CN109353658A - A kind of general storage box of unmanned plane - Google Patents
A kind of general storage box of unmanned plane Download PDFInfo
- Publication number
- CN109353658A CN109353658A CN201811359770.XA CN201811359770A CN109353658A CN 109353658 A CN109353658 A CN 109353658A CN 201811359770 A CN201811359770 A CN 201811359770A CN 109353658 A CN109353658 A CN 109353658A
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- case
- fixed case
- wing
- wing fixed
- case lid
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 45
- 238000013016 damping Methods 0.000 claims description 40
- 239000000463 material Substances 0.000 claims description 9
- 239000007787 solid Substances 0.000 claims description 8
- 238000003466 welding Methods 0.000 claims description 5
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 12
- 230000035939 shock Effects 0.000 description 4
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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
- 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
- B65D25/101—Springs, elastic lips, or other resilient elements to locate the articles by pressure
-
- 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
- B65D55/00—Accessories for container closures not otherwise provided for
- B65D55/02—Locking devices; Means for discouraging or indicating unauthorised opening or removal of closure
-
- 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
-
- 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
- B65D85/00—Containers, packaging elements or packages, specially adapted for particular articles or materials
- B65D85/30—Containers, packaging elements or packages, specially adapted for particular articles or materials for articles particularly sensitive to damage by shock or pressure
-
- 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
-
- 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
- B65D2585/686—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 vehicles
- B65D2585/687—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 vehicles aircrafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Buffer Packaging (AREA)
Abstract
The present invention relates to a kind of unmanned plane devices, it in particular be a kind of general storage box of unmanned plane include cabinet, wing fixed case, fuselage fixed case, case lid, can solve unmanned plane is that there are accurate structures inside a kind of high-altitude vehicle, it is vibrated to beat and will cause the problem of internal damage damages unmanned plane, it is easiest to jolt in the way of storage transport with unmanned plane to hit and damage, existing unmanned plane storage box structure is simply not thorough the problem of being easy to happen vibration to the unmanned plane fixation of internal storage, it also can solve the problem of existing unmanned plane storage is first all unable to store just for a kind of unmanned plane of the unmanned plane in model for different model mostly.
Description
Technical field
The present invention relates to a kind of unmanned plane devices, are in particular a kind of general storage boxes of unmanned plane.
Background technique
Unmanned plane is to be vibrated to beat there are accurate structure inside a kind of high-altitude vehicle to will cause internal damage
Bad to damage unmanned plane, unmanned plane, which is easiest to jolt in the way of storage transport, to be hit and damages, and existing unmanned plane is deposited
It puts box structure simply be not thorough fixed to the unmanned plane of internal storage and is easy to happen vibration and the storage of existing unmanned plane is first most
All it is unable to store just for a kind of unmanned plane of the unmanned plane in model for different model.
Summary of the invention
The present invention relates to a kind of unmanned plane devices, are in particular a kind of general storage boxes of unmanned plane.It can solve nothing
Man-machine is to be vibrated to beat there are accurate structure inside a kind of high-altitude vehicle to will cause internal damage and make unmanned plane
The problem of damage and unmanned plane, which are easiest to jolt in the way of storage transport, to be hit and damages, existing unmanned plane storage
Box structure is simply not thorough the problem of being easy to happen vibration to the unmanned plane fixation of internal storage, moreover it is possible to solve existing unmanned plane
The problem of storage is first all unable to store just for a kind of unmanned plane of the unmanned plane in model for different model mostly.
It is in particular a kind of general storage box of unmanned plane include cabinet, machine the present invention relates to a kind of unmanned plane device
Wing fixed case, fuselage fixed case, case lid, can solve unmanned plane is inside a kind of high-altitude vehicle there are accurate structure,
Being vibrated to beat will cause the problem of internal damage damages unmanned plane and unmanned plane and is easiest in the way of storage transport
It jolts and hits and damage, it is easy that existing unmanned plane storage box structure is simply not thorough the unmanned plane fixation of internal storage
The problem of shaking, moreover it is possible to solve existing unmanned plane storage first mostly all just for the unmanned plane in a kind of model for not
The problem of being unable to store with the unmanned plane of model.
The upper end of wing fixed case is provided with wing fixed case buckle support arm, wing fixed case buckles support arm spring,
Wing fixed case pinch plate, wing fixed case buckle, wing fixed case buckle slide block, wing fixed case slideway, wing fixed case
Spring, wing fixed case support arm, wing fixed case support arm spring seat, wing fixed case rotating disc, wing fixed case are solid
Determine bolt, wing fixed pedestal, wing fixed case non-slip mat, wing fixed case support arm fixture block, the inside of wing fixed case is sliding
Dynamic to have wing fixed case to buckle support arm, the upper end of wing fixed case buckle support arm is provided with wing fixed case buckle support arm
The upper end of spring, wing fixed case buckle support arm is welded with wing fixed case pinch plate, the upper end of wing fixed case pinch plate
It is welded with wing fixed case buckle, the lower end of wing fixed case pinch plate is welded with wing fixed case buckle slide block, and wing is fixed
Case is internally provided with wing fixed case slideway, and the upper end sliding of wing fixed case slideway has wing fixed case buckle slide block, machine
The interior welds of wing fixed case have wing fixed case spring, and the internal slide of wing fixed case has wing fixed case support arm, machine
The lower end of wing fixed case support arm is welded with wing fixed case spring, and the lower end of wing fixed case support arm is welded with wing and fixes
Case support arm spring seat, the upper end of wing fixed case support arm are welded with wing fixed case rotating disc, the rotation of wing fixed case
The upper end rotation of disk has wing fixed case fixing bolt, and the upper end rotation of wing fixed case rotating disc has wing fixed pedestal, machine
The upper end of wing fixed pedestal is fixed with wing fixed case non-slip mat, and the two sides of wing fixed case support arm are welded with wing fixed case
Support arm fixture block, wing fixed case support arm fixture block cooperate wing fixed case buckle to use.
The upper end of fuselage fixed case is provided with fuselage fixed case slideway, fuselage fixed case damping sleeve, fuselage fixed case and subtracts
Shake travelling arm, telescopic mast, damping spring, sliding panel, spherical axis pedestal, spherical axis support arm, support board, loading flat spring base
Seat, loading flat spring, fuselage clamping case, clamping case sliding sleeve, clamping housing-case cylinder slideway, pull ring, clamping case slide post, clamping
Case slide post limited block, triangle limited block, slide post fixed case, fixture block sleeve, fixture block, fixture block slide post, fixture block spring, linkage
Disk, fixing clamp, fixing clamp slideway, fixing clamp lead screw, fixing clamp spring, fixing clamp sliding panel, fixing clamp non-slip mat, fuselage are fixed
Case is internally provided with fuselage fixed case slideway, and the interior welds of fixed case have fuselage fixed case damping sleeve, fuselage fixed case
The internal slide of damping sleeve has fuselage fixed case damping travelling arm, and the upper end of fuselage fixed case damping sleeve is welded with flexible
Column, the upper end of telescopic mast are provided with damping spring, and the upper end sliding of fuselage fixed case slideway has sliding panel, the lower end weldering of sliding panel
It is connected to fuselage fixed case damping travelling arm, the upper end of sliding panel is welded with spherical axis pedestal, and the inner rotation of spherical axis pedestal has
Spherical axis support arm, the inner rotation of support board have spherical axis support arm, and the lower end of support board is welded with support board spring seat,
The upper end of support board spring seat is welded with loading flat spring, and the upper end of support board is welded with fuselage clamping case, clamping case sliding
Sleeve is internally provided with clamping housing-case cylinder slideway, and the upper end of clamping case sliding sleeve is welded with pull ring, clamps case sliding sleeve
Internal slide have clamping case slide post, the upper end of clamping case slide post is welded with clamping case slide post limited block, and clamping case is sliding
The lower end of dynamic column is welded with triangle limited block, and the lower end of clamping case sliding sleeve is welded with slide post fixed case, and fuselage clamps case
Interior welds have a slide post fixed case, the inner rotation of slide post fixed case has fixture block sleeve, the upper end welding of fixture block sleeve
There is fixture block, fixture block cooperates triangle limited block to use, and the internal slide of fixture block sleeve has fixture block slide post, and the lower end of fixture block sleeve is solid
Surely there is fixture block spring, the inside of slide post fixed case is fixed with fixture block spring, and the internal slide of fixture block sleeve has fixture block slide post
Upper end be hinged with linkage disk, the upper end of clamping case sliding sleeve is welded with fixing clamp, and fixing clamp is internally provided with fixing clamp
Slideway, the inner rotation of fixing clamp have fixing clamp lead screw, and the upper end of fixing clamp lead screw is provided with fixing clamp spring, fixing clamp slideway
Upper end sliding have fixing clamp sliding panel, the upper end of fixing clamp sliding panel is provided with threaded hole, fixing clamp sliding panel threaded hole
Inner rotation has fixing clamp lead screw, and the upper end of fixing clamp is provided with fixing clamp non-slip mat.
The upper end of case lid is provided with case lid slideway, case lid buckle, two-way lead screw, lead screw belt pulley, case lid belt, case lid control
Case processed, case lid control cabinet belt pulley, case lid rotation axis, case lid fixes sleeve, case lid spring, case lid travelling arm, case lid rotating disc,
Case lid fixed pedestal, case lid are internally provided with case lid slideway, and the upper end sliding of case lid slideway has case lid buckle, case lid buckle
It is internally provided with threaded hole, the inner rotation in case lid snap thread hole has two-way lead screw, and the upper end key connection of two-way lead screw has silk
Thick stick belt pulley, the upper end of lead screw belt pulley are provided with case lid belt, and the upper end of case lid is welded with case lid control cabinet, case lid control cabinet
Inner rotation have a case lid rotation axis, the upper end key connection of case lid rotation axis has case lid control cabinet belt pulley, case lid control cabinet skin
The upper end of belt wheel is provided with case lid belt, and the lower end of case lid is welded with case lid fixes sleeve, the inside setting of case lid fixes sleeve
There is case lid spring, the internal slide of case lid fixes sleeve has case lid travelling arm, and the lower end of case lid travelling arm is welded with case lid rotation
The lower end rotation of disk, case lid rotating disc has case lid fixed pedestal.
The interior welds of cabinet have wing fixed case, and the interior welds of cabinet have fuselage fixed case, the upper end setting of cabinet
Fluted, tank recess cooperates case lid buckle to use, and the upper end of cabinet is provided with case lid.
As advanced optimizing for the technical program, wing described in a kind of general storage box of unmanned plane of the present invention is fixed
Case, wing fixed case support arm, wing fixed case support arm spring seat, wing fixed case rotating disc, wing fixed case are fixed
Bolt, wing fixed pedestal are disposed as two.
As advanced optimizing for the technical program, wing fixed case described in a kind of general storage box of unmanned plane of the present invention
Support arm, wing fixed case rotating disc, wing fixed pedestal, case lid fixes sleeve, case lid travelling arm, case lid rotating disc, case lid
Fixed pedestal concentrically line.
As advanced optimizing for the technical program, cabinet, wing described in a kind of general storage box of unmanned plane of the present invention
Fixed case, fuselage fixed case, case lid material selection stainless steel material.
As advanced optimizing for the technical program, fuselage fixed case described in a kind of general storage box of unmanned plane of the present invention
Damping sleeve, fuselage fixed case damping travelling arm, telescopic mast, damping spring are disposed as two.
As advanced optimizing for the technical program, case lid belt material described in a kind of general storage box of unmanned plane of the present invention
Matter selects rubber.
A kind of general storage box of unmanned plane of the present invention has the beneficial effect that
The present invention relates to a kind of unmanned plane devices, are in particular a kind of general storage boxes of unmanned plane.It can solve nothing
Man-machine is to be vibrated to beat there are accurate structure inside a kind of high-altitude vehicle to will cause internal damage and make unmanned plane
The problem of damage and unmanned plane, which are easiest to jolt in the way of storage transport, to be hit and damages, existing unmanned plane storage
Box structure is simply not thorough the problem of being easy to happen vibration to the unmanned plane fixation of internal storage, moreover it is possible to solve existing unmanned plane
The problem of storage is first all unable to store just for a kind of unmanned plane of the unmanned plane in model for different model mostly.
Detailed description of the invention
The present invention will be further described in detail with specific implementation method with reference to the accompanying drawing.
Fig. 1 is a kind of overall structure diagram of the general storage box of unmanned plane of the present invention.
Fig. 2 is a kind of wing fixed case structural schematic diagram of the general storage box of unmanned plane of the present invention.
Fig. 3 is that a kind of wing fixed case of the general storage box of unmanned plane of the present invention buckles support arm structural schematic diagram.
Fig. 4 is a kind of wing fixed case support arm structural schematic diagram of the general storage box of unmanned plane of the present invention.
Fig. 5 is a kind of fuselage fixed case structural schematic diagram of the general storage box of unmanned plane of the present invention.
Fig. 6 is a kind of sliding panel structural schematic diagram of the general storage box of unmanned plane of the present invention.
Fig. 7 is that a kind of fuselage of the general storage box of unmanned plane of the present invention clamps box structure schematic diagram.
Fig. 8 is a kind of clamping case slide post structural schematic diagram of the general storage box of unmanned plane of the present invention.
Fig. 9 is a kind of slide post fixed case structural schematic diagram of the general storage box of unmanned plane of the present invention.
Figure 10 sets fixed folder structure schematic diagram for a kind of general storage box of unmanned plane of the present invention.
Figure 11 is a kind of cover structure schematic diagram of the general storage box of unmanned plane of the present invention.
Figure 12 is a kind of case lid fixes sleeve structural schematic diagram of the general storage box of unmanned plane of the present invention.In figure: cabinet 1；
Wing fixed case 2；Wing fixed case buckles support arm 2-1；Wing fixed case buckles support arm spring 2-2；Wing fixed case card
Buckle 2-3；Wing fixed case buckles 2-4；Wing fixed case buckle slide block 2-5；Wing fixed case slideway 2-6；Wing fixed case
Spring 2-7；Wing fixed case support arm 2-8；Wing fixed case support arm spring seat 2-9；Wing fixed case rotating disc 2-10；
Wing fixed case fixing bolt 2-11；Wing fixed pedestal 2-12；Wing fixed case non-slip mat 2-13；Wing fixed case support arm
Fixture block 2-14；Fuselage fixed case 3；Fuselage fixed case slideway 3-1；Fuselage fixed case damping sleeve 3-2；Fuselage fixed case damping is sliding
Swing arm 3-3；Telescopic mast 3-4；Damping spring 3-5；Sliding panel 3-6；Spherical axis pedestal 3-7；Spherical axis support arm 3-8；Support board
3-9；Support board spring seat 3-10；Loading flat spring 3-11；Fuselage clamps case 3-12；Clamp case sliding sleeve 3-13；Clamping
Housing-case cylinder slideway 3-14；Pull ring 3-15；Clamp case slide post 3-16；Clamp case slide post limited block 3-17；Triangle limited block 3-
18；Slide post fixed case 3-19；Fixture block sleeve 3-20；Fixture block 3-21；Fixture block slide post 3-22；Fixture block spring 3-23；Link disk
3-24；Fixing clamp 3-25；Fixing clamp slideway 3-26；Fixing clamp lead screw 3-27；Fixing clamp spring 3-28；Fixing clamp sliding panel 3-
29；Fixing clamp non-slip mat 3-30；Case lid 4；Case lid slideway 4-1；Case lid buckles 4-2；Two-way lead screw 4-3；Lead screw belt pulley 4-4；
Case lid belt 4-5；Case lid control cabinet 4-6；Case lid control cabinet belt pulley 4-7；Case lid rotation axis 4-8；Case lid fixes sleeve 4-9；
Case lid spring 4-10；Case lid travelling arm 4-11；Case lid rotating disc 4-12；Case lid fixed pedestal 4-13.
Specific embodiment
Specific embodiment 1:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11,12, the present invention relates to it is a kind of nobody
In particular machine device is a kind of general storage box of unmanned plane, including cabinet 1, wing fixed case 2, fuselage fixed case 3, case
Lid 4, can solve unmanned plane is to be vibrated to beat there are accurate structure inside a kind of high-altitude vehicle to will cause inside
Damage the problem of damaging unmanned plane and unmanned plane be easiest to jolt shock in the way of storage transport and damage, show
Some unmanned plane storage box structures are simply not thorough the problem of being easy to happen vibration to the unmanned plane fixation of internal storage, moreover it is possible to solve
Certainly existing unmanned plane storage first can not all be deposited just for a kind of unmanned plane of the unmanned plane in model for different model mostly
The problem of putting.
The upper end of wing fixed case 2 is provided with wing fixed case buckle support arm 2-1, wing fixed case buckle support arm bullet
Spring 2-2, wing fixed case pinch plate 2-3, wing fixed case buckle 2-4, wing fixed case buckle slide block 2-5, wing fixed case
Slideway 2-6, wing fixed case spring 2-7, wing fixed case support arm 2-8, wing fixed case support arm spring seat 2-9, machine
Wing fixed case rotating disc 2-10, wing fixed case fixing bolt 2-11, wing fixed pedestal 2-12, wing fixed case non-slip mat 2-
13, wing fixed case support arm fixture block 2-14, the internal slide of wing fixed case 2 have wing fixed case to buckle support arm 2-1, machine
The upper end of wing fixed case buckle support arm 2-1 is provided with wing fixed case buckle support arm spring 2-2, wing fixed case buckle branch
The upper end of brace 2-1 is welded with wing fixed case pinch plate 2-3, and it is solid that the upper end of wing fixed case pinch plate 2-3 is welded with wing
Determine case buckle 2-4, the lower end of wing fixed case pinch plate 2-3 is welded with wing fixed case buckle slide block 2-5, wing fixed case 2
Be internally provided with wing fixed case slideway 2-6, the upper end sliding of wing fixed case slideway 2-6 has wing fixed case buckle slide block
2-5, the interior welds of wing fixed case 2 have wing fixed case spring 2-7, and the internal slide of wing fixed case 2 has wing to fix
Case support arm 2-8, the lower end of wing fixed case support arm 2-8 are welded with wing fixed case spring 2-7, wing fixed case support arm
The lower end of 2-8 is welded with wing fixed case support arm spring seat 2-9, and the upper end welding of wing fixed case support arm 2-8 is organic
The upper end rotation of wing fixed case rotating disc 2-10, wing fixed case rotating disc 2-10 have wing fixed case fixing bolt 2-11, machine
The upper end rotation of wing fixed case rotating disc 2-10 has wing fixed pedestal 2-12, and the upper end fixation of wing fixed pedestal 2-12 is organic
Wing fixed case non-slip mat 2-13, the two sides of wing fixed case support arm 2-8 are welded with wing fixed case support arm fixture block 2-14, machine
Wing fixed case support arm fixture block 2-14 cooperates wing fixed case buckle 2-4 to use.
It is solid that the upper end of fuselage fixed case 3 is provided with fuselage fixed case slideway 3-1, fuselage fixed case damping sleeve 3-2, fuselage
Determine case damping travelling arm 3-3, telescopic mast 3-4, damping spring 3-5, sliding panel 3-6, spherical axis pedestal 3-7, spherical axis support arm
3-8, support board 3-9, support board spring seat 3-10, loading flat spring 3-11, fuselage clamping case 3-12, clamping case sliding sleeve
3-13, clamping housing-case cylinder slideway 3-14, pull ring 3-15, clamping case slide post 3-16, clamping case slide post limited block 3-17, triangle
Limited block 3-18, slide post fixed case 3-19, fixture block sleeve 3-20, fixture block 3-21, fixture block slide post 3-22, fixture block spring 3-
23, link disk 3-24, fixing clamp 3-25, fixing clamp slideway 3-26, fixing clamp lead screw 3-27, fixing clamp spring 3-28, fixing clamp
Sliding panel 3-29, fixing clamp non-slip mat 3-30, fuselage fixed case 3 are internally provided with fuselage fixed case slideway 3-1, fixed case 3
Interior welds have fuselage fixed case damping sleeve 3-2, the internal slide of fuselage fixed case damping sleeve 3-2 has fuselage fixed case
Damping travelling arm 3-3, the upper end of fuselage fixed case damping sleeve 3-2 are welded with telescopic mast 3-4, the upper end setting of telescopic mast 3-4
There is damping spring 3-5, the upper end sliding of fuselage fixed case slideway 3-1 has sliding panel 3-6, and the lower end welding of sliding panel 3-6 is organic
Body fixed case damping travelling arm 3-3, the upper end of sliding panel 3-6 are welded with spherical axis pedestal 3-7, the inside of spherical axis pedestal 3-7
Rotation has spherical axis support arm 3-8, and the inner rotation of support board 3-9 has spherical axis support arm 3-8, the lower end weldering of support board 3-9
It is connected to support board spring seat 3-10, the upper end of support board spring seat 3-10 is welded with loading flat spring 3-11, support board 3-9
Upper end be welded with fuselage clamping case 3-12, clamping case sliding sleeve 3-13 is internally provided with clamping housing-case cylinder slideway 3-14,
The upper end of clamping case sliding sleeve 3-13 is welded with pull ring 3-15, and the internal slide of clamping case sliding sleeve 3-13 has clamping case sliding
Dynamic column 3-16, the upper end of clamping case slide post 3-16 are welded with clamping case slide post limited block 3-17, clamp case slide post 3-16
Lower end be welded with triangle limited block 3-18, the lower end of clamping case sliding sleeve 3-13 is welded with slide post fixed case 3-19, machine
The interior welds of body clamping case 3-12 have slide post fixed case 3-19, and the inner rotation of slide post fixed case 3-19 has fixture block sleeve
3-20, the upper end of fixture block sleeve 3-20 are welded with fixture block 3-21, and fixture block 3-21 cooperates triangle limited block 3-18 to use, fixture block sleeve
The internal slide of 3-20 has fixture block slide post 3-22, and the lower end of fixture block sleeve 3-20 is fixed with fixture block spring 3-23, and slide post is solid
The inside for determining case 3-19 is fixed with fixture block spring 3-23, and the internal slide of fixture block sleeve 3-20 has the upper end of fixture block slide post 3-22
It is hinged with linkage disk 3-24, the upper end of clamping case sliding sleeve 3-13 is welded with fixing clamp 3-25, and the inside of fixing clamp 3-25 is set
It is equipped with fixing clamp slideway 3-26, the inner rotation of fixing clamp 3-25 has fixing clamp lead screw 3-27, the upper end of fixing clamp lead screw 3-27
It is provided with fixing clamp spring 3-28, the upper end sliding of fixing clamp slideway 3-26 has fixing clamp sliding panel 3-29, fixing clamp sliding panel
The upper end of 3-29 is provided with threaded hole, and the inner rotation of fixing clamp sliding panel 3-29 threaded hole has fixing clamp lead screw 3-27, fixed
The upper end of folder 3-25 is provided with fixing clamp non-slip mat 3-30.
The upper end of case lid 4 is provided with case lid slideway 4-1, case lid buckle 4-2, two-way lead screw 4-3, lead screw belt pulley 4-4, case
Lid belt 4-5, case lid control cabinet 4-6, case lid control cabinet belt pulley 4-7, case lid rotation axis 4-8, case lid fixes sleeve 4-9, case
Lid spring 4-10, case lid travelling arm 4-11, case lid rotating disc 4-12, case lid fixed pedestal 4-13, case lid 4 are internally provided with case
The upper end sliding of lid slideway 4-1, case lid slideway 4-1 have case lid to buckle 4-2, and case lid buckle 4-2's is internally provided with threaded hole, case
The inner rotation of cover latch 4-2 threaded hole has two-way lead screw 4-3, and the upper end key connection of two-way lead screw 4-3 has lead screw belt pulley 4-
4, the upper end of lead screw belt pulley 4-4 is provided with case lid belt 4-5, and the upper end of case lid 4 is welded with case lid control cabinet 4-6, case lid control
The inner rotation of case 4-6 processed has case lid rotation axis 4-8, and the upper end key connection of case lid rotation axis 4-8 has case lid control cabinet belt pulley
The upper end of 4-7, case lid control cabinet belt pulley 4-7 are provided with case lid belt 4-5, and the lower end of case lid 4 is welded with case lid fixes sleeve
4-9's, case lid fixes sleeve 4-9 is internally provided with case lid spring 4-10, and the internal slide of case lid fixes sleeve 4-9 has case lid sliding
Swing arm 4-11, the lower end of case lid travelling arm 4-11 are welded with case lid rotating disc 4-12, and the lower end rotation of case lid rotating disc 4-12 has
Case lid fixed pedestal 4-13.
The interior welds of cabinet 1 have wing fixed case 2, and the interior welds of cabinet 1 have fuselage fixed case 3, the upper end of cabinet 1
Be arranged it is fluted, 1 groove of cabinet cooperate case lid buckle 4-2 use, the upper end of cabinet 1 is provided with case lid 4.Specific embodiment
Two:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11,12, present embodiment is to embodiment party
Formula one is described further, the wing fixed case 2, wing fixed case support arm 2-8, wing fixed case support arm spring base
Seat 2-9, wing fixed case rotating disc 2-10, wing fixed case fixing bolt 2-11, wing fixed pedestal 2-12 are disposed as two
It is a.
Specific embodiment 3:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11,12, present embodiment is to embodiment party
Formula one is described further, the wing fixed case support arm 2-8, wing fixed case rotating disc 2-10, wing fixed pedestal
2-12, case lid fixes sleeve 4-9, case lid travelling arm 4-11, case lid rotating disc 4-12, case lid fixed pedestal 4-13 concentrically line.
Specific embodiment 4:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11,12, present embodiment is to embodiment party
Formula one is described further, the cabinet 1, wing fixed case 2, fuselage fixed case 3,4 material selection stainless steel material of case lid.
Specific embodiment 5:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11,12, present embodiment is to embodiment party
Formula one is described further, the fuselage fixed case damping sleeve 3-2, fuselage fixed case damping travelling arm 3-3, telescopic mast 3-
4, damping spring 3-5 is disposed as two.
Specific embodiment 6:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11,12, present embodiment is to embodiment party
Formula one is described further, the case lid belt 4-5 material selection rubber.
The working principle of the invention is:
A kind of working principle of the general storage box of unmanned plane be pull pull ring 3-15 drive clamping case sliding sleeve 3-13 to
The mobile elongation in two sides, clamping case sliding sleeve 3-13 drive clamping case slide post limited block 3-17 in clamping housing-case to two sides are mobile
The upper end sliding of cylinder slideway 3-14 plays protection clamping case sliding sleeve 3-13 and will not slide because of stretching transition, and clamping case is sliding
Moving sleeve 3-13 drives slide post fixed case 3-19 mobile to two sides to two sides are mobile, and slide post fixed case 3-19 is to two Slideslips
Drive fixture block 3-21 triangle limited block 3-18 upper end slide, regulate clamping case sliding sleeve 3-13 length after by fixture block
3-21 cooperation triangle limited block 3-18 is fixed, and rotation fixing clamp lead screw 3-27 drives fixing clamp sliding panel 3-29 in fixing clamp
The upper end upward sliding of slideway 3-26, since fixing clamp sliding panel 3-29 is that slide in fixing clamp slideway 3-26 be to limiting
Unmanned plane, is placed on the upper end of fixing clamp 3-25 by rotation, is then rotated fixing clamp lead screw 3-27 and is driven fixing clamp sliding panel 3-
29 slide downwards fix unmanned aerial vehicle body, and linkage disk 3- is pulled downward on when to reduce the length of clamping case sliding sleeve 3-13
24 drive fixture block slide post 3-22 rotation, and fixture block slide post 3-22 rotation drives fixture block sleeve 3-20 rotation, fixture block sleeve 3-20
Rotation compression fixture block spring 3-23 separates fixture block 3-21 with triangle limited block 3-18 simultaneously, while inwardly pushing clamping case sliding
Sleeve 3-13 can reduce the length of clamping case sliding sleeve 3-13, unclamp linkage disk 3-24 by fixing clamp bullet after regulating length
Spring 3-28 active force drives fixture block 3-21 reset to block triangle limited block 3-18 and is fixed, and pulls wing fixed case non-slip mat 2-
13 drive wing fixed case support arm 2-8 to adjust height, the support of wing fixed case to upward sliding in the inside of wing fixed case 2
Arm 2-8 upward sliding drives wing fixed case support arm fixture block 2-14 in the upper end upward sliding of wing fixed case buckle 2-4, will
Wing fixed pedestal 2-12 is stopped drag after adjusting to the height of unmanned plane wing by wing fixed case support arm fixture block 2-14 card
Live in wing fixed case buckle 2-4 is fixed, and adjusts angle according to the angular turn wing fixed pedestal 2-12 of unmanned plane wing
Then the fixation that angle is carried out with wing fixed case fixing bolt 2-11, when the height for needing to reduce wing fixed case support arm 2-8
It pulls wing fixed case buckle support arm 2-1 to drive wing fixed case pinch plate 2-3 mobile to two sides to two sides when spending while pressing
Contracting wing fixed case buckles support arm spring 2-2, and wing fixed case pinch plate 2-3 makes wing fixed case pinch plate to two sides movement
2-3 is separated with wing fixed case support arm fixture block 2-14, is pressed down on wing fixed pedestal 2-12 and is adjusted height, regulates height
Wing fixed case buckle support arm 2-1 is unclamped afterwards, and machine is pushed by wing fixed case buckle support arm spring 2-2 active force inwardly
Wing fixed case pinch plate 2-3 makes wing fixed case buckle 2-4 block wing fixed case support arm fixture block 2-14 and be fixed, by case
Lid 4 is placed on the upper end of cabinet 1, and case lid fixed pedestal 4-13 is stuck in the upper end of wing, sliding according to the thickness case lid of unmanned plane wing
Swing arm 4-11 can be adjusted in the inside of case lid fixes sleeve 4-9 to contract, and wing fixed pedestal 2-12 can be cooperated machine
The wing, which is clamped, to be fixed, the angle of the adjustable case lid fixed pedestal 4-13 of case lid rotating disc 4-12, rotates case lid rotation axis 4-8
Case lid control cabinet belt pulley 4-7 rotation is driven, case lid control cabinet belt pulley 4-7 rotation drives case lid belt 4-5 rotation, case lid skin
Band 4-5 rotation drives lead screw belt pulley 4-4 rotation, and lead screw belt pulley 4-4 rotation drives two-way lead screw 4-3 rotation, due to case lid
Buckle 4-2 is slided in the upper end of case lid slideway 4-1 to limit the rotation of case lid buckle 4-2, and two-way lead screw 4-3 rotates band
Dynamic case lid buckle 4-2 carries out consolidating for case lid 4 in the groove that the upper end of case lid slideway 4-1 slides in and out the setting of cooperation 1 upper end of cabinet
Fixed, fuselage fixed case damping travelling arm 3-3 subtracts in fuselage fixed case when encountering the section jolted during unmanned plane transport
The inside slide downward of shake sleeve 3-2 makes telescopic mast 3-4 contraction simultaneously while compression shock absorption spring 3-5 can solve to jolt and cause
The damage of unmanned plane, telescopic mast 3-4 plays the role of supporting fixed damping spring 3-5, outside unmanned plane transport case receives
Impact force drives fuselage clamping case 3-12 displacement when the shock of power, and fuselage clamps case 3-12 displacement and drives support board 3-9 mobile, carries
The mobile inner rotation for driving spherical shape axis support arm 3-8 in spherical axis pedestal 3-7 of object plate 3-9, while compressing loading flat spring 3-
11 can offset the impact force generated when shock, drive support board by loading flat spring 3-11 active force after impact force is cancelled
3-9 resets, solve unmanned plane be vibrated inside a kind of high-altitude vehicle there are accurate structure beat will cause it is interior
The problem of damage in portion damages unmanned plane and unmanned plane, which are easiest to jolt in the way of storage transport, to be hit and damages,
Existing unmanned plane storage box structure is simply not thorough the problem of being easy to happen vibration to the unmanned plane fixation of internal storage, moreover it is possible to
Solving existing unmanned plane storage first mostly all can not just for a kind of unmanned plane of the unmanned plane in model for different model
The problem of storage.
It states bright not limitation of the present invention, the present invention and is also not limited to the example above, the common skill of the art
The variations, modifications, additions or substitutions that art personnel are made within the essential scope of the present invention also belong to protection model of the invention
It encloses.
Claims (6)
1. a kind of general storage box of unmanned plane, including cabinet (1), wing fixed case (2), fuselage fixed case (3), case lid (4),
Be characterized in that: the upper end of the wing fixed case (2) is provided with wing fixed case buckle support arm (2-1), wing fixed case
Buckle support arm spring (2-2), wing fixed case pinch plate (2-3), wing fixed case buckle (2-4), wing fixed case buckle
Sliding block (2-5), wing fixed case slideway (2-6), wing fixed case spring (2-7), wing fixed case support arm (2-8), wing
Fixed case support arm spring seat (2-9), wing fixed case rotating disc (2-10), wing fixed case fixing bolt (2-11), machine
Wing fixed pedestal (2-12), wing fixed case non-slip mat (2-13), wing fixed case support arm fixture block (2-14), wing fixed case
(2) internal slide has wing fixed case to buckle support arm (2-1), and wing fixed case buckles the upper end setting of support arm (2-1)
There is wing fixed case to buckle support arm spring (2-2), the upper end of wing fixed case buckle support arm (2-1) is welded with wing and fixes
Case pinch plate (2-3), the upper end of wing fixed case pinch plate (2-3) are welded with wing fixed case buckle (2-4), wing fixed case
The lower end of pinch plate (2-3) is welded with wing fixed case buckle slide block (2-5), and wing fixed case (2) is internally provided with wing
The upper end sliding of fixed case slideway (2-6), wing fixed case slideway (2-6) has wing fixed case buckle slide block (2-5), and wing is solid
The interior welds for determining case (2) have wing fixed case spring (2-7), and the internal slide of wing fixed case (2) has wing fixed case branch
Brace (2-8), the lower end of wing fixed case support arm (2-8) are welded with wing fixed case spring (2-7), the support of wing fixed case
The lower end of arm (2-8) is welded with wing fixed case support arm spring seat (2-9), the upper end of wing fixed case support arm (2-8)
It is welded with wing fixed case rotating disc (2-10), the upper end rotation of wing fixed case rotating disc (2-10) has wing fixed case to fix
The upper end rotation of bolt (2-11), wing fixed case rotating disc (2-10) has wing fixed pedestal (2-12), wing fixed pedestal
The upper end of (2-12) is fixed with wing fixed case non-slip mat (2-13), and the two sides welding of wing fixed case support arm (2-8) is organic
Wing fixed case support arm fixture block (2-14), wing fixed case support arm fixture block (2-14) cooperation wing fixed case buckle (2-4) make
With；
The upper end of fuselage fixed case (3) is provided with fuselage fixed case slideway (3-1), fuselage fixed case damping sleeve (3-2), fuselage
Fixed case damping travelling arm (3-3), telescopic mast (3-4), damping spring (3-5), sliding panel (3-6), spherical axis pedestal (3-7),
Spherical axis support arm (3-8), support board (3-9), support board spring seat (3-10), loading flat spring (3-11), fuselage clamping
Case (3-12), clamping case sliding sleeve (3-13), clamping housing-case cylinder slideway (3-14), pull ring (3-15), clamping case slide post (3-
16) case slide post limited block (3-17), triangle limited block (3-18), slide post fixed case (3-19), fixture block sleeve (3-, are clamped
20), fixture block (3-21), fixture block slide post (3-22), fixture block spring (3-23), linkage disk (3-24), fixing clamp (3-25), fixation
Folder slideway (3-26), fixing clamp lead screw (3-27), fixing clamp spring (3-28), fixing clamp sliding panel (3-29), fixing clamp are anti-skidding
It pads (3-30), fuselage fixed case (3) is internally provided with fuselage fixed case slideway (3-1), and the interior welds of fixed case (3) are organic
Body fixed case damping sleeve (3-2), the internal slide of fuselage fixed case damping sleeve (3-2) have fuselage fixed case damping travelling arm
(3-3), the upper end of fuselage fixed case damping sleeve (3-2) are welded with telescopic mast (3-4), and the upper end of telescopic mast (3-4) is provided with
The upper end sliding of damping spring (3-5), fuselage fixed case slideway (3-1) has sliding panel (3-6), the lower end weldering of sliding panel (3-6)
It is connected to fuselage fixed case damping travelling arm (3-3), the upper end of sliding panel (3-6) is welded with spherical axis pedestal (3-7), spherical axis base
The inner rotation of seat (3-7) has spherical axis support arm (3-8), and the inner rotation of support board (3-9) has spherical axis support arm (3-
8), the lower end of support board (3-9) is welded with support board spring seat (3-10), the upper end welding of support board spring seat (3-10)
Have loading flat spring (3-11), the upper end of support board (3-9) is welded with fuselage clamping case (3-12), clamps case sliding sleeve (3-
13) be internally provided with clamps housing-case cylinder slideway (3-14), and the upper end of clamping case sliding sleeve (3-13) is welded with pull ring (3-
15) internal slide for, clamping case sliding sleeve (3-13) has clamping case slide post (3-16), clamps the upper of case slide post (3-16)
End is welded with clamping case slide post limited block (3-17), and the lower end of clamping case slide post (3-16) is welded with triangle limited block (3-
18) lower end for, clamping case sliding sleeve (3-13) is welded with slide post fixed case (3-19), and fuselage clamps the inside of case (3-12)
It is welded with slide post fixed case (3-19), the inner rotation of slide post fixed case (3-19) has fixture block sleeve (3-20), fixture block set
The upper end of cylinder (3-20) is welded with fixture block (3-21), and fixture block (3-21) cooperates triangle limited block (3-18) to use, fixture block sleeve (3-
20) internal slide has fixture block slide post (3-22), and the lower end of fixture block sleeve (3-20) is fixed with fixture block spring (3-23), sliding
The inside of column fixed case (3-19) is fixed with fixture block spring (3-23), and the internal slide of fixture block sleeve (3-20) has fixture block slide post
The upper end of (3-22) is hinged with linkage disk (3-24), and the upper end of clamping case sliding sleeve (3-13) is welded with fixing clamp (3-25),
Fixing clamp (3-25) is internally provided with fixing clamp slideway (3-26), and the inner rotation of fixing clamp (3-25) has fixing clamp lead screw
(3-27), the upper end of fixing clamp lead screw (3-27) are provided with fixing clamp spring (3-28), and the upper end of fixing clamp slideway (3-26) is sliding
Dynamic to have fixing clamp sliding panel (3-29), the upper end of fixing clamp sliding panel (3-29) is provided with threaded hole, fixing clamp sliding panel (3-
29) inner rotation of threaded hole has fixing clamp lead screw (3-27), and the upper end of fixing clamp (3-25) is provided with fixing clamp non-slip mat (3-
30)；
The upper end of case lid (4) is provided with case lid slideway (4-1), case lid buckle (4-2), two-way lead screw (4-3), lead screw belt pulley
(4-4), case lid belt (4-5), case lid control cabinet (4-6), case lid control cabinet belt pulley (4-7), case lid rotation axis (4-8), case
Lid fixes sleeve (4-9), case lid spring (4-10), case lid travelling arm (4-11), case lid rotating disc (4-12), case lid fixed pedestal
(4-13), case lid (4) are internally provided with case lid slideway (4-1), and the upper end sliding of case lid slideway (4-1) has case lid to buckle (4-
2), case lid buckles the threaded hole that is internally provided with of (4-2), and the inner rotation of case lid buckle (4-2) threaded hole has two-way lead screw (4-
3), the upper end key connection of two-way lead screw (4-3) has lead screw belt pulley (4-4), and the upper end of lead screw belt pulley (4-4) is provided with case lid
Belt (4-5), the upper end of case lid (4) are welded with case lid control cabinet (4-6), and the inner rotation of case lid control cabinet (4-6) has case lid
The upper end key connection of rotation axis (4-8), case lid rotation axis (4-8) has case lid control cabinet belt pulley (4-7), case lid control cabinet belt
The upper end of wheel (4-7) is provided with case lid belt (4-5), and the lower end of case lid (4) is welded with case lid fixes sleeve (4-9), and case lid is solid
Determine being internally provided with case lid spring (4-10) for sleeve (4-9), the internal slide of case lid fixes sleeve (4-9) has case lid travelling arm
(4-11), the lower end of case lid travelling arm (4-11) are welded with case lid rotating disc (4-12), and the lower end of case lid rotating disc (4-12) turns
It is dynamic to have case lid fixed pedestal (4-13)；
The interior welds of cabinet (1) have wing fixed case (2), and the interior welds of cabinet (1) have fuselage fixed case (3), cabinet (1)
Upper end setting it is fluted, cabinet (1) groove cooperate case lid buckle (4-2) use, the upper end of cabinet (1) is provided with case lid (4).
2. the general storage box of a kind of unmanned plane according to claim 1, it is characterised in that: the wing fixed case (2),
Wing fixed case support arm (2-8), wing fixed case support arm spring seat (2-9), wing fixed case rotating disc (2-10), machine
Wing fixed case fixing bolt (2-11), wing fixed pedestal (2-12) are disposed as two.
3. the general storage box of a kind of unmanned plane according to claim 1, it is characterised in that: the wing fixed case support
Arm (2-8), wing fixed case rotating disc (2-10), wing fixed pedestal (2-12), case lid fixes sleeve (4-9), case lid sliding
Arm (4-11), case lid rotating disc (4-12), case lid fixed pedestal (4-13) concentrically line.
4. the general storage box of a kind of unmanned plane according to claim 1, it is characterised in that: the cabinet (1), wing are solid
Determine case (2), fuselage fixed case (3), case lid (4) material selection stainless steel material.
5. the general storage box of a kind of unmanned plane according to claim 1, it is characterised in that: the fuselage fixed case damping
Sleeve (3-2), fuselage fixed case damping travelling arm (3-3), telescopic mast (3-4), damping spring (3-5) are disposed as two.
6. the general storage box of a kind of unmanned plane according to claim 1, it is characterised in that: the case lid belt (4-5)
Material selection rubber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811359770.XA CN109353658B (en) | 2018-11-15 | 2018-11-15 | General case of depositing of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811359770.XA CN109353658B (en) | 2018-11-15 | 2018-11-15 | General case of depositing of unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN109353658A true CN109353658A (en) | 2019-02-19 |
| CN109353658B CN109353658B (en) | 2020-12-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811359770.XA Active CN109353658B (en) | 2018-11-15 | 2018-11-15 | General case of depositing of unmanned aerial vehicle |
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| CN110155529A (en) * | 2019-05-28 | 2019-08-23 | 张志东 | A kind of multi-functional unmanned plane storage protective device |
| CN110154865A (en) * | 2019-05-30 | 2019-08-23 | 上海比茵沃汽车电子有限公司 | A kind of vehicle-mounted unmanned aerial vehicle recovery bin |
| CN110269356A (en) * | 2019-04-22 | 2019-09-24 | 天津丰威包装制品销售有限公司 | It is a kind of to fix the anti-Portable meal box overturned |
| CN111017382A (en) * | 2019-12-16 | 2020-04-17 | 肖荣辉 | Storage device is deposited to unmanned aerial vehicle |
| CN111977146A (en) * | 2020-08-29 | 2020-11-24 | 北京碳云科技有限公司 | Thing flow box for unmanned aerial vehicle |
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| CN107856960A (en) * | 2017-12-05 | 2018-03-30 | 成都环磊科技有限公司 | A kind of unmanned plane transport case |
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| Publication number | Publication date |
|---|---|
| CN109353658B (en) | 2020-12-22 |
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