CN114560104A - Modular aviation maintenance device - Google Patents
Modular aviation maintenance device Download PDFInfo
- Publication number
- CN114560104A CN114560104A CN202210192227.5A CN202210192227A CN114560104A CN 114560104 A CN114560104 A CN 114560104A CN 202210192227 A CN202210192227 A CN 202210192227A CN 114560104 A CN114560104 A CN 114560104A
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- Prior art keywords
- rotating shaft
- face
- supporting arm
- maintenance
- platform
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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.)
- Pending
Links
- 238000012423 maintenance Methods 0.000 title claims abstract description 50
- 238000000034 method Methods 0.000 claims description 10
- 230000035939 shock Effects 0.000 claims description 9
- 238000010521 absorption reaction Methods 0.000 claims description 6
- 238000013016 damping Methods 0.000 claims description 4
- 230000000712 assembly Effects 0.000 claims 2
- 238000000429 assembly Methods 0.000 claims 2
- 230000000694 effects Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The invention discloses a combined type aviation maintenance device which comprises a base, a maintenance platform, a rotating platform and a lifting assembly, wherein the rotating platform is arranged on the lower end face of the maintenance platform, the lifting assembly is arranged between the rotating platform and the base, a universal wheel assembly is arranged on the bottom end face of the base, two sides of the upper end face of the maintenance platform are respectively provided with a jacking assembly, and a part clamping assembly is also arranged on the upper end face of the maintenance platform.
Description
Technical Field
The invention relates to the technical field of aviation maintenance, in particular to a combined type aviation maintenance device.
Background
Aviation is a complex and strategic human activity, which refers to the flight activity of an aircraft in the earth atmosphere, the word of English aviation is from Latin birds or air, and the aircraft engaged in the flight activity, also called aircraft, is divided into two types, namely lighter-than-air aircraft and heavier-than-air aircraft, such as balloons and airships, and is lifted off by using air static buoyancy; the latter, like airplanes and helicopters, use aerodynamic to lift off.
The existing maintenance devices for aviation equipment in the market at present have the advantages of simple structure and convenient operation, but the maintenance efficiency is low, and improvement is necessary.
Disclosure of Invention
The invention aims to provide a combined type aviation maintenance device to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a modular aviation maintenance device, includes base, maintenance platform, rotary platform and lifting unit, rotary platform installs terminal surface under the maintenance platform, installation lifting unit between rotary platform and the base, universal wheel subassembly is installed to base bottom terminal surface, the tight subassembly in top is installed respectively to maintenance platform up end both sides, the maintenance platform up end still sets up spare part clamping assembly.
Preferably, the combined type aviation maintenance device provided by the application, wherein the lifting assembly comprises a first rotating shaft, a second rotating shaft, a third rotating shaft, a first supporting arm and a second supporting arm, the first rotating shaft and the second rotating shaft are respectively installed on the lower end face of the rotating platform, the third rotating shaft is installed on the upper end face of the base, one end of the first supporting arm is connected with the first rotating shaft, the other end of the first supporting arm is provided with a sliding block, the sliding block is in sliding connection with a sliding track arranged on the upper end face of the base, one end of the second supporting arm is connected with the second rotating shaft, the other end of the second supporting arm is connected with the third rotating shaft, the first supporting arm and the second supporting arm are arranged in a staggered mode, and a pin shaft is installed at the crossed position; the telescopic oil cylinder is characterized by further comprising a telescopic oil cylinder, the tail end of the telescopic oil cylinder is installed on the upper end face of the base, and the telescopic end of the telescopic oil cylinder is connected with the sliding block.
Preferably, the application provides a modular aviation maintenance device, wherein, the tight subassembly in top includes the tight board in top, upper sleeve and lower sleeve, lower sleeve perpendicular to maintenance platform, the upper sleeve sets up directly over the lower sleeve, the tight board in top is installed in upper sleeve top portion, go up and still install the high strength damping spring body between the sleeve under and the sleeve.
Preferably, the combined type aviation maintenance device provided by the application, wherein the part clamping assembly comprises a clamping plate and a push-pull oil cylinder, the push-pull oil cylinder is arranged between the lower sleeve and the clamping plate, and the part is clamped and fixed between the two clamping plates.
Preferably, the combined type aviation maintenance device provided by the application, wherein the universal wheel assembly comprises a shock absorption mounting frame and a universal wheel body, the shock absorption mounting frame is installed on the lower end face of the base, and the universal wheel body is installed on the shock absorption mounting frame.
Preferably, the application provides a modular aviation maintenance device, wherein, its method of use includes the following step:
A. firstly, moving the device below the aviation equipment;
B. then the lifting component is controlled to ascend, and the lifting component drives the maintenance platform to move upwards;
C. the jacking plate is tightly attached to the lower part of the aviation equipment;
D. and then the parts to be maintained are detached and placed on the maintenance platform, and are clamped by the clamping assembly for maintenance.
Compared with the prior art, the invention has the beneficial effects that: the aircraft part fixing device is novel in structural design, convenient to operate, capable of fixing and maintaining the aircraft parts quickly, high in maintenance efficiency, capable of reducing labor cost and capable of improving use convenience; the adopted lifting component has good lifting stability; the tight subassembly in top of adoption can prevent to remove to device monolithic stationary, further improves maintenance efficiency.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the lifting assembly of the present invention;
in the figure: the device comprises a base 1, a maintenance platform 2, a rotating platform 3, a jacking plate 4, an upper sleeve 5, a lower sleeve 6, a first rotating shaft 7, a second rotating shaft 8, a third rotating shaft 9, a first supporting arm 10, a second supporting arm 11, a sliding block 12, a sliding track 13, a pin shaft 14, a high-strength damping spring body 15, a clamping plate 16 and a push-pull oil cylinder 17.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be configured in a specific orientation, and operate, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; 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 meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-2, the present invention provides a technical solution: the utility model provides a modular aviation maintenance device, includes base 1, maintenance platform 2, rotary platform 3 and lifting unit, rotary platform 3 installs terminal surface under maintenance platform 2, install lifting unit between rotary platform 3 and the base 1, 1 bottom end face mounting universal wheel subassembly of base, universal wheel subassembly include shock attenuation mounting bracket 18 and universal wheel body 19, shock attenuation mounting bracket 18 is installed terminal surface under base 1, universal wheel body 19 is installed in shock attenuation mounting bracket 18. Tight subassembly in maintenance platform 2 up end both sides installation top respectively, maintenance platform 2 up end still sets up spare part clamping assembly.
According to the invention, the lifting assembly comprises a first rotating shaft 7, a second rotating shaft 8, a third rotating shaft 9, a first supporting arm 10 and a second supporting arm 11, wherein the first rotating shaft 7 and the second rotating shaft 8 are respectively arranged on the lower end surface of the rotating platform, the third rotating shaft 9 is arranged on the upper end surface of the base, one end of the first supporting arm 10 is connected with the first rotating shaft 7, the other end of the first supporting arm is provided with a sliding block 12, the sliding block 12 is in sliding connection with a sliding rail 13 arranged on the upper end surface of the base, one end of the second supporting arm 11 is connected with the second rotating shaft 8, the other end of the second supporting arm 11 is connected with the third rotating shaft 9, the first supporting arm 10 and the second supporting arm 11 are arranged in a staggered mode, and a pin shaft 14 is arranged at the crossed position; and the telescopic oil cylinder 18 is further included, the tail end of the telescopic oil cylinder 28 is installed on the upper end surface of the base, and the telescopic end of the telescopic oil cylinder 18 is connected with the sliding block 12.
According to the invention, the jacking assembly comprises a jacking plate 4, an upper sleeve 5 and a lower sleeve 6, wherein the lower sleeve 6 is perpendicular to the maintenance platform 2, the upper sleeve 5 is arranged right above the lower sleeve 6, the jacking plate 4 is arranged at the top end part of the upper sleeve 5, and a high-strength damping spring body 15 is further arranged between the upper sleeve 5 and the lower sleeve 6.
In addition, in the invention, the part clamping assembly comprises a clamping plate 16 and a push-pull oil cylinder 17, the push-pull oil cylinder 17 is arranged between the lower sleeve 6 and the clamping plate 16, and parts are clamped and fixed between the two clamping plates 16.
The working principle is as follows: the using method of the invention comprises the following steps:
A. firstly, moving the device below the aviation equipment;
B. then the lifting component is controlled to ascend, and the lifting component drives the maintenance platform to move upwards;
C. the jacking plate is tightly attached to the lower part of the aviation equipment;
D. and then the parts to be maintained are detached and placed on the maintenance platform, and are clamped by the clamping assembly for maintenance.
In conclusion, the aviation part fixing device is novel in structural design, convenient to operate, capable of fixing and maintaining aviation parts quickly, high in maintenance efficiency, capable of reducing labor cost and capable of improving use convenience; the adopted lifting component has good lifting stability; the tight subassembly in top of adoption can prevent to remove to device monolithic stationary, further improves maintenance efficiency.
It should be noted that, in this document, terms such as "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides a modular aviation maintenance device, includes base (1), maintenance platform (2), rotary platform (3) and lifting unit, its characterized in that: the rotary platform (3) is installed on the lower end face of the maintenance platform (2), a lifting assembly is installed between the rotary platform (3) and the base (1), universal wheel assemblies are installed on the bottom end face of the base (1), jacking assemblies are installed on two sides of the upper end face of the maintenance platform (2) respectively, and a part clamping assembly is further arranged on the upper end face of the maintenance platform (2).
2. A modular aerospace service unit according to claim 1, wherein: the lifting assembly comprises a first rotating shaft (7), a second rotating shaft (8), a third rotating shaft (9), a first supporting arm (10) and a second supporting arm (11), the first rotating shaft (7) and the second rotating shaft (8) are respectively installed on the lower end face of the rotating platform, the third rotating shaft (9) is installed on the upper end face of the base, one end of the first supporting arm (10) is connected with the first rotating shaft (7), the other end of the first supporting arm is provided with a sliding block (12), the sliding block (12) is in sliding connection with a sliding track (13) arranged on the upper end face of the base, one end of the second supporting arm (11) is connected with the second rotating shaft (8), the other end of the second supporting arm (11) is connected with the third rotating shaft (9), the first supporting arm (10) and the second supporting arm (11) are arranged in a staggered mode, and a pin shaft (14) is installed at the crossed position; the telescopic oil cylinder is characterized by further comprising a telescopic oil cylinder (18), the tail end of the telescopic oil cylinder (18) is installed on the upper end face of the base, and the telescopic end of the telescopic oil cylinder (18) is connected with the sliding block (12).
3. A modular aerospace service unit according to claim 1, wherein: the tight subassembly in top includes tight board in top (4), goes up sleeve (5) and lower sleeve (6), lower sleeve (6) perpendicular to maintenance platform (2), it sets up directly over lower sleeve (6) to go up sleeve (5), install in last sleeve (5) top portion in tight board in top (4), go up sleeve (5) and still install high strength damping spring body (15) down between sleeve (6).
4. A modular aerospace service unit according to claim 1, wherein: the part clamping assembly comprises clamping plates (16) and a push-pull oil cylinder (17), the push-pull oil cylinder (17) is arranged between the lower sleeve (6) and the clamping plates (16), and parts are clamped and fixed between the two clamping plates (16).
5. A modular aerospace service unit according to claim 1, wherein: the universal wheel assembly comprises a shock absorption mounting frame (18) and a universal wheel body (19), the shock absorption mounting frame (18) is installed on the lower end face of the base (1), and the universal wheel body (19) is installed on the shock absorption mounting frame (18).
6. Use method for realizing a combined aircraft maintenance device according to claim 1, characterized in that: the using method comprises the following steps:
A. firstly, moving the device below the aviation equipment;
B. then the lifting component is controlled to ascend, and the lifting component drives the maintenance platform to move upwards;
C. the jacking plate is tightly attached to the lower part of the aviation equipment;
D. and then the parts to be maintained are detached and placed on the maintenance platform, and are clamped by the clamping assembly for maintenance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210192227.5A CN114560104A (en) | 2022-02-28 | 2022-02-28 | Modular aviation maintenance device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210192227.5A CN114560104A (en) | 2022-02-28 | 2022-02-28 | Modular aviation maintenance device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114560104A true CN114560104A (en) | 2022-05-31 |
Family
ID=81716690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210192227.5A Pending CN114560104A (en) | 2022-02-28 | 2022-02-28 | Modular aviation maintenance device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114560104A (en) |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1317717A (en) * | 1971-04-16 | 1973-05-23 | Taylor Bros Ind Safety Guards | Scissor-type jacking mechanism |
| US20110037039A1 (en) * | 2009-08-12 | 2011-02-17 | Hong Fu Jin Precision Industry ( Shenzhen) Co., Ltd | Elevation mechanism |
| JP2019058932A (en) * | 2017-09-27 | 2019-04-18 | トヨタ自動車九州株式会社 | Support and welding system for vehicle frame member |
| CN109694026A (en) * | 2019-02-21 | 2019-04-30 | 南京工业职业技术学院 | Auxiliary lifting device is used in a kind of maintenance of space shuttle |
| CN111085813A (en) * | 2019-11-28 | 2020-05-01 | 湖北恒特汽车系统有限公司 | Support frame is used in commodity circulation automobile body welding |
| KR20200118608A (en) * | 2019-04-08 | 2020-10-16 | 황성일 | Automobile lift with a cylinder part embedded in the ground |
| CN212557882U (en) * | 2020-07-17 | 2021-02-19 | 唐山超迈机电自动化科技有限公司 | Household electrical appliances bear device |
| CN112497111A (en) * | 2020-12-08 | 2021-03-16 | 湖南人文科技学院 | Detachable VR anchor clamps for helmet manufacturing |
| CN214817933U (en) * | 2021-02-06 | 2021-11-23 | 科东自动化科技(嘉善)有限公司 | Adjustable kuppe mounting platform |
| CN215469240U (en) * | 2021-08-20 | 2022-01-11 | 大连威尔博合金科技有限公司 | Shaft welding device with noise reduction protection function |
| 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 |
| CN215798225U (en) * | 2021-04-30 | 2022-02-11 | 河南省瑞力特重型装备安装服务有限公司 | Crane installation and maintenance safety platform |
-
2022
- 2022-02-28 CN CN202210192227.5A patent/CN114560104A/en active Pending
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1317717A (en) * | 1971-04-16 | 1973-05-23 | Taylor Bros Ind Safety Guards | Scissor-type jacking mechanism |
| US20110037039A1 (en) * | 2009-08-12 | 2011-02-17 | Hong Fu Jin Precision Industry ( Shenzhen) Co., Ltd | Elevation mechanism |
| JP2019058932A (en) * | 2017-09-27 | 2019-04-18 | トヨタ自動車九州株式会社 | Support and welding system for vehicle frame member |
| CN109694026A (en) * | 2019-02-21 | 2019-04-30 | 南京工业职业技术学院 | Auxiliary lifting device is used in a kind of maintenance of space shuttle |
| KR20200118608A (en) * | 2019-04-08 | 2020-10-16 | 황성일 | Automobile lift with a cylinder part embedded in the ground |
| CN111085813A (en) * | 2019-11-28 | 2020-05-01 | 湖北恒特汽车系统有限公司 | Support frame is used in commodity circulation automobile body welding |
| CN212557882U (en) * | 2020-07-17 | 2021-02-19 | 唐山超迈机电自动化科技有限公司 | Household electrical appliances bear device |
| CN112497111A (en) * | 2020-12-08 | 2021-03-16 | 湖南人文科技学院 | Detachable VR anchor clamps for helmet manufacturing |
| CN214817933U (en) * | 2021-02-06 | 2021-11-23 | 科东自动化科技(嘉善)有限公司 | Adjustable kuppe mounting platform |
| CN215798225U (en) * | 2021-04-30 | 2022-02-11 | 河南省瑞力特重型装备安装服务有限公司 | Crane installation and maintenance safety platform |
| CN215469240U (en) * | 2021-08-20 | 2022-01-11 | 大连威尔博合金科技有限公司 | Shaft welding device with noise reduction protection function |
| 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 |
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