CN110040261A - A kind of bracket and unmanned plane handling method of small and medium size unmanned aerial vehicles packed and transported - Google Patents
A kind of bracket and unmanned plane handling method of small and medium size unmanned aerial vehicles packed and transported Download PDFInfo
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- CN110040261A CN110040261A CN201910306374.9A CN201910306374A CN110040261A CN 110040261 A CN110040261 A CN 110040261A CN 201910306374 A CN201910306374 A CN 201910306374A CN 110040261 A CN110040261 A CN 110040261A
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- 238000000034 method Methods 0.000 title claims abstract description 14
- 238000004806 packaging method and process Methods 0.000 claims abstract description 11
- 230000003014 reinforcing effect Effects 0.000 claims description 6
- 238000003466 welding Methods 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 4
- 239000010959 steel Substances 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 230000007935 neutral effect Effects 0.000 claims description 2
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- 230000032258 transport Effects 0.000 abstract description 18
- 230000008569 process Effects 0.000 abstract description 7
- 238000010586 diagram Methods 0.000 description 6
- 238000012856 packing Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 101100334009 Caenorhabditis elegans rib-2 gene Proteins 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
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- 230000007246 mechanism Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The present invention relates to a kind of bracket of small and medium size unmanned aerial vehicles packed and transported and unmanned plane handling methods, the present apparatus dramatically saves packaging space, the unmanned plane quantity that one transport vehicle once transports can be improved from 1 frame to 2 framves and interior space has surplus, surplus space can be used to place other spare parts, improve conevying efficiency.Secondly, transporting unmanned plane with this carrier package, packaging and disassembly process are simple and fast, time saving and energy saving, improve the efficiency of loading and unloading, have further adapted to modern operation and after sale to the requirement of quick dispatch.
Description
Technical field
The invention belongs to the packed and transported field of unmanned plane more particularly to a kind of middle-size and small-size fixed-wing unmanned plane complete machine packagings
The bracket of transport further relates to the quick handling method that unmanned plane is transported with this carrier package.
Background technique
Unmanned plane is important scientific and technological armed forces, main to realize investigation, examine and the functions such as beat, and is chiefly used in military field.Base
In the urgency of its use occasion and function, it is desirable that the packed and transported of unmanned plane saves space as far as possible, improves conevying efficiency, each portion
Part loads and unloads as far as possible fast to save the time, meets quickly rehearsal and flies to require with real.
Current existing unmanned plane packed and transported be by unmanned aerial vehicle body, wing centre section, left and right outer wing, horizontal tail, left and right vertical fin,
For each component such as antenna house respectively with case packing unified entrucking again is packed, a frame unmanned plane at least needs 4 packaging case packings, this
Manner of packing is maximum the disadvantage is that wasting space, a transportation guarantee vehicle can only load a frame unmanned plane, and conevying efficiency is too low；And
The loading, unloading of each packing case and each component of product are torn open too time-consuming, are not adapted to the rehearsal of quick despatch now and real are flown to want
It asks.
For this purpose, there is an urgent need to a kind of unmanned plane packaging scheme of optimization, design a kind of saving space, quick despatch nobody
Machine complete machine component manner of packing improves unmanned plane packed and transported efficiency, realizes quick despatch, meets modernization rehearsal and flight is wanted
It asks.
Summary of the invention
Technical problem solved by the present invention is in order to solve status, the present invention provide a kind of optimization, practical proof it is reliable
Middle-size and small-size fixed-wing unmanned plane packed and transported bracket, realize unmanned plane packed and transported save space, improve efficiency, quick dispatch
Purpose.
The technical scheme is that a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported, including bottom plate,
Supporting fuselage component, fuselage briquetting component, outer wing support component, wing centre section support component, shoe vertical fin support component, horizontal tail support
Component and antenna house support component；Supporting fuselage component, shoe vertical fin support component, horizontal tail support component and antenna house support group
Part is respectively positioned on bottom plate；Outer wing support component is frame space structure, is connected on bottom plate by shaft seat, wing centre section support component
It is connected in outer wing support component with fuselage briquetting component；Supporting fuselage component is used to support fuselage, and fuselage briquetting component is used for
Fuselage is pushed down, outer wing support component is used to support outer wing, and wing centre section support component is used to support wing centre section, and shoe vertical fin support component is used
In support shoe vertical fin, horizontal tail support component is used to support horizontal tail, and antenna house support component is used to support antenna house.
A further technical solution of the present invention is: the supporting fuselage component includes fuselage front support seat and fuselage rear support
Seat, structural type face is respectively one frame of fuselage, the seven frame position faces Chu Xing, and the two is fixed on the axis line position of bottom plate, longitudinal direction
Distance is one frame of fuselage to seven frame distances.
