CN208181398U - A kind of folding side wing mechanism - Google Patents
A kind of folding side wing mechanism Download PDFInfo
- Publication number
- CN208181398U CN208181398U CN201820756983.5U CN201820756983U CN208181398U CN 208181398 U CN208181398 U CN 208181398U CN 201820756983 U CN201820756983 U CN 201820756983U CN 208181398 U CN208181398 U CN 208181398U
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- CN
- China
- Prior art keywords
- wing
- lower panel
- flat
- hydraulic cylinder
- telescopic hydraulic
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Abstract
The utility model relates to a kind of folding side wing mechanisms, it is characterized in that, including main wing, main wing includes lower panel and top panel, it is Wing Tank between lower panel and top panel, telescopic hydraulic cylinder peace all-wing aircraft is installed in Wing Tank, flat all-wing aircraft is mounted above between plate and lower panel by flat wing axis and tangles top panel and lower panel, telescopic hydraulic cylinder is fixed on inside Wing Tank on lower panel by fixed turntable, after the output end of telescopic hydraulic cylinder installs connector by axis, flat all-wing aircraft is connected by connector, side is folded in main wing and fold mechanism is installed.The utility model structure is simple, and performance is stablized.
Description
Technical field
The utility model relates to a kind of folding side wing mechanisms, belong to flying wing technical field of structures.
Background technique
Aviation mechanism of the flank as flight instruments has extremely important effect.And the land, water and air three studied now are used
In equipment, the requirement to flying wing is just more more, in the design, not only needs flying wing to have stable gliding structure, more
It needs to consider for the beauty of flight instruments, and in different state of flights, flank is the unfolded state for needing to have different, especially
It is when ground is run, and flank does not need to open, and just needs one kind that can quickly fold side this when
The mechanism of the wing realizes packing up for flank, therefore folding flank is also the important directions of those skilled in the art's research.
Utility model content
The utility model provides a kind of folding side wing mechanism to solve the problems, such as that aircraft flank folds.
The utility model solve above-mentioned technical problem technical solution it is as follows: a kind of folding side wing mechanism, it is special it
It is in it is Wing Tank between lower panel and top panel, installation is stretched in Wing Tank that including main wing, main wing, which includes lower panel and top panel,
Contracting hydraulic cylinder peace all-wing aircraft, flat all-wing aircraft are mounted above between plate and lower panel by flat wing axis, and telescopic hydraulic cylinder passes through fixation
Turntable is fixed on inside Wing Tank on lower panel, after the output end of telescopic hydraulic cylinder installs connector by axis, is connected by connector
Flat all-wing aircraft folds side in main wing and installs fold mechanism.In the design, flat all-wing aircraft can be made by the telescopic hydraulic cylinder inside main wing
With flat all-wing aircraft is opened with telescopic hydraulic cylinder in this way when opening flying wing, play and prolong by folding of the realization on main wing
Long main wing, raising air-flow is to flying wing buoyancy, taking off and sliding convenient for flight equipment.Flat all-wing aircraft is to be mounted on master with flat wing axis
The upper surface of on the wing between plate and lower panel, when the main shaft of telescopic hydraulic cylinder is stretched out or retracted, flat all-wing aircraft just be will do it
Rotation.
Based on the above technical solution, the utility model is to reach the stability of the convenience and equipment that use,
Following improvement can also be made to above-mentioned technical solution:
Further, the fold mechanism includes oscillating motor, and the output end of oscillating motor is installed by terminal pad
Line shaft, line shaft are fixed on the rotation side of main wing by hinge.Oscillating motor has small in size, the big spy of active force
Point, power output are rotation output, rotation of the main wing on oscillating motor output axis may be implemented, to realize main wing
Vertical direction on folding, simultaneously as oscillating motor have biggish torsion, also guarantee main wing in flight course
Stablize.
Further, the hinge at least there are two, and be evenly distributed on main wing.
Utility model has the advantages that realizing the folding of the main wing peace all-wing aircraft of flank itself using simple framework
And the folding of flank in vertical direction, structure is simple, can but provide stable effect, realizes the safety of flank and practical
The unification of property.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of folding side wing mechanism of the utility model；
Fig. 2 is the partial sectional view of 1 internal structure of display diagram.
Appended drawing reference record is as follows: 1- main wing, 1.1- lower panel, 1.2- top panel, the flat all-wing aircraft of 2-, 3- oscillating motor,
4- line shaft, 5- terminal pad, 6- hinge, 7- telescopic hydraulic cylinder, 8- connector, the fixed turntable of 9-, the flat wing axis of 10-.
Specific embodiment
The principles of the present invention and feature are described below in conjunction with attached drawing, example is served only for explaining that this is practical
It is novel, it is not intended to limit the scope of the utility model.
A kind of folding side wing mechanism (referring to Fig. 1 and Fig. 2), including main wing 1, main wing 1 include lower panel 1.1 and top panel
1.2, it is Wing Tank between lower panel 1.1 and top panel 1.2, the peaceful all-wing aircraft 2 of installation telescopic hydraulic cylinder 7, flat all-wing aircraft 2 pass through in Wing Tank
Flat wing axis 10 is mounted above between plate 1.2 and lower panel 1.1, and telescopic hydraulic cylinder 7 passes through fixed turntable 9 and is fixed in Wing Tank
Portion connects flat all-wing aircraft 2 by connector 8 after the output end of telescopic hydraulic cylinder 7 installs connector 8 by axis, folds one in main wing 1
Side is installed by fold mechanism.Connector is fixed on the end of flat all-wing aircraft.
Based on the above technical solution, the utility model is to reach the stability of the convenience and equipment that use,
Following improvement can also be made to above-mentioned technical solution:
The fold mechanism includes oscillating motor 3, and the output end of oscillating motor 3 installs power by terminal pad 5
Axis 4, line shaft 4 are fixed on main wing 1 by hinge 6.
The hinge 6 at least there are two, and be evenly distributed on the rotation side of main wing 1
When in use, oscillating motor overturns main wing in vertical direction, after being turned to preset angle, starting
Telescopic hydraulic cylinder opens flat all-wing aircraft, and such flank is just at the state being fully deployed, and when packing up, carries out reverse operating and just realizes side
The wing is packed up.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all practical at this
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (3)
1. a kind of folding side wing mechanism, which is characterized in that including main wing, main wing includes lower panel and top panel, lower panel and
Be Wing Tank between top panel, telescopic hydraulic cylinder peace all-wing aircraft be installed in Wing Tank, flat all-wing aircraft by flat wing axis be mounted above plate and
Between lower panel, telescopic hydraulic cylinder is fixed on inside Wing Tank on lower panel by fixed turntable, and the output end of telescopic hydraulic cylinder is logical
After crossing axis installation connector, flat all-wing aircraft is connected by connector, side is folded in main wing and fold mechanism is installed.
2. folding side wing mechanism according to claim 1, which is characterized in that the fold mechanism includes that swing is hydraulic
The output end of cylinder, oscillating motor installs line shaft by terminal pad, and line shaft is fixed on main wing by hinge.
3. folding side wing mechanism according to claim 2, which is characterized in that the hinge at least there are two, and
On the even rotation side for being distributed in main wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820756983.5U CN208181398U (en) | 2018-05-21 | 2018-05-21 | A kind of folding side wing mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820756983.5U CN208181398U (en) | 2018-05-21 | 2018-05-21 | A kind of folding side wing mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208181398U true CN208181398U (en) | 2018-12-04 |
Family
ID=64427362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820756983.5U Expired - Fee Related CN208181398U (en) | 2018-05-21 | 2018-05-21 | A kind of folding side wing mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208181398U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111746783A (en) * | 2020-07-01 | 2020-10-09 | 西湖大学 | A flank structure and navigation ware for navigation ware |
-
2018
- 2018-05-21 CN CN201820756983.5U patent/CN208181398U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111746783A (en) * | 2020-07-01 | 2020-10-09 | 西湖大学 | A flank structure and navigation ware for navigation ware |
| CN111746783B (en) * | 2020-07-01 | 2022-07-01 | 西湖大学 | A flank structure and navigation ware for navigation ware |
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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: 20181204 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |