CN210640640U - Aircraft seat support cable mount - Google Patents
Aircraft seat support cable mount Download PDFInfo
- Publication number
- CN210640640U CN210640640U CN201921614247.7U CN201921614247U CN210640640U CN 210640640 U CN210640640 U CN 210640640U CN 201921614247 U CN201921614247 U CN 201921614247U CN 210640640 U CN210640640 U CN 210640640U
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- China
- Prior art keywords
- joint
- fixing
- aircraft seat
- fixed
- clamping
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- 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 relates to an aircraft seat support cable mount. Aircraft seat support cable mount includes base, telescopic link, fixed plate, baffle and fixed plate, the upper end middle part position connecting main pole of base, fixing bolt is connected to the one end of main pole, the telescopic link of mobile jib internalization joint. The utility model discloses a be connected with the mobile jib on the base, the activity joint has the telescopic link in the mobile jib, the mobile jib carries out the regulation of co-altitude not with the telescopic link cooperation and is connected with the joint ring on the telescopic link, joint ring and connecting block activity joint, the connecting block can carry out the slope of different angles, be provided with a plurality of baffles on the fixed plate, the baffle is parallel arrangement, a plurality of baffles carry out the space isolation, carry out the joint of different circuits, avoid the mixed and disorderly of circuit, fixed fastener and joint groove matching joint, it is fixed to carry out the joint through joint groove and fixed fastener, the joint is convenient, carry out elastic contact through the sponge layer, avoid the extrusion of circuit simultaneously.
Description
Technical Field
The utility model relates to an aircraft seat support cable mount belongs to the fixed technical field of cable.
Background
The cable is a general name of articles such as optical cables, electric cables and the like, has a plurality of purposes, is mainly used for controlling installation, connecting equipment, transmitting electric power and the like, and is a common and indispensable object in daily life. Because the cable is electrified, the installation needs to be particularly cautious, especially the cable line on the aircraft needs more cautious installation, avoids the arch of circuit, causes the maloperation easily, influences the transmission of signal.
Aircraft seat support cable generally adopts ordinary fixing device to fix, and fixing device simple structure can't be suitable for when needing different angle slopes to fix, and the fixed circuit of circuit is numerous and diverse, and the difficult clearance of circuit appears confusing easily.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
In order to solve the above problems in the prior art, the utility model provides an aircraft seat support cable mount.
(II) technical scheme
In order to achieve the above object, the utility model discloses a main technical scheme include: it includes base, telescopic link, fixed plate, baffle and presses the clamp plate, the upper end middle part position joint mobile jib of base, fixing bolt is connected to the one end of mobile jib, mobile jib internalization joint telescopic link, the upper end fixed connection joint ring of telescopic link, the bottom and the connecting block of fixed plate are connected, set up the fixed slot in the fixed plate, be provided with the baffle in the fixed slot, the both sides of fixed plate set up the joint groove, press the fixed fastener of both sides fixed connection of clamp plate, press the bottom connection sponge layer of clamp plate.
Preferably, the central position of the upper end of the base is connected with the main rod, the main rod is arranged in a hollow mode, and the main rod is connected with the telescopic rod in a matched and clamped mode.
Preferably, one side of the main rod is provided with a threaded hole matched with the fixing bolt, and one end of the fixing bolt is in contact connection with the main rod.
Preferably, the clamping ring is movably clamped with the connecting block, and the clamping ring is connected with the connecting block through a bolt.
Preferably, a plurality of partition plates are arranged in the fixing groove and are arranged in parallel.
Preferably, the two sides of the fixing plate are provided with symmetrical clamping grooves, clamping fixing clamping pieces are contacted and clamped in the clamping grooves, and the fixing clamping pieces are matched and clamped with the clamping grooves.
Preferably, the bottom of pressing the clamp plate is connected with the sponge layer, the sponge layer sets up certain thickness, the sponge layer is connected with the baffle contact.
(III) advantageous effects
Compared with the prior art, the utility model provides an aircraft seat support cable mount possesses following beneficial effect:
(1) this aircraft seat support cable mount through being connected with the mobile jib on the base, and the activity joint has the telescopic link in the mobile jib, and the mobile jib carries out the regulation of co-altitude not with the telescopic link cooperation, is suitable for different installation requirements, is connected with the joint ring on the telescopic link, joint ring and connecting block activity joint, and the connecting block can carry out the slope of different angles, is suitable for different installation angle, and application scope is wide.
(2) This aircraft seat support cable mount, through be provided with a plurality of baffles on the fixed plate, the baffle is parallel arrangement, and a plurality of baffles carry out the space isolation, carry out the joint of different circuits, avoid the mixed and disorderly of circuit, and fixed fastener matches the joint with the joint groove, carries out the joint through joint groove and fixed fastener and fixes, and the joint is convenient, carries out elastic contact through the sponge layer, guarantees the fixed of circuit, avoids the extrusion of circuit simultaneously.
Drawings
FIG. 1 is a schematic plan view of the present invention;
FIG. 2 is a schematic view of the fixing plate of the present invention;
fig. 3 is a schematic view of the connection of the pressing plate of the present invention.
In the figure: 1 base, 2 mobile jib, 3 fixing bolt, 4 telescopic links, 5 joint rings, 6 fixed plates, 7 connecting blocks, 8 fixed slots, 9 baffles, 10 joint grooves, 11 pressing plates, 12 fixed fasteners, 13 sponge layers.
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.
Please refer to fig. 1-3, aircraft seat support cable mount, it includes base 1, telescopic link 4, fixed plate 6, baffle 9 and pressing plate 11, the mobile jib 2 is connected to the upper end middle part position of base 1, fixing bolt 3 is connected to the one end of mobile jib 2, mobile jib 2 internalization joint telescopic link 4, the upper end fixed connection joint ring 5 of telescopic link 4, the bottom and the connecting block 7 of fixed plate 6 are connected, set up fixed slot 8 in the fixed plate 6, be provided with baffle 9 in the fixed slot 8, the both sides of fixed plate 6 set up joint groove 10, pressing plate 11's both sides fixed connection fixing clip 12, pressing plate 11's bottom connection sponge layer 13.
The connecting main rod 2 is arranged at the center of the upper end of the base 1, the main rod 2 is arranged in a hollow mode, the main rod 2 is connected with the telescopic rod 4 in a matched mode, the main rod 2 is matched with the telescopic rod 4 in a clamped mode, the main rod 2 is matched with the telescopic rod 4 to adjust different heights, and the connecting main rod is suitable for different height requirements.
One side of mobile jib 2 sets up and 3 assorted screw holes of fixing bolt, and fixing bolt 3's one end is connected with mobile jib 2 contact, fixes through fixing bolt 3 of one side, and is fixed effectual, and it is convenient that the installation is adjusted.
Clamping ring 5 and 7 movable joint of connecting block, clamping ring 5 and connecting block 7 pass through bolted connection, and clamping ring 5 and the cooperation of connecting block 7 carry out different inclination's regulation, are suitable for different inclination demands, and the bolt carries out fastening connection.
Be provided with a plurality of baffles 9 in the fixed slot 8, baffle 9 is parallel arrangement, and a plurality of baffles 9 carry out the space isolation, carry out the joint of different circuits, avoid mixed and disorderly of circuit.
The both sides of fixed plate 6 are provided with the joint groove 10 of symmetry, and the fixed fastener 12 of contact joint in the joint groove 10, and fixed fastener 12 matches the joint with joint groove 10, carries out the joint through joint groove 10 and fixed fastener 12 and fixes, and the joint is convenient, and the availability factor is high.
According to the bottom connection sponge layer 13 of pressing plate 11, sponge layer 13 sets up certain thickness, and sponge layer 13 is connected with the contact of baffle 9, carries out elastic contact through sponge layer 13, guarantees the fixed of circuit.
To sum up, this aircraft seat support cable mount, be connected with mobile jib 2 on base 1 during the use, mobile jib 2 internalization joint has telescopic link 4, mobile jib 2 carries out the regulation of co-altitude not with the cooperation of telescopic link 4, be suitable for different installation requirements, be connected with joint ring 5 on telescopic link 4, joint ring 5 and 7 movable joint of connecting block, connecting block 7 can carry out the slope of different angles, be suitable for different installation angle, be provided with a plurality of baffles 9 on the fixed plate 6, baffle 9 is parallel arrangement, a plurality of baffles 9 carry out the space isolation, carry out the joint of different circuits, avoid mixed and disorderly of circuit, fixed fastener 12 matches the joint with joint groove 10, it is fixed to carry out the joint through joint groove 10 and fixed fastener 12, the joint is convenient, carry out elastic contact through sponge layer 13, guarantee the fixed of circuit, avoid the extrusion of circuit simultaneously.
It is to be noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The cable fixing frame of the airplane seat support comprises a base (1), an expansion rod (4), a fixing plate (6), a partition plate (9) and a pressing plate (11), it is characterized in that the middle part of the upper end of the base (1) is connected with a main rod (2), one end of the main rod (2) is connected with a fixed bolt (3), the main rod (2) is movably clamped with a telescopic rod (4), the upper end of the telescopic rod (4) is fixedly connected with a clamping ring (5), the bottom of the fixed plate (6) is connected with a connecting block (7), a fixed groove (8) is arranged in the fixed plate (6), a clapboard (9) is arranged in the fixed groove (8), the clamping groove (10) is formed in the two sides of the fixing plate (6), the fixing clamping pieces (12) are fixedly connected to the two sides of the pressing plate (11), and the sponge layer (13) is connected to the bottom end of the pressing plate (11).
2. An aircraft seat carrier cable mount as claimed in claim 1 wherein: the base (1) upper end central point puts connecting main rod (2), main rod (2) are the cavity setting, main rod (2) and telescopic link (4) match the joint.
3. An aircraft seat carrier cable mount as claimed in claim 1 wherein: one side of mobile jib (2) set up with fixing bolt (3) assorted screw hole, the one end and the mobile jib (2) contact of fixing bolt (3) are connected.
4. An aircraft seat carrier cable mount as claimed in claim 1 wherein: the clamping ring (5) is movably clamped with the connecting block (7), and the clamping ring (5) is connected with the connecting block (7) through a bolt.
5. An aircraft seat carrier cable mount as claimed in claim 1 wherein: a plurality of partition plates (9) are arranged in the fixing groove (8), and the partition plates (9) are arranged in parallel.
6. An aircraft seat carrier cable mount as claimed in claim 1 wherein: the clamping device is characterized in that symmetrical clamping grooves (10) are formed in two sides of the fixing plate (6), clamping fixing clamping pieces (12) are contacted in the clamping grooves (10), and the fixing clamping pieces (12) are connected with the clamping grooves (10) in a matched mode.
7. An aircraft seat carrier cable mount as claimed in claim 1 wherein: the bottom end of the pressing plate (11) is connected with a sponge layer (13), the sponge layer (13) is arranged with a certain thickness, and the sponge layer (13) is in contact connection with the partition board (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921614247.7U CN210640640U (en) | 2019-09-26 | 2019-09-26 | Aircraft seat support cable mount |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921614247.7U CN210640640U (en) | 2019-09-26 | 2019-09-26 | Aircraft seat support cable mount |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210640640U true CN210640640U (en) | 2020-05-29 |
Family
ID=70798625
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921614247.7U Expired - Fee Related CN210640640U (en) | 2019-09-26 | 2019-09-26 | Aircraft seat support cable mount |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210640640U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117117709A (en) * | 2023-08-28 | 2023-11-24 | 金开新能科技有限公司 | Power transmission line erection device and method based on multi-rotor unmanned aerial vehicle |
-
2019
- 2019-09-26 CN CN201921614247.7U patent/CN210640640U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117117709A (en) * | 2023-08-28 | 2023-11-24 | 金开新能科技有限公司 | Power transmission line erection device and method based on multi-rotor unmanned aerial vehicle |
| CN117117709B (en) * | 2023-08-28 | 2024-04-26 | 金开新能科技有限公司 | Power transmission line erection device and method based on 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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200529 |