A further technical solution of the present invention is: the outer wing braced frame is Al pipe butt welding overall structure, by welding in length and breadth
8 aluminum pipes composition even, defining course after unmanned plane is placed is X-direction, direction vertical with X-direction and parallel with tray plate
For Y-direction, the direction vertical with X-direction, Y-direction is Z-direction, and the outer wing braced frame shaft on the axle bed i.e. X-direction that rotates is revolved
Turn, it, can be in Plane Rotation ± 90 ° YZ in the case where no shelter.It is equipped with U-shaped protrusion on the outside of frame, is used to support outer wing；
U-shaped briquetting is equipped on the inside of frame, for pushing down fuselage.
A further technical solution of the present invention is: the horizontal tail support component includes horizontal tail forward support block, horizontal tail rear support
Block, horizontal tail block are located between two supporting fuselage seats, and fore-and-aft distance is arranged according to horizontal tail length.
A further technical solution of the present invention is: the shoe vertical fin support component is U-shaped part, U-shaped type face is shoe
Vertical fin corresponding position type face after placing, is fixed by shoe vertical fin bandage；Including forward support block, middle supporting block is rear to prop up
Bracer is arranged at the neutral gear of tray plate according to shoe vertical fin length.Shoe vertical fin support component is U-shaped part, U-shaped type face
For shoe vertical fin corresponding position type face, after placing, it is fixed by shoe vertical fin bandage
A further technical solution of the present invention is: the antenna house support component includes three antenna house supporting blocks, according to
Antenna house shape is circumferentially distributed in bracket front fuselage side.
A further technical solution of the present invention is: several hollow holes are provided on the bottom plate, so that weight saving, convenient for support
Fortune；Further include reinforcing rib, positioned at the lower section of tray plate, is welded by 7 steel pipes in length and breadth and bracket, improve bracket rigidity.
A further technical solution of the present invention is: the antenna house support component is three pieces of plate-like pieces, it is provided with and engraves in plate face
Empty through-hole, three pieces of plate-like pieces are put as tripod-shaped, and plate face is mutually vertical with bottom plate；The side of three pieces of plate-like pieces is connected in bottom
On plate, antenna house is located on another side of three plate-like pieces, and other side sideband is cambered, mutually pastes with antenna house bottom surface
It closes；After placing, it is fixed by antenna house bandage.
A further technical solution of the present invention is: the wing centre section support component be two U-shaped supporting blocks, U-shaped type face with
Wooden fuselage briquetting is glued in the fitting of wing centre section corresponding position, its underpart, and fuselage briquetting is U-shaped part, U-shaped type face position corresponding with fuselage
Set fitting.
A further technical solution of the present invention is: a kind of unmanned plane handling method, which is characterized in that packaging unmanned plane complete machine
The following steps are included:
Step 1: horizontal tail is placed；Entire bracket is placed in ground, removes bolt, two wing centre section supporting blocks is taken out, by outer wing
Support component is rotated outward to ground is placed, and is placed horizontal tail in horizontal tail supporting block, is tightened with horizontal tail bandage；
Step 2: shoe vertical fin is placed；Left and right shoe vertical fin is placed respectively in shoe vertical fin supporting block, is hung down with shoe
Tail bandage tightens；
Step 3: fuselage is placed；Lifting fuselage is placed on supporting fuselage seat, supporting block type face and corresponding fuselage type face paste
It closes, fuselage front fulcrum is stuck in fuselage forward support block card slot；
Step 4: outer wing is placed；It outer wing braced frame is rotated into the fuselage briquetting to frame pushes down fuselage and correspond to type face,
Left and right outer wing is placed respectively in outer wing supporting block；
Step 5: wing centre section is placed；Forward and backward wing centre section supporting block is stuck in corresponding detent angled seat, will be propped up with bolt
Bracer is connected firmly with angled seat, and supporting block lower fuselage briquetting pushes down the fuselage of corresponding position, places wing centre section in wing centre section supporting block
On；
Step 6: wing tightener tightening.Wing tightener one end is hooked on the tightener hook base of side, tightening
Device bandage passes through the left outside wing-wing centre section-starboard outboard, and the other end is hooked on corresponding other side hook base, adjusts tightener
Ratchet tightens outer wing and wing centre section；
Step 7: antenna house is placed；It places antenna to cover in antenna house supporting block, be tightened with antenna house bandage；
Dismantle unmanned plane when the following steps are included:
Step 1: disassembly antenna house；It dismantles fastening screw of the bracket on transport vehicle, ceiling mount bracket is put to ground, is unclamped
Antenna house bandage takes out antenna house；
Step 2: wing tightener is torn open；Two wing tightener one end hooks are taken out respectively, unclamp wing tightener；
Step 3: disassembly wing centre section；After dismantling wing tightener, wing centre section is taken out, wing centre section supporting block and detent angle are then removed
The connection bolt of seat, removes forward and backward wing centre section supporting block；
Step 4: disassembly outer wing；Left and right outer wing is taken out respectively, then rotates left and right outer wing braced frame respectively to placement
Ground；
Step 5: disassembly fuselage；Fuselage upper holder block is all removed at this time, hangs out fuselage；
Step 6: disassembly shoe vertical fin；The bandage on left and right shoe vertical fin is unclamped respectively, takes out left and right shoe vertical fin；
Step 7: disassembly horizontal tail；The bandage in horizontal tail is unclamped, horizontal tail is taken out.
Invention effect
The technical effects of the invention are that: firstly, with the fixed-wing unmanned plane of the nearly 8m of this carrier package span, it can be by whole frame
The Package size of unmanned plane controls within the scope of 3600 (length) × 1100 (width) × 1100 (height) mm, and it is empty to dramatically save packaging
Between, the unmanned plane quantity that a transport vehicle once transports can be improved from 1 frame to 2 framves and interior space has surplus, surplus space
It can be used to place other spare parts, improve conevying efficiency.Secondly, transporting unmanned plane, packaging and disassembly process with this carrier package
It is simple and fast, it is time saving and energy saving, the efficiency of loading and unloading is improved, modern operation has further been adapted to and quick dispatch is wanted after sale
It asks.
Detailed description of the invention
Fig. 1 is the carrier structure schematic diagram of the middle-size and small-size fixed-wing unmanned plane complete machine of packed and transported；
Fig. 2 is the schematic diagram of the one frame fixed-wing unmanned plane of carrier package shown in Fig. 1；
Fig. 3 is wing braced frame schematic diagram；
Fig. 4 is shoe vertical fin aft support block schematic diagram；
Fig. 5 is wing centre section supporting block schematic diagram；
Fig. 6 is bottom plate and reinforcing rib schematic diagram；
Description of symbols: 1- tray plate, 2- tray plate reinforcing rib, 3- fuselage front support seat, 4- fuselage rear support
Seat, briquetting before 5- fuselage, briquetting after 6- fuselage, briquetting before 7- waist, briquetting after 8- waist, 9- outer wing support frame
Frame, 10- outer wing braced frame shaft seat, 11- outer wing root leading edge supporting block, 12- outer wing root trailing edge supporting block, 13- outer wing
Tip leading edge supporting block, 14- outer wing tip rear edge support block, 15- outer wing block, 16- wing centre section forward support block prop up after 17- wing centre section
Bracer, 18- wing centre section supporting block detent angled seat, 19- shoe vertical fin forward support block, supporting block in 20- shoe vertical fin, 21- shoe hang down
Tail aft support block, 22- horizontal tail forward support block, 23- horizontal tail aft support block, 24- horizontal tail block, 25- antenna house supporting block, 26- machine
Wing tightener, 27- wing tightener hook base, 28- shoe vertical fin bandage, 29-U type bolt, 30- horizontal tail bandage, 31- antenna house
Bandage, 32- lifting hanging ring, 33- bracket and transport vehicle shelter connecting screw hole.
Specific embodiment
Referring to Fig. 1-Fig. 6, a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported, including bracket base group
Part, supporting fuselage component, fuselage briquetting component, (including middle outer wing, outer wing are integrally connected shape both when packed and transported to outer wing
State) support component, wing centre section support component, shoe vertical fin support component, horizontal tail support component, antenna house support component, tightener
Component etc..
Bracket base component includes tray plate and bottom reinforcement, and tray plate is 4mm steel plate, thereon inoperative position
Utmostly mitigate, to reduce bracket overall weight.Bottom reinforcement is square steel finished parts, and bottom plate and reinforcing rib are soldered to one
Body.
Supporting fuselage component includes fuselage front support seat and fuselage rear support.Front support seat and rear support type face difference
With one frame position of fuselage, seven frame position topographies, there is the card slot for blocking aircraft front fulcrum on front support seat, to limit transport
The freedom degree that process middle fuselage is moved forward and backward.Fuselage back and front supporting seat is placed in the middle to pacify on the basis of tray plate longitudinal centre line
Row, is bolted on tray plate.It should be noted that herein forward and backward is to be along vector after being placed with fuselage
Before, after being on the contrary, similarly hereinafter.
Fuselage briquetting component includes the forward and backward briquetting of fuselage and the forward and backward briquetting of waist, the forward and backward briquetting spiral shell of fuselage
It tethers and connects in outer wing braced frame, on the one hand push down fuselage corresponding position type face, limitation transportational process fuselage up and down direction is altered
Dynamic freedom degree, on the other hand plays a transition role, and outer wing braced frame is enable to draw close on fuselage, by outer wing support component and
Fuselage collapses.Similarly, the forward and backward briquetting of waist is glued to below wing centre section supporting block, collapses wing centre section supporting block and fuselage.
Outer wing support component is left and right symmetrical member, is distributed in fuselage two sides.Every side outer wing support component includes outer wing branch
Support frame frame, outer wing braced frame shaft seat, outer wing root, tip, front and rear edges totally four supporting blocks and outer wing block.Outer wing branch
Support frame frame is aluminium pipe welding structure；Frame is connect by the shaft on shaft seat with shaft seat, and frame can the inside, outward turning along shaft
Turn, shaft seat is bolted on tray plate, and four supporting blocks and block are bolted on frame.It needs
It is bright, herein inside and outside be be close to bracket longitudinal centre line it is interior, it is opposite be it is outer, similarly hereinafter.
