CN208451588U - Aircraft hangs tooling with gauge - Google Patents
Aircraft hangs tooling with gauge Download PDFInfo
- Publication number
- CN208451588U CN208451588U CN201820345131.7U CN201820345131U CN208451588U CN 208451588 U CN208451588 U CN 208451588U CN 201820345131 U CN201820345131 U CN 201820345131U CN 208451588 U CN208451588 U CN 208451588U
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- gauge
- support rod
- aircraft
- tooling
- rod
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Abstract
The utility model discloses a kind of aircraft gauges to hang tooling, including pedestal, the support rod being set on pedestal, the hanger bar being set on support rod and is set to the hanged hook in hanger bar and for hanging gauge, hanged hook setting is multiple.The aircraft of the utility model hangs tooling with gauge, can effectively prevent the deformation of aircraft large scale gauge, improves aircraft manufacturing precision, extends gauge service life；Large scale hangs space and high density hanged hook is arranged, the suspension suitable for all kinds of gauges；Tooling is simple and effective, and simple process is easily realized, manufacturing cost is low.
Description
Technical field
The utility model belongs to General Aviation technical field of auxiliary equipment, specifically, the utility model relates to one kind to fly
Machine hangs tooling with gauge.
Background technique
With the graduallying relax control of China's low altitude airspace, the intensive appearance for related policy favourable of opening the navigation or air flight, China's navigation industry goes out
The development for the formula that bursts out is showed.Aircraft general assembly is the technical work that a technical difficulty is big, it is wide to be related to subject, comprehensive integration degree is high,
It decides the final mass, manufacturing cost and period of aircraft, and restricts the huge obstacle of China's aircraft rapid development, and restrict
One big bottleneck of aircraft final assembly technique development is exactly the development of all kinds of toolings.Equally, the maintenance of general-purpose aircraft is equally sent out by tooling
Open up the influence of lag.
Since aircraft manufacturing required precision is high, therefore to large scale gauge (various right angles used in aircraft manufacturing engineering
Ruler, ruler and aircraft rudder surface angle measurement tooling etc.) required precision is very high.And large scale gauge due to itself size is big,
Weight weight, therefore it is easy to deform under natural storage state, to influence measurement accuracy.In order to enable the big ruler of aircraft
Very little gauge deforms under storage configuration reaches minimum, and engineer can select suspension method to store it, and the prior art lacks energy
Hang the tooling of aircraft gauge.
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 mentions
Tooling is hung for a kind of aircraft gauge, it is therefore an objective to the deformation of aircraft gauge be made to reach minimum.
To achieve the goals above, the technical solution that the utility model is taken are as follows: aircraft hangs tooling, including bottom with gauge
It seat, the support rod being set on pedestal, the hanger bar that is set on support rod and is set in hanger bar and for hanging gauge
Hanged hook, hanged hook setting it is multiple.
Parallel two are arranged in the support rod, and support rod is vertically arranged, and the hanged hook is located at two support rods
Between.
The aircraft gauge suspension tooling further includes that first connect with the support rod and the hanger bar is reinforced
Bar.
First reinforcing rod is to be obliquely installed, and the hanger bar is horizontally disposed, the upper end of the first reinforcing rod and suspension
Bar connection, the lower end of the first reinforcing rod is connect with the support rod.
The aircraft gauge suspension tooling further includes the second reinforcing rod connecting with the pedestal and the support rod.
Second reinforcing rod is to be obliquely installed, and the upper end of the second reinforcing rod is connect with the support rod, the second reinforcing rod
Lower end connect with the pedestal.
The pedestal includes stringer and the crossbeam that connect with stringer, and parallel two are arranged in stringer, and crossbeam is located at two
Between stringer, the support rod and second reinforcing rod are connect with stringer.
Parallel two are arranged in the crossbeam.
The aircraft of the utility model hangs tooling with gauge, has the advantage that
1, it effectively prevent aircraft large scale gauge to deform, improves aircraft manufacturing precision, extend gauge service life；
2, large scale suspension space and high density hanged hook are arranged, the suspension suitable for all kinds of gauges；
3, tooling is simple and effective, and simple process is easily realized, manufacturing cost is low.
Detailed description of the invention
This specification includes the following drawings, and shown content is respectively:
Fig. 1 is the structural schematic diagram of the utility model aircraft gauge suspension tooling；
Fig. 2 is the structural schematic diagram of hanged hook；
In the figure, it is marked as 1, stringer；2, crossbeam；3, universal caster wheel；4, support rod；5, hanger bar；6, hanged hook；7, first
Reinforcing rod；8, the second reinforcing rod.
Specific embodiment
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 facilitate its implementation.
As depicted in figs. 1 and 2, the utility model provides a kind of aircraft gauge suspension tooling, including pedestal, is set to
Support rod 4 on pedestal, the hanger bar 5 being set on support rod 4 and it is set to the suspension in hanger bar 5 and for hanging gauge
Hook 6, hanged hook 6 are arranged multiple.
Specifically, stringer 1 is arranged parallel as shown in Figure 1, pedestal includes stringer 1 and the crossbeam connecting with stringer 12
Two, crossbeam 2 is located between two stringers 1, and parallel two are arranged in support rod 4, and support rod 4 is vertically arranged, suspension
Hook 6 is located between two support rods 4.Stringer 1 and crossbeam 2 are horizontally disposed, the length direction of stringer 1 and the length of crossbeam 2
Direction is perpendicular, and the lower end of support rod 4 is that the middle position on the length direction of stringer 1 is fixedly connected with stringer 1, support
The upper end of bar 4 is fixedly connected with hanger bar 5.
As shown in Figure 1, crossbeam 2 is arranged parallel two, two crossbeams 2 are located between two stringers 1, support rod 4 with
The tie point of stringer 1 is located at the middle position of two tie points of two crossbeams 2 and stringer 1, the understructure of this structure
Intensity is high, and stability is good, it is ensured that the reliability and stability after gauge suspension.
As shown in Figure 1, pedestal further includes the universal caster wheel 3 being set on stringer 1, convenient for the movement of tooling entirety.It is universal
Castor 3 is arranged multiple, and a universal caster wheel 3 is respectively set in the both ends of each stringer 1.
As shown in Figure 1, the aircraft gauge suspension tooling of the utility model further includes connecting with support rod 4 and hanger bar 5
The first reinforcing rod 7, the first reinforcing rod 7 is to be obliquely installed, the length direction of the length direction of the first reinforcing rod 7 and support rod 4
Between there is angle and the angle to be acute angle, hanger bar 5 be it is horizontally disposed, hanger bar 5 is parallel with crossbeam 2, and hanger bar 5 is located at
The upper end of the top of crossbeam 2, the first reinforcing rod 7 is connect with hanger bar 5, and the lower end of the first reinforcing rod 7 is connect with support rod 4.Branch
Strut 4 is arranged two, and the first reinforcing rod 7 is also provided with two, and each first reinforcing rod 7 is connect with a support rod 4 respectively, each
Support rod 4 is fixedly connected with one end of a stringer 1 and hanger bar 5 respectively.The setting of first reinforcing rod 7, it is ensured that support rod 4 with
Hanger bar 5 connects reliably, further improves the structural strength of tooling.
As depicted in figs. 1 and 2, hanged hook 6 is L-shaped structure, and the upper end of hanged hook 6 is fixedly connected and hangs with hanger bar 5
Hook 6 is stretched out towards the lower section of hanger bar 5.All hanged hooks 6 are located between two the first reinforcing rods 7, and all hanged hooks 6 are along outstanding
The length direction of hanging rod 5 is sequentially arranged and to be equally spaced, so as to hang multiple gauges.
As shown in Figure 1, the aircraft gauge suspension tooling of the utility model further includes the connect with pedestal and support rod 4
Two reinforcing rods 8, support rod 4 and the second reinforcing rod 8 are connect with stringer 1.Second reinforcing rod 8 is to be obliquely installed, the second reinforcing rod 8
Upper end is connect with support rod 4, and the lower end of the second reinforcing rod 8 is connect with pedestal, the length direction and support rod 4 of the second reinforcing rod 8
Length direction between there is angle and the angle to be acute angle.Each stringer 1 passes through two the second reinforcing rods 8 and support rod respectively
4 connections are on the same straight line parallel with the length direction of stringer 1 with two the second reinforcing rods 8 of same stringer 1 connection
And this two the second reinforcing rods 8 are located at the side of support rod 4.The setting of second reinforcing rod 8, it is ensured that support rod 4 and stringer
Connection is reliable, further improves the structural strength of tooling.
The utility model is exemplarily described in conjunction with attached drawing above.Obviously, the utility model implements not
It is limited by aforesaid way.As long as the various unsubstantialities that the method concept and technical solution that use the utility model carry out
Improvement；Or it is not improved, the above-mentioned conception and technical scheme of the utility model are directly applied into other occasions, at this
Within the protection scope of utility model.
Claims (3)
1. aircraft hangs tooling with gauge, it is characterised in that: including pedestal, the support rod being set on pedestal, be set to support
Hanger bar on bar is set in hanger bar and the hanged hook for hanging gauge and the first reinforcing rod and the second reinforcing rod,
Hanged hook setting is multiple, and the first reinforcing rod is to be obliquely installed, and hanger bar is horizontally disposed, the upper end of the first reinforcing rod and hanger bar
Connection, the lower end of the first reinforcing rod connect with support rod, the second reinforcing rod to be obliquely installed, the length direction of the second reinforcing rod and
There is angle between the length direction of support rod and the angle is acute angle, the upper end of the second reinforcing rod is connect with support rod, and second
The lower end of reinforcing rod is connect with pedestal；Parallel two are arranged in support rod and support rod is vertically arranged, and hanged hook is located at two
Between a support rod, the first reinforcing rod is also provided with two, and each first reinforcing rod is connect with a support rod respectively.
2. aircraft according to claim 1 hangs tooling with gauge, it is characterised in that: the pedestal include stringer and with it is vertical
Parallel two are arranged in the crossbeam of beam connection, stringer, and crossbeam is located between two stringers, and the support rod and described second adds
Strong bar is connect with stringer.
3. aircraft according to claim 2 hangs tooling with gauge, it is characterised in that: parallel two are arranged in the crossbeam
It is a.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820345131.7U CN208451588U (en) | 2018-03-14 | 2018-03-14 | Aircraft hangs tooling with gauge |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820345131.7U CN208451588U (en) | 2018-03-14 | 2018-03-14 | Aircraft hangs tooling with gauge |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208451588U true CN208451588U (en) | 2019-02-01 |
Family
ID=65155245
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820345131.7U Active CN208451588U (en) | 2018-03-14 | 2018-03-14 | Aircraft hangs tooling with gauge |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208451588U (en) |
-
2018
- 2018-03-14 CN CN201820345131.7U patent/CN208451588U/en active Active
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