CN111994469A - Storage and transportation box for storage and transportation of aircraft engine - Google Patents
Storage and transportation box for storage and transportation of aircraft engine Download PDFInfo
- Publication number
- CN111994469A CN111994469A CN202010875492.4A CN202010875492A CN111994469A CN 111994469 A CN111994469 A CN 111994469A CN 202010875492 A CN202010875492 A CN 202010875492A CN 111994469 A CN111994469 A CN 111994469A
- Authority
- CN
- China
- Prior art keywords
- storage
- transportation
- buffer
- box body
- box
- 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.)
- Withdrawn
Links
- 238000007789 sealing Methods 0.000 claims abstract description 10
- 230000006835 compression Effects 0.000 claims abstract description 9
- 238000007906 compression Methods 0.000 claims abstract description 9
- 230000001681 protective effect Effects 0.000 claims 2
- 238000000034 method Methods 0.000 description 3
- 230000006978 adaptation Effects 0.000 description 2
- 230000005489 elastic deformation Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000007791 dehumidification Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
Images
Classifications
-
- 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
- B65D81/07—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 using resilient suspension means
-
- 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
-
- 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
- B65D81/24—Adaptations for preventing deterioration or decay of contents; Applications to the container or packaging material of food preservatives, fungicides, pesticides or animal repellants
- B65D81/26—Adaptations for preventing deterioration or decay of contents; Applications to the container or packaging material of food preservatives, fungicides, pesticides or animal repellants with provision for draining away, or absorbing, or removing by ventilation, fluids, e.g. exuded by contents; Applications of corrosion inhibitors or desiccators
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Food Science & Technology (AREA)
- Buffer Packaging (AREA)
- Packaging Of Machine Parts And Wound Products (AREA)
Abstract
The invention belongs to the field of storage and transportation boxes, and particularly relates to a storage and transportation box for storage and transportation of an aero-engine, which comprises a storage and transportation box body and a buffer box positioned in the storage and transportation box body, wherein one end of a plurality of compression springs is fixedly arranged at the bottom of the buffer box, the other end of each compression spring is fixedly arranged on the inner wall of the bottom of the storage and transportation box body, a cover plate is arranged at the top of the storage and transportation box body, a sealing seat is fixedly arranged at the bottom of the cover plate and is matched with the corresponding storage and transportation box body, two symmetrically arranged vertical rods are fixedly arranged at the bottom of the sealing seat, the two vertical rods are movably sleeved with the same fixing plate, one ends of the plurality of fixing springs are fixedly arranged at the top of the fixing plate, and the other ends. The engine protection device is reasonable in design, simple in structure, convenient to operate, convenient to fix the engine and capable of performing buffer protection on the engine, so that the engine can be prevented from being damaged.
Description
Technical Field
The invention relates to the technical field of storage and transportation boxes, in particular to a storage and transportation box for storage and transportation of 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. Over the course of centuries, aircraft engines have developed into mature products of extremely high reliability, and the aircraft engines in use include various types of turbojet/turbofan engines, turboshaft/turboprop engines, ramjets and piston engines.
At present, when an aircraft engine is stored and transported, the engine needs to be placed by means of a storage and transportation box, and when the engine is not firmly fixed in the storage and transportation process, the engine is easily collided with the storage and transportation box, so that the engine is damaged, and the problems that the engine is not convenient to fix and buffer and protect exist, so that the storage and transportation box for storing and transporting the aircraft engine is provided for solving the problems.
Disclosure of Invention
The invention aims to solve the defects that the prior art is inconvenient to fix and buffer and protect an engine, and provides a storage and transportation box for storing and transporting an aircraft engine.
In order to achieve the purpose, the invention adopts the following technical scheme:
a storage and transportation box for storage and transportation of an aircraft engine comprises a storage and transportation box body and a buffer box positioned in the storage and transportation box body, wherein one end of a plurality of compression springs is fixedly arranged at the bottom of the buffer box, the other end of each compression spring is fixedly arranged on the inner wall of the bottom of the storage and transportation box body, a cover plate is arranged at the top of the storage and transportation box body, a sealing seat is fixedly arranged at the bottom of the cover plate and is matched with the corresponding storage and transportation box body, two vertical rods which are symmetrically arranged are fixedly arranged at the bottom of the sealing seat, the two vertical rods are movably sleeved with a same fixed plate, one end of each fixing spring is fixedly arranged at the top of the fixed plate, the other end of each fixing spring is fixedly arranged on the sealing seat, connecting seats are fixedly arranged at the two sides of the storage and transportation box body, mounting rods are rotatably arranged on the connecting plates, mounting holes are formed in the tops of, a transverse plate is fixedly installed at the top of the installation rod, a first threaded hole is formed in the transverse plate, a fixing bolt is installed in the first threaded hole in a threaded mode, two symmetrically-arranged fixing grooves are formed in the top of the cover plate, and the fixing bolts are matched with the corresponding fixing grooves;
the buffer box is internally and slidably provided with two symmetrically arranged clamping plates, the inner walls of two sides of the buffer box are respectively provided with a second threaded hole, the inner threads of the second threaded holes are provided with an adjusting screw rod, one end of the adjusting screw rod is rotatably arranged on the corresponding clamping plate, the other end of the adjusting screw rod extends to the outer side of the buffer box and is fixedly provided with a rotating plate, the side surface of the buffer box is respectively and fixedly provided with one end of a first buffer spring, the other end of the first buffer spring is fixedly arranged on the inner wall of the storage and transportation box body, the inner wall of the bottom of the storage and transportation box body is provided with two symmetrically arranged first grooves, the first grooves are internally and slidably provided with a movable seat, the top of the movable seat is hinged with one end of a push rod, the other end of the push rod is hinged on the corresponding buffer box, one side of the movable seat is fixedly provided with, the second groove has been seted up on one side inner wall in first groove, and slidable mounting has the one end of push rod in the second groove, and the other end fixed mounting of push rod has the rack on removing the seat, rotates the one end of installing the pivot on the bottom inner wall in second groove, and the other end of pivot extends to this internal and fixed mounting of storage and transportation case has the blade, and fixed cover is equipped with the gear in the pivot, and the gear meshes with the rack mutually.
Preferably, set up the shifting chute that two symmetries set up on the bottom inner wall of baffle-box, and splint slidable mounting is in the shifting chute, can make splint carry out stable removal.
Preferably, the rotation groove has all been seted up to one side that two splint kept away from each other, and adjusting screw's one end is rotated and is installed in the rotation inslot that corresponds.
Preferably, a round hole is formed in the inner wall of the top of the second groove, and the rotating shaft is rotatably connected with the round hole.
Preferably, two splint are close to equal fixed mounting in one side each other and are protected the pad, and two protection pad looks adaptations.
Preferably, the top of the storage and transportation box body is fixedly provided with two symmetrically arranged positioning seats, the bottom of the cover plate is provided with two symmetrically arranged positioning grooves, and the positioning grooves are matched with the corresponding positioning seats.
Preferably, the top of connecting plate is fixed with two connecting seats, rotates on the connecting seat and has the round pin axle, and the fixed cover of installation pole is established at the round pin epaxially.
Preferably, the bottom of the vertical rod is fixedly provided with a limiting plate, and the limiting plate is matched with the corresponding fixing plate.
In the invention, when the aircraft engine is stored and transported, the engine is firstly placed in the buffer tank, the rotary plate can rotate the adjusting screw rod by rotating the rotary plate, the adjusting screw rod can rotate and move under the action of the second threaded hole, the adjusting screw rod can drive the clamping plate to move by moving, the engine can be clamped and fixed by moving the clamping plate, then the cover plate is covered, the positioning seat is clamped into the corresponding positioning groove, the cover plate can be positioned, the buffer tank can be extruded by the fixed plate, the fixed plate compresses the fixing spring, then the mounting rod is rotatably mounted, the mounting rod is rotatably clamped into the corresponding mounting hole, the position of the fixing bolt corresponds to the position of the corresponding fixing groove, the fixing bolt is rotated, and the fixing bolt can be clamped into the corresponding fixing groove under the action of the first threaded hole, the fixing bolt can downwards extrude the cover plate through the fixing groove, so that the cover plate is stably arranged on the storage and transportation box body;
in the in-process of storage fortune, when storage fortune case body takes place vibrations, the baffle-box can compress first buffer spring this moment, elastic deformation through first buffer spring can cushion the protection to the baffle-box in the horizontal direction, when the baffle-box takes place vibrations in vertical direction, make the baffle-box drive through the push rod and remove the seat and remove and compress second buffer spring, can cushion the protection on vertical direction to the baffle-box through second buffer spring, thereby can cushion the protection to the engine, the removal that removes the seat can drive the gear through push rod and rack and rotate, the gear drives the blade through the pivot and rotates, can be to this internal drying and dehumidification of storage fortune case.
The engine protection device is reasonable in design, simple in structure, convenient to operate, convenient to fix the engine and capable of performing buffer protection on the engine, so that the engine can be prevented from being damaged.
Drawings
FIG. 1 is a schematic illustration of a storage and transportation box for aircraft engine storage and transportation according to the present invention;
FIG. 2 is a schematic structural view of part A of a storage and transportation box for aircraft engine storage and transportation according to the present invention;
FIG. 3 is a schematic structural view of part B of a storage and transportation box for aircraft engine storage and transportation according to the present invention;
FIG. 4 is a schematic structural view of a portion C of a storage and transportation box for aircraft engine storage and transportation according to the present invention;
fig. 5 is a schematic structural diagram of part D of a storage and transportation box for aircraft engine storage and transportation according to the present invention.
In the figure: 1. a storage and transportation box body; 2. a buffer tank; 3. a compression spring; 4. a cover plate; 5. a sealing seat; 6. a vertical rod; 7. a fixing plate; 8. fixing the spring; 9. a connecting plate; 10. mounting a rod; 11. mounting holes; 12. a transverse plate; 13. fixing grooves; 14. a first threaded hole; 15. fixing the bolt; 16. a splint; 17. a second threaded hole; 18. adjusting the screw rod; 19. rotating the plate; 20. a first buffer spring; 21. a rotating groove; 22. a first groove; 23. a push rod; 24. a movable seat; 25. a second buffer spring; 26. a push rod; 27. a moving groove; 28. a protection pad; 29. a second groove; 30. a rack; 31. a rotating shaft; 32. a blade; 33. a gear.
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.
Referring to fig. 1-5, a storage and transportation box for storage and transportation of an aircraft engine comprises a storage and transportation box body 1 and a buffer box 2 positioned in the storage and transportation box body 1, wherein one end of a plurality of compression springs 3 is fixedly arranged at the bottom of the buffer box 2, the other end of each compression spring 3 is fixedly arranged on the inner wall of the bottom of the storage and transportation box body 1, a cover plate 4 is arranged at the top of the storage and transportation box body 1, a seal seat 5 is fixedly arranged at the bottom of the cover plate 4, the seal seat 5 is matched with the corresponding storage and transportation box body 1, two symmetrically arranged vertical rods 6 are fixedly arranged at the bottom of the seal seat 5, the two vertical rods 6 are movably sleeved with a same fixing plate 7, one end of a plurality of fixing springs 8 is fixedly arranged at the top of the fixing plate 7, the other end of each fixing spring 8 is fixedly arranged on the seal seat 5, connecting plates 9 are fixedly arranged at both sides of the storage and, the top of the cover plate 4 is provided with mounting holes 11, an inner wall of one side, far away from each other, of each mounting hole 11 is provided with an opening, the top of the mounting rod 10 is fixedly provided with a transverse plate 12, the transverse plate 12 is provided with a first threaded hole 14, a fixing bolt 15 is arranged in the first threaded hole 14 in a threaded manner, the top of the cover plate 4 is provided with two symmetrically-arranged fixing grooves 13, and the fixing bolt 15 is matched with the corresponding fixing groove 13;
two symmetrically-arranged clamping plates 16 are slidably mounted in the buffer box 2, second threaded holes 17 are formed in the inner walls of two sides of the buffer box 2, adjusting screws 18 are mounted in the second threaded holes 17 in a threaded manner, one ends of the adjusting screws 18 are rotatably mounted on the corresponding clamping plates 16, the other ends of the adjusting screws 18 extend to the outer side of the buffer box 2 and are fixedly mounted with rotating plates 19, one ends of first buffer springs 20 are fixedly mounted on the side surfaces of the buffer box 2, the other ends of the first buffer springs 20 are fixedly mounted on the inner wall of the storage and transportation box body 1, two symmetrically-arranged first grooves 22 are formed in the inner wall of the bottom of the storage and transportation box body 1, movable seats 24 are slidably mounted in the first grooves 22, one ends of push rods 26 are hinged to the tops of the movable seats 24, the other ends of the push rods 26 are hinged to the corresponding buffer boxes 2, one ends of second buffer springs 25 are fixedly mounted, second buffer spring 25's the other end fixed mounting has been seted up on the inner wall of first groove 22 on the one side inner wall of first groove 22 second groove 29, slidable mounting has the one end of push rod 23 in second groove 29, the other end fixed mounting of push rod 23 is on removing seat 24, push rod 23 one side fixed mounting has rack 30, rotate the one end of installing pivot 31 on the bottom inner wall of second groove 29, the other end of pivot 31 extends to in the case body 1 of storage and transportation and fixed mounting has blade 32, fixed cover is equipped with gear 33 on the pivot 31, and gear 33 meshes with rack 30 mutually.
In this embodiment, set up the shifting chute 27 that two symmetries set up on the bottom inner wall of baffle-box 2, and splint 16 slidable mounting is at shifting chute 27, can make splint 16 carry out stable removal.
In this embodiment, the rotating grooves 21 are formed on the sides of the two clamping plates 16 away from each other, and one end of the adjusting screw 18 is rotatably installed in the corresponding rotating groove 21.
In this embodiment, a circular hole is formed on the inner wall of the top of the second groove 29, and the rotating shaft 31 is rotatably connected with the circular hole.
In this embodiment, the two clamping plates 16 are fixedly mounted with a protection pad 28 on one side, and the two protection pads 28 are matched with each other.
In this embodiment, the top of the storage and transportation box body 1 is fixedly provided with two symmetrically arranged positioning seats, the bottom of the cover plate 4 is provided with two symmetrically arranged positioning grooves, and the positioning grooves are matched with the corresponding positioning seats.
In this embodiment, two connecting seats are fixed at the top of the connecting plate 9, a pin shaft is rotated on the connecting seats, and the mounting rod 10 is fixedly sleeved on the pin shaft.
In this embodiment, the bottom fixed mounting of montant 6 has the limiting plate, and the limiting plate and the 7 looks adaptations of fixed plate that correspond.
In the invention, when the aircraft engine is stored and transported, firstly, the engine is placed in the buffer tank 2, the rotary plate 19 can rotate the adjusting screw 18 by rotating the rotary plate 19, the adjusting screw 18 can rotate and move under the action of the second threaded hole 17, the adjusting screw 18 can drive the clamping plate 16 to move by moving, the clamping plate 16 can clamp and fix the engine by moving, then the cover plate 4 is covered, the positioning seat is clamped into the corresponding positioning groove, the cover plate 4 can be positioned, the buffer tank 2 can be extruded by the fixing plate 7, the fixing plate 7 compresses the fixing spring 8, then the mounting rod 10 is rotatably installed, the mounting rod 10 is rotated and clamped into the corresponding mounting hole 11, the position of the fixing bolt 15 corresponds to the position of the corresponding fixing groove 13, the fixing bolt 15 is rotated, under the action of the first threaded holes 14, the fixing bolts 15 can be clamped into the corresponding fixing grooves 13, the fixing bolts 15 can downwards extrude the cover plate 4 through the fixing grooves 13, and the cover plate 4 is stably installed on the storage and transportation box body 1;
in the process of storage and transportation, when the storage and transportation box body 1 vibrates, the buffer box 2 can compress the first buffer spring 20, the buffer box 2 can be buffered and protected in the horizontal direction through the elastic deformation of the first buffer spring 20, when the buffer box 2 vibrates in the vertical direction, the buffer box 2 drives the moving seat 24 to move through the push rod 26 and compress the second buffer spring 25, the buffer box 2 can be buffered and protected in the vertical direction through the second buffer spring 25, so that the engine can be buffered and protected, when the moving seat 24 reciprocates left and right, the moving seat 24 can drive the push rod 23 to move left and right, the push rod 23 drives the gear 33 to reciprocate through the rack 30, the gear 33 can drive the blade 32 to reciprocate through the rotating shaft 31, and the storage and transportation box body 1 can be dried and dehumidified through the reciprocating rotation of the blade 32, the damage of the engine caused by the transportation of the storage box body 1 in an environment with heavy moisture can be prevented.
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 (8)
1. The storage and transportation box for storage and transportation of the aircraft engine comprises a storage and transportation box body (1) and a buffer box (2) positioned in the storage and transportation box body (1), and is characterized in that one end of a plurality of compression springs (3) is fixedly arranged at the bottom of the buffer box (2), the other end of each compression spring (3) is fixedly arranged on the inner wall of the bottom of the storage and transportation box body (1), a cover plate (4) is arranged at the top of the storage and transportation box body (1), a sealing seat (5) is fixedly arranged at the bottom of the cover plate (4), the sealing seat (5) is matched with the corresponding storage and transportation box body (1), two symmetrically arranged vertical rods (6) are fixedly arranged at the bottom of the sealing seat (5), the two vertical rods (6) are movably sleeved with a same fixing plate (7), one end of a plurality of fixing springs (8) is fixedly arranged at the top of the fixing plate (7), and the other end of each fixing spring (8) is fixedly arranged on the sealing seat (5, the conveying box comprises a conveying box body (1), wherein connecting plates (9) are fixedly mounted on two sides of the conveying box body (1), mounting rods (10) are rotatably mounted on the connecting plates (9), mounting holes (11) are formed in the top of a cover plate (4), an opening is formed in the inner wall of one side, away from each other, of each mounting hole (11), a transverse plate (12) is fixedly mounted at the top of each mounting rod (10), a first threaded hole (14) is formed in each transverse plate (12), a fixing bolt (15) is mounted in each first threaded hole (14) through internal threads, two symmetrically-arranged fixing grooves (13) are formed in the top of each cover plate (4), and each fixing bolt (15) is matched with the corresponding;
the buffer box is characterized in that two clamp plates (16) which are symmetrically arranged are arranged in the buffer box (2) in a sliding manner, second threaded holes (17) are formed in the inner walls of the two sides of the buffer box (2), adjusting screws (18) are arranged in the second threaded holes (17) in an internal thread manner, one ends of the adjusting screws (18) are rotatably arranged on the corresponding clamp plates (16), the other ends of the adjusting screws (18) extend to the outer side of the buffer box (2) and are fixedly provided with rotating plates (19), one ends of first buffer springs (20) are fixedly arranged on the side surfaces of the buffer box (2), the other ends of the first buffer springs (20) are fixedly arranged on the inner wall of the storage and transportation box body (1), two first grooves (22) which are symmetrically arranged are formed in the inner wall of the bottom of the storage and transportation box body (1), a moving seat (24) is arranged in the first grooves (22) in a sliding manner, and one end of, the other end of push rod (26) articulates on buffer tank (2) that corresponds, one side fixed mounting who removes seat (24) has the one end of second buffer spring (25), the other end fixed mounting of second buffer spring (25) is on the inner wall of first groove (22), second groove (29) have been seted up on one side inner wall of first groove (22), slidable mounting has the one end of push rod (23) in second groove (29), the other end fixed mounting of push rod (23) is on removing seat (24), push rod (23) one side fixed mounting has rack (30), rotate the one end of installing pivot (31) on the bottom inner wall of second groove (29), the other end of pivot (31) extends to in storage and transportation case body (1) and fixed mounting has blade (32), fixed cover is equipped with gear (33) on pivot (31), and gear (33) mesh with rack (30) mutually.
2. The storage and transportation tank for aircraft engine storage and transportation according to claim 1, characterized in that the inner wall of the bottom of the buffer tank (2) is provided with two symmetrically arranged moving grooves (27), and the clamping plate (16) is slidably mounted in the moving grooves (27).
3. The storage and transportation box for aircraft engine storage and transportation according to claim 1, characterized in that the sides of the two clamping plates (16) which are far away from each other are provided with a rotating groove (21), and one end of the adjusting screw (18) is rotatably mounted in the corresponding rotating groove (21).
4. The storage and transportation tank for aircraft engine storage and transportation according to claim 1, characterized in that a circular hole is formed in the inner wall of the top of the second groove (29), and the rotating shaft (31) is rotatably connected with the circular hole.
5. A container for the storage and transportation of aircraft engines, according to claim 1, characterised in that a protective mat (28) is fixedly mounted on both sides of the clamping plates (16) adjacent to each other, and the two protective mats (28) are fitted together.
6. The storage and transportation box for aircraft engine storage and transportation according to claim 1, wherein two symmetrically arranged positioning seats are fixedly installed at the top of the storage and transportation box body (1), two symmetrically arranged positioning grooves are formed at the bottom of the cover plate (4), and the positioning grooves are matched with the corresponding positioning seats.
7. The storage and transportation box for aircraft engine storage and transportation according to claim 1, characterized in that two connecting seats are fixed on the top of the connecting plate (9), a pin shaft is rotatably arranged on the connecting seats, and the mounting rod (10) is fixedly sleeved on the pin shaft.
8. The storage and transportation box for aircraft engine storage and transportation according to claim 1, characterized in that the bottom of the vertical rod (6) is fixedly provided with a limiting plate, and the limiting plate is matched with the corresponding fixing plate (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010875492.4A CN111994469A (en) | 2020-08-27 | 2020-08-27 | Storage and transportation box for storage and transportation of aircraft engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010875492.4A CN111994469A (en) | 2020-08-27 | 2020-08-27 | Storage and transportation box for storage and transportation of aircraft engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111994469A true CN111994469A (en) | 2020-11-27 |
Family
ID=73471361
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010875492.4A Withdrawn CN111994469A (en) | 2020-08-27 | 2020-08-27 | Storage and transportation box for storage and transportation of aircraft engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111994469A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112918887A (en) * | 2021-03-04 | 2021-06-08 | 亳州道智盛智能科技有限公司 | Communication radio transmission storage device |
| CN113716224A (en) * | 2021-09-10 | 2021-11-30 | 无锡市迈特动力机械有限公司 | Vapour fortune frame convenient to fixed engine |
| CN114044251A (en) * | 2021-10-28 | 2022-02-15 | 商洛学院 | Semiconductor device removes transportation protection device |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN208076487U (en) * | 2018-05-08 | 2018-11-09 | 郭少星 | A kind of portable formaldehyde testing equipment |
| CN109830626A (en) * | 2019-01-25 | 2019-05-31 | 杨松梅 | A kind of new energy car battery group anticollision assistor |
| CN109914080A (en) * | 2019-04-08 | 2019-06-21 | 湖南车霸房车实业有限公司 | A kind of caravan dried disinfecting wardrobe wind circulator |
| CN209071452U (en) * | 2018-12-18 | 2019-07-05 | 广州市捷巨电子科技有限公司 | A kind of lithium battery of good heat dissipation effect |
| CN209796326U (en) * | 2018-12-31 | 2019-12-17 | 安徽奥瑞格新能源有限公司 | Anti-collision transportation box for battery pack of electric bicycle |
| CN210054418U (en) * | 2019-05-14 | 2020-02-14 | 西安市中心医院 | Specimen preservation bottle for endoscope biopsy pathological tissue |
| CN210235911U (en) * | 2019-05-31 | 2020-04-03 | 王伟盛 | Novel material is with sealed storage device of rare noble metal |
| CN211040187U (en) * | 2019-10-12 | 2020-07-17 | 胡特 | Damping device for civil engineering |
| CN111463954A (en) * | 2020-04-16 | 2020-07-28 | 杭州藏储科技有限公司 | Shock-absorbing cooling automobile motor mechanical equipment box utilizing gravitation |
| CN211175170U (en) * | 2019-09-23 | 2020-08-04 | 邳州市景鹏创业投资有限公司 | Magnetic suspension automobile hydraulic shock absorber |
| CN211307546U (en) * | 2019-12-17 | 2020-08-21 | 青岛中乾机械制造有限公司 | A press mold tooling |
-
2020
- 2020-08-27 CN CN202010875492.4A patent/CN111994469A/en not_active Withdrawn
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN208076487U (en) * | 2018-05-08 | 2018-11-09 | 郭少星 | A kind of portable formaldehyde testing equipment |
| CN209071452U (en) * | 2018-12-18 | 2019-07-05 | 广州市捷巨电子科技有限公司 | A kind of lithium battery of good heat dissipation effect |
| CN209796326U (en) * | 2018-12-31 | 2019-12-17 | 安徽奥瑞格新能源有限公司 | Anti-collision transportation box for battery pack of electric bicycle |
| CN109830626A (en) * | 2019-01-25 | 2019-05-31 | 杨松梅 | A kind of new energy car battery group anticollision assistor |
| CN109914080A (en) * | 2019-04-08 | 2019-06-21 | 湖南车霸房车实业有限公司 | A kind of caravan dried disinfecting wardrobe wind circulator |
| CN210054418U (en) * | 2019-05-14 | 2020-02-14 | 西安市中心医院 | Specimen preservation bottle for endoscope biopsy pathological tissue |
| CN210235911U (en) * | 2019-05-31 | 2020-04-03 | 王伟盛 | Novel material is with sealed storage device of rare noble metal |
| CN211175170U (en) * | 2019-09-23 | 2020-08-04 | 邳州市景鹏创业投资有限公司 | Magnetic suspension automobile hydraulic shock absorber |
| CN211040187U (en) * | 2019-10-12 | 2020-07-17 | 胡特 | Damping device for civil engineering |
| CN211307546U (en) * | 2019-12-17 | 2020-08-21 | 青岛中乾机械制造有限公司 | A press mold tooling |
| CN111463954A (en) * | 2020-04-16 | 2020-07-28 | 杭州藏储科技有限公司 | Shock-absorbing cooling automobile motor mechanical equipment box utilizing gravitation |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112918887A (en) * | 2021-03-04 | 2021-06-08 | 亳州道智盛智能科技有限公司 | Communication radio transmission storage device |
| CN113716224A (en) * | 2021-09-10 | 2021-11-30 | 无锡市迈特动力机械有限公司 | Vapour fortune frame convenient to fixed engine |
| CN114044251A (en) * | 2021-10-28 | 2022-02-15 | 商洛学院 | Semiconductor device removes transportation protection device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111994469A (en) | Storage and transportation box for storage and transportation of aircraft engine | |
| CN209062282U (en) | A kind of aluminium plate processing unit (plant) with adjustable-width blank pressing device | |
| CN213010082U (en) | Be used for commodity circulation warehouse freight buffer | |
| CN212306003U (en) | Heat dissipation protection device of electromechanical device | |
| CN216717811U (en) | Detection platform for aeroengine | |
| CN214987625U (en) | Novel ash storage tank | |
| CN219948017U (en) | Goods fixing device for road goods transportation | |
| CN216332869U (en) | Aerospace craft separation device | |
| CN116969051A (en) | An energy storage electric box protection structure and an energy storage electric box | |
| CN113099644B (en) | Energy storage rack heat dissipation shock attenuation strutting arrangement | |
| CN110470546B (en) | A testing machine and testing method for testing the swing strength of support legs of a load-molded pallet | |
| CN212722061U (en) | Brake disc testing arrangement | |
| CN221439114U (en) | Dampproofing storage device of pneumatic element | |
| CN114537895A (en) | Storage damping device for goods logistics storage and damping method thereof | |
| CN102909353A (en) | Piston-vibrating shakeout device | |
| CN211494536U (en) | Automatic weighing and packaging device for powder auxiliaries | |
| CN113105109A (en) | Glass cutting device | |
| CN219874627U (en) | Switch board convenient to maintenance | |
| CN220163950U (en) | Refrigerating equipment conveyer | |
| CN220722091U (en) | Composite material storage box | |
| CN222064692U (en) | A surface galvanizing device for automobile shock absorber spring processing | |
| CN222327308U (en) | A fan blade drilling and grinding device in fan production | |
| CN213567191U (en) | A transportation protector for aerogenerator part | |
| CN223327754U (en) | Many rotors fold arm delivery unmanned aerial vehicle fast | |
| CN219054087U (en) | Clamp for machining aero-engine blades for preventing parts from falling |
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 | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20201127 |