Wing centre section support component includes wing centre section back and front supporting block and wing centre section supporting block detent angled seat, supporting block type face and wing centre section
Corresponding position type face paste is closed, and supporting block both ends have the Y-piece by tightener bandage, and Y-piece can prevent in transportational process
Belt tensioner is moved forward and backward, close to the shoe connector on wing centre section when passing through wing centre section due to belt tensioner, to prevent transportational process again
The mobile freedom degree of wing centre section front-rear direction.By two angled seat detents when wing centre section supporting block is installed, then it is connected with, detent angle
Seat is welded to connect in outer wing braced frame.
Shoe vertical fin support component is left and right symmetrical member, and three supporting blocks, are used to support shoe before, during and after respectively including
Vertical fin, three supporting blocks are bolted on tray plate.
Horizontal tail support component includes former and later two horizontal tail supporting blocks and former and later two horizontal tail blocks, and supporting block is used to support
Horizontal tail, block are used to limit the mobile freedom degree of horizontal tail front-rear direction.Supporting block and block are bolted to tray plate
On.
Antenna house support component includes three antenna house supporting blocks, and three supporting blocks are circumferential on the basis of antenna house center
Uniformly support antenna house.Supporting block is bolted on tray plate.
Tightening device assembly includes wing tightening device assembly, shoe vertical fin tightening component, horizontal tail bandage, antenna house bandage.Machine
It includes wing tightener and wing tightener hook base that the wing, which tightens device assembly, and wing tightener hook base is bolted to bracket
On bottom plate, tightener two ends of the hook is hooked on hook base, and the belt tensioner of tightener will be outer by the left outside wing-wing centre section-starboard outboard
The wing, wing centre section, fuselage are integrally tightened, and product play in transportational process is prevented.Shoe vertical fin tightening component includes shoe vertical fin bandage
And U-bolt, U-bolt are bolted on tray plate, bandage both ends lie in tightening shoe vertical fin on U-bolt.Horizontal tail bandage
Both ends are lain on handle designed by horizontal tail supporting block, and antenna house bandage is tied up on the footstalk designed by antenna house supporting block.
Wherein it should be noted that wing tightener is the finished parts that can be bought on the market, buy above just with
Retaining mechanism；Other bandages are also the common belt tensioner that can be bought on the market, and shoe vertical fin bandage both ends are tied up in U-shaped spiral shell
On bolt, horizontal tail bandage both ends are lain on handle designed by horizontal tail supporting block, and antenna house bandage is tied up set by the antenna house supporting block
On the footstalk of meter.There are four U-shaped supporting blocks in wing braced frame, are used to support outer wing, U-shaped type face and outer wing corresponding position
Type face paste is closed.
Using this carrier package UAV Components, specific step is as follows:
Step 1: horizontal tail is placed.Entire bracket is placed in ground, removes the connection spiral shell of wing centre section supporting block and detent angled seat
Bolt takes out two wing centre section supporting blocks, outer wing support component is rotated outward to ground is placed, and places horizontal tail in horizontal tail supporting block
On, it is tightened with horizontal tail bandage.
Step 2: shoe vertical fin is placed.Left and right shoe vertical fin is placed respectively in shoe vertical fin supporting block, is hung down with shoe
Tail bandage tightens.
Step 3: fuselage is placed.Lifting fuselage is placed on supporting fuselage seat, supporting block type face and corresponding fuselage type face paste
It closes, fuselage front fulcrum is stuck in fuselage forward support block card slot.
Step 4: outer wing is placed.It outer wing braced frame is rotated into the fuselage briquetting to frame pushes down fuselage and correspond to type face,
Left and right outer wing is placed respectively in outer wing supporting block.
Step 5: wing centre section is placed.Forward and backward wing centre section supporting block is stuck in corresponding detent angled seat, will be propped up with bolt
Bracer is connected firmly with angled seat, and supporting block lower fuselage briquetting pushes down the fuselage of corresponding position, places wing centre section in wing centre section supporting block
On.
Step 6: wing tightener tightening.Wing tightener one end is hooked on the tightener hook base of side, tightening
Device bandage passes through the left outside wing-wing centre section-starboard outboard, and the other end is hooked on corresponding other side hook base, adjusts tightener
Ratchet tightens outer wing and wing centre section.
Step 7: antenna house is placed.It places antenna to cover in antenna house supporting block, be tightened with antenna house bandage.
By above step, the packaging of unmanned plane complete machine is completed.Entire bracket is lifted again to be placed in transport vehicle shelter, is used
Bracket and transport vehicle shelter are connected firmly by bolt, then achievable all vanning work, starts to transport.
Using this bracket disassembly each component of unmanned plane, specific step is as follows:
Step 1: disassembly antenna house.It dismantles fastening screw of the bracket on transport vehicle, ceiling mount bracket is put to ground, is unclamped
Antenna house bandage takes out antenna house.
