CN207791132U - A kind of flying wing for unmanned plane - Google Patents
A kind of flying wing for unmanned plane Download PDFInfo
- Publication number
- CN207791132U CN207791132U CN201721686656.9U CN201721686656U CN207791132U CN 207791132 U CN207791132 U CN 207791132U CN 201721686656 U CN201721686656 U CN 201721686656U CN 207791132 U CN207791132 U CN 207791132U
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- flying wing
- shaft
- screw
- box cover
- flying
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Abstract
The utility model discloses a kind of flying wings for unmanned plane,Including lower casing and upper box cover,Activity is plugged with shaft in the first through hole that the upper box cover opens up,And the upper end of upper box cover is fixedly connected with shaft upper end by the first spring,The lower end of the shaft is fixedly plugged on lower casing,And runs through lower casing and reach the bottom end of lower casing,The flying wing that this is used for unmanned plane is simple in structure,By the way that lower casing is added,Upper box cover,Limited block,First screw,Holder,Sleeve and ball,When without using unmanned plane,Unclamp the second screw and the first screw,Second spring pulls downward on,Sleeve slide downward,First spring pulls up,Upper box cover also up moves,The first flying wing is under the drive of holder at this time,Start to receive in lower casing,The interior intracavitary that second flying wing is also formed toward the first flying wing and the second flying wing is received,Third flying wing lies across the upper end of lower casing,With very strong practicability.
Description
Technical field
The utility model is related to air vehicle technique fields, specially a kind of flying wing for unmanned plane.
Background technology
UAV, abbreviation unmanned plane are manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle, unmanned plane is actually the general designation of unmanned vehicle, from technical standpoint definition can be divided into：Nobody
Fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, unmanned parasol
Deng, compared with manned aircraft, it have small, low cost, it is easy to use, to operational environment require low, battlefield survival
The advantages that stronger, since UAV has great significance to Future Air Combat, environmental protection, plant protection, agricultural etc., but at present
The flying wing of unmanned plane be fixed greatly, be not easy to store, during transport, or during storage, fly
The row wing be easy to be crushed out of shape cause unmanned plane can not normal flight, the consequence that machine may be brought to ruin, thus propose one kind be used for
The unmanned plane during flying wing.
Utility model content
The purpose of this utility model is to provide a kind of flying wings for unmanned plane, to solve to carry in above-mentioned background technology
The problem of going out.
To achieve the above object, the utility model provides the following technical solutions：
A kind of flying wing for unmanned plane, including lower casing and upper box cover, in the first through hole that the upper box cover opens up
Activity is plugged with shaft, and the upper end of upper box cover is fixedly connected with shaft upper end by the first spring, and the lower end of the shaft is solid
Surely it is plugged on lower casing, and shaft runs through the bottom end by lower casing, the upper end of the shaft is located at the top of upper box cover
One section of pivot bush unit has limited block, is threaded with the first screw in the second through-hole opened up on the limited block, and described first
Screw is in one end of shaft to the annular groove opened up positioned at shaft outer wall, and the first screw offsets with groove inner wall, institute
The lower end edge for stating first through hole is symmetrically arranged with holder, and the both ends of the holder are respectively hinged at first through hole lower end edge
With the upper end of the first flying wing, first flying wing is hinged on close to one end of shaft on the lateral wall of sleeve, the sleeve
It is actively socketed in shaft, the lower end of the sleeve is fixedly connected by second spring with the upper end of lower casing, and described first flies
The other end of the row wing is hinged with the second flying wing, and first flying wing offers with the second flying wing close to hinged place rectangular
Groove is plugged with the both ends of same fixing card in the square groove, and the upper end of the fixing card is fixedly connected on upper box cover
Both ends lower end, the other end of second flying wing is hinged with third flying wing, second flying wing and third flying wing
Upper end be equipped with same fixed plate, the both ends of the fixed plate offer the second through-hole, the second through-hole internal thread connection
There is the second screw, and the lower end of the second screw is located at the lower section of fixed plate, the lower thread of second screw is connected to second
In the upper end screw hole of flying wing and third flying wing.
Preferably, the inside of spherical groove that the inner wall of the sleeve opens up is rotatably connected to ball, and sleeve by ball with
It is slidably connected between the groove opened up in shaft.
Preferably, the upper and lower ends of first flying wing and the second flying wing hinged place, the first flying wing and sleeve are cut with scissors
The upper and lower ends at the place of connecing are respectively connected with arc rubber slab.
Preferably, one end lower end of second flying wing far from the first flying wing is rotatably connected to idler wheel.
Compared with prior art, the utility model has the beneficial effects that：The flying wing that this is used for unmanned plane is simple in structure, leads to
Cross addition lower casing, upper box cover, limited block, the first screw, holder, sleeve, ball, the first spring, fixing card, the second screw and
Fixed plate unclamps the second screw and the first screw, second spring pulls downward on, sleeve slide downward when without using unmanned plane,
First spring pulls up, and upper box cover also up moves, and the first flying wing starts under the drive of holder in lower casing at this time
It receives, the interior intracavitary that the second flying wing is also formed toward the first flying wing and the second flying wing is received, and third flying wing lies across lower casing
Upper end has very strong practicability.
Description of the drawings
FIG. 1 is a schematic structural view of the utility model.
In figure：Shaft 1, lower casing 2, upper box cover 3, limited block 4, the first screw 5, holder 6, the first flying wing 7, arc rubber
Offset plate 8, sleeve 9, ball 10, the first spring 11, fixing card 12, idler wheel 13, the second screw 14, fixed plate 15.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
Referring to Fig. 1, the utility model provides a kind of technical solution：
A kind of flying wing for unmanned plane, including lower casing 2 and upper box cover 3, it is living in the first through hole that upper box cover 3 opens up
It is dynamic to be plugged with shaft 1, and the upper end of upper box cover 3 is fixedly connected with 1 upper end of shaft by the first spring, the lower end of shaft 1 is fixed
It is plugged on lower casing 2, and shaft 1 runs through the bottom end by lower casing 2, the upper end of shaft 1 is located at the one of the top of upper box cover 3
Section pivot bush unit has limited block 4, the first screw 5 is threaded in the second through-hole opened up on limited block 4, the first screw 5 leans on
One end of nearly shaft 1, which is arrived, to be located in the annular groove that 1 outer wall of shaft opens up, and the first screw 5 offsets with groove inner wall, and first leads to
The lower end edge in hole is symmetrically arranged with holder 6, and the both ends of holder 6 are respectively hinged at first through hole lower end edge and the first flight
The upper end of the wing 7, for the first flying wing 7 on the lateral wall that one end of shaft 1 is hinged on sleeve 9, sleeve 9 is actively socketed on shaft
On 1, the lower end of sleeve 9 is fixedly connected by second spring with the upper end of lower casing 2, and the other end of the first flying wing 7 is hinged with
Second flying wing, the first flying wing 7 and the second flying wing offer square groove close to hinged place, equal grafting in square groove
Have a both ends of same fixing card 12, the upper end of fixing card 12 is fixedly connected on the both ends lower end of upper box cover 3, the second flying wing it is another
One end is hinged with third flying wing, and the upper end of the second flying wing and third flying wing is equipped with same fixed plate 15, fixed plate 15
Both ends offer the second through-hole, the second through-hole internal thread is connected with the second screw 14, and the lower end of the second screw 14 be located at it is solid
The lower thread of the lower section of fixed board 15, the second screw 14 is connected in the upper end screw hole of the second flying wing and third flying wing, set
The inside of spherical groove that opens up of inner wall of cylinder 9 is rotatably connected to ball 10, and sleeve 9 by ball 10 with opened up in shaft 1 it is recessed
It is slidably connected between slot, the upper and lower ends of the first flying wing 7 and the second flying wing hinged place, the first flying wing 7 and sleeve 9 are hinged
The upper and lower ends at place are respectively connected with arc rubber slab 8, and one end lower end of second flying wing far from the first flying wing is rotatably connected to
Idler wheel 13.
Operation principle：When without using unmanned plane, the second screw 14 and the first screw 5 are unclamped, pulls upper box cover 3 is also past to move up
It is dynamic, 2 times movements of lower casing are pulled, second spring is pressed and moves downward, 9 slide downward of sleeve, so that lower casing 2 and upper box
The separation of lid 3 forms cavity to store the first flying wing 7, the second flying wing and third flying wing, and then, the first flying wing 7 is propping up
Under the drive of frame 6, starts to receive in lower casing 2, be cut with scissors between the first flying wing 7, the second flying wing and third flying wing three
It connects, you can its three is very easily recovered to lower casing 2 and the separation of upper box cover 3 is formed in cavity.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (4)
1. a kind of flying wing for unmanned plane, including lower casing（2）And upper box cover（3）, it is characterised in that：The upper box cover
（3）Activity is plugged with shaft in the first through hole opened up（1）, and upper box cover（3）Upper end and shaft（1）Upper end passes through the first bullet
Spring is fixedly connected, the shaft（1）Lower end be fixedly plugged in lower casing（2）On, and shaft（1）Through by lower casing（2）
Bottom end, the shaft（1）Upper end be located at upper box cover（3）One section of pivot bush unit of top have limited block（4）, the limit
Block（4）On be threaded with the first screw in the second through-hole for opening up（5）, first screw（5）Close to shaft（1）One end
To positioned at shaft（1）In the annular groove that outer wall opens up, and the first screw（5）It offsets with groove inner wall, the first through hole
Lower end edge is symmetrically arranged with holder（6）, the holder（6）Both ends be respectively hinged at first through hole lower end edge and first
Flying wing（7）Upper end, first flying wing（7）Close to shaft（1）One end be hinged on sleeve（9）Lateral wall on, institute
State sleeve（9）It is actively socketed on shaft（1）On, the sleeve（9）Lower end pass through second spring and lower casing（2）Upper end it is solid
Fixed connection, first flying wing（7）The other end be hinged with the second flying wing, first flying wing（7）With the second flight
The wing offers square groove close to hinged place, and same fixing card is plugged in the square groove（12）Both ends, it is described
Fixing card（12）Upper end be fixedly connected on upper box cover（3）Both ends lower end, the other end of second flying wing is hinged with
The upper end of three flying wings, second flying wing and third flying wing is equipped with same fixed plate（15）, the fixed plate（15）'s
Both ends offer the second through-hole, and the second through-hole internal thread is connected with the second screw（14）, and the second screw（14）Lower end
Positioned at fixed plate（15）Lower section, second screw（14）Lower thread be connected to the second flying wing and third flying wing
In the screw hole of upper end.
2. a kind of flying wing for unmanned plane according to claim 1, it is characterised in that：The sleeve（9）Inner wall
The inside of spherical groove opened up is rotatably connected to ball（10）, and sleeve（9）Pass through ball（10）With shaft（1）On the groove that opens up
Between be slidably connected.
3. a kind of flying wing for unmanned plane according to claim 1, it is characterised in that：First flying wing（7）
Upper and lower ends, the first flying wing with the second flying wing hinged place（7）With sleeve（9）The upper and lower ends of hinged place are respectively connected with arc
Shape rubber slab（8）.
4. a kind of flying wing for unmanned plane according to claim 1, it is characterised in that：Second flying wing is separate
One end lower end of first flying wing is rotatably connected to idler wheel（13）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721686656.9U CN207791132U (en) | 2017-12-07 | 2017-12-07 | A kind of flying wing for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721686656.9U CN207791132U (en) | 2017-12-07 | 2017-12-07 | A kind of flying wing for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207791132U true CN207791132U (en) | 2018-08-31 |
Family
ID=63283192
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721686656.9U Expired - Fee Related CN207791132U (en) | 2017-12-07 | 2017-12-07 | A kind of flying wing for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207791132U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109677595A (en) * | 2019-01-29 | 2019-04-26 | 深圳市律远汇智科技有限公司 | A kind of unmanned flight's device convenient for storage for taking photo by plane |
| CN109774948A (en) * | 2019-02-13 | 2019-05-21 | 山东蜂巢航空科技有限公司 | It is a kind of can a variety of load of carry oil electricity mixing multi-rotor unmanned aerial vehicle |
-
2017
- 2017-12-07 CN CN201721686656.9U patent/CN207791132U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109677595A (en) * | 2019-01-29 | 2019-04-26 | 深圳市律远汇智科技有限公司 | A kind of unmanned flight's device convenient for storage for taking photo by plane |
| CN109774948A (en) * | 2019-02-13 | 2019-05-21 | 山东蜂巢航空科技有限公司 | It is a kind of can a variety of load of carry oil electricity mixing multi-rotor unmanned aerial vehicle |
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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: 20180831 Termination date: 20191207 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |