CN114054457A - Blade storage vehicle device - Google Patents
Blade storage vehicle device Download PDFInfo
- Publication number
- CN114054457A CN114054457A CN202210034203.7A CN202210034203A CN114054457A CN 114054457 A CN114054457 A CN 114054457A CN 202210034203 A CN202210034203 A CN 202210034203A CN 114054457 A CN114054457 A CN 114054457A
- Authority
- CN
- China
- Prior art keywords
- blade
- storage
- storage vehicle
- arrangement according
- aircraft engine
- 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.)
- Pending
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B13/00—Accessories or details of general applicability for machines or apparatus for cleaning
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
- B25H3/00—Storage means or arrangements for workshops facilitating access to, or handling of, work tools or instruments
- B25H3/02—Boxes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
- B25H5/00—Tool, instrument or work supports or storage means used in association with vehicles; Workers' supports, e.g. mechanics' creepers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Cleaning In General (AREA)
- Automatic Assembly (AREA)
Abstract
The invention discloses a blade storage vehicle device, which comprises a storage vehicle, wherein the storage vehicle is provided with a blade loading and unloading station and a blade storage device, the blade loading and unloading station is arranged on one side of the blade storage device, the other side of the blade storage device is provided with a shim clamping mechanism, and one side of the bottom of the storage vehicle is fixedly provided with a positioning device; blade storage device includes the flange axle, the flange axle is installed in the upper end top central authorities of storage car rotation, the bottom mounting of flange axle is equipped with the ratchet, the fixed rotary disk that is equipped with in top of flange axle, the fixed fore-set that is equipped with vertical setting in top of rotary disk, the fore-set has a plurality of and circumference array to distribute in the top outer fringe side of rotary disk, blade loading and unloading station includes the bottom plate, the fixed blade that is equipped with in bottom plate top adds holds the mechanism, the blade adds and holds the mechanism and go up the centre gripping and be fixed with aircraft engine blade, the fixed electro-magnet connecting block that is equipped with in bottom of bottom plate, set up on the electro-magnet connecting block with fore-set assorted through-hole.
Description
Technical Field
The invention relates to the technical field of aviation equipment, in particular to a blade storage vehicle device.
Background
When the existing cleaning device for the blades of the aircraft engine cleans the blades, the blades need to be assembled on the cleaning device one by one for automatic cleaning before the cleaning device cleans the blades, and the mode of modular separation of the cleaning device and equipment for placing the blades is not adopted, so that the cleaning efficiency of automatic cleaning is low, the pre-assembly of a plurality of stations cannot be realized, and the cleaning operation is carried out again, thereby reducing the working efficiency of cleaning.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention provides a blade storage vehicle device, which realizes the automatic cleaning of each aircraft engine blade by utilizing the rotation of the aircraft engine blade and realizes the cleaning of a group of aircraft engine blades at one time.
In order to solve the technical problems, the invention provides the following technical scheme: a blade storage vehicle device comprises a storage vehicle, wherein a blade loading and unloading station and a blade storage device are arranged on the storage vehicle, the blade loading and unloading station is arranged on one side of the blade storage device, a shim holding mechanism is arranged on the other side of the blade storage device, and a positioning device is fixedly arranged on one side of the bottom of the storage vehicle;
according to a preferable technical scheme, the blade storage device comprises a flange shaft, the flange shaft is rotatably mounted in the center of the top of the upper end of the storage vehicle, a ratchet wheel is fixedly arranged at the bottom end of the flange shaft, a rotating disc is fixedly arranged at the top end of the flange shaft, a plurality of top pillars which are longitudinally arranged are fixedly arranged at the top of the rotating disc, the top pillars are circumferentially distributed on the outer edge side of the top of the rotating disc in an array mode, the blade loading and unloading station comprises a bottom plate, a blade clamping mechanism is fixedly arranged at the top of the bottom plate, an aircraft engine blade is clamped and fixed on the blade clamping mechanism, an electromagnet connecting block is fixedly arranged at the bottom of the bottom plate, and a through hole matched with the top pillars is formed in the electromagnet connecting block.
As a preferable technical scheme of the invention, a driving mechanism for driving the ratchet wheel to rotate is arranged in the storage vehicle, and the flange shaft and the ratchet wheel complete the pushing rotation of the rotating disc.
According to a preferable technical scheme of the invention, each aircraft engine blade is fixed on a top post at the top of a rotating disc through a through hole in an electromagnet connecting block, and each aircraft engine blade is arranged on the top post in the same rotating direction.
In a preferred embodiment of the present invention, the shim holding mechanism is used for storing a shim workpiece to be cleaned, and a plurality of shim blocks are placed on the empty plate tray at the rear of the storage vehicle.
As a preferable technical solution of the present invention, the storage cart is provided with a parts box at a rear portion thereof.
As a preferable technical solution of the present invention, a storage cart cover fixed to the storage cart is provided outside the storage cart.
As a preferred technical scheme of the invention, the positioning device comprises a positioning guide rail and an adjusting plate arranged at the bottom of the storage vehicle, and the storage vehicle can be pushed onto the positioning guide rail to be butted with cleaning and lubricating equipment to wait for automatic cleaning, detection and lubricating operations.
As a preferable technical scheme of the invention, a plurality of heavy casters which are uniformly distributed are arranged at the bottom of the storage vehicle, and one side of the storage vehicle is provided with a handrail.
As a preferred technical scheme of the invention, the top column has twenty-four and can be used for placing a group of aircraft engine blades.
Compared with the prior art, the invention can achieve the following beneficial effects:
by designing the blade storage device, driving the rotating disk to rotate in a single direction by arranging the flange shaft and the ratchet wheel, arranging the blade loading and unloading station, a blade clamping mechanism is arranged on the blade loading and unloading station, the blade of the aircraft engine is clamped and fixed on the blade clamping mechanism, meanwhile, the blade clamping mechanism is connected and fixed on the rotating disk, twenty-four aircraft engine blades which are grouped together are arranged on the rotating disk, the storage vehicle is positioned and fixed on the blade cleaning and spraying equipment through the positioning of the positioning device, the automatic cleaning of each aircraft engine blade is realized by utilizing the rotation of the aircraft engine blades, the cleaning of a group of aircraft engine blades is realized at one time, simultaneously, a shim holding mechanism is arranged and a shim is placed, after the aircraft engine blade is cleaned, the filler block can be fixed on the rotating disk in the same way for cleaning.
The cleaning device and the blade storage device adopt a modularized separation design, and when automatic cleaning is realized, another group of blades can be pre-assembled simultaneously, so that the cleaning work efficiency is increased.
Drawings
Fig. 1 is a schematic structural view of a blade storage cart device.
Wherein: 1. a base plate; 2. an electromagnet connecting block; 3. an aircraft engine blade; 4. a blade holding mechanism; 5. a shield; 6. a top pillar; 7. rotating the disc; 8. a shim holding mechanism; 9. a shim block; 10. a handrail; 11. a parts box; 12. positioning the guide rail; 13. an adjusting plate; 14. a ratchet wheel; 15. a flange plate; 16. heavy duty casters.
Detailed Description
The present invention will be further described with reference to specific embodiments for the purpose of facilitating an understanding of technical means, characteristics of creation, objectives and functions realized by the present invention, but the following embodiments are only preferred embodiments of the present invention, and are not intended to be exhaustive. Based on the embodiments in the implementation, other embodiments obtained by those skilled in the art without any creative efforts belong to the protection scope of the present invention. The experimental methods in the following examples are conventional methods unless otherwise specified, and materials, reagents and the like used in the following examples are commercially available unless otherwise specified.
Example (b):
as shown in fig. 1, the invention provides a blade storage cart device, which comprises a storage cart, wherein the storage cart is provided with a blade loading and unloading station and a blade storage device, the blade storage device comprises a flange shaft 15, the center of the top of the upper end of the storage cart is rotatably provided with the flange shaft 15, the bottom end of the flange shaft 15 is fixedly provided with a ratchet 14, the other end of the flange shaft 15 is fixedly provided with a rotating disk 7, the storage cart is internally provided with a driving mechanism for driving the ratchet 14 to rotate, the flange shaft 15 and the ratchet 14 complete the pushing and rotating of the rotating disk 7, the ratchet 14 is arranged to avoid the reverse rotation of the rotating disk 7, the top of the rotating disk 7 is fixedly provided with a longitudinally arranged top post 6, twenty-four top posts 6 are arranged, and the top posts are circumferentially arrayed on the outer edge side of the top of the rotating disk 7.
The blade loading and unloading station is arranged at one side of the blade storage device and comprises a bottom plate 1, a blade clamping mechanism 4 is fixedly arranged at the top of the bottom plate 1, an aircraft engine blade 3 is clamped and fixed on the blade clamping mechanism 4, an operator fixes the blade clamping mechanism 4 through the bottom plate 1 and then installs the aircraft engine blade 3 on the blade clamping mechanism 4 to complete loading and unloading operation, an electromagnet connecting block 2 is fixedly arranged at the bottom of the bottom plate 1, a through hole matched with a top column 6 is formed in the electromagnet connecting block 2, each aircraft engine blade 3 is fixed on the top column 6 at the top of a rotating disk 7 through the through hole in the electromagnet connecting block 2, each aircraft engine blade 3 is arranged on the top column 6 in the same rotation direction, the electromagnet connecting block 2 is arranged to enable the aircraft engine blade 3 to be firmly adsorbed on the rotating disk 7, and the aircraft engine blade 3 and the blade clamping mechanism 4 are assembled at the loading and unloading station, placed on the top post 6 of the rotating disc 7.
In the embodiment, the other side of the blade storage device is provided with a shim holding mechanism 8, the shim holding mechanism 8 is used for storing shim workpieces to be cleaned, and a plurality of shim blocks 9 are placed on a blank plate disc at the tail part of the storage vehicle, so that when the aircraft engine blade 3 is cleaned, the shim blocks 9 of the engine can be clamped and cleaned.
In this embodiment, the storage vehicle tail is equipped with parts box 11, through setting up parts box 11, and the operating personnel of being convenient for deposits equipment.
In this embodiment, the outer side of the storage cart is provided with a storage cart shield 5 fixed on the storage cart, and the storage cart shield 5 constitutes a display part of the storage cart shell, and simultaneously realizes protection of the interior of the storage cart.
In this embodiment, the fixed positioner that is equipped with in bottom one side of storage car, positioner include location guide rail 12 and establish the regulating plate 13 in the storage car bottom, and the storage car propelling movement can accomplish the butt joint with the lubricated equipment of washing on locating guide rail 12, waits for automatic washing, detection and lubricated operation.
In this embodiment, the bottom of storage vehicle is equipped with a plurality of evenly distributed's heavy truckle 16, and one side of storage vehicle is equipped with handrail 10, through setting up handrail 10 and heavy truckle 16, makes things convenient for operating personnel to transport and remove this blade storage vehicle device.
The storage vehicle is characterized in that a blade storage device is designed, a ratchet wheel 14 arranged at the bottom of a flange shaft 15 and the bottom of the flange shaft 15 drives an upper rotating disc 7 of the storage vehicle to rotate in a single direction, a blade loading and unloading station is arranged, a blade clamping mechanism 4 is arranged on the blade loading and unloading station, an aircraft engine blade 3 is clamped and fixed on the blade clamping mechanism 4, the blade clamping mechanism 4 is connected and fixed on the rotating disc 7 through an electromagnet connecting block 2 at the bottom of a bottom plate 1, a group of twenty-four aircraft engine blades 3 are arranged on the rotating disc 7, when the aircraft engine blades 3 are cleaned, the storage vehicle can be positioned and fixed on blade cleaning and spraying equipment through the positioning of a positioning device, the automatic cleaning of each aircraft engine blade 3 is realized by utilizing the rotation of the aircraft engine blades 3, and simultaneously a shim clamping mechanism 8 and a shim 9 are arranged, after the aircraft engine blade 3 has been cleaned, the shim 9 can be cleaned in the same way by being fastened to the rotary disk 7.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (10)
1. The utility model provides a blade storage vehicle device, includes the storage vehicle, its characterized in that: the blade loading and unloading device is characterized in that a blade loading and unloading station and a blade storage device are arranged on the storage vehicle, the blade loading and unloading station is arranged on one side of the blade storage device, a shim clamping mechanism (8) is arranged on the other side of the blade storage device, and a positioning device is fixedly arranged on one side of the bottom of the storage vehicle.
2. A blade storing cart arrangement according to claim 1, wherein: the blade storage device comprises a flange shaft (15), the center of the top of the upper end of the storage vehicle is rotatably provided with the flange shaft (15), the bottom end of the flange shaft (15) is fixedly provided with a ratchet wheel (14), the top end of the flange shaft (15) is fixedly provided with a rotating disc (7), the top of the rotating disc (7) is fixedly provided with a plurality of longitudinally arranged support pillars (6), the support pillars (6) are distributed on the outer edge side of the top of the rotating disc (7) in a circumferential array, the blade loading and unloading station comprises a bottom plate (1), a blade loading and holding mechanism (4) is fixedly arranged at the top of the bottom plate (1), the blade holding mechanism (4) is fixedly clamped with an aircraft engine blade (3), the bottom of bottom plate (1) is fixed and is equipped with electro-magnet connecting block (2), set up on electro-magnet connecting block (2) with fore-set (6) assorted through-hole.
3. A blade storing cart arrangement according to claim 2, wherein: the storage trolley is internally provided with a driving mechanism for driving the ratchet wheel (14) to rotate, and the flange shaft (15) and the ratchet wheel (14) complete the pushing rotation of the rotating disk (7).
4. A blade storing cart arrangement according to claim 3, wherein: each aircraft engine blade (3) is fixed on a top column (6) at the top of the rotating disc (7) through a through hole in the electromagnet connecting block (2), and each aircraft engine blade (3) is arranged on the top column (6) in the same rotating direction.
5. A blade storing cart arrangement according to claim 1, wherein: the shim holding mechanism (8) is used for storing a shim workpiece to be cleaned, and a plurality of shim blocks (9) are placed on the empty plate disc at the tail part of the storage vehicle.
6. A blade storing cart arrangement according to claim 1, wherein: the tail part of the storage vehicle is provided with a part box (11).
7. A blade storing cart arrangement according to claim 1, wherein: and a storage vehicle shield (5) fixed on the storage vehicle is arranged on the outer side of the storage vehicle.
8. A blade storing cart arrangement according to claim 1, wherein: positioner includes location guide rail (12) and establishes regulating plate (13) in storage car bottom, the storage car propelling movement can accomplish the butt joint with washing lubricating apparatus on location guide rail (12), waits for automatic washing, detection and lubricated operation.
9. A blade storing cart arrangement according to claim 1, wherein: the bottom of the storage vehicle is provided with a plurality of heavy casters (16) which are uniformly distributed, and one side of the storage vehicle is provided with a handrail (10).
10. A blade storing cart arrangement according to claim 2, wherein: the top column (6) is twenty-four and can be used for placing a group of aircraft engine blades (3).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210034203.7A CN114054457A (en) | 2022-01-13 | 2022-01-13 | Blade storage vehicle device |
| PCT/CN2022/086867 WO2023134044A1 (en) | 2022-01-13 | 2022-04-14 | Blade storage vehicle device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210034203.7A CN114054457A (en) | 2022-01-13 | 2022-01-13 | Blade storage vehicle device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114054457A true CN114054457A (en) | 2022-02-18 |
Family
ID=80230817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210034203.7A Pending CN114054457A (en) | 2022-01-13 | 2022-01-13 | Blade storage vehicle device |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN114054457A (en) |
| WO (1) | WO2023134044A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023134044A1 (en) * | 2022-01-13 | 2023-07-20 | 中国民航大学 | Blade storage vehicle device |
| WO2023137887A1 (en) * | 2022-01-20 | 2023-07-27 | 中国民航大学 | Aircraft engine fan blade cleaning and lubricating system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110038721A1 (en) * | 2009-08-17 | 2011-02-17 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Fan with dust-resistant coating |
| CN106628877A (en) * | 2017-01-22 | 2017-05-10 | 广州飞机维修工程有限公司 | Transportation maintenance platform of fan blade of large aircraft engine |
| CN209140852U (en) * | 2018-09-29 | 2019-07-23 | 国电联合动力技术(连云港)有限公司 | A kind of universal tooling of fan blade storage transhipment |
| CN111168636A (en) * | 2020-03-04 | 2020-05-19 | 福州鹰高电子有限公司 | Tool access device and method for quartz clock assembly |
| DE102019130536B3 (en) * | 2019-11-12 | 2020-10-01 | Christian Stephan Berner | Cleaning device for rotor blades |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206132336U (en) * | 2016-10-27 | 2017-04-26 | 中国民航大学 | Non -destructive inspection detection device of aircraft engine blade |
| CN112474112A (en) * | 2020-11-17 | 2021-03-12 | 武汉惟景三维科技有限公司 | Automatic measurement and detection system for size precision of blade |
| CN112547697A (en) * | 2020-12-03 | 2021-03-26 | 江苏大学 | Laser cleaning device and method suitable for automatic streamlined airplane blade |
| CN114042695B (en) * | 2022-01-13 | 2022-04-29 | 中国民航大学 | Cleaning and lubricating equipment for fan blades of aircraft engine |
| CN114054457A (en) * | 2022-01-13 | 2022-02-18 | 中国民航大学 | Blade storage vehicle device |
-
2022
- 2022-01-13 CN CN202210034203.7A patent/CN114054457A/en active Pending
- 2022-04-14 WO PCT/CN2022/086867 patent/WO2023134044A1/en unknown
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110038721A1 (en) * | 2009-08-17 | 2011-02-17 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Fan with dust-resistant coating |
| CN106628877A (en) * | 2017-01-22 | 2017-05-10 | 广州飞机维修工程有限公司 | Transportation maintenance platform of fan blade of large aircraft engine |
| CN209140852U (en) * | 2018-09-29 | 2019-07-23 | 国电联合动力技术(连云港)有限公司 | A kind of universal tooling of fan blade storage transhipment |
| DE102019130536B3 (en) * | 2019-11-12 | 2020-10-01 | Christian Stephan Berner | Cleaning device for rotor blades |
| CN111168636A (en) * | 2020-03-04 | 2020-05-19 | 福州鹰高电子有限公司 | Tool access device and method for quartz clock assembly |
Non-Patent Citations (1)
| Title |
|---|
| 朱通: "《飞机发动机风扇叶片压力面清洗参数优化研究》", 《中国优秀硕士学位论文全文数据库（电子期刊）》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023134044A1 (en) * | 2022-01-13 | 2023-07-20 | 中国民航大学 | Blade storage vehicle device |
| WO2023137887A1 (en) * | 2022-01-20 | 2023-07-27 | 中国民航大学 | Aircraft engine fan blade cleaning and lubricating system |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2023134044A1 (en) | 2023-07-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN114054457A (en) | Blade storage vehicle device | |
| CN111168384B (en) | Automatic production process of tire pressure sensor | |
| CN108528566B (en) | Chassis collinear assembly production line for different vehicle bodies and use method thereof | |
| CN110653529A (en) | Rim and spoke combined welding equipment | |
| WO2023134043A1 (en) | Cleaning and lubrication apparatus for fan blades of aircraft engine | |
| CN211208590U (en) | Automobile new energy battery part assembling equipment | |
| CN111376033A (en) | Sealing washer equipment | |
| CN205906625U (en) | A conveying mechanism for multi -vehicle type switches | |
| CN212761800U (en) | Concrete mixer truck tank body head and track welding auxiliary device | |
| CN110562688B (en) | Quick switching system of positioning fixture | |
| CN210189373U (en) | Full-automatic grinding machine | |
| CN211732949U (en) | Rotating shaft transmission mechanism of hub assembling device of electric vehicle | |
| CN210414089U (en) | Automatic polishing device for automobile flange shaft | |
| CN114082710B (en) | Cleaning and lubricating system for fan blades of aircraft engine | |
| CN115365925A (en) | Metal part precision machining equipment and method | |
| CN212095186U (en) | Sealing washer equipment | |
| CN211249300U (en) | Pneumatic automatic feed bin | |
| CN212705291U (en) | Automatic disassembling device for railway scrapped wagon carriage | |
| CN113369889A (en) | Ignition coil automatic assembly equipment of new forms of energy car | |
| CN218289280U (en) | Motorcycle cylinder body part is transfer device in batches | |
| CN110757161A (en) | Equipment for automatically assembling planet carrier assembly of washing machine | |
| CN220299621U (en) | Automatic CCD detection device | |
| CN218745748U (en) | Car transmission shaft processing welded subassembly | |
| CN111266661B (en) | Cutting machine tool of steel drum cutting and dumping assembly line | |
| CN216883094U (en) | Burr scraping workstation |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20220218 |
|
| RJ01 | Rejection of invention patent application after publication |