CN205802913U - The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail - Google Patents
The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail Download PDFInfo
- Publication number
- CN205802913U CN205802913U CN201620658593.5U CN201620658593U CN205802913U CN 205802913 U CN205802913 U CN 205802913U CN 201620658593 U CN201620658593 U CN 201620658593U CN 205802913 U CN205802913 U CN 205802913U
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- China
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- hoistable platform
- guardrail
- multiple material
- electrical moving
- horizontal tail
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Abstract
The utility model discloses a kind of aircraft outer wing, the multiple material tests special-purpose vehicle of horizontal tail, including electrical moving hoistable platform, high back chair, detecting instrument Hanging Basket, work top controller, guardrail, guardrail is arranged on the upper end of electrical moving hoistable platform, high back chair is symmetrically mounted on the upper rear of electrical moving hoistable platform, high back chair is positioned at guardrail, work top controller is arranged on the upper center of electrical moving hoistable platform, detecting instrument Hanging Basket is mounted on the left front portion of guardrail, arm support is installed on high back chair, work top controller is connected by wire with electrical moving hoistable platform.This utility model has reasonable in design, the advantage such as easy to use, solves traditional equipment and can not arrive problem in detection site, greatly facilitates operator's operation, and safe and reliable, degree of flexibility is high, improves the efficiency of maintenance.
Description
Technical field
This utility model relates to aeronautical product detection technique field, the multiple material of a kind of aircraft outer wing, horizontal tail
Detection special-purpose vehicle.
Background technology
After composite structure Non-Destructive Testing on aircraft is taken a flight test, before transition, need to carry out ultrasound examination, now outside
The big parts installation and debugging the most such as the wing, horizontal tail are complete.Carrying out in situ detection, the detection operation of its lower wall panels is extremely difficult.Because these are several
The big parts of item need to carry out the inspection of Zone Full, uses the frocks such as ladder, can not arbitrarily move, and respective regions is by aircraft components
Blocking, ladder does not has placement space yet, it is therefore necessary to design a applicable frock, helps flaw detection personnel to carry out inspection in situ on machine
Survey.
Summary of the invention
In order to solve above-mentioned technical problem, this utility model provides a kind of aircraft outer wing, horizontal tail multiple material tests special-purpose vehicle.
This utility model solves its technical problem and realizes by the following technical solutions:
The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail, including electrical moving hoistable platform, high back chair, inspection
Surveying instrument Hanging Basket, work top controller, guardrail, described guardrail is arranged on the upper end of electrical moving hoistable platform, described height
Chair is symmetrically mounted on the upper rear of electrical moving hoistable platform, and described high back chair is positioned at guardrail, described work
Table top controller is arranged on the upper center of electrical moving hoistable platform, and described detecting instrument Hanging Basket is mounted on the left front of guardrail
Portion, high back chair is provided with arm support, and described work top controller and electrical moving hoistable platform are by wire phase
Even.After this utility model uses electrical moving hoistable platform, it is possible to achieve overall height freely regulates, the arbitrarily side of regulation
Arbitrarily control to, translational speed, after have employed guardrail, overall security can be made to be improved simultaneously, provide for staff
The operating platform of safety.
Described high back chair is arranged on the upper rear of electrical moving hoistable platform by locking device, and described locking fills
Putting and include bolt, plain washer, standard check ring, nut one, clip, described bolt, plain washer, standard check ring are constituted
Locking member, the middle part of clip is sleeved on the bottom of high back chair, and the two ends, left and right of clip are fixed on electronic movement by locking member
The upper rear of formula hoistable platform, described electrical moving hoistable platform is set with rubber with the junction of clip.This practicality is new
After type uses high back chair, such staff, when overhauling, can take, to alleviate the labor intensity of workman.
Described arm support includes nut two, pad, nylon spacer, arm bracket, support shaft and axle sleeve, described support shaft
Bottom be fixed on high back chair by nut two, pad, nylon spacer, the top spiral shell of the bottom of described axle sleeve and support shaft
Stricture of vagina coordinates, and described arm bracket is fixed on the upper end of axle sleeve.Arm support of the present utility model can be according to the use of user
The height of demand regulation self, thus improve comfort level.
The upper end of described arm bracket is provided with the rubber blanket one of arc.
The right-hand member of described electrical moving hoistable platform is provided with label.
The right-hand member of described guardrail is provided with guardrail wicket, to facilitate staff to come in and go out.
The left end of described electrical moving hoistable platform is provided with handle, i.e. can also manually promote integral device to move
Dynamic.
The top surrounding outer edge of described electrical moving hoistable platform is mounted on rubber blanket two, on the one hand protection behaviour
Make personnel, on the other hand avoid detecting when car clashes into aircraft and cause body to damage.
The model of described electrical moving hoistable platform is ZW51601.
The beneficial effects of the utility model are:
This utility model has reasonable in design, the advantage such as easy to use, solves traditional equipment in detected portion
Position can not arrive problem, greatly facilitates operator's operation, and safe and reliable, degree of flexibility is high, improves the efficiency of maintenance.
Accompanying drawing explanation
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is front view of the present utility model；
Fig. 2 is the right view after this utility model removes handle；
Fig. 3 is the structural representation of locking device of the present utility model；
Fig. 4 is the structural representation of arm support of the present utility model.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and beneficial effect clearer, below in conjunction with accompanying drawing, to this
The preferred embodiment of utility model is described in detail, and is described further this utility model, to facilitate technical staff to manage
Solve.
As shown in Figures 1 to 4, the multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail is flat including electrical moving lifting
Platform 1, high back chair 9, detecting instrument Hanging Basket 14, work top controller 15, guardrail 16, described guardrail 16 is arranged on electronic movement
The upper end of formula hoistable platform 1, described high back chair 9 is symmetrically mounted on the upper rear of electrical moving hoistable platform 1, described height
Chair 9 is positioned at guardrail 16, and described work top controller 15 is arranged on the upper center of electrical moving hoistable platform 1,
Described detecting instrument Hanging Basket 14 is mounted on the left front portion of guardrail 16, and high back chair 9 is provided with arm support 13, described workbench
Face controller 15 is connected by wire with electrical moving hoistable platform 1.This utility model uses electrical moving hoistable platform 1
After, it is possible to achieve overall height freely regulates, and arbitrarily regulates direction, translational speed arbitrarily controls, and have employed guardrail 16 simultaneously
After, overall security can be made to be improved, provide safe operating platform for staff.
Described high back chair 9 is arranged on the upper rear of electrical moving hoistable platform 1, described locking by locking device
Device includes bolt 3, plain washer 4, standard check ring 5, nut 1, clip 7, described bolt 3, plain washer 4, standard spring
Back-up ring 5 constitutes locking member, and the middle part of clip 7 is sleeved on the bottom of high back chair 9, and the two ends, left and right of clip 7 are solid by locking member
Being scheduled on the upper rear of electrical moving hoistable platform 1, described electrical moving hoistable platform 1 is set with the junction of clip 7
There is rubber 2.After this utility model uses high back chair 9, such staff, when overhauling, can take, to alleviate work
The labor intensity of people.
Described arm support 13 includes nut 2 10, pad 11, nylon spacer 12, arm bracket 18, support shaft 19 and axle
Set 20, the bottom of described support shaft 19 is fixed on high back chair 9 by nut 2 10, pad 11, nylon spacer 12, described axle
The bottom of set 20 and the top threaded engagement of support shaft 19, described arm bracket 18 is fixed on the upper end of axle sleeve 20.This practicality is new
The arm support 13 of type can regulate the height of self according to the use demand of user, thus improves comfort level.
The upper end of described arm bracket 18 is provided with rubber blanket one 18a of arc.
The right-hand member of described electrical moving hoistable platform 1 is provided with label 8.
The right-hand member of described guardrail 16 is provided with guardrail wicket 17, to facilitate staff to come in and go out.
The left end of described electrical moving hoistable platform 1 is provided with handle 1a, i.e. can also manually promote integral device
Mobile.
The top surrounding outer edge of described electrical moving hoistable platform 1 is mounted on rubber blanket two 1b, on the one hand protects
Protect operator, on the other hand avoid detecting when car clashes into aircraft and cause body to damage.
The model of described electrical moving hoistable platform 1 is ZW51601.
During use, according to the demand of use, by manipulation work top controller 15, thus it is flat to control electrical moving lifting
The movement of platform 1 and lifting, to facilitate the maintenance of staff.
Finally illustrating, preferred embodiment above is only in order to illustrate the technical solution of the utility model and unrestricted, to the greatest extent
This utility model is described in detail by pipe by above preferred embodiment, but those skilled in the art should manage
Solve, in the form and details it can be made various change, without departing from this utility model claims institute
The scope limited.
Claims (8)
1. aircraft outer wing, the multiple material tests special-purpose vehicle of horizontal tail, including electrical moving hoistable platform (1), high back chair
(9), detecting instrument Hanging Basket (14), work top controller (15), guardrail (16), it is characterised in that: described guardrail (16) is installed
In the upper end of electrical moving hoistable platform (1), described high back chair (9) is symmetrically mounted on electrical moving hoistable platform (1)
Upper rear, described high back chair (9) is positioned at guardrail (16), and described work top controller (15) is arranged on electronic movement
The upper center of formula hoistable platform (1), described detecting instrument Hanging Basket (14) is mounted on the left front portion of guardrail (16), high back chair
(9) being provided with arm support (13) on, described work top controller (15) and electrical moving hoistable platform (1) pass through wire
It is connected.
A kind of aircraft outer wing the most according to claim 1, the multiple material tests special-purpose vehicle of horizontal tail, it is characterised in that: described height
Chair (9) is arranged on the upper rear of electrical moving hoistable platform (1) by locking device, and described locking device includes spiral shell
Bolt (3), plain washer (4), standard check ring (5), nut one (6), clip (7), described bolt (3), plain washer (4), standard
Check ring (5) constitutes locking member, and the middle part of clip (7) is sleeved on the bottom of high back chair (9), the two ends, left and right of clip (7)
The upper rear of electrical moving hoistable platform (1), described electrical moving hoistable platform (1) and card it is fixed on by locking member
The junction of hoop (7) is set with rubber (2).
A kind of aircraft outer wing the most according to claim 1, the multiple material tests special-purpose vehicle of horizontal tail, it is characterised in that: described hands
Arm support (13) includes nut two (10), pad (11), nylon spacer (12), arm bracket (18), support shaft (19) and axle sleeve
(20), the bottom of described support shaft (19) is fixed on high back chair by nut two (10), pad (11), nylon spacer (12)
(9), on, the bottom of described axle sleeve (20) and the top threaded engagement of support shaft (19), described arm bracket (18) is fixed on axle sleeve
(20) upper end.
A kind of aircraft outer wing the most according to claim 3, the multiple material tests special-purpose vehicle of horizontal tail, it is characterised in that: described hands
The upper end of bracket support (18) is provided with the rubber blanket one (18a) of arc.
A kind of aircraft outer wing the most according to claim 1, the multiple material tests special-purpose vehicle of horizontal tail, it is characterised in that: described electricity
The right-hand member of dynamic mobile hoistable platform (1) is provided with label (8).
A kind of aircraft outer wing the most according to claim 1, the multiple material tests special-purpose vehicle of horizontal tail, it is characterised in that protect described in:
The right-hand member on hurdle (16) is provided with guardrail wicket (17).
A kind of aircraft outer wing the most according to claim 1, the multiple material tests special-purpose vehicle of horizontal tail, it is characterised in that: described electricity
The left end of dynamic mobile hoistable platform (1) is provided with handle (1a).
A kind of aircraft outer wing the most according to claim 1, the multiple material tests special-purpose vehicle of horizontal tail, it is characterised in that: described electricity
The top surrounding outer edge of dynamic mobile hoistable platform (1) is mounted on rubber blanket two (1b).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620658593.5U CN205802913U (en) | 2016-06-28 | 2016-06-28 | The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620658593.5U CN205802913U (en) | 2016-06-28 | 2016-06-28 | The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205802913U true CN205802913U (en) | 2016-12-14 |
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ID=57512199
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620658593.5U Active CN205802913U (en) | 2016-06-28 | 2016-06-28 | The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205802913U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106006493A (en) * | 2016-06-28 | 2016-10-12 | 国营芜湖机械厂 | Special vehicle for airplane outer wing and horizontal tail composite material detection |
-
2016
- 2016-06-28 CN CN201620658593.5U patent/CN205802913U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106006493A (en) * | 2016-06-28 | 2016-10-12 | 国营芜湖机械厂 | Special vehicle for airplane outer wing and horizontal tail composite material detection |
| CN106006493B (en) * | 2016-06-28 | 2018-08-31 | 国营芜湖机械厂 | A kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |