CN207644660U - A kind of aircraft answers material covering supporting rack - Google Patents
A kind of aircraft answers material covering supporting rack Download PDFInfo
- Publication number
- CN207644660U CN207644660U CN201721847574.8U CN201721847574U CN207644660U CN 207644660 U CN207644660 U CN 207644660U CN 201721847574 U CN201721847574 U CN 201721847574U CN 207644660 U CN207644660 U CN 207644660U
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- Prior art keywords
- strut
- annulus
- aircraft
- patch
- supporting rack
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Abstract
The utility model discloses a kind of aircrafts to answer material covering supporting rack, belongs to aircraft package technique field.Including annulus and telescopic rod, an opposite face of annulus is uniformly provided with several orifice plates along outer edge, is mutually perpendicular on the through-hole of orifice plate and the lead to the hole site of annulus；One surface of annulus is uniformly provided with a notch along outer edge, is welded with patch in notch, and homogeneously to being provided with half circular groove on the binding face of patch and annulus, a conduit being mutually communicated is provided on patch and annulus；Telescopic rod includes the first strut and the second strut, first strut one end and one end of the second strut are slidably connected, and the other end of the first strut is equipped with a shaft, and the first strut is mounted on by shaft on annulus, one end of first strut is equipped with a rubber bulb, and a pressure sensor is equipped in rubber bulb.The utility model is supported when being assembled by the laying of aircraft skin and outer skeleton, accelerates the process of aircraft assembling.
Description
Technical field
The utility model belongs to aircraft package technique field, and material covering supporting rack is answered more particularly to a kind of aircraft.
Background technology
Aircraft skin refers to being enclosed in outside airframe structure and being fixed on skeleton with bonding agent or rivet, forms aircraft
The dimension shape component of aerodynamic shape.Aircraft skin has with the stressed-skin construction that skeleton is constituted compared with large bearing capacity and rigidity, and from
Weight is but very light, plays the role of bearing and transmitting aerodynamic loading.Covering bears that active force is transmitted to phase after aerodynamic effect
On fuselage wing skeleton even, stress is complicated, and covering is directly contacted with the external world in addition, so not requiring nothing more than skin material intensity
Height, plasticity are good, also require surface smooth, there is higher resistance to corrosion, and when fuselage skin is laid with, branch is placed in fuselage framework
Support is supported the covering of laying, and then ensures the progress of covering efficiently and accurately.
Invention content
The purpose of this utility model is to provide a kind of aircrafts to answer material covering supporting rack, by passing through branch in covering laying
Support is supported laying so that when aircraft is assembled, the progress of efficient stable and following process prevent deformation.
In order to solve the above technical problems, the utility model is achieved through the following technical solutions：
The utility model is that a kind of aircraft answers material covering supporting rack, including annulus and telescopic rod, a phase of the annulus
Opposite is uniformly provided with several orifice plates along outer edge, is mutually perpendicular on the through-hole of the orifice plate and the lead to the hole site of annulus；
One surface of the annulus is uniformly provided with a notch along outer edge, and patch, the benefit are welded in the notch
A slot being mutually communicated homogeneously is provided on the patch and annulus to being provided with half circular groove on the binding face of block and annulus
Road；Wherein it is mutually perpendicular to and is mutually communicated on conduit and semicircle conduit position；The telescopic rod includes the first strut and second
Strut, first strut one end and one end of the second strut are slidably connected, and the other end of first strut is equipped with one turn
Axis, first strut are mounted on by shaft on annulus, and shaft cooperation is in two halves circular groove；First strut
One end is equipped with a rubber bulb, and a pressure sensor is equipped in the rubber bulb.
Further, the end of first strut is designed for " V " shape, and one wedge is housed by bolt installation on the orifice plate
Shape block, the inclined-plane of the wedge block are bonded with the " V " shape end of the first strut.
Further, a pressure sensor is equipped in the rubber bulb, and the end of second connecting rod is equipped with a data
Coffret.
The utility model has the advantages that：
The utility model is simple in structure, easy to use, and telescopic rod is mounted on by shaft on annulus, when not in use, into
Row collapses and telescopic rod closes up, and greatly reduces parking space and easy to carry, in the end of telescopic rod is equipped with rubber
Glueballs head, and pressure sensor is equipped in rubber bulb, and then when carrying out flying shore, science passes through pressure sensing
The data that device is acquired judge the length that telescopic rod is stretched.
Certainly, any product for implementing the utility model does not necessarily require achieving all the advantages described above at the same time.
Description of the drawings
In order to illustrate more clearly of the technical solution of the utility model embodiment, make required for being described below to embodiment
Attached drawing is briefly described, it should be apparent that, the accompanying drawings in the following description is only some embodiments of the utility model,
For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings
Other attached drawings.
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the partial structural diagram of the use of the new type annulus.
Fig. 3 is the structure chart of the utility model wedge block and annulus.
Fig. 4 is the partial sectional view of the utility model annulus.
Fig. 5 is the structural representation of the rubber bulb of the utility model.
In attached drawing, parts list represented by the reference numerals are as follows：
1- annulus, 2- telescopic rods, 3- wedge blocks, 101- orifice plates, 102- notches, 103- patch, 104- semicircle conduits,
The first struts of 201-, the second struts of 202-, 203- rubber bulbs, 204- shafts, 205- pressure sensors, 206- data transmissions connect
Mouthful, 301- through-holes.
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.Based on the embodiments of the present invention, those of ordinary skill in the art are without creative efforts
The all other embodiment obtained, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be understood that term " trepanning ", "upper", "lower", " thickness ", "top",
" in ", " length ", "inner", indicating positions or the position relationship such as " surrounding ", be merely for convenience of description the utility model and simplification
Description, does not indicate or imply the indicated component or element must have a particular orientation, with specific azimuth configuration and behaviour
Make, therefore should not be understood as limiting the present invention.
It please refers to Fig.1 shown in -5, the utility model is that a kind of aircraft answer material covering supporting rack, including annulus 1 and stretches
Bar 2,.
Wherein, an opposite face of annulus 1 is uniformly provided with several orifice plates 101 along outer edge, the through-hole 301 of orifice plate 101 with
It is mutually perpendicular on 301 position of through-hole of annulus 1；
One surface of annulus 1 is uniformly provided with a notch 102 along outer edge, and notch 102 offers eight, in notch 102
Be welded with patch 103, patch 103 is a rectangular block, patch 103 on the binding face of annulus 1 homogeneously to being provided with half circular trough
A conduit being mutually communicated is provided on road 104, patch 103 and annulus 1；
Wherein it is mutually perpendicular to and is mutually communicated on 104 position of conduit and semicircle conduit；
Telescopic rod 2 includes the first strut 201 and the second strut 202,201 one end of the first strut and the one of the second strut 202
End is slidably connected, and the other end of the first strut 201 is equipped with a shaft 204, and the first strut 201 is mounted on circle by shaft 204
On ring 1, and shaft 204 coordinates in two halves circular groove 104, wherein being equipped with a telescopic rod 2, annulus 1 in each patch 103
A pair of of orifice plate 101 is equipped at upper each patch 102；
One end of first strut 201 is equipped with a rubber bulb 203, and a pressure sensor 205 is equipped in rubber bulb 203.
Wherein, the end of the first strut 201 is designed for " V " shape, and one wedge block 3 is housed by bolt installation on orifice plate 101,
The inclined-plane of wedge block 3 is bonded with the " V " shape end of the first strut 201, when telescopic rod 2 is supported by wedge block 3 into line position
Set restriction.
Wherein, a pressure sensor 205 is equipped in rubber bulb 203, and the end of second connecting rod is equipped with data biography
Defeated interface 206 carries out judging telescopic rod when telescopic rod 2 is supported by the pressure sensor 205 on rubber bulb 203
Collapsing length, when external tester detects that the data that pressure sensor 205 is fed back reach volume by data transmission interface 206
When definite value, telescopic rod 2 stops elongation.
One of the present embodiment has particular application as：.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
Particular features, structures, materials, or characteristics described in conjunction with this embodiment or example are contained in at least one of the utility model
In embodiment or example.In the present specification, schematic expression of the above terms be not necessarily referring to identical embodiment or
Example.Moreover, particular features, structures, materials, or characteristics described can be in any one or more embodiments or example
In can be combined in any suitable manner.
The preferred embodiment in the utility model disclosed above is only intended to help to illustrate the utility model.Preferred embodiment is simultaneously
There is no the details that detailed descriptionthe is all, does not limit the specific implementation mode that the utility model is only described yet.Obviously, according to this theory
The content of bright book can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to preferably
The principles of the present invention and practical application are explained, to enable skilled artisan to be best understood by and utilize this
Utility model.The utility model is limited only by the claims and their full scope and equivalents.
Claims (3)
1. a kind of aircraft answers material covering supporting rack, including annulus（1）And telescopic rod（2）, it is characterised in that：
The annulus（1）An opposite face several orifice plates are uniformly provided with along outer edge（101）, the orifice plate（101）Through-hole
（301）With annulus（1）Through-hole（301）It is mutually perpendicular on position；
The annulus（1）A surface notch is uniformly provided with along outer edge（102）, the notch（102）Inside it is welded with benefit
Block（103）, the patch（103）With annulus（1）Binding face on homogeneously to being provided with half circular groove（104）, the patch
（103）And annulus（1）On be provided with a conduit being mutually communicated；
Wherein conduit and semicircle conduit（104）It is mutually perpendicular to and is mutually communicated on position；
The telescopic rod（2）Including the first strut（201）With the second strut（202）, first strut（201）One end and second
Strut（202）One end be slidably connected, first strut（201）The other end one shaft is installed（204）, described first
Bar（201）Pass through shaft（204）Mounted on annulus（1）On, and shaft（204）Cooperation is in two halves circular groove（104）It is interior；
First strut（201）One end be equipped with a rubber bulb（203）, the rubber bulb（203）Inside it is equipped with a pressure
Sensor（205）.
2. a kind of aircraft according to claim 1 answers material covering supporting rack, which is characterized in that first strut
（201）End designed for " V " shape, the orifice plate（101）It is upper that a wedge block is equipped with by bolt installation（3）, the wedge block
（3）Inclined-plane and the first strut（201）" V " shape end fitting.
3. a kind of aircraft according to claim 1 answers material covering supporting rack, which is characterized in that the rubber bulb
（203）Inside it is equipped with a pressure sensor（205）, and the end of second connecting rod is equipped with a data transmission interface（206）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721847574.8U CN207644660U (en) | 2017-12-26 | 2017-12-26 | A kind of aircraft answers material covering supporting rack |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721847574.8U CN207644660U (en) | 2017-12-26 | 2017-12-26 | A kind of aircraft answers material covering supporting rack |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207644660U true CN207644660U (en) | 2018-07-24 |
Family
ID=62875513
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721847574.8U Active CN207644660U (en) | 2017-12-26 | 2017-12-26 | A kind of aircraft answers material covering supporting rack |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207644660U (en) |
-
2017
- 2017-12-26 CN CN201721847574.8U patent/CN207644660U/en active Active
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