CN106006493B - A kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle - Google Patents
A kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle Download PDFInfo
- Publication number
- CN106006493B CN106006493B CN201610486309.5A CN201610486309A CN106006493B CN 106006493 B CN106006493 B CN 106006493B CN 201610486309 A CN201610486309 A CN 201610486309A CN 106006493 B CN106006493 B CN 106006493B
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- China
- Prior art keywords
- hoistable platform
- electrical moving
- guardrail
- purpose vehicle
- horizontal tail
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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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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F11/00—Lifting devices specially adapted for particular uses not otherwise provided for
- B66F11/04—Lifting devices specially adapted for particular uses not otherwise provided for for movable platforms or cabins, e.g. on vehicles, permitting workmen to place themselves in any desired position for carrying out required operations
- B66F11/042—Lifting devices specially adapted for particular uses not otherwise provided for for movable platforms or cabins, e.g. on vehicles, permitting workmen to place themselves in any desired position for carrying out required operations actuated by lazy-tongs mechanisms or articulated levers
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- Engineering & Computer Science (AREA)
- Structural Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Mechanical Engineering (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The invention discloses a kind of aircraft outer wings, horizontal tail answers material tests special-purpose vehicle, including electrical moving hoistable platform, two high back chairs, detecting instrument Hanging Basket, work top controller, guardrail, guardrail is mounted on the upper end of electrical moving hoistable platform, two high back chairs are symmetrically mounted on the upper rear of electrical moving hoistable platform, two high back chairs are located in guardrail, work top controller is mounted on the upper center of electrical moving hoistable platform, detecting instrument Hanging Basket is mounted on the left front portion of guardrail, it is mounted on arm support on two high back chairs, work top controller is connected with electrical moving hoistable platform by conducting wire.The present invention has many advantages, such as reasonable in design, easy to use, solves the problems, such as that traditional equipment is not reachable in detection site, greatly facilitates operating personnel's operation, securely and reliably, degree of flexibility is high, improves the efficiency of maintenance.
Description
Technical field
The present invention relates to aeronautical product detection technique field, specifically a kind of aircraft outer wing, horizontal tail answer material tests
Special-purpose vehicle.
Background technology
After composite structure non-destructive testing on aircraft is taken a flight test, need to carry out ultrasound examination before transition, it is outer at this time
Installation and debugging are complete for the big component such as the wing, horizontal tail.In situ detection is carried out, the detection operation of lower wall panels is extremely difficult.Because this is several
The inspection that the big component of item need to carry out whole region can not be moved arbitrarily, respective regions are by aircraft components using toolings such as ladders
It blocks, ladder is also without placement space, it is therefore necessary to design a applicable tooling, help is detected a flaw and examined in situ on personnel's carry out machine
It surveys.
Invention content
In order to solve the above technical problem, the present invention provides a kind of aircraft outer wing, horizontal tails to answer material tests special-purpose vehicle.
The present invention solves its technical problem using following technical scheme to realize：
A kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle, including electrical moving hoistable platform, two high backs
Chair, detecting instrument Hanging Basket, work top controller, guardrail, the guardrail be mounted on electrical moving hoistable platform upper end, two
A high back chair is symmetrically mounted on the upper rear of electrical moving hoistable platform, and two high back chairs are located at guardrail
Interior, the work top controller is mounted on the upper center of electrical moving hoistable platform, and the detecting instrument Hanging Basket mounts
Arm support, the work top controller and electrical moving are mounted in the left front portion of guardrail, two high back chairs
Hoistable platform is connected by conducting wire.After the present invention uses electrical moving hoistable platform, whole height may be implemented and freely adjust
Section arbitrarily adjusts direction, movement speed and arbitrarily controls, while after using guardrail, overall security can be made to be improved, be
Staff provides safe operating platform.
Two high back chairs are mounted on the upper rear of electrical moving hoistable platform, the lock by locking device
Tight device includes bolt, plain washer, standard check ring, nut one, clip, the bolt, plain washer, standard check ring structure
At locking member, the bottom of corresponding high back chair is sleeved in the middle part of clip, the left and right ends of clip are fixed on by locking member
The junction of the upper rear of electrical moving hoistable platform, the electrical moving hoistable platform and clip is set with rubber.
After the present invention uses high back chair, such staff can take when overhauling, to mitigate the labor intensity of worker.
The arm support includes nut two, gasket, nylon spacer, arm bracket, support shaft and axle sleeve, the support shaft
Lower part be fixed on corresponding high back chair by nut two, gasket, nylon spacer, the lower part of the axle sleeve and support shaft
Top screw-thread fit, the arm bracket are fixed on the upper end of axle sleeve.The arm support of the present invention can make according to user
The height that itself is adjusted with demand, to improve comfort level.
The upper end of the arm bracket is equipped with the rubber pad one of arc.
The right end of the electrical moving hoistable platform is equipped with label.
The right end of the guardrail is equipped with guardrail wicket, to facilitate staff to come in and go out.
The left end of the electrical moving hoistable platform is equipped with handle, i.e., can also carry out that integral device is pushed to move manually
It is dynamic.
The top surrounding outer edge of the electrical moving hoistable platform is mounted on rubber pad two, on the one hand protection behaviour
Make personnel, causes body to damage when detection vehicle on the other hand being avoided to hit aircraft..
The model ZW51601 of the electrical moving hoistable platform.
The beneficial effects of the invention are as follows：
The present invention have many advantages, such as it is reasonable in design, easy to use, solve traditional equipment detection site not
Reachable problem greatly facilitates operating personnel's operation, and securely and reliably, degree of flexibility is high, improves the efficiency of maintenance.
Description of the drawings
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the front view of the present invention；
Fig. 2 is the right view after present invention removal handle；
Fig. 3 is the structural schematic diagram of the locking device of the present invention；
Fig. 4 is the structural schematic diagram of the arm support of the present invention.
Specific implementation mode
In order to keep the purpose of the present invention, technical solution and advantageous effect clearer, below in conjunction with attached drawing, to the present invention
Preferred embodiment be described in detail, the present invention will be further described, to facilitate the technical staff to understand.
As shown in Figures 1 to 4, a kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle, including electrical moving lifting is put down
Platform 1, two high back chair 9, detecting instrument Hanging Basket 14, work top controller 15, guardrail 16, the guardrail 16 are mounted on electronic
The upper end of mobile hoistable platform 1, after two high back chairs 9 are symmetrically mounted on the upper end of electrical moving hoistable platform 1
Portion, two high back chairs 9 are located in guardrail 16, and the work top controller 15 is mounted on electrical moving hoistable platform
1 upper center, the detecting instrument Hanging Basket 14 are mounted on the left front portion of guardrail 16, hand are mounted on two high back chairs 9
Arm support 13, the work top controller 15 are connected with electrical moving hoistable platform 1 by conducting wire.The present invention is using electronic
After mobile hoistable platform 1, whole height may be implemented and freely adjust, arbitrarily adjusting direction, movement speed arbitrarily control, together
When use guardrail 16 after, overall security can be made to be improved, safe operating platform is provided for staff.
Two high back chairs 9 are mounted on the upper rear of electrical moving hoistable platform 1 by locking device, described
Locking device includes bolt 3, plain washer 4, standard check ring 5, nut 1, clip 7, the 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 corresponding high back chair 9, and the left and right ends of clip 7 are logical
Cross the upper rear that locking member is fixed on electrical moving hoistable platform 1, the electrical moving hoistable platform 1 and clip 7
Junction is set with rubber 2.After the present invention uses high back chair 9, such staff can take when overhauling, with
Mitigate the labor intensity of worker.
The arm support 13 includes nut 2 10, gasket 11, nylon spacer 12, arm bracket 18, support shaft 19 and axis
Set 20, the lower part of the support shaft 19 is fixed on by nut 2 10, gasket 11, nylon spacer 12 on corresponding high back chair 9,
The lower part of the axle sleeve 20 and the top screw-thread fit of support shaft 19, the arm bracket 18 are fixed on the upper end of axle sleeve 20.This
The arm support 13 of invention can adjust the height of itself according to the use demand of user, to improve comfort level.
The upper end of the arm bracket 18 is equipped with one 18a of rubber pad of arc.
The right end of the electrical moving hoistable platform 1 is equipped with label 8.
The right end of the guardrail 16 is equipped with guardrail wicket 17, to facilitate staff to come in and go out.
The left end of the electrical moving hoistable platform 1 is equipped with handle 1a, i.e., can also carry out pushing integral device manually
It is mobile.
The top surrounding outer edge of the electrical moving hoistable platform 1 is mounted on two 1b of rubber pad, on the one hand protects
Operating personnel are protected, cause body to damage when detection vehicle on the other hand being avoided to hit aircraft..
The model ZW51601 of the electrical moving hoistable platform 1.
In use, according to use demand, it is flat to control electrical moving lifting by manipulating work top controller 15
The movement and lifting of platform 1, to facilitate the maintenance of staff.
Finally illustrate, preferred embodiment above is merely illustrative of the technical solution of the present invention and unrestricted, although logical
It crosses above preferred embodiment the present invention is described in detail, however, those skilled in the art should understand that, can be
Various changes are made to it in form and in details, without departing from claims of the present invention limited range.
Claims (7)
1. a kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle, including electrical moving hoistable platform（1）, two high backs
Chair（9）, detecting instrument Hanging Basket（14）, work top controller（15）, guardrail（16）, it is characterised in that：The guardrail（16）Peace
Mounted in electrical moving hoistable platform（1）Upper end, two high back chairs（9）It is flat to be symmetrically mounted on electrical moving lifting
Platform（1）Upper rear, two high back chairs（9）Positioned at guardrail（16）It is interior, the work top controller（15）Installation
In electrical moving hoistable platform（1）Upper center, the detecting instrument Hanging Basket（14）It is mounted on guardrail（16）Left front portion,
Two high back chairs（9）On be mounted on arm support（13）, the work top controller（15）It is lifted with electrical moving
Platform（1）It is connected by conducting wire, two high back chairs（9）It is mounted on electrical moving hoistable platform by locking device
（1）Upper rear, the locking device includes bolt（3）, plain washer（4）, standard check ring（5）, nut one（6）, card
Hoop（7）, the bolt（3）, plain washer（4）, standard check ring（5）Constitute locking member, clip（7）Middle part be sleeved on correspondence
High back chair（9）Bottom, clip（7）Left and right ends electrical moving hoistable platform is fixed on by locking member（1）'s
Upper rear, the electrical moving hoistable platform（1）With clip（7）Junction be set with rubber（2）.
2. a kind of aircraft outer wing according to claim 1, horizontal tail answer material tests special-purpose vehicle, it is characterised in that：The hand
Arm support（13）Including nut two（10）, gasket（11）, nylon spacer（12）, arm bracket（18）, support shaft（19）And axle sleeve
（20）, the support shaft（19）Lower part pass through nut two（10）, gasket（11）, nylon spacer（12）Corresponding height is fixed on to lean on
Chair with back（9）On, the axle sleeve（20）Lower part and support shaft（19）Top screw-thread fit, the arm bracket（18）It is fixed on
Axle sleeve（20）Upper end.
3. a kind of aircraft outer wing according to claim 2, horizontal tail answer material tests special-purpose vehicle, it is characterised in that：The hand
Bracket support（18）Upper end be equipped with arc rubber pad one（18a）.
4. a kind of aircraft outer wing according to claim 1, horizontal tail answer material tests special-purpose vehicle, it is characterised in that：The electricity
Dynamic mobile hoistable platform（1）Right end label is installed（8）.
5. a kind of aircraft outer wing according to claim 1, horizontal tail answer material tests special-purpose vehicle, it is characterised in that：The shield
Column（16）Right end guardrail wicket is installed（17）.
6. a kind of aircraft outer wing according to claim 1, horizontal tail answer material tests special-purpose vehicle, it is characterised in that：The electricity
Dynamic mobile hoistable platform（1）Left end be equipped with handle（1a）.
7. a kind of aircraft outer wing according to claim 1, horizontal tail answer material tests special-purpose vehicle, it is characterised in that：The electricity
Dynamic mobile hoistable platform（1）Top surrounding outer edge be mounted on rubber pad two（1b）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610486309.5A CN106006493B (en) | 2016-06-28 | 2016-06-28 | A kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610486309.5A CN106006493B (en) | 2016-06-28 | 2016-06-28 | A kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106006493A CN106006493A (en) | 2016-10-12 |
| CN106006493B true CN106006493B (en) | 2018-08-31 |
Family
ID=57084525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610486309.5A Active CN106006493B (en) | 2016-06-28 | 2016-06-28 | A kind of aircraft outer wing, horizontal tail answer material tests special-purpose vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106006493B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108975241A (en) * | 2018-09-14 | 2018-12-11 | 苏州科讯机械设备有限公司 | A kind of elevator mounting seat |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB819884A (en) * | 1957-09-12 | 1959-09-09 | Scanners Ltd | Improvements in or relating to mobile suspension units |
| CN2844096Y (en) * | 2005-09-14 | 2006-12-06 | 李善文 | Liftable and foldable operating platform |
| CN201442831U (en) * | 2008-12-24 | 2010-04-28 | 贵阳黔江机械厂 | Hydraulic lifting work ladder with extendable platform |
| CN202457362U (en) * | 2012-03-20 | 2012-10-03 | 广力达企业有限公司 | Height regulating structure of seat armrest |
| CN204304278U (en) * | 2014-08-15 | 2015-04-29 | 郑磊 | Relaying maintenance Special lift truck |
| CN204508739U (en) * | 2015-03-13 | 2015-07-29 | 湖北脉辉科技有限公司 | Self-walking aerial working platform |
| CN205313020U (en) * | 2016-01-12 | 2016-06-15 | 商旭东 | Scissor fork type hydraulic elevator |
| CN205802913U (en) * | 2016-06-28 | 2016-12-14 | 国营芜湖机械厂 | The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail |
-
2016
- 2016-06-28 CN CN201610486309.5A patent/CN106006493B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB819884A (en) * | 1957-09-12 | 1959-09-09 | Scanners Ltd | Improvements in or relating to mobile suspension units |
| CN2844096Y (en) * | 2005-09-14 | 2006-12-06 | 李善文 | Liftable and foldable operating platform |
| CN201442831U (en) * | 2008-12-24 | 2010-04-28 | 贵阳黔江机械厂 | Hydraulic lifting work ladder with extendable platform |
| CN202457362U (en) * | 2012-03-20 | 2012-10-03 | 广力达企业有限公司 | Height regulating structure of seat armrest |
| CN204304278U (en) * | 2014-08-15 | 2015-04-29 | 郑磊 | Relaying maintenance Special lift truck |
| CN204508739U (en) * | 2015-03-13 | 2015-07-29 | 湖北脉辉科技有限公司 | Self-walking aerial working platform |
| CN205313020U (en) * | 2016-01-12 | 2016-06-15 | 商旭东 | Scissor fork type hydraulic elevator |
| CN205802913U (en) * | 2016-06-28 | 2016-12-14 | 国营芜湖机械厂 | The multiple material tests special-purpose vehicle of a kind of aircraft outer wing, horizontal tail |
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| Publication number | Publication date |
|---|---|
| CN106006493A (en) | 2016-10-12 |
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