CN207826526U - Outer wing lower wall panels in a kind of aircraft convenient for assembly - Google Patents
Outer wing lower wall panels in a kind of aircraft convenient for assembly Download PDFInfo
- Publication number
- CN207826526U CN207826526U CN201721904331.3U CN201721904331U CN207826526U CN 207826526 U CN207826526 U CN 207826526U CN 201721904331 U CN201721904331 U CN 201721904331U CN 207826526 U CN207826526 U CN 207826526U
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- CN
- China
- Prior art keywords
- slide bar
- slot
- rod
- connecting rod
- hole
- 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.)
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Abstract
The utility model discloses outer wing lower wall panels in a kind of aircraft convenient for assembly, including outer wing in aircraft, outer wing bottom is opened up there are two connecting rod slot in the aircraft, it is slidably fitted with connecting rod in connecting rod slot, and the bottom end of connecting rod extends to outside connecting rod slot, the bottom end of two connecting rods is welded with the same lower wall panels ontology, two connecting rod slots, which are located remotely from each other on the inner wall of side, offers slide bar slot, it is slidably fitted with slide bar in slide bar slot, and one end of slide bar extends to outside slide bar slot, connecting rod offers fixing groove close to the side of slide bar slot, slide bar is slidably connected close to one end of connecting rod with fixing groove, tension rod thru-hole is offered on the inner wall of slide bar slot bottom side, pull rod is slidably fitted in tension rod thru-hole, and the both ends of pull rod all extend to outside tension rod thru-hole.The utility model is simple in structure, easy to use, and assembly lower wall panels ontology of being more convenient for, operation is easy, and is saved the time, is more conducive to the work of people, improves working efficiency.
Description
Technical field
The utility model is related to outer wing lower wall panels in aircraft technology field more particularly to a kind of aircraft convenient for assembly.
Background technology
Aircraft refers to advancing by self power driving with wing, a tool or more tool engines, can be in space or air
In the density of itself be more than the aircraft of air, if the density of aircraft is less than air, it is exactly balloon or dirigible, if
There is no power plant, can only glide in the air, then be referred to as aerodone, if the wing of aircraft is not fixed, is rotated by wing
Lift is generated, is exactly helicopter or gyroplane, fixed wing aircraft is most common aircraft kenel.
Currently, outer wing lower wall panels majority is not easy to be assembled in existing aircraft, when assembly, is often more troublesome, when delaying
Between, it is unfavorable for the action of people, influences working efficiency, with the progress of science and technology, social development, people is to aircraft China and foreign countries
More stringent requirements are proposed for wing lower wall panels, so, we have proposed outer wing lower wall panels in a kind of aircraft convenient for assembly for solving
The certainly above problem.
Utility model content
Purpose of the utility model is to solve disadvantage existing in the prior art, and propose a kind of convenient for assembly
Outer wing lower wall panels in aircraft.
To achieve the goals above, the utility model uses following technical solution：
Outer wing lower wall panels in a kind of aircraft convenient for assembly, including outer wing in aircraft, outer wing bottom opens up in the aircraft
There are two connecting rod slot, it is slidably fitted with connecting rod in connecting rod slot, and the bottom end of connecting rod extends to outside connecting rod slot, two
The bottom end of connecting rod is welded with the same lower wall panels ontology, and two connecting rod slots are located remotely from each other on the inner wall of side and offer cunning
Bar slot is slidably fitted with slide bar in slide bar slot, and one end of slide bar extends to outside slide bar slot, and connecting rod is close to the side of slide bar slot
Fixing groove is offered, slide bar is slidably connected close to one end of connecting rod with fixing groove, and drawing is offered on the inner wall of slide bar slot bottom side
Rod through-hole is slidably fitted with pull rod in tension rod thru-hole, and the both ends of pull rod all extend to outside tension rod thru-hole, and pull rod is located at slide bar slot
Interior one end is welded and fixed with slide bar, and positioning rod through-hole is offered on the inner wall of slide bar slot bottom side, and positioning rod through-hole is located at connection
Between bar slot and tension rod thru-hole, positions in rod through-hole and be slidably fitted with locating rod, and the both ends of locating rod all extend to locating rod
Outside through-hole, the bottom of slide bar offers positioning runner, and top and the positioning runner of locating rod are slidably connected, positioning runner top side
Locating groove is offered on inner wall, locating groove is located at one end in positioning runner with locating rod and is adapted.
Preferably, the slide bar is located at the side in slide bar slot and offers kelly slot, and kelly is slidably fitted in kelly slot,
And one end of kelly extends to outside kelly slot, kelly is located at one end outside kelly slot and the inner wall of slide bar slot is welded and fixed.
Preferably, it is welded with the first spring being set on kelly on the inner wall of the slide bar slot far from slide bar side, the
One spring is welded and fixed with slide bar.
Preferably, it is installed with non-slip mat on the inner wall of the fixing groove, non-slip mat is in contact with slide bar.
Preferably, sliding slot is offered on the inner wall of the positioning rod through-hole both sides, the both sides of locating rod are welded with cunning
Block, two sliding blocks are slidably mounted on respectively in two sliding slots.
Preferably, be installed with fixed link in the sliding slot, sliding block is slidably located in fixed link, sliding slot bottom side it is interior
Second spring is welded on wall, second spring is welded and fixed with sliding block.
Compared with prior art, the utility model has the beneficial effects that：
(1), pass through outer wing, connecting rod slot, connecting rod, lower wall panels ontology, slide bar slot, slide bar, fixing groove, pull rod in aircraft
Through-hole, pull rod, the cooperation for positioning rod through-hole, locating rod, positioning runner, locating groove, kelly slot, kelly and the first spring, when
When needing that lower wall panels ontology is installed, first, under the cooperation of slide bar slot, slide bar, tension rod thru-hole and pull rod, slide bar is pulled in into slide bar
In slot；
(2), under the cooperation of positioning rod through-hole, locating rod, positioning runner and locating groove, locating rod is caught in positioning card
In slot, fixed slip bar connects connecting rod and the sliding of connecting rod slot under the cooperation of connecting rod slot, connecting rod and lower wall panels ontology
It connects, then, locating rod is skidded off out of locating groove, slide bar is caught in fixing groove, so as to complete the peace of lower wall panels ontology
Fill work；
The utility model is simple in structure, easy to use, and assembly lower wall panels ontology of being more convenient for, operation is easy, and saves the time, more
Contribute to the work of people, improves working efficiency.
Description of the drawings
Fig. 1 be the utility model proposes it is a kind of convenient for assembly aircraft in outer wing lower wall panels structural schematic diagram；
Fig. 2 be the utility model proposes it is a kind of convenient for assembly aircraft in outer wing lower wall panels part A structural schematic diagram.
In figure：Outer wing in 1 aircraft, 2 connecting rod slots, 3 connecting rods, 4 lower wall panels ontologies, 5 slide bar slots, 6 slide bars, 7 fixing grooves,
8 tension rod thru-holes, 9 pull rods, 10 positioning rod through-holes, 11 locating rods, 12 positioning runners, 13 locating grooves, 14 kelly slots, 15 kellies,
16 first springs.
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.
Referring to Fig.1-2, outer wing lower wall panels in a kind of aircraft convenient for assembly, including outer wing 1 in aircraft, outer wing 1 in aircraft
Bottom is opened up there are two connecting rod slot 2, is slidably fitted with connecting rod 3 in connecting rod slot 2, and the bottom end of connecting rod 3 extends to company
Outside extension bar slot 2, the bottom end of two connecting rods 3 is welded with the same lower wall panels ontology 4, and two connecting rod slots 2 are located remotely from each other side
Inner wall on offer slide bar slot 5, slide bar 6 is slidably fitted in slide bar slot 5, and one end of slide bar 6 extends to slide bar slot 5
Outside, connecting rod 3 offers fixing groove 7 close to the side of slide bar slot 5, and slide bar 6 is slided close to one end of connecting rod 3 and fixing groove 7
Connection offers tension rod thru-hole 8 on the inner wall of 5 bottom side of slide bar slot, is slidably fitted with pull rod 9 in tension rod thru-hole 8, and pull rod 9
Both ends all extend to outside tension rod thru-hole 8, and pull rod 9 is located at one end in slide bar slot 5 and is welded and fixed with slide bar 6,5 bottom side of slide bar slot
Positioning rod through-hole 10 is offered on inner wall, positioning rod through-hole 10 positions rod through-hole between connecting rod slot 2 and tension rod thru-hole 8
Locating rod 11 is slidably fitted in 10, and the both ends of locating rod 11 all extend to outside positioning rod through-hole 10, the bottom of slide bar 6 opens up
There are positioning runner 12, top and the positioning runner 12 of locating rod 11 to be slidably connected, offered on the inner wall of 12 top side of positioning runner
Locating groove 13, locating groove 13 are located at one end in positioning runner 12 with locating rod 11 and are adapted, by outer wing in aircraft 1,
Connecting rod slot 2, connecting rod 3, lower wall panels ontology 4, slide bar slot 5, slide bar 6, fixing groove 7, tension rod thru-hole 8, pull rod 9, locating rod are logical
The cooperation in hole 10, locating rod 11, positioning runner 12, locating groove 13, kelly slot 14, kelly 15 and the first spring 16, works as needs
When lower wall panels ontology 4 is installed, first, under the cooperation of slide bar slot 5, slide bar 6, tension rod thru-hole 8 and pull rod 9, slide bar 6 is pulled in into cunning
In bar slot 5, under the cooperation of positioning rod through-hole 10, locating rod 11, positioning runner 12 and locating groove 13, locating rod 11 is caught in
In locating groove 13, fixed slip bar 6, under the cooperation of connecting rod slot 2, connecting rod 3 and lower wall panels ontology 4, by connecting rod 3 and even
Extension bar slot 2 is slidably connected, and then, locating rod 11 is skidded off out of locating groove 13, slide bar 6 is caught in fixing groove 7, to complete
At the installment work of lower wall panels ontology 4, the utility model is simple in structure, easy to use, assembly lower wall panels of being more convenient for ontology 4,
Operation is easy, and saves the time, is more conducive to the work of people, improves working efficiency.
In the utility model, slide bar 6 is located at the side in slide bar slot 5 and offers kelly slot 14, and peace is slided in kelly slot 14
One end equipped with kelly 15, and kelly 15 extends to outside kelly slot 14, and kelly 15 is located at one end and slide bar slot 5 outside kelly slot 14
Inner wall be welded and fixed, slide bar slot 5 is welded with the first spring 16 being set on kelly 15 on the inner wall far from 6 side of slide bar,
First spring 16 is welded and fixed with slide bar 6, and non-slip mat is installed on the inner wall of fixing groove 7, and non-slip mat connects with slide bar 6
It touches, sliding slot is offered on the inner wall of 10 both sides of positioning rod through-hole, the both sides of locating rod 11 are welded with sliding block, two sliding blocks point
It is not slidably mounted in two sliding slots, fixed link is installed in sliding slot, sliding block is slidably located in fixed link, sliding slot bottom side
Inner wall on be welded with second spring, second spring is welded and fixed with sliding block, pass through outer wing in aircraft 1, connecting rod slot 2, connection
Bar 3, lower wall panels ontology 4, slide bar slot 5, slide bar 6, fixing groove 7, tension rod thru-hole 8, pull rod 9, positioning rod through-hole 10, locating rod 11,
The cooperation of positioning runner 12, locating groove 13, kelly slot 14, kelly 15 and the first spring 16, when needing to install lower wall panels ontology 4
When, first, under the cooperation of slide bar slot 5, slide bar 6, tension rod thru-hole 8 and pull rod 9, slide bar 6 is pulled in slide bar slot 5, is being positioned
Rod through-hole 10, locating rod 11, positioning runner 12 and locating groove 13 cooperation under, locating rod 11 is caught in locating groove 13,
Fixed slip bar 6 connects connecting rod 3 and the sliding of connecting rod slot 2 under the cooperation of connecting rod slot 2, connecting rod 3 and lower wall panels ontology 4
It connects, then, locating rod 11 is skidded off out of locating groove 13, slide bar 6 is caught in fixing groove 7, so as to complete lower wall panels sheet
The installment work of body 4, the utility model is simple in structure, easy to use, and assembly lower wall panels of being more convenient for ontology 4, operation is easy, and is saved
Time is more conducive to the work of people, improves working efficiency.
In the utility model, when needing to assemble lower wall panels ontology 4, first, pull rod 9 is pulled, makes pull rod 9 with moving slide-bar 6
It is slided to the direction far from connecting rod slot 2, slide bar 6 is slid completely into slide bar slot 5, by locating groove 13 and positioning rod through-hole 10
It aligning, under the action of second spring, locating rod 11 is slided to the direction of close slide bar 6 and is entered in locating groove 13, Gu
Determine slide bar 6, at this point, connecting rod 3 and connecting rod slot 2 are slidably connected, connecting rod 3 is made to be slided to close to the direction of outer wing 1 in aircraft
It is dynamic, when sliding into fixing groove 7 and slide bar slot 5 aligns, locating rod 11 is pulled, makes locating rod 11 to the direction far from slide bar 6
Sliding, when locating rod 11 is skidded off out of locating groove 13, under the action of the first spring 16, slide bar 6 is to close to connecting rod 3
Direction is slided and is entered in fixing groove 7, fixed connecting rod 3, so as to complete the work of assembly lower wall panels ontology 4.
The preferable specific implementation mode of the above, only the utility model, but the scope of protection of the utility model is not
Be confined to this, any one skilled in the art within the technical scope disclosed by the utility model, according to this practicality
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
1. outer wing lower wall panels in a kind of aircraft convenient for assembly, including outer wing (1) in aircraft, which is characterized in that in the aircraft
Outer wing (1) bottom is opened up there are two connecting rod slot (2), and connecting rod slot (2) is interior to be slidably fitted with connecting rod (3), and connecting rod (3)
Bottom end extend to connecting rod slot (2) outside, the bottom end of two connecting rods (3) is welded with the same lower wall panels ontology (4), two companies
Extension bar slot (2) is located remotely from each other on the inner wall of side and offers slide bar slot (5), and slide bar (6) is slidably fitted in slide bar slot (5),
And one end of slide bar (6) extends to slide bar slot (5) outside, connecting rod (3) offers fixing groove (7) close to the side of slide bar slot (5),
Slide bar (6) is slidably connected close to one end of connecting rod (3) with fixing groove (7), and pull rod is offered on the inner wall of slide bar slot (5) bottom side
Through-hole (8), tension rod thru-hole (8) is interior to be slidably fitted with pull rod (9), and the both ends of pull rod (9) all extend to tension rod thru-hole (8) outside,
Pull rod (9) is located at one end in slide bar slot (5) and is welded and fixed with slide bar (6), and positioning is offered on the inner wall of slide bar slot (5) bottom side
Rod through-hole (10), positioning rod through-hole (10) are located between connecting rod slot (2) and tension rod thru-hole (8), sliding in positioning rod through-hole (10)
It is dynamic that locating rod (11) is installed, and the both ends of locating rod (11) all extend to positioning rod through-hole (10) outside, the bottom of slide bar (6) is opened
Equipped with positioning runner (12), top and the positioning runner (12) of locating rod (11) are slidably connected, positioning runner (12) top side it is interior
Locating groove (13) is offered on wall, locating groove (13) is located at one end in positioning runner (12) with locating rod (11) and mutually fits
Match.
2. outer wing lower wall panels in a kind of aircraft convenient for assembly according to claim 1, which is characterized in that the slide bar
(6) it is located at the side in slide bar slot (5) and offers kelly slot (14), kelly (15) is slidably fitted in kelly slot (14), and block
One end of bar (15) extends to kelly slot (14) outside, and kelly (15) is located at the interior of the one end of kelly slot (14) outside and slide bar slot (5)
Wall is welded and fixed.
3. outer wing lower wall panels in a kind of aircraft convenient for assembly according to claim 1, which is characterized in that the slide bar slot
(5) be welded with the first spring (16) being set on kelly (15) on the inner wall far from slide bar (6) side, the first spring (16) with
Slide bar (6) is welded and fixed.
4. outer wing lower wall panels in a kind of aircraft convenient for assembly according to claim 1, which is characterized in that the fixing groove
(7) non-slip mat is installed on inner wall, non-slip mat is in contact with slide bar (6).
5. outer wing lower wall panels in a kind of aircraft convenient for assembly according to claim 1, which is characterized in that the locating rod
Sliding slot is offered on the inner wall of through-hole (10) both sides, the both sides of locating rod (11) are welded with sliding block, and two sliding blocks are slided respectively
It is dynamic to be mounted in two sliding slots.
6. outer wing lower wall panels in a kind of aircraft convenient for assembly according to claim 5, which is characterized in that in the sliding slot
It is installed with fixed link, sliding block is slidably located in fixed link, and second spring, the second bullet are welded on the inner wall of sliding slot bottom side
Spring is welded and fixed with sliding block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721904331.3U CN207826526U (en) | 2017-12-29 | 2017-12-29 | Outer wing lower wall panels in a kind of aircraft convenient for assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721904331.3U CN207826526U (en) | 2017-12-29 | 2017-12-29 | Outer wing lower wall panels in a kind of aircraft convenient for assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207826526U true CN207826526U (en) | 2018-09-07 |
Family
ID=63390766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721904331.3U Expired - Fee Related CN207826526U (en) | 2017-12-29 | 2017-12-29 | Outer wing lower wall panels in a kind of aircraft convenient for assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207826526U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110040237A (en) * | 2019-03-25 | 2019-07-23 | 天津大学 | A kind of lift sub pin device for realizing quick assembling wing |
-
2017
- 2017-12-29 CN CN201721904331.3U patent/CN207826526U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110040237A (en) * | 2019-03-25 | 2019-07-23 | 天津大学 | A kind of lift sub pin device for realizing quick assembling wing |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180907 Termination date: 20181229 |