CN209739384U - Lifting platform for aircraft maintenance - Google Patents
Lifting platform for aircraft maintenance Download PDFInfo
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- CN209739384U CN209739384U CN201920440162.5U CN201920440162U CN209739384U CN 209739384 U CN209739384 U CN 209739384U CN 201920440162 U CN201920440162 U CN 201920440162U CN 209739384 U CN209739384 U CN 209739384U
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- platform
- base
- aircraft maintenance
- guardrail
- telescopic arm
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Abstract
The application discloses a lifting platform for aircraft maintenance, which comprises a base and an operation platform, wherein a hydraulic telescopic arm is vertically arranged on the base, the top end of the hydraulic telescopic arm is detachably connected with a fixed seat, and a slide rail is arranged on the fixed seat; the bottom surface of the operating platform is provided with a pulley matched with the slide rail, and the pulley is provided with a sliding motor; the bottom surface of the base is provided with a universal wheel with a self-locking structure. According to the scheme provided by the application, the lifting of the operating platform is controlled through the hydraulic telescopic arm, so that parts with different heights can be maintained conveniently; meanwhile, the operation platform can horizontally slide relative to the fixed seat, so that the horizontal maintenance range of the operation platform is further expanded, and the problem that the whole operation platform needs to be frequently moved when adjacent parts are maintained is avoided. The sliding motor is controlled to be opened or closed through the control switch, so that the horizontal position of the operating platform can be rapidly moved, and great convenience is further brought to workers.
Description
Technical Field
the utility model relates to an aircraft maintenance technical field, in particular to lift platform of aircraft maintenance.
Background
Maintenance personnel are required to access various parts of the aircraft including landing gear, wheel wells, aircraft flaps, etc. by the aircraft maintenance task. The positions to be maintained are located in different places of the airplane and have different heights, and maintenance personnel generally need to maintain a working ladder by means of the airplane when approaching the positions.
The defects of the existing airplane maintenance work ladder are as follows: the structure is simple, the function is single, and the working ladder needs to be frequently moved if a user needs to approach different parts of the airplane or the airplane needs to be switched to a jacked state.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a lift platform of aircraft maintenance to solve the problem of proposing among the above-mentioned background art.
The utility model provides a lifting platform for aircraft maintenance, which comprises a base and an operation platform, wherein a hydraulic telescopic arm is vertically arranged on the base, the top end of the hydraulic telescopic arm is detachably connected with a fixed seat, and a slide rail is arranged on the fixed seat; a pulley matched with the sliding rail is arranged on the bottom surface of the operating platform, and a sliding motor is arranged on the pulley; a first guardrail is arranged on one side of the operating platform, a control switch is arranged on the first guardrail, and the control switch is electrically connected with the sliding motor; a second guardrail is arranged on the other side of the operating platform, an escalator is arranged on the second guardrail, and a barrier is arranged between the first guardrail and the second guardrail; the bottom surface of the base is provided with a universal wheel with a self-locking structure.
Optionally, a retraction slot capable of storing the hydraulic telescopic arm is arranged on the base.
Optionally, a limiting block for limiting the sliding of the pulley is arranged on the sliding rail on the fixing seat.
Optionally, a support leg is further disposed on the bottom surface of the base, and the support leg is located on the outer side of the universal wheel.
Optionally, the lower end of the leg is provided with a cushion pad.
Optionally, the leg is a telescoping leg.
Optionally, an anti-slip layer is arranged on the operating platform, and the anti-slip layer is a plurality of strip-shaped protrusions or a rubber layer.
Optionally, a service tool box is arranged in the operation platform.
Optionally, a distance measuring sensor is arranged on the base.
Optionally, a storage battery is arranged on the base, and the storage battery is electrically connected with the sliding motor.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) The lifting platform for aircraft maintenance comprises a base and an operating platform, wherein the base is vertically provided with a hydraulic telescopic arm, and the lifting of the operating platform is controlled by the hydraulic telescopic arm, so that parts with different heights can be maintained conveniently; meanwhile, the operation platform can horizontally slide relative to the fixed seat, so that the horizontal maintenance range of the operation platform is further expanded, and the problem that the whole operation platform needs to be frequently moved when adjacent parts are maintained is avoided.
(2) The utility model discloses the lift platform of aircraft maintenance still includes sliding motor, and this sliding motor sets up on the pulley, through opening or closing of control switch control sliding motor to horizontal position that just can quick travel operation platform has further brought very big convenience for the staff.
Drawings
Other features, objects and advantages of the present application will become more apparent upon reading of the following detailed description of non-limiting embodiments thereof, made with reference to the accompanying drawings in which:
Fig. 1 is a schematic structural view of a lifting platform for aircraft maintenance provided by an embodiment of the present invention
fig. 2 is a schematic structural diagram of an operating platform provided in an embodiment of the present invention;
fig. 3 is a schematic structural view of a second guardrail provided by an embodiment of the present invention.
Description of reference numerals:
1. A base; 2. a storage battery; 3. a hydraulic telescopic arm; 4. an operating platform; 5. a retraction slot; 6. a support leg; 7. a cushion pad; 8. a universal wheel; 9. a first guardrail; 10. a control switch; 11. a control button; 12. a barrier; 13. a fixed seat; 14. a slide rail; 15. a limiting block; 16. a ranging sensor; 17. a second guard rail; 18. a pulley; 19. an escalator; 20. a slide motor.
Detailed Description
The present application will be described in further detail with reference to the following drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the relevant invention and not restrictive of the invention. It should be noted that, for convenience of description, only the portions related to the present invention are shown in the drawings.
In the description of the present application, it is to be understood that the terms "central," "longitudinal," "lateral," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientation or positional relationship indicated in the drawings for convenience in describing the present invention and to simplify the description, but are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
It should be noted that unless expressly stated or limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly and include, for example, fixed or removable connections or integral connections; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
The embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.
referring to fig. 1-3, an embodiment of the present invention provides a lifting platform for aircraft maintenance, including a base 1 and an operating platform 4, wherein a hydraulic telescopic arm 3 is vertically disposed on the base 1, a fixing seat 13 is detachably connected to a top end of the hydraulic telescopic arm 3, and a slide rail 14 is disposed on the fixing seat 13; a pulley 18 matched with the slide rail 14 is arranged on the bottom surface of the operating platform 4, and a sliding motor 20 is arranged on the pulley 18; a first guardrail 9 is arranged on one side of the operating platform 4, a control switch 10 is arranged on the first guardrail 9, specifically, a control button 11 is arranged on the control switch 10, and the control switch 10 is electrically connected with the sliding motor 20; a second guardrail 17 is arranged on the other side of the operating platform 4, an escalator 19 is arranged on the second guardrail 17, and a barrier 12 is arranged between the first guardrail 9 and the second guardrail 17; the bottom surface of the base 1 is provided with a universal wheel 8 with a self-locking structure.
According to the embodiment of the application, the lifting of the operating platform is controlled through the hydraulic telescopic arm, so that parts with different heights can be maintained conveniently; meanwhile, the operation platform can horizontally slide relative to the fixed seat, so that the horizontal maintenance range of the operation platform is further expanded, and the problem that the whole operation platform needs to be frequently moved when a nearby part is maintained is avoided; the sliding motor is controlled to be opened or closed through the control switch, so that the horizontal position of the operating platform can be rapidly moved, and great convenience is further brought to workers.
Further, the base 1 is provided with a storage groove 5 capable of storing the hydraulic telescopic arm 3, and the storage groove is used for storing the hydraulic telescopic arm 3 and is convenient to store.
Furthermore, a limiting block 15 for limiting the sliding of the pulley 18 is arranged on the sliding rail 14 on the fixed seat 13, so as to prevent the pulley 18 from sliding out of the sliding rail 14.
Further, still be provided with landing leg 6 on the bottom surface of base 1, landing leg 6 is located the outside of universal wheel 8 for realize supporting the platform, whole device is more reliable and more stable.
Further, the lower end of the leg 6 is provided with a cushion pad 7.
Furthermore, the supporting legs 6 are telescopic supporting legs, the height of the whole platform can be adjusted, and the use is convenient.
Further, an anti-slip layer is arranged on the operating platform 4, and the anti-slip layer is a plurality of strip-shaped bulges or a rubber layer.
Further, a maintenance tool box is arranged in the operating platform 4.
Further, a distance measuring sensor 16 is arranged on the base 1.
Further, a storage battery 2 is arranged on the base 1, and the storage battery 2 is electrically connected with the sliding motor 20.
In summary, the lifting platform for aircraft maintenance provided by the embodiment of the application comprises a base and an operation platform, wherein a hydraulic telescopic arm is vertically arranged on the base, and the lifting of the operation platform is controlled by the hydraulic telescopic arm, so that the lifting platform can be conveniently maintained at different height parts; meanwhile, the operation platform can horizontally slide relative to the fixed seat, so that the horizontal maintenance range of the operation platform is further expanded, and the problem that the whole operation platform needs to be frequently moved when adjacent parts are maintained is avoided. Still include the sliding motor, this sliding motor sets up on the pulley, through opening or closing of control switch control sliding motor to just can the quick travel operation platform's horizontal position, further brought very big convenience for the staff.
the above is the preferred embodiment of the present invention, and the technical personnel in the field of the present invention can also change and modify the above-mentioned embodiment, therefore, the present invention is not limited to the above-mentioned specific embodiment, and any obvious improvement, replacement or modification made by the technical personnel in the field on the basis of the present invention all belong to the protection scope of the present invention.
Claims (10)
1. A lifting platform for aircraft maintenance is characterized by comprising a base (1) and an operating platform (4), wherein a hydraulic telescopic arm (3) is vertically arranged on the base (1), the top end of the hydraulic telescopic arm (3) is detachably connected with a fixed seat (13), and a slide rail (14) is arranged on the fixed seat (13);
A pulley (18) matched with the sliding rail (14) is arranged on the bottom surface of the operating platform (4), and a sliding motor (20) is arranged on the pulley (18);
A first guardrail (9) is arranged on one side of the operating platform (4), a control switch (10) is arranged on the first guardrail (9), and the control switch (10) is electrically connected with the sliding motor (20); a second guardrail (17) is arranged on the other side of the operating platform (4), an escalator (19) is arranged on the second guardrail (17), and a barrier (12) is arranged between the first guardrail (9) and the second guardrail (17);
The bottom surface of the base (1) is provided with a universal wheel (8) with a self-locking structure.
2. Lifting platform for aircraft maintenance according to claim 1, characterised in that the base (1) is provided with a storage slot (5) in which the hydraulically telescopic arm (3) can be stored.
3. Lifting platform for aircraft maintenance according to claim 1, characterized in that the sliding rails (14) on the fixed seat (13) are provided with stop blocks (15) for limiting the sliding of the pulleys (18).
4. an elevating platform for aircraft maintenance according to claim 1, characterised in that the base (1) is also provided with legs (6) on its underside, which legs (6) are located outside the universal wheels (8).
5. Landing platform for aircraft maintenance according to claim 4, characterized in that the lower end of the leg (6) is provided with a cushion (7).
6. An elevating platform for aircraft maintenance as claimed in claim 4, characterised in that said legs (6) are telescopic legs.
7. An aircraft maintenance lifting platform according to claim 1, characterized in that the operating platform (4) is provided with an anti-slip layer, which is a plurality of strip-shaped protrusions or a rubber layer.
8. An elevator platform for aircraft maintenance according to claim 1, characterized in that a maintenance kit is also arranged in the operation platform (4).
9. An aircraft maintenance lifting platform according to claim 1, characterized in that a distance measuring sensor (16) is arranged on the base (1).
10. Lifting platform for aircraft maintenance according to claim 1, characterized in that a battery (2) is arranged on the base (1), the battery (2) being electrically connected to the sliding motor (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920440162.5U CN209739384U (en) | 2019-04-02 | 2019-04-02 | Lifting platform for aircraft maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920440162.5U CN209739384U (en) | 2019-04-02 | 2019-04-02 | Lifting platform for aircraft maintenance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209739384U true CN209739384U (en) | 2019-12-06 |
Family
ID=68720077
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920440162.5U Active CN209739384U (en) | 2019-04-02 | 2019-04-02 | Lifting platform for aircraft maintenance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209739384U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113954989A (en) * | 2021-11-17 | 2022-01-21 | 春秋航空技术发展江苏有限公司 | Civil aircraft repairs and uses manned operating equipment |
| CN114261531A (en) * | 2021-12-21 | 2022-04-01 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
-
2019
- 2019-04-02 CN CN201920440162.5U patent/CN209739384U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113954989A (en) * | 2021-11-17 | 2022-01-21 | 春秋航空技术发展江苏有限公司 | Civil aircraft repairs and uses manned operating equipment |
| CN113954989B (en) * | 2021-11-17 | 2024-01-05 | 春秋航空技术发展江苏有限公司 | Manned operation equipment for repairing civil aircraft |
| CN114261531A (en) * | 2021-12-21 | 2022-04-01 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
| CN114261531B (en) * | 2021-12-21 | 2023-04-11 | 电子科技大学 | Intelligent flexible clamping equipment for wing |
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