in outward appearance and spatially, and " simulation model " is exactly
To all completely being reproduced with local for object, " simulation model " be exactly to these in outward appearance and spatially, whole drawn game
In portion according to certain proportionate relationship, the type body in kind zoomed in or out.The model plane of displaying are a kind of large-scale emulation
Model, usual wing is only connected on fuselage by its side and supported without other, for the wider wing of the span, connects place
The weight to be born is quite greatly, it is necessary to which enough structural strengths, traditional wing uses steel frame construction, and cost of manufacture is high, weight
Greatly, the load of junction is big, easily occurs that wing is sagging or even situation of breaking releasing, also results in wing is assembled on fuselage
When labor intensity it is big.
Utility model content
Technical problem to be solved in the utility model and propose technical assignment be prior art is improved there is provided
A kind of model plane wing, solves model plane wing weight traditional in current technology greatly, cost of manufacture is high, connected load is big, assembling is difficult
Spend the problem of big labor intensity is high.
To solve above technical problem, the technical solution of the utility model is：
A kind of model plane wing, including floor, it is characterised in that described floor is the sheet material of strip, and some floors are in length and breadth
Staggeredly it is spliced into gap, two on the upside of gap on the downside of frame structure, one of floor of floor intersection, another floor
It is connected together above and below floor, while the side of the framework constituted in floor is provided with engaging lug.Model plane described in the utility model
Wing structure is light-duty, and easy to assembly quick, wing is connected on the fuselage of model plane by low manufacture cost by engaging lug, wing
Lightweight using full rib structure, the physical burden of engaging lug is low, can ensure the connective stability of wing, it is to avoid wing itself
Deformation, also avoids the occurrence of that wing is sagging or even situation of breaking releasing, improves security.
Further, described floor intersection is reinforced using gusset, improves connective stability.
Further, some through holes have been opened up on described floor, have mitigated weight, the physical burden of engaging lug is reduced,
Ensure connective stability.
Further, described through hole is circle, and through hole edge is provided with flange, is carried while lightened plate floor weight
The structural strength of deep floor, it is to avoid floor bending deformation, ensures that wing structure is stable, profile is accurate.
Further, the side for the framework that described floor is constituted also is connected with wing rudder face by rotating shaft.
Further, the framework that described floor is constituted sets stiffener at engaging lug, improves structural strength, it is to avoid even
It is broken between the framework that lug and floor are constituted.
Compared with prior art, the utility model advantage is：
The light-duty weight of model plane wing structure described in the utility model is low, reduces the physical burden of junction, ensures wing
Connective stability, it is to avoid wing self-deformation, it is to avoid sagging or even breaking releasing situation occurs in wing, improve security,
And wing efficiency high easy to make, dimensional accuracy is high, low manufacture cost.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the connection diagram of floor；
Fig. 3 is the structural representation of through hole.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
A kind of model plane wing disclosed in the utility model embodiment, the light-duty intensity of structure is high, and stability is good, reduces junction
Weight-bearing load, reduction assembling difficulty and labor intensity reduces cost of manufacture.
As shown in Figure 1 to Figure 3, a kind of model plane wing, including floor 1, described floor 1 is the sheet material of strip, some ribs
Plate 1 is crisscross to be spliced into frame structure, the downside gap 11 of one of floor 1 of the intersection of floor 1, another floor 1
Upside gap 11, two floors 1 are connected together by breach about 11, and are reinforced in the intersection of floor 1 using gusset, are improved
Connective stability, ensures wing dimension precision, while the side of the framework constituted in floor 1 is provided with for connecting with model plane fuselage
The engaging lug 2 connect, and be provided with the stiffener 6 being connected with floor 1 at engaging lug 2, and the framework that constitutes of floor 1
Other side is also connected with wing rudder face 5 by rotating shaft 4.
Open up some through holes 3 on floor 1, the weight of further lightened plate floor 1, meanwhile, through hole 3 is circle, and
Through hole edge is provided with flange 31, is not easily broken, while the structural strength of deep floor 1, it is to avoid the Bending Deformation of floor 1 influences machine
Contour of flange size.
It the above is only preferred embodiment of the present utility model, it is noted that above-mentioned preferred embodiment should not be regarded
For to limitation of the present utility model, protection domain of the present utility model should be defined by claim limited range.For
For those skilled in the art, do not departing from spirit and scope of the present utility model, can also make some
Improvements and modifications, these improvements and modifications also should be regarded as protection domain of the present utility model.
Claims (6)
1. a kind of model plane wing, including floor (1), it is characterised in that described floor (1) is the sheet material of strip, some floors
(1) it is crisscross to be spliced into gap, another floor on the downside of frame structure, one of floor (1) of floor (1) intersection
(1) upside gap, two floors (1) are connected together up and down, while the side of the framework constituted in floor (1) is provided with engaging lug
(2)。
2. model plane wing according to claim 1, it is characterised in that described floor (1) intersection is reinforced using gusset.
3. model plane wing according to claim 1, it is characterised in that opened up some through holes on described floor (1)
(3)。
4. model plane wing according to claim 3, it is characterised in that described through hole (3) is circle, and through hole edge
It is provided with flange (31).
5. model plane wing according to claim 1, it is characterised in that the side for the framework that described floor (1) is constituted is also
Wing rudder face (5) is connected with by rotating shaft (4).
6. model plane wing according to claim 1, it is characterised in that the framework that described floor (1) is constituted is in engaging lug
(2) place sets stiffener (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621464833.4U CN206424575U (en) | 2016-12-29 | 2016-12-29 | A kind of model plane wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621464833.4U CN206424575U (en) | 2016-12-29 | 2016-12-29 | A kind of model plane wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206424575U true CN206424575U (en) | 2017-08-22 |
Family
ID=59585309
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621464833.4U Expired - Fee Related CN206424575U (en) | 2016-12-29 | 2016-12-29 | A kind of model plane wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206424575U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108274416A (en) * | 2018-01-29 | 2018-07-13 | 广东工业大学 | A kind of aerodynamics fin and fin assembling jig |
-
2016
- 2016-12-29 CN CN201621464833.4U patent/CN206424575U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108274416A (en) * | 2018-01-29 | 2018-07-13 | 广东工业大学 | A kind of aerodynamics fin and fin assembling jig |
| CN108274416B (en) * | 2018-01-29 | 2020-05-19 | 广东工业大学 | Aerodynamic wing and wing assembling clamp |
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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: 20170822 Termination date: 20201229 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |