CN109733588A - A kind of wing attaching/detaching apparatus - Google Patents
A kind of wing attaching/detaching apparatus Download PDFInfo
- Publication number
- CN109733588A CN109733588A CN201811511802.3A CN201811511802A CN109733588A CN 109733588 A CN109733588 A CN 109733588A CN 201811511802 A CN201811511802 A CN 201811511802A CN 109733588 A CN109733588 A CN 109733588A
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- CN
- China
- Prior art keywords
- wing
- fuselage
- detaching apparatus
- centre section
- attaching
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Abstract
The present invention relates to a kind of wing attaching/detaching apparatus.Wing attaching/detaching apparatus, comprising: starter is located at fuselage wing centre section；And fixed device is popped up, it is configured to fix the fuselage wing centre section and the side wing；Wherein, when the fixed device of the pop-up is further configured to starter triggering, the side wing is popped up from the fuselage wing centre section.Unmanned plane wing rapid dismounting apparatus of the invention can use the starter and the fixed device of the pop-up, and the side wing of fuselage wing centre section two sides described in fast assembling-disassembling improves unmanned plane in outer operating efficiency.
Description
Technical field
The present invention relates to air vehicle technique field, a kind of particularly wing attaching/detaching apparatus.
Background technique
Unmanned plane field in China's is quickly grown in recent years, and the unmanned plane yield in China occupies first place in the world.Currently on the market without
Man-machine fuselage and airfoil member occupies a large amount of empty still by the way of being fixedly connected during packaging, transport and collection
Between, and be easily damaged, transport is got up very inconvenient.Some unmanned planes use insertion airfoil.That is, wing is pluggablely by arriving
On fuselage, and it is screwed.But the position of screw is not easy to dismount than more covert.Unmanned plane wing also and body
Connection type adopt be screwed, the modes such as rubber band is fixed, these fixed form reliabilities are bad, damage easy to aging, dismounting
Cumbersome, part mostly etc., can cause lower in outer operating efficiency.
Similar unmanned plane wing device for quickly disassembling currently on the market, including wing and fuselage are fixed with wing protheca on wing
Pipe, wing rear sleeve and wing tubular girder, the wing anterior cannula, wing rear sleeve and wing tubular girder are inserted embedding respectively
In the corresponding set hole of fuselage, also it is connected and fixed by clamp button of the spring mechanism between the wing and fuselage.This fast dismounting
Although setting cracking can be mounted on wing on fuselage, when requiring wing being stably connected with upper, clamp button of the spring needs
There are enough stiffness factors, but wing can be disassembled by just needing very big power just in disassembly, using simultaneously inconvenient.
Therefore, this field needs a kind of new wing attaching/detaching apparatus to be able to solve the mode that existing wing is fixedly connected with body techniques generation
The problem of, it improves in outer operating efficiency.
Summary of the invention
For the technical problems in the prior art, the invention discloses a kind of wing attaching/detaching apparatus, comprising: starting dress
It sets, is located at fuselage wing centre section；And fixed device is popped up, it is configured to fix the fuselage wing centre section and the side wing；Wherein, institute
When stating the fixed device of pop-up and being further configured to starter triggering, the side is popped up from the fuselage wing centre section
The wing.
Further, the wing attaching/detaching apparatus, wherein the starter is connect with the fixed device of the pop-up；?
The starter touches the pop-up fixed device when triggering.
Further, the wing attaching/detaching apparatus further includes one or more pins；One or more of pins positions are in institute
On the end face for stating fuselage wing centre section or the side wing；Wherein one or more of pins are adapted for insertion into positioned at the fuselage wing centre section or institute
It states on the end face of the side wing in corresponding pin hole.
Further, the wing attaching/detaching apparatus, wherein the fixed device of the pop-up includes fixing pipe and limitting casing；Its
Described in fixing pipe be arranged on the side wing, the limitting casing is arranged on the fuselage wing centre section and accommodates the fixing pipe,
The elastic slice of the fixing pipe is suitable for engaging the limitting casing.
Further, the wing attaching/detaching apparatus is set to institute wherein the fixed device of the pop-up further includes spring
It states in fixing pipe, when the fuselage wing centre section and the fixed side wing, the spring is in compressive state.
Further, the wing attaching/detaching apparatus, wherein the limitting casing includes card slot, the elastic slice is suitable for engagement institute
State the edge of card slot.
Further, the wing attaching/detaching apparatus, wherein the starter is further configured to touch the bullet
Piece, so that the elastic slice is detached from the edge of card slot.
Further, the wing attaching/detaching apparatus, wherein the starter further includes sliding pin and sliding pin spring, it is described
Sliding pin slidably touches the elastic slice, sliding pin described in the sliding pin spring reset.
Further, the wing attaching/detaching apparatus, wherein a part of the sliding pin or sliding pin is located in the wing.
A kind of unmanned plane wing rapid dismounting apparatus of the invention, including any unmanned plane wing fast assembling-disassembling dress
It sets.
Dismounting can be rapidly completed using the fixed device of pop-up in packaging, transport and collection in unmanned plane wing of the invention
Wing work, reduces space shared by unmanned plane wing, while improving unmanned plane in outer operating efficiency.
Detailed description of the invention
In the following, the preferred embodiment of the present invention will be described in more detail in conjunction with attached drawing, in which:
Fig. 1 is the wing attaching/detaching apparatus overall structure figure according to one embodiment of the invention；
Fig. 2 a is the wing junction schematic layout pattern according to one embodiment of the invention；
Fig. 2 b is the wing junction schematic layout pattern according to one embodiment of the invention；
Fig. 3 is that fixed principle of device partial enlarged view is popped up according to the disassembly wing of one embodiment of the invention；
Fig. 4 is that fixed principle of device schematic diagram is popped up according to the disassembly wing of one embodiment of the invention；
Fig. 5 is the device for rapidly starting explosive view according to one embodiment of the invention.
[symbol description]
1 fuselage wing centre section 11 fixes limitting casing groove
12 one or more fixed starter grooves of pin 13
The 2 side wings 21 are fixed to pop up the fixed matching of device groove 22 pin hole
3 pop up fixed 31 fixing pipe of device
311 elastic slice, 312 spring
32 limitting casing, 321 card slot
4 starter, 41 sliding pin
42 sliding pin frame, 421 frame lid
4211 second through-hole, 422 first through hole, 43 sliding pin spring
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is
A part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art
Every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the following detailed description, the specific embodiment for being used to illustrate the application as the application a part may refer to
Each Figure of description.In the accompanying drawings, similar appended drawing reference describes substantially similar component in different drawings.This Shen
Each specific embodiment please has carried out description detailed enough following, so that having the general of ability domain-dependent knowledge and technology
Logical technical staff can implement the technical solution of the application.It should be appreciated that can also be using other embodiments or to the application
Embodiment carry out structure, logic or electrical property change.
Below by a specific embodiment to further illustrate the technical scheme of the present invention.Those skilled in the art should
Understand, description below should not be used to limit the present invention just for the sake of the convenient understanding for technical solution of the present invention
Protection scope.
It is according to the present invention one that Fig. 1, which is according to the wing attaching/detaching apparatus overall structure figure of one embodiment of the invention, Fig. 2 a,
Wing junction schematic layout pattern, Fig. 2 b of a embodiment are to be laid out to illustrate according to the wing junction of one embodiment of the invention
Figure.As shown, wing attaching/detaching apparatus, comprising: fuselage wing centre section 1, Bian Yi 2, pop up fixed device 3, starter 4.Starting dress
4 are set, fuselage wing centre section 1 is located at.Fixed device 3 is popped up, is configured to fuselage wing centre section 1 and the side wing 2 is fixed；Wherein, it pops up
When fixed device 3 is further configured to the triggering of starter 3, the side wing 2 is popped up from fuselage wing centre section 1.Starter 4 and bullet
Device 3 is fixed out to connect, and is touched when starter 4 triggers and is popped up fixed device 3.
As shown, according to one embodiment of present invention, wing attaching/detaching apparatus further includes one or more pins；One or
Multiple pins 12 are located on the end face of fuselage wing centre section 1 or the side wing 2；Wherein one or more pins 12 are adapted for insertion into positioned at fuselage wing centre section 1
Or on the end face of the side wing 2 in corresponding pin hole 22.Such as shown in Fig. 2 a embodiment, one or more pins 12 are located in fuselage
On 1 end face of the wing, pin hole 22 is located on 2 end face of the side wing.Fuselage wing centre section 1 and the side wing 2 pass through one or more pins 12 with match pin hole
22 clampings, it should be understood by those skilled in the art that snap fit is only a kind of embodiment connected, it is existing in this field
Other connection types also can be applied to one or more pins 12 with match the connection between pin hole 22.
As shown, according to one embodiment of present invention, wherein one or more pins 12, can be used one it is flat convex
Connector out, it should be understood by those skilled in the art that the shape of the replaceable one or more pins 12 of the connector of other shapes, due to
The connection as fixed main body wing centre section 1 and the side wing 2 of the connector, if one flat protrusion connector of selection, the connector area
Size is not preferably less than the area of limitting casing 32.22 interface internal structural relation of respective pin hole and a flat protrusion connector phase
Match.
Optionally, according to another embodiment of the invention, one or more pins 12 can be selected multiple flat protrusions and connect
Head optionally adds multiple respective pin holes 22, to increase the fixed-area of fuselage wing centre section 1 Yu the side wing 2, prevents fuselage wing centre section 1
It is detached from work with the side wing 2.
As shown, according to one embodiment of present invention, popping up fixed device 3 includes fixing pipe 31 and limitting casing 32.
Limitting casing 32 is fixed in fixed limitting casing groove 11, is located at 1 end face of fuselage wing centre section.The fixed corresponding limit of limitting casing groove 11
32 position of frame is located at the end face of fuselage wing centre section 1, and in the same plane with 32 end face of limitting casing and 1 end face of fuselage wing centre section.Machine
Body wing centre section 1 is by limitting casing 32 and pops up the fixed clamping of device 3, it should be understood by those skilled in the art that snap fit is only to connect
A kind of embodiment connect, other existing connection types also can be applied to fuselage wing centre section 1 and the fixed dress of pop-up in this field
Set the connection between 3.
As shown, according to one embodiment of present invention, fixing pipe 31 is arranged on the side wing 2, the setting of limitting casing 32 exists
1 and fixing pipe 31 is accommodated on fuselage wing centre section.Above 31 outer wall of fixing pipe, the elastic slice 311 in fixing pipe 31 is suitable for nibbling elastic slice 311
Close limitting casing 32.Optionally, other existing connection types also can be applied between elastic slice 311 and limitting casing 32 in this field
Connection.
As shown, according to one embodiment of present invention, popping up fixed device 3 further includes spring 312, and spring 312 is set
It is placed in fixing pipe 31, when fuselage wing centre section 1 and the fixed side wing 2, spring 312 is in compressive state.Spring 312 and fixing pipe 31
Welding can be used or adhesion mode connects, it should be understood by those skilled in the art that welding manner is only a kind of implementation connected
Mode, other existing connection types also can be applied to the connection of spring 312 Yu fixing pipe 31 in this field.Fixing pipe 31 is another
Outer one end is fixed on the fixed of 2 end face of the side wing and pops up fixed device groove 21.
As shown, according to one embodiment of present invention, starter 4 includes fixed starter groove 13, fixed
Starter groove 13 is for the fixed starter 4 of fuselage wing centre section 1.Fixed starter groove 13 leads to above fuselage wing centre section 1
Crossing fixed starter groove 13 can be fixed by fuselage wing centre section 1 and starter 4, and fuselage wing centre section 1 can use with starter 4
Starter pit 13 is clamped, it should be understood by those skilled in the art that snap fit is only a kind of embodiment connected, this
Other existing connection types also can be applied to the connection between fuselage wing centre section 1 and starter 4 in field.
It is root that Fig. 3, which is according to the fixed principle of device partial enlarged view of the disassembly wing of one embodiment of the invention pop-up, Fig. 4,
Fixed principle of device schematic diagram is popped up according to the disassembly wing of one embodiment of the invention.As shown, one according to the present invention
Embodiment, elastic slice 311 is by the pressure of 32 outer wall of limitting casing lower than 32 inner wall of limitting casing when fixing pipe 31 is matched with limitting casing 32
Pressure, elastic slice 311 pass through 32 port of limitting casing, and elastic slice 311 passes through card slot 321 when fixing pipe 31 and limitting casing 32 arrive relative position
Elastic slice 311 restores to the original state.Spring 312 is fixed pipe 31 and limitting casing 32 simultaneously, when generating compression generation elastic deformation, elasticity
Power acts on the edge of elastic slice 311 and the edge of card slot 321.
As shown, according to one embodiment of present invention, limitting casing 32 includes card slot 321, card slot 321 and limitting casing 32
It is fixedly connected.Elastic slice 311 and fixing pipe inner spring 312 pass through card slot 321 and engage connection with fixing pipe 31.Elastic slice 311 and limit
32 one end of frame can be used engagement, occlusion or snap fit and be fixedly connected, it should be understood by those skilled in the art that engagement, occlusion or
Person's snap fit is only a kind of embodiment connected, other existing connection types also can be applied to elastic slice in this field
311 with the connection of limitting casing 32, present invention preferably uses engagements to connect.
As shown, according to one embodiment of present invention, starter 3 is further configured to after touching elastic slice 311,
The edge of the disengaging card slot 321 of elastic slice 311.That is, trigger shrapnel 311 engages connection with the releasing of limitting casing 32, so that in compression shape
The spring 312 of state starts, and drives the pop-up outward together of fixing pipe 31, completes the disengaging work of wing 2 and fuselage wing centre section 1.
Fig. 5 is the device for rapidly starting explosive view according to one embodiment of the invention.As shown, starter 4 includes
Sliding pin 41 and sliding pin spring 43.Sliding pin 41 slidably touches elastic slice 311, and sliding pin spring 43 is resetted by the sliding of sliding pin 41.Its
In, frame lid 421, sliding pin 41, sliding pin spring 43 are on limitting casing 32.Sliding pin 41 is in sliding pin frame 42 and between slip lid 421.Sliding pin
The first through hole 422 and the second through-hole 4211 that restricted sliding pin 41 slides on frame 42 and slip lid 421.Sliding pin frame 42 and sliding pin 41 it
Between the sliding pin spring 43 that slides of restricted sliding pin 41.
As shown, according to one embodiment of present invention, operator makes sliding pin 41 in first through hole by lower slide pin 41
422 and second through-hole 4211 axis direction slide downward, 41 sliding scale of sliding pin is in sliding pin frame 42 and frame lid 421, sliding pin
41 slide downwards withstand elastic slice 311, and deformation occurs downwards by 41 pressure of sliding pin for elastic slice 311, and 311 outer wall height of elastic slice is lower than limit
When 32 inside wall height of frame, the release of 312 elastic force of spring pops up fixed device 3 and controls the pop-up of the side wing 2, is detached from fuselage wing centre section 1.Starting
Between sliding pin 41 and sliding pin frame 42, sliding pin 41 moves downward sliding pin spring 43 and bullet is occurred by pressure the sliding pin spring 43 of device 4
Property deformation, when unclamping sliding pin 41, sliding pin 41 sliding pin spring 43 elastic force effect under return to origin-location.
Above-described embodiment is used for illustrative purposes only, and not be limitation of the present invention, correlative technology field it is general
Logical technical staff can also make a variety of changes and modification without departing from the present invention, therefore, all equivalent
Technical solution also should belong to scope disclosed by the invention.
Claims (10)
1. a kind of wing attaching/detaching apparatus, comprising:
Starter is located at fuselage wing centre section；And
Fixed device is popped up, is configured to fix the fuselage wing centre section and the side wing；
Wherein, when the fixed device of the pop-up is further configured to starter triggering, from the fuselage wing centre section
Pop up the side wing.
2. wing attaching/detaching apparatus according to claim 1, wherein the starter is connect with the fixed device of the pop-up；
The fixed device of the pop-up is touched in starter triggering.
3. wing attaching/detaching apparatus according to claim 1 further includes one or more pins；One or more of pins positions in
On the end face of the fuselage wing centre section or the side wing；Wherein one or more of pins be adapted for insertion into positioned at the fuselage wing centre section or
On the end face of the side wing in corresponding pin hole.
4. wing attaching/detaching apparatus according to claim 1, wherein the fixed device of the pop-up includes fixing pipe and limitting casing；
Wherein the fixing pipe is arranged on the side wing, and the limitting casing is arranged on the fuselage wing centre section and accommodates the fixation
Pipe, the elastic slice of the fixing pipe are suitable for engaging the limitting casing.
5. wing attaching/detaching apparatus according to claim 4 is set to wherein the fixed device of the pop-up further includes spring
In the fixing pipe, when the fuselage wing centre section and the fixed side wing, the spring is in compressive state.
6. wing attaching/detaching apparatus according to claim 5, wherein the limitting casing includes card slot, the elastic slice is suitable for engagement
The edge of the card slot.
7. wing attaching/detaching apparatus according to claim 5, wherein the starter is further configured to described in touch
Elastic slice, so that the elastic slice is detached from the edge of card slot.
8. wing attaching/detaching apparatus according to claim 7, wherein the starter further includes sliding pin and sliding pin spring, institute
It states sliding pin slidably and touches the elastic slice, sliding pin described in the sliding pin spring reset.
9. wing attaching/detaching apparatus according to claim 8, wherein a part of the sliding pin or sliding pin is located at the wing
In.
10. a kind of unmanned plane, including the wing attaching/detaching apparatus as described in claim 1-9 is any.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811511802.3A CN109733588A (en) | 2018-12-11 | 2018-12-11 | A kind of wing attaching/detaching apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811511802.3A CN109733588A (en) | 2018-12-11 | 2018-12-11 | A kind of wing attaching/detaching apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109733588A true CN109733588A (en) | 2019-05-10 |
Family
ID=66358806
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811511802.3A Pending CN109733588A (en) | 2018-12-11 | 2018-12-11 | A kind of wing attaching/detaching apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109733588A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278240A (en) * | 2020-11-06 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
| US20220234717A1 (en) * | 2019-09-05 | 2022-07-28 | Autel Robotics Co., Ltd. | Wing detachment assembly and aerial vehicle |
| CN114987734A (en) * | 2022-05-31 | 2022-09-02 | 观典防务技术股份有限公司 | Wing quick assembly disassembly device and aircraft |
-
2018
- 2018-12-11 CN CN201811511802.3A patent/CN109733588A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20220234717A1 (en) * | 2019-09-05 | 2022-07-28 | Autel Robotics Co., Ltd. | Wing detachment assembly and aerial vehicle |
| CN112278240A (en) * | 2020-11-06 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
| CN112278240B (en) * | 2020-11-06 | 2021-12-28 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
| CN114987734A (en) * | 2022-05-31 | 2022-09-02 | 观典防务技术股份有限公司 | Wing quick assembly disassembly device and aircraft |
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