CN216834346U - Aircraft windshield maintenance platform - Google Patents
Aircraft windshield maintenance platform Download PDFInfo
- Publication number
- CN216834346U CN216834346U CN202220218500.2U CN202220218500U CN216834346U CN 216834346 U CN216834346 U CN 216834346U CN 202220218500 U CN202220218500 U CN 202220218500U CN 216834346 U CN216834346 U CN 216834346U
- Authority
- CN
- China
- Prior art keywords
- support frame
- frame body
- top surface
- maintenance platform
- fixedly arranged
- Prior art date
- 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.)
- Expired - Fee Related
Links
- 238000012423 maintenance Methods 0.000 title claims abstract description 23
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 9
- 239000010959 steel Substances 0.000 claims abstract description 9
- 238000004804 winding Methods 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims description 3
- 230000001681 protective effect Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims 2
- 238000010030 laminating Methods 0.000 description 2
- 230000009194 climbing Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
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Abstract
The utility model discloses an aircraft windshield maintenance platform belongs to maintenance platform technical field. The utility model provides an aircraft windscreen maintenance platform, includes and supports the support body, supports the support body bottom surface and has set firmly the rubber layer, supports support body right-hand member bottom surface and is equipped with bunch subassembly, supports support body top surface right side and has set firmly place the platform, places the bench face and has set firmly the hoist engine, the outside coiling of hoist engine has the steel cable, places the platform antetheca and has set firmly spacing slide, spacing slide top surface rotates and is connected with the fixed pulley, spacing slide lower part cover is equipped with the promotion platform, supports the support body top surface and has set firmly the rail guard. The utility model discloses a bunch subassembly is connected this device and aircraft leg fixedly, and then improves the stability that the device was placed, has improved staff's safety greatly.
Description
Technical Field
The utility model relates to a maintenance platform technical field, more specifically say, relate to an aircraft windshield maintenance platform.
Background
An aircraft is an aircraft which has a power device with one or more engines to generate forward thrust or pull force, generates lift force by fixed wings of a fuselage, and flies in the atmosphere and is heavier than air. Whereas aircraft windshield maintenance operations typically include maintenance, replacement of the windshield, inspection, and maintenance of the windshield mounting bulkhead. Because the windshield is large in size, a plurality of maintenance personnel are required to work simultaneously, but the standing area of the existing airplane windshield maintenance platform is not enough to meet the use requirement, and therefore the airplane windshield maintenance platform is provided.
SUMMERY OF THE UTILITY MODEL
1. Technical problem to be solved
An object of the utility model is to provide an aircraft windshield maintenance platform to solve the problem that proposes among the above-mentioned background art.
2. Technical scheme
An aircraft windshield maintenance platform comprises a support frame body, wherein an anti-skid steel plate layer is laid on the top surface of the support frame body, the bottom surface of the support frame body is fixedly provided with a rubber layer, the bottom surface of the right end of the support frame body is provided with a wire bunching component, the wire harness assembly comprises a mounting shell, an adjusting worm is rotationally connected in the mounting shell, a worm wheel is arranged on the bottom surface of the adjusting worm, a winding wheel is fixedly arranged on the rear wall of the worm wheel, a pulling and holding wire is wound outside the winding wheel, a spring buckle is fixedly arranged at the other end of the pulling and holding wire, a placing table is fixedly arranged on the right side of the top surface of the support frame body, a winch is fixedly arranged on the top surface of the placing table, a steel cable is wound outside the winch, a limiting sliding plate is fixedly arranged on the front wall of the placing table, a fixed pulley is rotatably connected to the top surface of the limiting sliding plate, the lower part of the limiting sliding plate is sleeved with a lifting platform, and the top surface of the support frame body is fixedly provided with a protective guard.
Preferably, the mounting shell is fixedly connected with the support frame body.
Preferably, the adjusting worm is in meshed transmission with the worm wheel.
Preferably, the lifting platform is in sliding fit with the limit sliding plate.
3. Advantageous effects
Compared with the prior art, the utility model has the advantages of:
1. the utility model discloses support the support body can with aircraft nose laminating, and then provide the work area that the large tracts of land stood, and then improve aircraft windshield maintenance efficiency, and this device goes up and down through promoting platform transportation personnel, has saved personnel's climbing, has further improved maintenance efficiency.
2. The utility model discloses a bunch subassembly is connected this device and aircraft leg fixedly, and then improves the stability that the device was placed, has improved staff's safety greatly, and this device rubber layer and aircraft nose laminating avoid supporting support body scratch aircraft.
Drawings
Fig. 1 is a left side schematic view of the overall structure of the present invention;
FIG. 2 is a right side schematic view of the overall structure of the present invention;
fig. 3 is an internal schematic view of the structure of the wire harness assembly of the present invention;
FIG. 4 is an enlarged schematic view of the structure at the position A of the present invention;
the reference numbers in the figures illustrate: 1. a support frame body; 2. a rubber layer; 3. a wire harness assembly; 4. a placing table; 5. a limiting sliding plate; 6. lifting the platform; 7. protecting a fence; 101. an anti-skid steel plate layer; 301. mounting a shell; 302. adjusting the worm; 303. a worm gear; 304. a winding wheel; 305. pulling and holding the wire; 306. a spring buckle; 401. a winch; 501. and a fixed pulley.
Detailed Description
Referring to fig. 1-4, the present invention provides a technical solution:
an aircraft windshield maintenance platform comprises a support frame body 1, an anti-skid steel plate layer 101 is laid on the top surface of the support frame body 1 to form a standing platform, a rubber layer 2 is fixedly arranged on the bottom surface of the support frame body 1 to avoid damage caused by collision with a machine head, a wire bunching assembly 3 is arranged on the bottom surface of the right end of the support frame body 1, the wire bunching assembly 3 comprises a mounting shell 301, an adjusting worm 302 is rotatably connected in the mounting shell 301, a worm wheel 303 is arranged on the bottom surface of the adjusting worm 302, a wire winding wheel 304 is fixedly arranged on the rear wall of the worm wheel 303, a pull wire 305 is wound outside the wire winding wheel 304, a spring buckle 306 is fixedly arranged at the other end of the pull wire 305, a placing table 4 is fixedly arranged on the right side of the top surface of the support frame body 1, a winch 401 is fixedly arranged on the top surface of the placing table 4, a steel cable is wound outside the winch 401, a limit sliding plate 5 is fixedly arranged on the front wall of the placing table 4, a fixed sliding plate 5 is rotatably connected with a fixed pulley 501, a lifting platform 6 is sleeved on the lower portion of the limit sliding plate 5, the top surface of the support frame body 1 is fixedly provided with a protective guard 7.
Specifically, the mounting shell 301 is fixedly connected with the support frame body 1, so that the wire harness assembly 3 can be mounted and used conveniently.
Furthermore, the adjusting worm 302 is meshed with the worm wheel 303 for transmission, so that the pull-hold wire 305 is limited and fixed conveniently.
In addition, promote 6 and 5 sliding fit of spacing slide, be convenient for promote 6 spacing lifts of platform.
The working principle is as follows: when the device is used, firstly, the support frame body 1 of the device is moved to an aircraft nose, the rubber layer 2 is attached to the aircraft nose, then the pull holding wire 305 bypasses a leg on the bottom surface of the aircraft nose, the spring buckle 306 is fixedly connected with the other end of the support frame body 1 in a hanging mode, then the adjusting worm 302 rotates clockwise, the winding wheel 304 is driven to tighten the pull holding wire 305, the support frame body 1 is fixedly attached to the aircraft nose, and finally, a maintenance worker ascends to the anti-skid steel plate layer 101 through the lifting platform 6 and then maintains and operates the aircraft windshield.
Claims (4)
1. The utility model provides an aircraft windshield maintenance platform, includes support frame body (1), its characterized in that: the anti-skid steel plate layer (101) is laid on the top surface of the support frame body (1), the rubber layer (2) is fixedly arranged on the bottom surface of the support frame body (1), the wire harness assembly (3) is arranged on the bottom surface of the right end of the support frame body (1), the wire harness assembly (3) comprises an installation shell (301), an adjusting worm (302) is rotationally connected in the installation shell (301), a worm wheel (303) is arranged on the bottom surface of the adjusting worm (302), a winding wheel (304) is fixedly arranged on the rear wall of the worm wheel (303), a pulling wire (305) is wound outside the winding wheel (304), a spring buckle (306) is fixedly arranged at the other end of the pulling wire (305), a placing table (4) is fixedly arranged on the right side of the top surface of the support frame body (1), a winch (401) is fixedly arranged on the top surface of the placing table (4), a steel cable is wound outside the winch (401), a limiting sliding plate (5) is fixedly arranged on the placing table (4), the top surface of the limiting sliding plate (5) is rotatably connected with a fixed pulley (501), the lower part of the limiting sliding plate (5) is sleeved with a lifting platform (6), and the top surface of the support frame body (1) is fixedly provided with a protective guard (7).
2. An aircraft windshield maintenance platform according to claim 1, wherein: the mounting shell (301) is fixedly connected with the support frame body (1).
3. An aircraft windshield maintenance platform according to claim 1, wherein: the adjusting worm (302) is in meshed transmission with the worm wheel (303).
4. An aircraft windshield maintenance platform according to claim 1, wherein: the lifting platform (6) is in sliding fit with the limiting sliding plate (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220218500.2U CN216834346U (en) | 2022-01-26 | 2022-01-26 | Aircraft windshield maintenance platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220218500.2U CN216834346U (en) | 2022-01-26 | 2022-01-26 | Aircraft windshield maintenance platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216834346U true CN216834346U (en) | 2022-06-28 |
Family
ID=82087081
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220218500.2U Expired - Fee Related CN216834346U (en) | 2022-01-26 | 2022-01-26 | Aircraft windshield maintenance platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216834346U (en) |
-
2022
- 2022-01-26 CN CN202220218500.2U patent/CN216834346U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220628 |