CN208070048U - Aircraft harness wiring plate supporting device - Google Patents
Aircraft harness wiring plate supporting device Download PDFInfo
- Publication number
- CN208070048U CN208070048U CN201820506085.4U CN201820506085U CN208070048U CN 208070048 U CN208070048 U CN 208070048U CN 201820506085 U CN201820506085 U CN 201820506085U CN 208070048 U CN208070048 U CN 208070048U
- Authority
- CN
- China
- Prior art keywords
- wiring plate
- swivel mount
- harness wiring
- rack body
- supporting rod
- 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 a kind of aircraft harness wiring plate supporting device, including rack body, it is rotatably arranged on rack body and the swivel mount for installing aircraft harness wiring plate and for making swivel mount and the relatively-stationary lockable mechanism of rack body holding.The aircraft harness wiring plate supporting device of the utility model, has many advantages, such as simple in structure and highly practical, and the placement of aircraft harness wiring plate may be implemented, can effectively improve working efficiency and operability, and production cost is relatively low.
Description
Technical field
The utility model belongs to General Aviation technical field of auxiliary equipment, specifically, the utility model is related to one kind to fly
Machine harness wiring plate supporting device.
Background technology
In the making of Aircraft wirning harness, especially for some complicated harness, generally require by wiring plate auxiliary system
Make harness.The back side of these wiring plates has a large amount of conducting wire, therefore places wiring plate and have to vacantly, it is also contemplated that operation
The operability of personnel, existing support device cannot meet this requirement sheet.
Utility model content
The utility model aims to solve at least one of the technical problems existing in the prior art.For this purpose, the utility model carries
For a kind of aircraft harness wiring plate supporting device, it is therefore an objective to realize the placement of aircraft harness wiring plate.
To achieve the goals above, the technical solution that the utility model is taken is：Aircraft harness wiring plate supporting device, packet
Rack body is included, is rotatably arranged on rack body and for installing the swivel mount of aircraft harness wiring plate and for making rotation
Pivoted frame keeps relatively-stationary lockable mechanism with rack body.
The swivel mount is rectangular frame structure, and the rotation centerline of swivel mount is located in horizontal plane.
The lockable mechanism includes the first bolt, is sheathed on the first bolt the first nut and be bolted with first and
The handle rotated for controlling the first bolt, the rack body and the swivel mount have allow the first bolt to pass through to lead to
Hole.
The upper cross that the rack body includes longeron, the bottom end rail being connect with longeron and supporting rod and connect with supporting rod
Beam, longeron are arranged parallel two, and bottom end rail is located between two longerons, and supporting rod is vertically arranged, the swivel mount with
Supporting rod is rotatablely connected.
Parallel two are arranged in the supporting rod, and the lockable mechanism is disposed therein on a supporting rod, it is described on
Crossbeam is located between two supporting rods.
The aircraft harness wiring plate supporting device of the utility model, have many advantages, such as it is simple in structure and highly practical, can be with
The placement for realizing aircraft harness wiring plate, can effectively improve working efficiency and operability, and production cost is relatively low.
Description of the drawings
This specification includes the following drawings, and shown content is respectively：
Fig. 1 is the structural schematic diagram of the utility model aircraft harness wiring plate supporting device；
Fig. 2 is the vertical view of the utility model aircraft harness wiring plate supporting device；
In figure label for：1, longeron；2, bottom end rail；3, universal caster wheel；4, bracing piece；5, supporting rod；6, swivel mount；7,
One bolt；8, the first nut；9, handle；10, the second bolt；11, the second nut；12, upper beam.
Specific implementation mode
Below against attached drawing, by the description of the embodiment, making to specific embodiment of the present utility model further detailed
Thin explanation, it is therefore an objective to help those skilled in the art to the design of the utility model, technical solution have it is more complete, accurate and
Deep understanding, and contribute to its implementation.
As depicted in figs. 1 and 2, the utility model provides a kind of aircraft harness wiring plate supporting device, including holder master
Body, be rotatably arranged on rack body and for install aircraft harness wiring plate swivel mount 6 and for make swivel mount 6 with
Rack body keeps relatively-stationary lockable mechanism.
Specifically, as depicted in figs. 1 and 2, aircraft harness wiring plate is the fastener by being made of screw bolt and nut
It is fixedly mounted on swivel mount 6, swivel mount 6, which has, allows the through-hole that bolt passes through, swivel mount 6 to be arranged to rotatable, swivel mount 6
Rotation centerline be located in horizontal plane so that aircraft harness wiring plate can be spun upside down, and adjust aircraft harness wiring plate
Position and angle facilitate operation when wiring, improve the operability of operating personnel, are also beneficial to remove aircraft harness wiring plate
On tiny sundries.Swivel mount 6 can be made to be maintained at suitable angular position by the way that lockable mechanism is arranged, facilitate control and tune
Section.
As depicted in figs. 1 and 2, preferably, swivel mount 6 is rectangular frame structure, 6 structure of swivel mount of this shape
Simply, operating space is big, operation when convenient for wiring.Swivel mount 6 is middle position and rack body in the direction of the width
Connection, it is parallel that the length direction of swivel mount 6 rotates center line.
As depicted in figs. 1 and 2, lockable mechanism include the first bolt 7, the first nut 8 for being sheathed on the first bolt 7 and with
First bolt 7 connects and for control the handle 9 that the first bolt 7 is rotated, and rack body and swivel mount 6 are with allowing the first spiral shell
The through-hole that bolt 7 passes through.Lockable mechanism is set to one end on the length direction of swivel mount 6, another on the length direction of swivel mount 6
One end is connect by the second bolt 10 with rack body, and the end of swivel mount 6, which has, allows the through-hole that the second bolt 10 passes through, and second
The second nut 11 is arranged on bolt 10, the first bolt 7 and the second bolt 10 are matched, are provided a supporting role to swivel mount 6, and
Swivel mount 6 is rotated relative to rack body.Handle 9 is fixedly connected with the hexagon-head of the first bolt 7, pedestal
And swivel mount 6 is located between the hexagon-head and the first nut 8 of the first bolt 7, after rotating handles 9 tighten the first bolt 7,
First bolt 7 and the first nut 8 match, and clamp rack body and swivel mount 6, so that swivel mount 6 keeps phase with rack body
To fixation, and then keep harness wiring plate motionless.
As depicted in figs. 1 and 2, rack body include longeron 1, the bottom end rail being connect with longeron 12 and supporting rod 5 and with
Parallel two are arranged in the upper beam 12 that supporting rod 5 connects, longeron 1, and bottom end rail 2 is located between two longerons 1, upper beam 12
Positioned at the top of bottom end rail 2, supporting rod 5 is vertically arranged, and swivel mount 6 is rotatablely connected with supporting rod 5, and supporting rod 5 is arranged equal
Capable two, upper beam 12 are located between two supporting rods 5 and are fixedly connected with two supporting rods 5.Lockable mechanism is set to it
In on a supporting rod 5, the second bolt 10 is arranged on another supporting rod 5, and swivel mount 6 is located between two supporting rods 5, two
The upper end of a supporting rod 5 is equipped with and allows the through-hole that bolt passes through.Longeron 1, bottom end rail 2 and upper beam 12 are horizontally disposed, upper cross
Beam 12 and bottom end rail 2 are parallel, and the length direction of the length direction and bottom end rail 2 and upper beam 12 of longeron 1 is perpendicular, supporting rod
5 lower end is that the middle position on the length direction of longeron 1 is fixedly connected with longeron 1.The length direction of bottom end rail 2 and rotation
The rotation centerline of pivoted frame 6 is parallel, and upper beam 12 and bottom end rail 2 are located at the lower section of swivel mount 6, and two bottom end rails 2 are located at two
Between a longeron 1, bottom end rail 2 is that the middle position on the length direction of longeron 1 is fixedly connected with longeron 1.This structure
Rack body structural strength it is high, stability is good, it is ensured that the reliability and stability after the installation of aircraft harness wiring plate.
As shown in Figure 1, rack body further includes the universal caster wheel 3 being set on longeron 1, it is convenient for the movement of tooling entirety.
Universal caster wheel 3 is arranged multiple, and a universal caster wheel 3 is respectively set in the both ends of each longeron 1.
As shown in Figure 1, the aircraft harness wiring plate supporting device of the utility model further includes connecting with longeron 1 and supporting rod 5
The bracing piece 4 connect, supporting rod 5 and bracing piece 4 are connect with longeron 1.Bracing piece 4 is to be obliquely installed, the upper end of bracing piece 4 and support
Bar 5 connects, and the lower end of bracing piece 4 connect with longeron 1, has between the length direction and the length direction of supporting rod 5 of bracing piece 4
The angle and angle is acute angle.Each longeron 1 is connect by two bracing pieces 4 with supporting rod 5 respectively, is connect with same longeron 1
Two bracing pieces 4 be on the same straight line parallel with the length direction of longeron 1 and two bracing pieces 4 are located at branch
The side of strut 5.The setting of bracing piece 4, it is ensured that supporting rod 5 is connect reliably with longeron 1, and the structure for further improving tooling is strong
Degree.
The utility model is exemplarily described above in association with attached drawing.Obviously, the utility model implements not
It is limited by aforesaid way.As long as using the various unsubstantialities of the methodology and technical solution progress of the utility model
Improvement；Or it is not improved, above-mentioned design and technical solution by the utility model directly apply to other occasions, at this
Within the protection domain of utility model.
Claims (5)
1. aircraft harness wiring plate supporting device, it is characterised in that：Including rack body, it is rotatably arranged on rack body
And swivel mount for installing aircraft harness wiring plate and for making swivel mount and rack body keep relatively-stationary locking machine
Structure.
2. aircraft harness wiring plate supporting device according to claim 1, it is characterised in that：The swivel mount is rectangle frame
The rotation centerline of frame structure, swivel mount is located in horizontal plane.
3. aircraft harness wiring plate supporting device according to claim 1 or 2, it is characterised in that：The lockable mechanism packet
The first bolt is included, the first nut for being sheathed on the first bolt and is bolted with first and is turned for controlling the first bolt
Dynamic handle, the rack body and the swivel mount, which have, allows the through-hole that the first bolt passes through.
4. aircraft harness wiring plate supporting device according to claim 1 or 2, it is characterised in that：The rack body packet
Parallel two are arranged in the upper beam for including longeron, the bottom end rail being connect with longeron and supporting rod and being connect with supporting rod, longeron
A, bottom end rail is located between two longerons, and supporting rod is vertically arranged, and the swivel mount is rotatablely connected with supporting rod.
5. aircraft harness wiring plate supporting device according to claim 4, it is characterised in that：The supporting rod setting is equal
Capable two, the lockable mechanism are disposed therein on a supporting rod, and the upper beam is located between two supporting rods.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820506085.4U CN208070048U (en) | 2018-04-11 | 2018-04-11 | Aircraft harness wiring plate supporting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820506085.4U CN208070048U (en) | 2018-04-11 | 2018-04-11 | Aircraft harness wiring plate supporting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208070048U true CN208070048U (en) | 2018-11-09 |
Family
ID=64040509
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820506085.4U Active CN208070048U (en) | 2018-04-11 | 2018-04-11 | Aircraft harness wiring plate supporting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208070048U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109817390A (en) * | 2019-03-28 | 2019-05-28 | 中电科芜湖钻石飞机制造有限公司 | General-purpose aircraft wing Wire harness ranging device |
-
2018
- 2018-04-11 CN CN201820506085.4U patent/CN208070048U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109817390A (en) * | 2019-03-28 | 2019-05-28 | 中电科芜湖钻石飞机制造有限公司 | General-purpose aircraft wing Wire harness ranging device |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |