CN204368408U - For being fixedly connected with the mounting structure of model plane fuselage and wing - Google Patents
For being fixedly connected with the mounting structure of model plane fuselage and wing Download PDFInfo
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- CN204368408U CN204368408U CN201420523555.XU CN201420523555U CN204368408U CN 204368408 U CN204368408 U CN 204368408U CN 201420523555 U CN201420523555 U CN 201420523555U CN 204368408 U CN204368408 U CN 204368408U
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- wing
- model plane
- fixedly connected
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- plane fuselage
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Abstract
The utility model discloses a kind of mounting structure for being fixedly connected with model plane fuselage and wing; comprise the wing latch and plug housing that are used in conjunction with each other; screw bolt and nut; described plug housing is arranged on on wing axis; described model airplane machine is provided with the through hole corresponding with plug housing with it; described wing latch is fixedly connected with plug housing along the longitudinal midline direction of model plane fuselage through described through hole, and described bolt is fixedly connected with nut pre-buried in model plane fuselage with model plane fuselage axis perpendicular to wing.The utility model is with low cost, and has good reliability, is applicable to multiple fixed-wing type.
Description
Technical field
The utility model relates to fixed-wing model airplane, particularly relates to a kind of mounting structure for being connected and fixed model plane and unmanned plane wing.
Background technology
In the Flight Vehicle Structure of the fixed-wing type in model airplane or unmanned plane, wing has key role for generation of lift, the lift that wing produces, resistance need to pass to fuselage by mounting structure, the wing (hereinafter referred to as wing) of model airplane according to types of models need there is different specifications, but be all the parts that in the middle of mold elements, size is maximum substantially, and need, with fuselage, there is good connection, gravity and the overload of model can be born, also wanting can convenient disassembly, makes model be convenient to deposit, transport.
The connection mode of model plane fuselage and unmanned plane wing has following several usually: one is that screw is fixed; the mounting structure that screw is fixed is most popular version; its structure is relatively simple; but require that the size of the connecting portion of model plane fuselage and wing is more roomy; just can have enough rigidity; if the aircraft that size is more very thin; larger elastic deformation may be there is in the connecting portion of wing, fuselage; the structural stability of aircraft can be affected, or structure, the weight of productive costs and aircraft can be increased to reinforce fuselage.Two is that grafting rod connects, this mounting structure adopts two vertical slotting lower connection fuselages of latch rod and left and right two wing, go for the aircraft of part airframe structure moderate dimensions, but for the wing that relative thickness is thinner, the thickness of the upper and lower lap of left and right wing is respectively the half of wing thickness, thus thinner, this will affect structural strength and the rigidity of aircraft, can not be applied on product.
Therefore, existing mounting structure range of use is all various restricted, and once misapplication, and wing and fuselage can be caused in conjunction with insecure and deviate from, and reliability is lower not good, and has the shortcomings such as dismounting is loaded down with trivial details, part is many.
Summary of the invention
The purpose of this utility model is to solve above-mentioned problems of the prior art, propose a kind of mounting structure for being fixedly connected with model plane fuselage and wing, comprise the wing latch and plug housing that are used in conjunction with each other, screw bolt and nut, described plug housing is arranged on parallel with the longitudinal midline direction of model plane fuselage with on wing axis, described model airplane machine is provided with the through hole corresponding with plug housing with it, described wing latch is fixedly connected with plug housing along the longitudinal midline direction of model plane fuselage through described through hole, described bolt is fixedly connected with nut pre-buried in model plane fuselage with model plane fuselage axis perpendicular to wing.
In the technical program, wing latch can adopt the latch of band stopping function.Plug housing is located at unmanned module one end near model plane fuselage, wing axis, and described through hole is located on the rear wall of unmanned module.
In one embodiment, wing is integral type wing.
In another embodiment, wing is split left and right formula wing, and described port wing is fixedly connected with by the wing latch rod crossing fuselage with starboard wing, and the coupling end of described port wing or starboard wing is fixed wtih a catch that can pass for bolt.
Compared with prior art, wing mounting structure of the present utility model solves the shortcoming that traditional wing attachment structure exists preferably, and go for the installation of left and right compound type wing and left and right integral type wing, because the part of mounting structure own is less, processing is very simple, and installation site is very ingenious, also very convenient in fitting process, improve the Performance And Reliability of model plane product, but also the monnolithic case of model plane can not be affected.
Accompanying drawing explanation
Below, contrast accompanying drawing and preferred embodiment are described in detail to the utility model, wherein:
Fig. 1 is the exploded view of the utility model first embodiment;
Fig. 2 is the block diagram of the utility model first embodiment;
Fig. 3 is the exploded view of the utility model second embodiment;
Fig. 4 is the block diagram of the utility model second embodiment.
Detailed description of the invention
Below in conjunction with drawings and Examples, utility model is described in detail.Should be appreciated that to the explanation of specific embodiment only in order to explain the technical scheme that the utility model proposes, and non-limiting the utility model.
Fig. 1 to Fig. 2 is the first embodiment of the present utility model, the wing 5 of this embodiment is integral type wing, two wings in left and right connect into an entirety respectively by port wing attaching parts 8 and starboard wing attaching parts 9, model plane fuselage 4 is provided with the groove 11 that wing can be supplied laterally inserted, one end near unmanned module on the axis of wing 5 is provided with plug housing 10, plug housing 10 is arranged on parallel with the longitudinal midline direction of model plane fuselage with on wing axis, model plane fuselage 4 can be provided with the through hole 6 corresponding with plug housing 10, in the present embodiment, through hole 6 is just arranged on the rear wall in unmanned module, when wing latch 1 installed by needs, open canopy 3, latch just can be inserted in plug housing 10 fixing through through hole 6 by latch 1, very convenient.Except latch is fixed, also have a bolt 2 perpendicular to the axis of wing 5 and model plane fuselage 4, be directly fixedly connected with (in figure, nut is not shown) with nut pre-buried in model plane fuselage 4 with model plane fuselage 4 through wing 5 from top to bottom.
Fig. 3 to Fig. 4 is the second embodiment of the present utility model, this embodiment and the first embodiment basically identical, but wing 5 have employed split left and right formula wing, port wing 52 is respectively equipped with port wing attaching parts 8 and starboard wing attaching parts 9 with the coupling end of starboard wing 51, and port wing 52 is fixedly connected with by the wing latch rod 7 crossing fuselage with starboard wing 51.Plug housing is arranged on the axis of wing 5 equally, wherein half is positioned on port wing attaching parts 8, second half is positioned on starboard wing attaching parts 9, and through hole 6 is arranged on the rear wall in unmanned module, and wing latch 1 is fixedly connected with plug housing 10 through through hole 6 in unmanned module.The setting position of bolt 2 is the same with the first embodiment, its half is also be positioned on port wing attaching parts 8, and second half is positioned on starboard wing attaching parts 9, in addition, port wing attaching parts 8 is provided with a catch that can pass for bolt, the connection of left and right wing can be reinforced further.
Wing latch 1 of the present utility model can adopt the latch of band stopping function; by wing latch 1, plug housing 10 and bolt 2, nut with the use of; mounting structure is made to have enough rigidity; model plane fuselage firmly can be connected with wing; good stability; and due to installation site very ingenious, the no matter thickness of wing, all can not make wing produce deformation.
Claims (5)
1. one kind for being fixedly connected with the mounting structure of model plane fuselage and wing, comprise the wing latch (1) and plug housing (10) that are used in conjunction with each other, bolt (2) and nut, it is characterized in that, described plug housing (10) is arranged on wing (5) axis parallel with the longitudinal midline direction of model plane fuselage, described model plane fuselage (4) is provided with the through hole corresponding with plug housing (10), described wing latch (1) is fixedly connected with plug housing (10) along the longitudinal midline direction of model plane fuselage (4) through described through hole, described bolt (2) is fixedly connected with nut pre-buried in model plane fuselage (4) with model plane fuselage (4) axis perpendicular to wing (5).
2. as claimed in claim 1 for being fixedly connected with the mounting structure of model plane fuselage and wing, it is characterized in that, described wing latch (1) is the latch of band stopping function.
3. as claimed in claim 1 for being fixedly connected with the mounting structure of model plane fuselage and wing, it is characterized in that, described plug housing is located at unmanned module one end near model plane fuselage, wing axis, and described through hole is located on the rear wall of unmanned module.
4. as claimed in claim 1 for being fixedly connected with the mounting structure of model plane fuselage and wing, it is characterized in that, described wing (5) is integral type wing.
5. as claimed in claim 1 for being fixedly connected with the mounting structure of model plane fuselage and wing; it is characterized in that; described wing (5) is split left and right formula wing; described port wing (52) is fixedly connected with by the wing latch rod (7) crossing fuselage with starboard wing (51), and the coupling end of described port wing or starboard wing is fixed wtih a catch that can pass for bolt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420523555.XU CN204368408U (en) | 2014-09-12 | 2014-09-12 | For being fixedly connected with the mounting structure of model plane fuselage and wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420523555.XU CN204368408U (en) | 2014-09-12 | 2014-09-12 | For being fixedly connected with the mounting structure of model plane fuselage and wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204368408U true CN204368408U (en) | 2015-06-03 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420523555.XU Expired - Fee Related CN204368408U (en) | 2014-09-12 | 2014-09-12 | For being fixedly connected with the mounting structure of model plane fuselage and wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204368408U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107970621A (en) * | 2017-11-21 | 2018-05-01 | 高天宇 | A kind of modularization aeromodelling airplane |
| CN113955075A (en) * | 2021-10-09 | 2022-01-21 | 西安远方航空技术发展有限公司 | Aircraft |
| WO2023142702A1 (en) * | 2022-01-25 | 2023-08-03 | 航天时代飞鸿技术有限公司 | Locking device and unmanned aerial vehicle |
-
2014
- 2014-09-12 CN CN201420523555.XU patent/CN204368408U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107970621A (en) * | 2017-11-21 | 2018-05-01 | 高天宇 | A kind of modularization aeromodelling airplane |
| CN113955075A (en) * | 2021-10-09 | 2022-01-21 | 西安远方航空技术发展有限公司 | Aircraft |
| WO2023142702A1 (en) * | 2022-01-25 | 2023-08-03 | 航天时代飞鸿技术有限公司 | Locking device and unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20150603 Termination date: 20210912 |