CN205876162U - Combination working stand that uses on aircraft fuselage - Google Patents
Combination working stand that uses on aircraft fuselage Download PDFInfo
- Publication number
- CN205876162U CN205876162U CN201620775918.8U CN201620775918U CN205876162U CN 205876162 U CN205876162 U CN 205876162U CN 201620775918 U CN201620775918 U CN 201620775918U CN 205876162 U CN205876162 U CN 205876162U
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- China
- Prior art keywords
- bench
- column
- stand
- side stand
- handrail
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Abstract
The utility model relates to a combination working stand that uses on aircraft fuselage belongs to aircraft maintenance device field. Be equipped with work platform, a serial communication port, circular work platform projection is installed respectively in the four corners of the last side of work platform, the pipe difference cartridge of left side handrail and right handrail is on the work platform projection, be connected with the connecting rod between left side handrail and the right handrail, four minutes of work platform downside leave and preceding bench left side stand, preceding bench right side stand and back bench left side stand, the upper end of back bench right side stand is passed through the bolt and is linked to each other, preceding bench left side stand, install the running -board between the stand of the preceding bench right side, back bench left side stand, install the crossbeam between the stand of the back bench right side, install the connecting rod between preceding bench right side stand and the back bench right side stand and between preceding bench left side stand and the back bench left side stand, back bench left side stand, rubber is installed by the dish in back bench right side stand upper end.
Description
Technical field
This utility model relates to aircraft maintenance tool field, is the work in combination used on a kind of airframe in detail
Ladder.
Background technology
It is known that the work in combination ladder used on existing airframe is all to use metal material, there is structure weight, become
The use problems such as shape is big, it is big to take up room, carrying inconvenience.And cannot be carried out disassembly and assembly, the height of ladder lower limb can not be only
Vertical regulation.
Summary of the invention
In order to overcome the deficiencies in the prior art, this utility model provides the work in combination ladder used on a kind of airframe,
Simple in construction, easy to operate, this working stand is divided into several separate module, separately manufactured.In use, combination is one
Rise and make to be joined with bolts, be assembled into working stand；When not in use, it is split into several module, conveniently transports and deposit
Storage, hence it is evident that improve ease of use.
This utility model solves its technical problem and be the technical scheme is that the combination work used on a kind of airframe
Make ladder, be provided with work platforms, it is characterised in that the corner of work platforms upper side is separately installed with circular work platform projection,
The pipe of left handrail and right handrail is inserted on work platforms projection respectively, and being connected between left handrail with right handrail has connecting rod, work
Make four angles of platform underside to stand with front bench left column, front bench right column and rear bench left column, the rear bench right side respectively
The upper end of post is connected by bolt, is provided with pedal between front bench left column, front bench right column, rear bench left column,
Crossbeam is installed between rear bench right column, between front bench right column and rear bench right column and front bench left column with after
Being provided with connecting rod between bench left column, rear bench left column, rear bench right column upper end are provided with rubber by dish.
This utility model realizes also by following measure: front bench left column, front bench right column and rear bench
Left column, the lower end of rear bench right column are adjusted bolt and are provided with rubber feet.
The beneficial effects of the utility model are, this work in combination ladder can quickly disassembly and assembly, the height of four columns
All can independent regulation, convenient adapt to airframe upper shape, all there are preventing rubber, user in the position that may contact with aircraft
Just, stable, firm, meet the use demand of fast reserve.
Accompanying drawing explanation
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the guardrail scheme of installation of this utility model embodiment.
Fig. 3 is the lower margin structural representation of this utility model embodiment.
1. guardrail in figure, 101. left handrails, 102. right handrails, 103. connecting rods, 2. work platforms, 201. work platformses are convex
Post, 3. before bench, bench left column before 301., bench right column before 302., 303. pedals, 304. lower margins, 4. after bench,
Bench left column after 401., bench right column after 402., 403. crossbeams, 404. rubber lean on dish, 5. connecting rod, 6. regulation bolt,
7. fix nut, 8. rubber feet.
Detailed description of the invention
As shown in Figure 1, Figure 2, Figure 3 shows, this utility model includes guardrail 1, work platforms 2, front bench 3, rear bench 4, connects
Bar 5 grade five part composition.Described guardrail 1 includes three parts such as left handrail 101, right handrail 102 and connecting rod 103, described
Front bench 3 includes four parts such as front bench left column 301, front bench right column 302, pedal 303 and lower margin 304, described
Rear bench 4 includes that rear bench left column 401, rear bench right column 402, crossbeam 403, rubber are by five, dish 404 and lower margin 304 etc.
Point.The corner of work platforms 2 upper side is separately installed with circular work platform projection 201, left handrail 101 and right handrail 102
Pipe is inserted on work platforms projection 201 respectively, and being connected between left handrail 101 with right handrail 102 has connecting rod 103, and work is flat
Angle, four, platform 2 downside respectively with front bench left column 301, front bench right column 302 and rear bench left column 401, afterwards ladder
The upper end of section right column 402 is connected by bolt, is provided with pedal between front bench left column 301, front bench right column 302
303, crossbeam 403, front bench right column 302 and rear bench are installed between rear bench left column 401, rear bench right column 402
Being provided with connecting rod 5 between right column 402 and between front bench left column 301 and rear bench left column 401, a rear bench left side is stood
Post 401, rear bench right column 402 upper end are provided with rubber and lean on dish 404, to prevent ladder from colliding aircraft.Described front bench 3
Front bench left column 301, front bench right column 302 and the rear rear bench left column 401 of bench 4, rear bench right column 402
Lower end is equipped with the rubber feet 304 of band regulation bolt, and described rubber feet 304 has regulation bolt 6, fixing nut 7 and rubber
Glue leg 8 forms.
Claims (2)
1. the work in combination ladder used on an airframe, is provided with work platforms, it is characterised in that work platforms upper side
Corner is separately installed with circular work platform projection, and the pipe of left handrail and right handrail is inserted on work platforms projection respectively,
Being connected between left handrail with right handrail and have connecting rod, angle, four, work platforms downside is right with front bench left column, front bench respectively
The upper end of column and rear bench left column, rear bench right column is connected by bolt, front bench left column, front bench right column
Between pedal is installed, crossbeam is installed, front bench right column and rear bench between rear bench left column, rear bench right column
Connecting rod, rear bench left column, rear bench are installed between right column and between front bench left column and rear bench left column
Right column upper end is provided with rubber by dish.
The work in combination ladder used on airframe the most according to claim 1, it is characterised in that a described front bench left side is stood
Post, front bench right column and rear bench left column, the lower end of rear bench right column are adjusted bolt and are provided with rubber feet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620775918.8U CN205876162U (en) | 2016-07-22 | 2016-07-22 | Combination working stand that uses on aircraft fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620775918.8U CN205876162U (en) | 2016-07-22 | 2016-07-22 | Combination working stand that uses on aircraft fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205876162U true CN205876162U (en) | 2017-01-11 |
Family
ID=57696859
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620775918.8U Active CN205876162U (en) | 2016-07-22 | 2016-07-22 | Combination working stand that uses on aircraft fuselage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205876162U (en) |
-
2016
- 2016-07-22 CN CN201620775918.8U patent/CN205876162U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant |