CN112320016A - Anticorrosive type packing box of aeroengine - Google Patents
Anticorrosive type packing box of aeroengine Download PDFInfo
- Publication number
- CN112320016A CN112320016A CN202011398353.3A CN202011398353A CN112320016A CN 112320016 A CN112320016 A CN 112320016A CN 202011398353 A CN202011398353 A CN 202011398353A CN 112320016 A CN112320016 A CN 112320016A
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- Prior art keywords
- gear
- fixedly connected
- frame
- aircraft engine
- bottom plate
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/02—Internal fittings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/02—Internal fittings
- B65D25/10—Devices to locate articles in containers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/20—External fittings
- B65D25/24—External fittings for spacing bases of containers from supporting surfaces, e.g. legs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D53/00—Sealing or packing elements; Sealings formed by liquid or plastics material
- B65D53/04—Discs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/02—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
- B65D81/05—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/18—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents providing specific environment for contents, e.g. temperature above or below ambient
- B65D81/20—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents providing specific environment for contents, e.g. temperature above or below ambient under vacuum or superatmospheric pressure, or in a special atmosphere, e.g. of inert gas
- B65D81/2069—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents providing specific environment for contents, e.g. temperature above or below ambient under vacuum or superatmospheric pressure, or in a special atmosphere, e.g. of inert gas in a special atmosphere
- B65D81/2076—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents providing specific environment for contents, e.g. temperature above or below ambient under vacuum or superatmospheric pressure, or in a special atmosphere, e.g. of inert gas in a special atmosphere in an at least partially rigid container
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D85/00—Containers, packaging elements or packages, specially adapted for particular articles or materials
- B65D85/68—Containers, packaging elements or packages, specially adapted for particular articles or materials for machines, engines or vehicles in assembled or dismantled form
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D2585/00—Containers, packaging elements or packages specially adapted for particular articles or materials
- B65D2585/68—Containers, packaging elements or packages specially adapted for particular articles or materials for machines, engines, or vehicles in assembled or dismantled form
- B65D2585/6802—Containers, packaging elements or packages specially adapted for particular articles or materials for machines, engines, or vehicles in assembled or dismantled form specific machines, engines or vehicles
- B65D2585/6875—Containers, packaging elements or packages specially adapted for particular articles or materials for machines, engines, or vehicles in assembled or dismantled form specific machines, engines or vehicles engines, motors, machines and vehicle parts
- B65D2585/6877—Containers, packaging elements or packages specially adapted for particular articles or materials for machines, engines, or vehicles in assembled or dismantled form specific machines, engines or vehicles engines, motors, machines and vehicle parts engines or motors
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Packaging Of Machine Parts And Wound Products (AREA)
Abstract
The invention discloses an aircraft engine anticorrosion packaging box in the field of engine protection, which comprises a device bottom plate, wherein the upper end of the device bottom plate is provided with a first chute and is fixedly connected with a device frame, the left end and the right end of the device frame are symmetrically and fixedly connected with a fixed frame, the middle position of the fixed frame is rotationally connected with a first bevel gear, the first bevel gear is fixedly connected with a rotary table, the left end and the right end of the first bevel gear are symmetrically meshed with a second bevel gear, the second bevel gear is fixedly connected with a worm and is rotationally connected with the fixed frame, the worm is meshed with the worm gear, the worm gear is fixedly connected; the third gears are symmetrically distributed on two sides of the first gear and are meshed with racks, the racks are fixedly connected with the device door, and the device door is connected with the device bottom plate and the device frame in a sliding mode; the device easy operation, labour saving and time saving has good protecting effect and anticorrosion effect simultaneously, can effectual promotion aeroengine's service quality.
Description
Technical Field
The invention relates to the field of engine protection, in particular to an anticorrosive packaging box for an aircraft engine.
Background
The aircraft engine is a highly complex and precise thermal machine, is used as the heart of an aircraft, is not only the power of the aircraft flight, but also an important driving force for promoting the development of aviation industry, and each important change in human aviation history is inseparable from the technical progress of the aircraft engine.
The traditional aircraft engine is generally wrapped on the engine by a polyethylene film (or other composite materials) when being stored, and the air in the film is packaged by a method of drawing out the air as much as possible.
Therefore, the invention provides an anti-corrosion type packing box for an aircraft engine, which aims to solve the problems in the background technology.
Disclosure of Invention
The invention aims to provide an anti-corrosion type packing box for an aircraft engine, which aims to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: an anti-corrosion type packing box for an aircraft engine comprises a device bottom plate, wherein a first sliding groove is formed in the upper end of the device bottom plate and is fixedly connected with a device frame, the left end and the right end of the device frame are symmetrically and fixedly connected with a fixing frame, the middle position of the fixing frame is rotationally connected with a first bevel gear, the first bevel gear is fixedly connected with a rotating disc, the left end and the right end of the first bevel gear are symmetrically meshed with a second bevel gear, the second bevel gear is fixedly connected with a worm and is rotationally connected with the fixing frame, the worm is meshed with a worm gear, the worm gear is fixedly connected with a threaded rod, and; the threaded rod is in threaded fit with a device top cover, the bottom end of the device top cover is uniformly and rotatably connected with a connecting rod, the other end of the connecting rod is rotatably connected with a fixed plate, and the fixed plate is in sliding connection with a device bottom plate; the device comprises a device base plate, a first gear, a second gear, a third gear, a rack, a device door, a device base plate and a device frame, wherein the first gear is connected with the device base plate in a rotating mode, the upper end of the first gear is fixedly connected with a first synchronizing wheel, the first synchronizing wheel drives the second synchronizing wheel through a synchronous belt, the first gear is meshed with the second gear, the second gear and the second synchronizing wheel are fixedly connected with the third gear, the third gear is symmetrically distributed on two sides of the first gear and is meshed with the rack, the rack is fixedly connected with the device door, and the device.
As a further scheme of the invention: a plurality of universal wheels are uniformly arranged at the bottom end of the bottom plate of the device, and the universal wheels are all self-locking universal wheels; the universal wheels can play a role in moving the device conveniently, and can play a role in fixing the device.
As a still further scheme of the invention: the connecting rod is a telescopic connecting rod, a spring is arranged in the connecting rod, and the spring is a spring with a large stiffness coefficient; under the action of the spring and the telescopic connecting rod, the fixing plate can fix various aircraft engines with different sizes.
As a still further scheme of the invention: the diameters of the first gear and the second gear are equal, the diameters of the first synchronous wheel and the second synchronous wheel are equal, and the diameter of the first gear is smaller than that of the third gear; the diameters of the first gear and the second gear are equal, and the diameters of the first synchronous wheel and the second synchronous wheel are equal, so that the rotating speeds of the third gears at the two ends are the same; through first gear diameter and third gear diameter the same, can make first gear laborsaving more drive the rotation that the third gear is slow.
As a still further scheme of the invention: the bottom end of the device bottom plate is provided with an inflation inlet, and the surface of the device top cover is provided with an air outlet; nitrogen can be flushed into the device through the inflation inlet at the bottom end; then the air in the device can be discharged through the air outlet at the upper end, and the nitrogen is heavier than the air, so that the air in the device can be more fully discharged by being filled into the device from the bottom end of the device, and the anti-corrosion effect of the device is improved.
As a still further scheme of the invention: the bottom end of the fixed plate is provided with a pulley, and the pulley is in rolling fit with the first sliding chute; a second sliding groove is formed in the upper portion of the device frame, and the fixing plate is connected with the second sliding groove in a sliding mode; through the stability of fixed plate and the further promotion fixed plate of second spout sliding fit, simultaneously through the frictional force that reduces the fixed plate that the pulley can be further.
As a still further scheme of the invention: sealing gaskets are arranged at the inner side position of the device door and the lower end position of the device top cover; the sealing gasket can be used for sealing the inside of the device when the device top cover and the device door are closed.
As a still further scheme of the invention: the end, close to the inner side, of the fixing plate is made of a soft foam material; the fixing plate made of the foam material can further protect the aircraft engine while improving the friction force.
As a still further scheme of the invention: the length of the device frame is equal to the total length of the two device doors; the front end and the rear end of the device frame can be completely sealed just when the two device doors are closed, so that the effect of effectively protecting the aircraft engine can be achieved.
As a still further scheme of the invention: when the threaded rod rotates for multiple circles to drive the device top cover to cover the device frame, the threaded rod rotates for multiple circles to provide power so that the device doors on the left side and the right side can move to a closed state; when the device top cover is driven to move downwards to seal the upper end of the device frame by rotating the threaded rod, the threaded rod stops rotating, and when the device top cover is driven to move to the upper end of the device frame, power provided by rotation of the threaded rod can drive the device door to be closed just, so that the effect of effectively saving power and improving convenience of operation can be achieved.
Advantageous effects
Compared with the prior art, the invention has the beneficial effects that:
the invention directly places the aero-engine on the device bottom plate, then directly rotates the rotary plate, the rotary plate drives the first bevel gear to rotate, the first bevel gear drives the second bevel gears at the left and right sides to rotate the worms at the left and right sides, the worms drive the threaded rods to rotate through the worm gears, the device top cover can be driven to move downwards under the action of the threaded rods to cover the upper end of the device frame, the rotating power can be provided to drive the device doors at the left and right sides of the front and rear ends of the device frame to move towards the middle position simultaneously, when the device top cover covers the upper end of the device frame, the device doors at the left and right sides are just closed to seal the front and rear sides of the device frame, at the moment, the aero-engine is in a sealing state, then nitrogen can be injected into the device through the inflation inlet to protect the aero, waste trouble hard, the relatively poor problem of protective effect and anticorrosion effect has simultaneously reached easy operation, labour saving and time saving has good protective effect and anticorrosion effect simultaneously, the effectual effect that promotes aeroengine service quality.
Drawings
FIG. 1 is a schematic structural view of the present invention as a whole;
FIG. 2 is a schematic structural view in partial cross-section of a front view of the present invention;
FIG. 3 is an enlarged view of A in FIG. 2;
FIG. 4 is a schematic top view of the present invention;
fig. 5 is an enlarged structural diagram of B in fig. 4.
In the figure: 1-device bottom plate, 2-first sliding chute, 3-device frame, 4-fixed frame, 5-first bevel gear, 6-rotating disc, 7-second bevel gear, 8-worm, 9-worm gear, 10-threaded rod, 11-first gear, 12-device top cover, 13-connecting rod, 14-fixed plate, 15-first synchronous wheel, 16-synchronous belt, 17-second synchronous wheel, 18-second gear, 19-third gear, 20-rack, 21-device door, 22-universal wheel, 23-spring, 24-inflation inlet, 25-air outlet, 26-pulley and 27-second sliding chute.
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.
Referring to fig. 1 to 5, in the embodiment of the invention, an aircraft engine anticorrosion packaging box comprises a device bottom plate 1, wherein a first chute 2 is arranged at the upper end of the device bottom plate 1 and fixedly connected with a device frame 3, the left end and the right end of the device frame 3 are symmetrically and fixedly connected with a fixed frame 4, the middle position of the fixed frame 4 is rotatably connected with a first bevel gear 5, the first bevel gear 5 is fixedly connected with a turntable 6, the left end and the right end of the first bevel gear are symmetrically meshed with a second bevel gear 7, the second bevel gear 7 is fixedly connected with a worm 8 and rotatably connected with the fixed frame 4, the worm 8 is meshed with a worm wheel 9, the worm wheel 9 is fixedly connected with a threaded rod 10; the threaded rod 10 is in threaded fit with a device top cover 12, the bottom end of the device top cover 12 is uniformly and rotatably connected with a connecting rod 13, the other end of the connecting rod 13 is rotatably connected with a fixed plate 14, and the fixed plate 14 is in sliding connection with the device bottom plate 1; the first gear 11 is rotatably connected with the device bottom plate 1, the upper end of the first gear is fixedly connected with a first synchronous wheel 15, the first synchronous wheel 15 drives a second synchronous wheel 17 through a synchronous belt 16, the first gear 11 is meshed with a second gear 18, the second gear 18 and the second synchronous wheel 17 are fixedly connected with a third gear 19, the third gears 19 are symmetrically distributed on two sides of the first gear 11 and are meshed with a rack 20, the rack 20 is fixedly connected with a device door 21, and the device door 21 is slidably connected with the device bottom plate 1 and the device frame 3.
Wherein, a plurality of universal wheels 22 are uniformly arranged at the bottom end of the device bottom plate 1, and the universal wheels 22 are all self-locking universal wheels 22; the universal wheels 22 can be used for facilitating the movement of the device and fixing the device; the connecting rod 13 is a telescopic connecting rod 13, a spring 23 is arranged in the connecting rod 13, and the spring 23 is a spring 23 with a larger stiffness coefficient; the fixing plate 14 can fix various aircraft engines with different sizes under the action of the spring 23 and the telescopic connecting rod 13; the first gear 11 and the second gear 18 have the same diameter, the first synchronous wheel 15 and the second synchronous wheel 17 have the same diameter, and the diameter of the first gear 11 is smaller than that of the third gear 19; the diameters of the first gear 11 and the second gear 18 are equal, and the diameters of the first synchronous wheel 15 and the second synchronous wheel 17 are equal, so that the rotating speeds of the third gears 19 at the two ends are the same; the diameter of the first gear 11 is the same as that of the third gear 19, so that the first gear 11 can drive the third gear 19 to rotate slowly in a labor-saving manner.
The bottom end of the device bottom plate 1 is provided with an inflation inlet 24, and the surface of the device top cover 12 is provided with an air outlet 25; nitrogen can be flushed into the device through the bottom inflation port 24; then, air in the device can be discharged through the air outlet 25 at the upper end, and the nitrogen is heavier than the air, so that the air in the device can be more fully discharged after being filled into the device from the bottom end of the device, and the anti-corrosion effect of the device is improved; the bottom end of the fixing plate 14 is provided with a pulley 26, and the pulley 26 is in rolling fit with the first chute 2; the upper part of the device frame 3 is provided with a second sliding chute 27, and the fixed plate 14 is connected with the second sliding chute 27 in a sliding way; the stability of the fixing plate 14 can be further improved by the sliding fit of the fixing plate 14 and the second sliding groove 27, and the friction force of the fixing plate 14 can be further reduced by the pulley 26; sealing gaskets are arranged at the inner side position of the device door 21 and the lower end position of the device top cover 12; the inside of the device can be in a sealed state when the device top cover 12 and the device door 21 are closed through the gasket; the material of the fixing plate 14 near the inner side is soft foam material; the fixing plate 14 made of the foam material can further protect the aircraft engine while improving the friction force; the length of the device frame 3 is equal to the total length of the two device doors 21; the front end and the rear end of the device frame 3 can be completely sealed just when the two device doors 21 are closed, so that the effect of effectively protecting an aircraft engine can be achieved; when the threaded rod 10 rotates for a plurality of circles to drive the device top cover 12 to cover the device frame 3, the device doors 21 on the left side and the right side can be moved to a closed state by the power provided by the threaded rod 10 rotating for a plurality of circles; when the threaded rod 10 rotates to drive the device top cover 12 to move downwards to seal the upper end of the device frame 3, the threaded rod 10 stops rotating, and when the device top cover 12 moves to the upper end of the device frame 3, the power provided by the rotation of the threaded rod 10 can drive the device door 12 to be closed just, so that the effects of effectively saving power and improving the convenience of operation can be achieved.
The working principle of the invention is as follows:
when the device is used by a user, the device is moved to a proper position through the universal wheel 22, then the aircraft engine is placed on the device bottom plate 1, then the rotating disc 6 is rotated, the rotating disc 6 drives the first bevel gear 5 to rotate, the first bevel gear 5 drives the second bevel gears 7 at the left end and the right end to rotate in opposite directions, the second bevel gears 7 drive the worms 8 to rotate, the worms 8 drive the worm wheels 9 to rotate, the worm wheels 9 drive the threaded rods 10 to rotate, the device top cover 12 starts to move downwards under the action of the threaded rods 10, when the device top cover 12 moves downwards, the fixing plates 14 at the left side and the right side start to move towards a middle position under the action of the connecting rods 13, meanwhile, the threaded rods 10 drive the first gear 11 and the first synchronizing wheel 15 to rotate, the first gear 11 drives the second gear 18 to rotate, and simultaneously the first synchronizing wheel 15 drives the second synchronizing wheel 17 to rotate through the synchronous belt 16, the second synchronous wheel 17 and the second gear 18 respectively drive the corresponding third gear 19 to rotate in opposite directions, and under the action of the third gear 19, the rack 20 drives the device door 21 to start to move towards the middle position; when the threaded rod 10 drives the device top cover 12 to tightly cover the top end of the device frame 3 of the device, the device door 21 of the device is just closed, the device is in a sealing state at the moment, then a user flushes nitrogen into the device through the air charging opening 24 at the bottom end, then air in the device is discharged through the air outlet 25 at the upper end, and when the device is filled with the nitrogen, the air charging opening 24 and the air outlet 25 are sealed.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (10)
1. The utility model provides an aeroengine anticorrosion type packing box, includes device bottom plate (1), its characterized in that: the device is characterized in that a first sliding chute (2) is formed in the upper end of a bottom plate (1) of the device and is fixedly connected with a device frame (3), the left end and the right end of the device frame (3) are symmetrically and fixedly connected with a fixed frame (4), the middle position of the fixed frame (4) is rotationally connected with a first bevel gear (5), the first bevel gear (5) is fixedly connected with a turntable (6) and the left end and the right end of the first bevel gear are symmetrically meshed with a second bevel gear (7), the second bevel gear (7) is fixedly connected with a worm (8) and is rotationally connected with the fixed frame (4), the worm (8) is meshed with a worm wheel (9), the worm wheel (9) is fixedly connected with a threaded rod (10), and the bottom end of the threaded rod; the threaded rod (10) is in threaded fit with a device top cover (12), the bottom end of the device top cover (12) is uniformly and rotatably connected with a connecting rod (13), the other end of the connecting rod (13) is rotatably connected with a fixed plate (14), and the fixed plate (14) is in sliding connection with a device bottom plate (1); first gear (11) rotate with device bottom plate (1) and be connected and upper end fixed connection first synchronizing wheel (15), first synchronizing wheel (15) pass through hold-in range (16) transmission second synchronizing wheel (17) and first gear (11) meshing second gear (18), equal fixed connection third gear (19) of second gear (18) and second synchronizing wheel (17), third gear (19) symmetric distribution just meshes rack (20) in first gear (11) both sides, rack (20) fixed connection device door (21), device door (21) and device bottom plate (1) and the equal sliding connection of device frame (3).
2. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: a plurality of universal wheels (22) are uniformly arranged at the bottom end of the device bottom plate (1), and the universal wheels (22) are all self-locking universal wheels (22).
3. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: connecting rod (13) are scalable connecting rod (13), and connecting rod (13) inside is equipped with spring (23), spring (23) are great spring (23) of coefficient of stiffness.
4. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: the diameters of the first gear (11) and the second gear (18) are equal, the diameters of the first synchronous wheel (15) and the second synchronous wheel (17) are equal, and the diameter of the first gear (11) is smaller than that of the second gear (18).
5. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: the bottom end of the device bottom plate (1) is provided with an inflation inlet (24), and the surface of the device top cover (12) is provided with an air outlet (25).
6. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: a pulley (26) is arranged at the bottom end of the fixing plate (14), and the pulley (26) is in rolling fit with the first sliding chute (2); the upper part of the device frame (3) is provided with a second sliding chute (27), and the fixed plate (14) is connected with the second sliding chute (27) in a sliding manner.
7. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: and sealing gaskets are arranged at the inner side position of the device door (21) and the lower end position of the device top cover (12).
8. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: the material of one end of the fixing plate (14) close to the inner side is soft foam material.
9. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: the length of the device frame (3) is equal to the total length of the two device doors (21).
10. The aircraft engine anticorrosive packaging box of claim 1, characterized in that: when the threaded rod (10) rotates for a plurality of circles to drive the device top cover (12) to cover the device frame (3), the device doors (21) on the left side and the right side can be moved to a closed state by the power provided by the threaded rod (10) rotating for a plurality of circles.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011398353.3A CN112320016B (en) | 2020-12-02 | 2020-12-02 | Anticorrosive type packing box of aeroengine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011398353.3A CN112320016B (en) | 2020-12-02 | 2020-12-02 | Anticorrosive type packing box of aeroengine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112320016A true CN112320016A (en) | 2021-02-05 |
| CN112320016B CN112320016B (en) | 2022-04-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011398353.3A Active CN112320016B (en) | 2020-12-02 | 2020-12-02 | Anticorrosive type packing box of aeroengine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112320016B (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020011175A1 (en) * | 2000-07-18 | 2002-01-31 | Miner Enterprises, Inc. | Gate assembly for a railroad hopper car |
| CN106955821A (en) * | 2017-04-26 | 2017-07-18 | 深圳市新嘉拓自动化技术有限公司 | A kind of supply disk governor motion for coating machine roller |
| CN206927044U (en) * | 2017-05-02 | 2018-01-26 | 庄敏珍 | A kind of frequency converter protector |
| CN107983051A (en) * | 2017-11-29 | 2018-05-04 | 龙泉市宏盛科技咨询服务有限公司 | A kind of bamboo and wood cuts dust collection and treatment device |
| CN209874842U (en) * | 2019-03-26 | 2019-12-31 | 杭州腾睿源人防工程有限公司 | Steel construction biparting airtight door |
| CN209947177U (en) * | 2019-04-18 | 2020-01-14 | 邢台职业技术学院 | Movable teaching display device for dress designing |
| CN211392114U (en) * | 2019-12-23 | 2020-09-01 | 漳州市七洞刀网络科技有限公司 | Damping device for lamp transportation |
-
2020
- 2020-12-02 CN CN202011398353.3A patent/CN112320016B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020011175A1 (en) * | 2000-07-18 | 2002-01-31 | Miner Enterprises, Inc. | Gate assembly for a railroad hopper car |
| CN106955821A (en) * | 2017-04-26 | 2017-07-18 | 深圳市新嘉拓自动化技术有限公司 | A kind of supply disk governor motion for coating machine roller |
| CN206927044U (en) * | 2017-05-02 | 2018-01-26 | 庄敏珍 | A kind of frequency converter protector |
| CN107983051A (en) * | 2017-11-29 | 2018-05-04 | 龙泉市宏盛科技咨询服务有限公司 | A kind of bamboo and wood cuts dust collection and treatment device |
| CN209874842U (en) * | 2019-03-26 | 2019-12-31 | 杭州腾睿源人防工程有限公司 | Steel construction biparting airtight door |
| CN209947177U (en) * | 2019-04-18 | 2020-01-14 | 邢台职业技术学院 | Movable teaching display device for dress designing |
| CN211392114U (en) * | 2019-12-23 | 2020-09-01 | 漳州市七洞刀网络科技有限公司 | Damping device for lamp transportation |
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| CN112320016B (en) | 2022-04-19 |
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