Step 2: wing tightener is torn open.Two wing tightener one end hooks are taken out respectively, unclamp wing tightener.
Step 3: disassembly wing centre section.After dismantling wing tightener, wing centre section is taken out, wing centre section supporting block and detent angle are then removed
The connection bolt of seat, removes forward and backward wing centre section supporting block.
Step 4: disassembly outer wing.Left and right outer wing is taken out respectively, then rotates outward left and right outer wing braced frame respectively extremely
Place ground.
Step 5: disassembly fuselage.Fuselage upper holder block is all removed at this time, hangs out fuselage.
Step 6: disassembly shoe vertical fin.The bandage on left and right shoe vertical fin is unclamped respectively, takes out left and right shoe vertical fin.
Step 7: disassembly horizontal tail.The bandage in horizontal tail is unclamped, horizontal tail is taken out.
It by above step, completes UAV Components and is dismantled from bracket, and then carry out UAV Components connection dress on ground
Match, bracket is restored to the original state, to transport of casing next time.
Further, the tray plate reinforcing rib 2 and tray plate 1 are welded to connect.Fuselage front support 3 and fuselage
Rear support 4 is bolted on tray plate 1.Briquetting 6 is bolted to outer wing support frame after briquetting 5 and fuselage before fuselage
On frame 9.Before waist after briquetting 7 and waist briquetting 8 be glued respectively be connected to wing centre section forward support block 16 and wing centre section after prop up
The lower section of bracer 17.Outer wing braced frame 9 is Al pipe butt welding frame structure, and outer wing braced frame shaft seat 10 is bolted to
On tray plate 1, shaft of the outer wing braced frame 9 on outer wing braced frame shaft seat 13 realizes rotation.Each supporting block of outer wing
11-14 and outer wing block 15 are bolted in outer wing braced frame 9.Wing centre section forward support block 16 and wing centre section aft support block 17
It is bolted in wing centre section supporting block detent angled seat 18, wing centre section supporting block detent angled seat 18 is welded to connect in outer wing braced frame
On 9.Shoe vertical fin supporting block 19-21, horizontal tail supporting block and block 22-24, day lower cover supporting block 25 are bolted to hold in the palm
On frame bottom plate 1.26 two ends of the hook of wing tightener is hooked on the pivot pin of wing tightener hook base 27, shoe vertical fin bandage 28
It is tightened by U-bolt 29, horizontal tail bandage 30 directly tightens on the handle designed by horizontal tail supporting block 22,23, and antenna house is tied up
It is directly tied up on the footstalk designed by antenna house supporting block 25 with 31.
Using the middle-size and small-size fixed-wing unmanned plane of carrier package shown in Fig. 1, specific step is as follows as shown in Figure 2:
Step 1: horizontal tail is placed.Bracket is placed in ground, wing centre section back and front supporting of dismantling block 16,17 and wing centre section supporting block card
The connection bolt of parallactic angle seat 18 removes wing centre section back and front supporting block 16 and 17, and outer wing braced frame 9 is turned along outer wing braced frame
The shaft of axle bed 10 is rotated outward to ground is placed, and places horizontal tail in horizontal tail supporting block 22 and 23, horizontal tail front and back is by horizontal tail
Baffle 24 limits, and is tightened with horizontal tail bandage 30.
Step 2: shoe vertical fin is placed.Left and right shoe vertical fin is placed respectively in shoe vertical fin supporting block 19,20,21,
It is tightened with shoe vertical fin bandage 28 by U-bolt 29.
Step 3: fuselage is placed.Lifting fuselage is placed on fuselage back and front supporting seat 3,4, supporting block type face and fuselage pair
Type face paste is answered to close, fuselage front fulcrum is stuck in 3 card slot of fuselage front support seat.
Step 4: outer wing is placed.Shaft by outer wing braced frame 9 along outer wing braced frame shaft seat 10 rotates inwardly
The forward and backward briquetting 5,6 of the fuselage connected on to frame pushes down fuselage corresponding position type face, places left and right outer wing respectively in outer wing branch
On bracer 11-14, airfoil root is limited by outer wing block 15.
Step 5: wing centre section is placed.Forward and backward wing centre section supporting block 16,17 is stuck in corresponding detent angled seat 18, spiral shell is used
Supporting block and angled seat are connected firmly by bolt, and forward and backward briquetting 7,8 pushes down fuselage corresponding position type face in the middle part of supporting block lower fuselage,
Wing centre section is placed on wing centre section back and front supporting block 16,17.
Step 6: wing tightener tightening.26 one end of wing tightener is hooked on side tightener hook base 27,
Tightener is hooked on the tightener hook base of the other side by the left outside wing-wing centre section-starboard outboard, the other end, adjusts tightener
Ratchet tightens outer wing and wing centre section.
Step 7: antenna house is placed.It places antenna to cover in antenna house supporting block 25, be tightened with antenna house bandage 31.
By above step, the packaging of this fixed-wing unmanned plane complete machine is completed.Entire support is lifted by lifting hanging ring 32 again
Frame is placed in transport vehicle shelter, and bracket is connect fastening with transport vehicle shelter by bolt hole 33 with bolt, then achievable complete
Portion's vanning work, starts to transport.
Using this bracket disassembly UAV Components, specific step is as follows:
Step 1: disassembly antenna house.It dismantles fastening screw of the bracket on transport vehicle, ceiling mount bracket is put to ground, is unclamped
Antenna house bandage 31 takes out antenna house.
Step 2: wing tightener is torn open.It dismantles respectively two 26 one end of wing tightener hook, unclamps wing tightener.
Step 3: disassembly wing centre section.After dismantling wing tightener, wing centre section, wing centre section supporting block of then dismantling 16,17 and branch are taken out
The connection bolt of bracer detent angled seat 18 removes wing centre section supporting block 16,17.
Step 4: disassembly outer wing.Left and right outer wing is taken out respectively, then rotates outward left and right outer wing braced frame 9 respectively
To placement ground.
Step 5: disassembly fuselage.Each briquetting is all removed with wing centre section supporting block and outer wing braced frame on fuselage at this time,
Hang out fuselage.
Step 6: disassembly shoe vertical fin.The bandage 28 on left and right shoe vertical fin is unclamped respectively, is taken out left and right shoe and is hung down
Tail.
Step 7: disassembly horizontal tail.The bandage 30 in horizontal tail is unclamped, horizontal tail is taken out.
It by above step, completes this UAV Components and is taken out from bracket, and then carry out UAV Components connection on ground
Assembly, bracket is restored to the original state, to transport of casing next time.
Claims (10)
1. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported, which is characterized in that including bottom plate (1), fuselage branch
Support component, fuselage briquetting component, outer wing support component, wing centre section support component, shoe vertical fin support component, horizontal tail support component and
Antenna house support component；Supporting fuselage component, shoe vertical fin support component, horizontal tail support component and the equal position of antenna house support component
In on bottom plate；Outer wing support component is frame space structure, is connected on bottom plate by shaft seat, wing centre section support component and fuselage
Briquetting component is connected in outer wing support component；Supporting fuselage component is used to support fuselage, and fuselage briquetting component is for pushing down machine
Body, outer wing support component are used to support outer wing, and wing centre section support component is used to support wing centre section, and shoe vertical fin support component is used to support
Shoe vertical fin, horizontal tail support component are used to support horizontal tail, and antenna house support component is used to support antenna house.
2. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
Stating supporting fuselage component includes fuselage front support seat (3) and fuselage rear support (4), structural type face be respectively one frame of fuselage,
The seven frame positions face Chu Xing, the two are fixed on the axis line position of bottom plate (1), and fore-and-aft distance is one frame of fuselage to seven frame distances.
3. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
Stating outer wing braced frame is Al pipe butt welding overall structure, is made of 8 aluminum pipes of the company of weldering in length and breadth, and course after unmanned plane is placed is defined
For X-direction, direction vertical with X-direction and parallel with tray plate is Y-direction, and the direction vertical with X-direction, Y-direction is the side Z
To outer wing braced frame rotates the i.e. X-direction rotation of the shaft on axle bed can be in YZ plane turn in the case where no shelter
It is ± 90 ° dynamic.It is equipped with U-shaped protrusion on the outside of frame, is used to support outer wing；U-shaped briquetting is equipped on the inside of frame, for pushing down fuselage.
4. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
Stating horizontal tail support component includes horizontal tail forward support block (22), horizontal tail aft support block (23), horizontal tail block (24), positioned at two machines
Between body support base, fore-and-aft distance is arranged according to horizontal tail length.
5. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
Stating shoe vertical fin support component is U-shaped part, and U-shaped type face is shoe vertical fin corresponding position type face, after placing, is hung down by shoe
Tail bandage is fixed；Including forward support block (19), middle supporting block (20), aft support block (21), according to shoe vertical fin length cloth
It is placed at the neutral gear of tray plate.Shoe vertical fin support component is U-shaped part, and U-shaped type face is shoe vertical fin corresponding position type face,
After placing, it is fixed by shoe vertical fin bandage.
6. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
Stating antenna house support component includes three antenna house supporting blocks (25), is circumferentially distributed in bracket front fuselage according to antenna house shape
Side.
7. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
It states and is provided with several hollow holes on bottom plate (1), so that weight saving, convenient for delivery；It further include reinforcing rib, under tray plate
Side is welded by 7 steel pipes in length and breadth and bracket, improves bracket rigidity.
8. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
Stating antenna house support component is three pieces of plate-like pieces, is provided with hollow out through-hole in plate face, and three pieces of plate-like pieces are put as tripod-shaped, and plate
Face and bottom plate (1) are mutually vertical；The side of three pieces of plate-like pieces is connected on bottom plate (1), and antenna house is located at the another of three plate-like pieces
In a side, and other side sideband is cambered, is bonded to each other with antenna house bottom surface；After placing, carried out by antenna house bandage
It is fixed.
9. a kind of bracket of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported as described in claim 1, which is characterized in that institute
Stating wing centre section support component is two U-shaped supporting blocks, and U-shaped type face is bonded with wing centre section corresponding position, and wooden fuselage is glued in its underpart
Briquetting, fuselage briquetting are U-shaped part, and U-shaped type face is bonded with fuselage corresponding position.
10. based on a kind of unmanned plane handling of middle-size and small-size fixed-wing unmanned plane complete machine packed and transported bracket described in claim 1
Method, which is characterized in that packaging unmanned plane complete machine the following steps are included:
Step 1: horizontal tail is placed；Entire bracket is placed in ground, removes bolt, takes out two wing centre section supporting blocks, outer wing is supported
Component is rotated outward to ground is placed, and is placed horizontal tail in horizontal tail supporting block, is tightened with horizontal tail bandage；
Step 2: shoe vertical fin is placed；Left and right shoe vertical fin is placed respectively in shoe vertical fin supporting block, is tied up with shoe vertical fin
Band tightens；
Step 3: fuselage is placed；Lifting fuselage is placed on supporting fuselage seat, and supporting block type face and corresponding fuselage type face paste are closed,
Fuselage front fulcrum is stuck in fuselage forward support block card slot；
Step 4: outer wing is placed；It outer wing braced frame is rotated into the fuselage briquetting to frame pushes down fuselage and correspond to type face, respectively
Left and right outer wing is placed in outer wing supporting block；
Step 5: wing centre section is placed；Forward and backward wing centre section supporting block is stuck in corresponding detent angled seat, with bolt by supporting block
It is connected firmly with angled seat, supporting block lower fuselage briquetting pushes down the fuselage of corresponding position, places wing centre section in wing centre section supporting block；
Step 6: wing tightener tightening.Wing tightener one end is hooked on the tightener hook base of side, and tightener is taut
Band passes through the left outside wing-wing centre section-starboard outboard, and the other end is hooked on corresponding other side hook base, adjusts tightener ratchet,
Tighten outer wing and wing centre section；
Step 7: antenna house is placed；It places antenna to cover in antenna house supporting block, be tightened with antenna house bandage；
Dismantle unmanned plane when the following steps are included:
Step 1: disassembly antenna house；It dismantles fastening screw of the bracket on transport vehicle, ceiling mount bracket is put to ground, and antenna is unclamped
Cover bandage takes out antenna house；
Step 2: wing tightener is torn open；Two wing tightener one end hooks are taken out respectively, unclamp wing tightener；
Step 3: disassembly wing centre section；After dismantling wing tightener, wing centre section is taken out, then removes wing centre section supporting block and detent angled seat
Bolt is connected, forward and backward wing centre section supporting block is removed；
Step 4: disassembly outer wing；Left and right outer wing is taken out respectively, then rotates left and right outer wing braced frame respectively to placing ground
Face；
Step 5: disassembly fuselage；Fuselage upper holder block is all removed at this time, hangs out fuselage；
Step 6: disassembly shoe vertical fin；The bandage on left and right shoe vertical fin is unclamped respectively, takes out left and right shoe vertical fin；
Step 7: disassembly horizontal tail；The bandage in horizontal tail is unclamped, horizontal tail is taken out.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910306374.9A CN110040261B (en) | 2019-04-17 | 2019-04-17 | Bracket for packaging and transporting small and medium unmanned aerial vehicle and unmanned aerial vehicle loading and unloading method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910306374.9A CN110040261B (en) | 2019-04-17 | 2019-04-17 | Bracket for packaging and transporting small and medium unmanned aerial vehicle and unmanned aerial vehicle loading and unloading method |
Publications (2)
| Publication Number | Publication Date |
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| CN110040261A true CN110040261A (en) | 2019-07-23 |
| CN110040261B CN110040261B (en) | 2024-04-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910306374.9A Active CN110040261B (en) | 2019-04-17 | 2019-04-17 | Bracket for packaging and transporting small and medium unmanned aerial vehicle and unmanned aerial vehicle loading and unloading method |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110816951A (en) * | 2019-09-30 | 2020-02-21 | 中航成飞民用飞机有限责任公司 | Transportation mechanism for packaging and dispatching aircraft parts and method for packaging and dispatching aircraft parts |
| CN110979727A (en) * | 2019-12-09 | 2020-04-10 | 中航沈飞民用飞机有限责任公司 | Aircraft tail cone transportation bracket |
| CN112606754A (en) * | 2020-12-14 | 2021-04-06 | 石家庄飞机工业有限责任公司 | Road transport aircraft device |
| CN113978909A (en) * | 2021-12-30 | 2022-01-28 | 四川腾盾科技有限公司 | Large unmanned aerial vehicle transportation fixing device and sedan type constraint method |
| CN114955172A (en) * | 2022-06-17 | 2022-08-30 | 四川腾盾科技有限公司 | Medium-large double-engine unmanned aerial vehicle integrated packaging and transporting equipment |
| CN115123683A (en) * | 2022-06-17 | 2022-09-30 | 四川腾盾科技有限公司 | Universal self-loading and self-unloading type packaging and transporting system and method for medium and large unmanned aerial vehicles |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882941A (en) * | 2014-12-31 | 2016-08-24 | 航天神舟飞行器有限公司 | Rapid connector for vertical tail and horizontal tail of small portable unmanned aerial vehicle |
| KR20170072069A (en) * | 2015-12-16 | 2017-06-26 | 주식회사 샘코 | Multi-purpose hybrid VTOL UAV with a detachable wings |
| CN108502206A (en) * | 2018-03-16 | 2018-09-07 | 中国航天空气动力技术研究院 | A kind of multipurpose double-layer unmanned aerial vehicle body pallet for transporting |
| CN108891618A (en) * | 2018-07-06 | 2018-11-27 | 西安爱生技术集团公司 | A kind of quick dispatch mechanism of unmanned plane antenna house |
| CN109264018A (en) * | 2018-09-10 | 2019-01-25 | 西安爱生技术集团公司 | A kind of compact storage and transportation unmanned plane fast assembling disassembling structure layout |
| CN109552595A (en) * | 2018-12-24 | 2019-04-02 | 西安爱生技术集团公司 | A kind of the quick dispatch mechanism and quick dispatch method of unmanned plane hatchcover |
| CN109572984A (en) * | 2018-11-02 | 2019-04-05 | 海空天科技股份有限公司 | A kind of fast assembly and disassembly mechanism of unmanned plane |
| CN210028546U (en) * | 2019-04-17 | 2020-02-07 | 西安爱生技术集团公司 | Bracket for whole-machine packaging and transportation of small and medium-sized fixed-wing unmanned aerial vehicle |
-
2019
- 2019-04-17 CN CN201910306374.9A patent/CN110040261B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882941A (en) * | 2014-12-31 | 2016-08-24 | 航天神舟飞行器有限公司 | Rapid connector for vertical tail and horizontal tail of small portable unmanned aerial vehicle |
| KR20170072069A (en) * | 2015-12-16 | 2017-06-26 | 주식회사 샘코 | Multi-purpose hybrid VTOL UAV with a detachable wings |
| CN108502206A (en) * | 2018-03-16 | 2018-09-07 | 中国航天空气动力技术研究院 | A kind of multipurpose double-layer unmanned aerial vehicle body pallet for transporting |
| CN108891618A (en) * | 2018-07-06 | 2018-11-27 | 西安爱生技术集团公司 | A kind of quick dispatch mechanism of unmanned plane antenna house |
| CN109264018A (en) * | 2018-09-10 | 2019-01-25 | 西安爱生技术集团公司 | A kind of compact storage and transportation unmanned plane fast assembling disassembling structure layout |
| CN109572984A (en) * | 2018-11-02 | 2019-04-05 | 海空天科技股份有限公司 | A kind of fast assembly and disassembly mechanism of unmanned plane |
| CN109552595A (en) * | 2018-12-24 | 2019-04-02 | 西安爱生技术集团公司 | A kind of the quick dispatch mechanism and quick dispatch method of unmanned plane hatchcover |
| CN210028546U (en) * | 2019-04-17 | 2020-02-07 | 西安爱生技术集团公司 | Bracket for whole-machine packaging and transportation of small and medium-sized fixed-wing unmanned aerial vehicle |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110816951A (en) * | 2019-09-30 | 2020-02-21 | 中航成飞民用飞机有限责任公司 | Transportation mechanism for packaging and dispatching aircraft parts and method for packaging and dispatching aircraft parts |
| CN110816951B (en) * | 2019-09-30 | 2022-07-12 | 中航成飞民用飞机有限责任公司 | Transportation mechanism for packaging and dispatching aircraft parts and method for packaging and dispatching aircraft parts |
| CN110979727A (en) * | 2019-12-09 | 2020-04-10 | 中航沈飞民用飞机有限责任公司 | Aircraft tail cone transportation bracket |
| CN112606754A (en) * | 2020-12-14 | 2021-04-06 | 石家庄飞机工业有限责任公司 | Road transport aircraft device |
| CN113978909A (en) * | 2021-12-30 | 2022-01-28 | 四川腾盾科技有限公司 | Large unmanned aerial vehicle transportation fixing device and sedan type constraint method |
| CN114955172A (en) * | 2022-06-17 | 2022-08-30 | 四川腾盾科技有限公司 | Medium-large double-engine unmanned aerial vehicle integrated packaging and transporting equipment |
| CN115123683A (en) * | 2022-06-17 | 2022-09-30 | 四川腾盾科技有限公司 | Universal self-loading and self-unloading type packaging and transporting system and method for medium and large unmanned aerial vehicles |
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