Blade storage vehicle device
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.