CN215205387U - Stable form attach fitting that aviation seat used - Google Patents
Stable form attach fitting that aviation seat used Download PDFInfo
- Publication number
- CN215205387U CN215205387U CN202120900379.7U CN202120900379U CN215205387U CN 215205387 U CN215205387 U CN 215205387U CN 202120900379 U CN202120900379 U CN 202120900379U CN 215205387 U CN215205387 U CN 215205387U
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- column
- connecting rod
- connecting block
- guide rail
- clamping
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Abstract
The utility model discloses a stable form connector for aviation seat, which comprises a guide rail and a connecting rod, wherein a moving groove is arranged at the center of the top of the guide rail, the inside of the moving groove is slidably connected with the connecting rod, a limit block is sleeved at the middle part of the connecting rod, the other end block at the top of the limit block is connected with a positioning column, the bottom of the side surface of the positioning column is in threaded connection with one end of the bottom of the moving groove, the connecting rod comprises a support column, a first connecting block, a clamping column, a second connecting block and an anti-falling sleeve, the bottom of the support column is in threaded connection with the first connecting block, and the bottom of the first connecting block is provided with a clamping groove. Avoid the connecting rod to take place to rock, loosen with the guide rail and take off, security when increasing the use.
Description
Technical Field
The utility model relates to an aviation seat technical field specifically is a stable form attach fitting that aviation seat used.
Background
The aviation seat is a seat for flying personnel and passengers on an airplane, a pneumatic or mechanical mechanism is arranged in the aviation seat, a seat back is operated to be inclined backwards, so that the passengers can be in a supine state, and the aviation seat is connected and fixed with a guide rail on the floor of the aviation airplane through a connecting joint, however, the existing aviation seat connecting joint has the following defects: the connector structure is complicated, unable quick location, and dismantles and install inconveniently, and the aircraft takes place to jolt under the effect of air current and rocks, leads to taking off between connector and the guide rail and taking off, has certain potential safety hazard.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a stable form attach fitting that aviation seat was used to solve the attach fitting structure that proposes in the above-mentioned background art complicacy, unable quick location, and dismantle with the installation inconvenient, the aircraft takes place to jolt and rocks under the effect of air current, leads to the pine to take off between attach fitting and the guide rail, has the problem of certain potential safety hazard.
In order to achieve the above object, the utility model provides a following technical scheme: a stable type connecting joint for an aviation seat comprises a guide rail and a connecting rod, wherein a moving groove is formed in the center of the top of the guide rail, a connecting rod is connected inside the moving groove in a sliding manner, a limiting block is sleeved in the middle of the connecting rod, the other end of the top of the limiting block is connected with a positioning column in a clamping way, the bottom of the side surface of the positioning column is in threaded connection with one end of the bottom of the moving groove, the connecting rod comprises a supporting column, a first connecting block, a clamping column, a second connecting block and an anti-falling sleeve, the bottom of the supporting column is in threaded connection with the first connecting block, the bottom of the first connecting block is provided with a clamping groove, the inside of the clamping groove is clamped and connected with a clamping column, the bottom of the clamping column is fixedly provided with a second connecting block, the joint of the clamping column and the clamping groove is fixedly connected with one end of the inner wall of the anti-drop sleeve, the junction of support column and first connecting block and the other end fixed connection of anticreep cover inner wall.
As an optimal technical scheme of the utility model, the shock pad has been laid with the junction of guide rail to the reference column.
As an optimized technical solution of the utility model, the outside of anticreep cover and the other end sliding connection of removal tank bottom portion.
As an optimized technical scheme of the utility model, the mounting hole has all been seted up to the corner at guide rail top.
As an optimal technical scheme of the utility model, the inside fixed mounting of support column has a plurality of support piece, a plurality of support piece all includes stand and a plurality of resistance to compression board, the equal fixed mounting in both sides of stand has a plurality of resistance to compression board, a plurality of the equal fixed mounting in inside of stand has the stiffening rib.
As an optimal technical scheme of the utility model, a plurality of fixed connection is at the both ends of support column inner wall respectively at the both ends of stand.
Compared with the prior art, the beneficial effects of the utility model are that: connecting rod convenient to use person installs the dismantlement, and when the aircraft took place to jolt and rock under the effect of air current, the reference column was fixed the position of stopper from one side, and the stopper was fixed the connecting rod from the opposite side, avoids the connecting rod to take place to rock, takes off with the guide rail pine, increases the security when using.
Drawings
FIG. 1 is an exploded view of the present invention;
FIG. 2 is a schematic structural view of the present invention;
FIG. 3 is a schematic structural view of the connecting rod of the present invention;
fig. 4 is a schematic structural diagram of the support pillar of the present invention.
In the figure: 1. a guide rail; 2. mounting holes; 3. a shock pad; 4. a limiting block; 5. a positioning column; 6. a connecting rod; 7. a moving groove; 8. a support pillar; 9. a first connection block; 10. a card slot; 11. clamping the column; 12. a second connecting block; 13. the anti-drop sleeve; 14. a support member; 15. a pressure resistant plate; 16. and (4) a column.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the utility model provides a stable form connector for an aviation seat, which comprises a guide rail 1 and a connecting rod 6, wherein a moving groove 7 is arranged at the center of the top of the guide rail 1, the connecting rod 6 is slidably connected inside the moving groove 7, a stopper 4 is sleeved at the middle part of the connecting rod 6, the other end of the top of the stopper 4 is connected with a positioning column 5 in a clamping manner, the bottom of the side surface of the positioning column 5 is in threaded connection with one end of the bottom of the moving groove 7, the connecting rod 6 comprises a supporting column 8, a first connecting block 9, a clamping column 11, a second connecting block 12 and an anti-falling sleeve 13, the bottom of the supporting column 8 is in threaded connection with the first connecting block 9, the bottom of the first connecting block 9 is provided with a clamping groove 10, the internal clamping of the clamping groove 10 is connected with a clamping column 11, the bottom of the clamping column 11 is fixedly provided with the second connecting block 12, the joint of the clamping column 11 and the clamping groove 10 is fixedly connected at one end of the inner wall of the anti-falling sleeve 13, support column 8 and the junction of first connecting block 9 and the other end fixed connection of anticreep cover 13 inner wall, the user will block 11 alignment draw-in grooves 10 of post, make second connecting block 12 be connected with 9 blocks of first connecting block, the user rotates support column 8, first connecting block 9 and 8 threaded connection of support column, the user passes through the bolt with anticreep cover 13 fixed mounting at the both ends of support column 8 and second connecting block 12, therefore, 6 concatenations of connecting rod are accomplished, the user slides connecting rod 6 in shift chute 7, adjust connecting rod 6 to assigned position, reach the ideal position after, the user embolias stopper 4 from the outside of connecting rod 6.
Preferably, the shock pad 3 is laid at the joint of the positioning column 5 and the guide rail 1, and the shock pad 3 buffers the oscillation force generated by the airplane during the flying bump.
Preferably, the outer side of the anti-slip sleeve 13 is slidably connected with the other end of the bottom of the moving groove 7, and the user slides the anti-slip sleeve 13 in the moving groove 7 to determine the position of the connecting rod 6.
Preferably, mounting hole 2 has all been seted up to the corner at guide rail 1 top, and the user carries out fixed mounting with guide rail 1 through mounting hole 2.
Preferably, the inside fixed mounting of support column 8 has a plurality of support piece 14, a plurality of support piece 14 all includes stand 16 and a plurality of resistance to compression board 15, the equal fixed mounting in both sides of stand 16 has a plurality of resistance to compression board 15, the equal fixed mounting in inside of a plurality of stand 16 has the stiffening rib, stand 16 carries out vertical support from the middle part of support column 8, the installation of stiffening rib increases stand 16's hardness, the resistance to compression board 15 of stand 16 both sides carries out the resistance to compression from the outside force of the both sides of stand 16 to the side, reinforcing support column 8's support dynamics.
Preferably, two ends of the plurality of columns 16 are fixedly connected to two ends of the inner wall of the supporting column 8, respectively, and the supporting member 14 is supported in the supporting column 8.
When the stable form attach fitting that the utility model relates to an aviation seat used, the user aims at draw-in groove 10 with card post 11, make second connecting block 12 and first connecting block 9 block connection, the user rotates support column 8, first connecting block 9 and support column 8 threaded connection, stand 16 carries out longitudinal support from the middle part of support column 8, the installation of stiffening rib increases the hardness of stand 16, the resistance to compression board 15 of stand 16 both sides is to the external force of side from the both sides of stand 16 resistance to compression, strengthen the support dynamics of support column 8, the user passes through the bolt with anticreep cover 13 fixed mounting at the both ends of support column 8 and second connecting block 12, therefore, connecting rod 6 splices to accomplish, user sliding connection rod 6 in shifting chute 7, adjust connecting rod 6 to the assigned position, after reaching the ideal position, the user embolias 4 from the outside stopper of connecting rod 6, the user is from a side-mounting reference column 5 of stopper 4, reference column 5 and shifting chute 7 threaded connection, and stopper 4 is fixed from one end to reference column 5, avoids stopper 4 to take place the offset for connecting rod 6 firmly fixes on guide rail 1, and shock pad 3 cushions the shock power that the aircraft flight was jolted and is produced.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.
Claims (6)
1. The utility model provides a stable form attach fitting that aircraft seat used, includes guide rail (1) and connecting rod (6), its characterized in that: a moving groove (7) is formed in the center of the top of the guide rail (1), a connecting rod (6) is connected to the inside of the moving groove (7) in a sliding mode, a limiting block (4) is sleeved at the middle of the connecting rod (6), a positioning column (5) is connected to the other end of the top of the limiting block (4) in a clamping mode, the bottom of the side face of the positioning column (5) is in threaded connection with one end of the bottom of the moving groove (7), the connecting rod (6) comprises a supporting column (8), a first connecting block (9), a clamping column (11), a second connecting block (12) and an anti-falling sleeve (13), the bottom of the supporting column (8) is in threaded connection with the first connecting block (9), a clamping groove (10) is formed in the bottom of the first connecting block (9), the inside of the clamping groove (10) is connected with the clamping column (11), and the second connecting block (12) is fixedly installed at the bottom of the clamping column (11), the junction fixed connection of card post (11) and draw-in groove (10) is in the one end of anticreep cover (13) inner wall, the junction of support column (8) and first connecting block (9) and the other end fixed connection of anticreep cover (13) inner wall.
2. A stabilized attachment joint for aircraft seats according to claim 1, wherein: and a shock pad (3) is laid at the joint of the positioning column (5) and the guide rail (1).
3. A stabilized attachment joint for aircraft seats according to claim 1, wherein: the outer side of the anti-falling sleeve (13) is connected with the other end of the bottom of the moving groove (7) in a sliding manner.
4. A stabilized attachment joint for aircraft seats according to claim 1, wherein: the corner at the top of the guide rail (1) is provided with mounting holes (2).
5. A stabilized attachment joint for aircraft seats according to claim 1, wherein: the inside fixed mounting of support column (8) has a plurality of support piece (14), a plurality of support piece (14) all include stand (16) and a plurality of resistance to compression board (15), the equal fixed mounting in both sides of stand (16) has a plurality of resistance to compression board (15), a plurality of the equal fixed mounting in inside of stand (16) has the stiffening rib.
6. A stabilized attachment joint for aircraft seats according to claim 5, wherein: the two ends of the upright columns (16) are respectively and fixedly connected with the two ends of the inner wall of the supporting column (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120900379.7U CN215205387U (en) | 2021-04-28 | 2021-04-28 | Stable form attach fitting that aviation seat used |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120900379.7U CN215205387U (en) | 2021-04-28 | 2021-04-28 | Stable form attach fitting that aviation seat used |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215205387U true CN215205387U (en) | 2021-12-17 |
Family
ID=79447409
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120900379.7U Active CN215205387U (en) | 2021-04-28 | 2021-04-28 | Stable form attach fitting that aviation seat used |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215205387U (en) |
-
2021
- 2021-04-28 CN CN202120900379.7U patent/CN215205387U/en active Active
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