CN207697983U - A kind of shipping unmanned aerial vehicle body structure - Google Patents

Abstract

The utility model discloses a kind of shipping unmanned aerial vehicle body structure, which includes the head hatch door or tail hatch door or fuselage side wall cabin door structure and corresponding mechanism of fuselage cargo hold.Head hatch door and tail hatch door assist being opened and closed in many ways by electric servomechanism or man-operated mechanism.The insulation construction that the inside installation of fuselage cargo hold can be made with thermal insulation material, the shipping environment of refrigeration or heating can be provided using special equipment, the auxiliary mobile mechanism of power saving moving is devised to fuselage cargo deck.The utility model provides the easy access that suitable cargo passes in and out fuselage cargo hold for shipping unmanned aerial vehicle automated handling, provides heat preservation shipping environment for short-distance cold fresh goods object, improves efficiency for shipping unmanned plane, extend the source of goods, promote value.

Description

A kind of shipping unmanned aerial vehicle body structure

Technical field

The utility model is related to aircraft and shipping fields, especially automate air-cargo system.

Background technology

The development and application of shipping unmanned plane are in the exploratory stage at present.The unmanned plane designed dedicated for shipping is also In starting, the problem of being entangled with the most is how to reduce airfreight cost.A kind of visible selection is to use UAV system It substitutes manned aircraft and reduces buying or the cost of manufacture of unmanned plane equipment.The selection that another kind mays be seen indistinctly is to pass through object Stream link entirety business circuit and link reduce cost, for how to realize molding scheme not yet.

Utility model content

The purpose of this utility model, which is logistics links, integrally reduces cost, proposes a kind of shipping unmanned plane in handling goods Link helps to improve the solution of efficiency.

The technical solution of the utility model is as follows：

A kind of shipping unmanned aerial vehicle body construction design method of the utility model is such, design a kind of head hatch door or Tail hatch door, and design fuselage side wall hatch door, constitute the airframe structure that may be selected to be custom made with one or more hatch doors；In fuselage Cargo hold inner wall designs insulation construction, and insulation airframe structure is provided for cargo hold.

Further, it in the Front-end Design head hatch door of airframe structure, is provided from fuselage axial forward end for cargo and passes in and out machine Body cargo hold can standard-sized sheet cabin door structure, including concordant hinge type, half cover hinge type, mobile model.

Further, tail hatch door is designed in the tail end of airframe structure, is provided from fuselage axial rearward end for cargo and passes in and out machine Body cargo hold can standard-sized sheet cabin door structure；Including upper and lower hinge type, bilateral hinge type.

Further, it in the sidewall design fuselage side wall hatch door of airframe structure, is provided from fuselage side wall for cargo and passes in and out machine The cabin door structure of body cargo hold；Include the knot of univalve door, bivalve door, hanging ladder door, upward-acting door and layout in fuselage unilateral side or both sides Configuration formula.

Further, selection designs head hatch door or tail hatch door or fuselage side according to requirements on airframe structure The topology layout of wall hatch door；The unlocking and locking of these hatch doors on airframe structure, using mechanical lock or electronic lock, wherein electronics The unlocking and blocking order of lock are generated by wireless remote control or on-site manual by compressing switch；The design side on the floor of airframe structure Just the low cost of goods movement assists mobile hard slippery surface texture and bedding above removably non-slip mat structure；On ground Plate upper edge fuselage axis can design semi-buried installation and cover the independent transmission mechanism mechanically or electrically moved more；In fuselage cargo compartment knot Respective design fixation cargo location is tethered at mechanism and structure and lighting apparatus on structure.

Further, insulation construction is designed in the inner structural wall of fuselage cargo compartment, and enhancing is constituted using special equipment Refrigeration or heating heat preservation cargo hold, and ventilating drainage drain outlet is designed in fuselage cargo compartment structure.

Further, shipping unmanned plane is reequiped to service aircraft, original machine body structure is carried out plus reequips design and constitutes institute Retention mechanism, ventilation and the illumination for needing the airframe structure of hatch door, assisting mobile structure or mechanism, fixed cargo on cargo deck Equipment, and increase insulation construction in fuselage cargo hold inner wall；Inside the wing structure of airframe structure, or in the outer of fuselage back Portion or inside, and in the structure of floor panel structure bottom, integrally-built or absolute construction fuel tank is installed in design.

Thinking based on more design method, a kind of shipping unmanned aerial vehicle body structure of the utility model, including fuselage sheet The shaft that passes on left of body and head, the fuselage body surface is connected with upward-acting door, the right side of the fuselage body bottom Side by articulate be connected with it is double open tail-gate plate, double sides for opening tail-gate plate are provided with loading ramp, the head The top in left side is connected with head hatch door by shaft, the left side of the head and is provided with below head hatch door Fuselage cargo deck, is provided with guid arm between the fuselage body and head, the both sides of the fuselage body bottom are fixed It is connected with holder, the bottom of the holder is connected with idler wheel by shaft, wing is provided at the top of the fuselage body, The both sides of the wing inner cavity are both provided with wing fuel volume, and the inner cavity of the fuselage body is provided with insulating layer, the fuselage The inner cavity of ontology, which is provided with, is tethered at hole slot, and the fuselage body inner cavity has been fixedly connected with the machine of being tethered at the top and bottom of both sides The inner cavity of structure, the fuselage body is provided with floor panel structure, and the inner cavity of the floor panel structure is provided with floor fuel tank, describedly It is fixedly connected with smooth surface at the top of harden structure, the inner cavity of the fuselage body and is all provided with positioned at the both sides of smooth surface bottom It is equipped with discharge-channel, the both sides of the fuselage body inner cavity are both provided with cooling device, the top of fuselage body inner cavity both sides Portion is both provided with lighting apparatus, and ventilation equipment are communicated at the top of the fuselage body, and the both sides at the top of the fuselage body are equal Organic back of the body fuel tank is set, and the top of the machine back of the body fuel tank is fixedly connected with the bottom of wing.

Wherein, non-slip mat can be loaded and unloaded by being provided at the top of the smooth surface, the surface setting for loading and unloading non-slip mat There is anti-skid chequer.The both sides of the floor panel structure bottom have been fixedly connected with fixed block, the bottom of the fixed block and fuselage body Inner cavity be fixedly connected；It is provided with hanging ladder door on the right side of the fuselage body surface bottom portion.

The beneficial effects of the utility model：The utility model is convenient using head hatch door or the design scheme of tail hatch door The handling of large scale cargo provide the quick handling goods of Handling Ground Equipment easy to use, support automated handling fuselage The cabin door structure design method and organization plan of cargo hold, the door design scheme on airframe structure are on manned aircraft Ripe, it is applied to here on shipping unmanned plane and has carried out technological improvement design, also to designing low cost on fuselage cargo deck Smooth surface structure and the auxiliary moving structure of non-slip mat can be covered, being capable of relatively labor-saving mobile cargo.Meanwhile it proposing a kind of The thinking of innovation, design fuselage cargo hold insulation construction is to support the extraordinary shipping such as refrigeration, by promoting shipping value.

This airframe structure of the utility model can cool down the cargo of fuselage body inner cavity by cooling device, Cooling heat preservation is carried out to the cargo of fuselage body inner cavity by insulating layer, by ventilation equipment to fuselage sheet during transport Intracoelomic cavity is aerated, and can also be illuminated to the inner cavity of fuselage body by lighting apparatus, by being tethered at mechanism and being tethered at Hole slot is used cooperatively, and the cargo of fuselage body inner cavity can be fixed, and prevents cargo from the phenomenon that arbitrary sliding occur, is led to The setting for crossing guid arm increases the accommodation space of fuselage, convenient for being carried to more cargos, therefore has automatic makeup The advantages of unloading cargo disengaging fuselage cargo hold provides heat preservation shipping environment for short-distance cold fresh goods object, effect is improved for shipping unmanned plane Rate extends the source of goods, promotes value, is convenient for using.

Description of the drawings

Fig. 1 is that the concordant hinge type of head hatch door (is opened and closed schematic diagram above and below head hatch door, customization side opening and closing hinge may be selected Chain) schematic diagram；

Fig. 2 is that (head platform outstanding opens signal to one of half cover hinge type of head hatch door without side wall, head hatch door Figure)；

Fig. 3 is that one of half cover hinge type of head hatch door (goes out platform band side wall, side wall is one of nose shell before head Point)；

Fig. 4 is head hatch door back-and-forth motion type (dotted line indicates customized mechanism in figure)；

Fig. 5 is that downward open of the tail-gate plate of tail hatch door is supported on ground schematic diagram (dotted line expression closed position and top Auxiliary hatch door)；

Fig. 6 is that schematic diagram is opened in the tail-gate plate both sides of the utility model tail hatch door；

Fig. 7 is fuselage side wall hatch door (hanging ladder door, the schematic diagram of the opening state of upward-acting door-dotted line)；

For the Functional Design on fuselage cargo component section, (floor is tethered at hole slot structure, insulating layer, fuel tank, row to Fig. 8 It puts, divulges information and illuminate)；

Fig. 9 is cargo handling place schematic layout pattern (handling can distinguish both sides, or handling homonymy)；

Figure 10 is the airframe structure overall schematic of the one of which embodiment of the utility model；

Figure 11 is the airframe structure vertical view in Figure 10.

Reference sign：1- fuselage bodies, 2- heads, 3- upward-acting doors, 4- is bis- to open tail-gate plate, 5- loading ramps, 6- Head hatch door, 7- fuselage cargo decks, 8- guid arms, 9- holders, 10- idler wheels, 11- wings, 12- wing fuel volumes, 13- heat preservations Layer, 14- are tethered at hole slot, and 15- is tethered at mechanism, 16- floor panel structures, the floors 17- fuel tank, 18- smooth surfaces, 19- discharge-channels, 20- cooling devices, 21- lighting apparatus, 22- ventilation equipment, 23- machines carry on the back fuel tank, and 24- can load and unload non-slip mat, 25- fixed blocks, 26- hanging ladder doors, 27- head hatch doors interface, floor in 28- cargo holds, 29- assist hatch door, 30- tail-gate plates, 31- warehouse districts, 32- Face transfer station.

Specific implementation mode

The utility model is described in further detail with reference to the accompanying drawings and examples, but appoints not as to the utility model What is limited.

Please refer to Fig.1-7：A kind of shipping unmanned aerial vehicle body construction design method and structure of the utility model, are being constituted On the airframe structure of cargo hold, tail cabin can be designed in the Front-end Design head hatch door 6 of fuselage axial direction, or in the rear end of fuselage axial direction Door, and fuselage side wall hatch door is designed on fuselage side wall, constitute the airframe structure that may be selected to be custom made with one or more hatch doors. Insulation construction can also be designed on airframe structure, and the airframe structure of insulation is provided for fuselage cargo hold.

Wherein, it in the Front-end Design head hatch door 6 of airframe structure, is provided from fuselage axial forward end for cargo and passes in and out fuselage goods Cabin can standard-sized sheet through-type cabin door structure, the contour dimension of hatch door coincide with fuselage compartment door physical dimension, inner dimensions and machine Body inner wall size is coincide substantially, installs sealing material at head hatch door interface 27, big build cargo can conveniently pass through fuselage axial direction Front end pass in and out fuselage cargo hold, especially adapt to ground installation docking, realize automated handling cargo.Head hatch door 6 is beaten Open and close frame mode and servo mechanism are beaten it can be selected that being rotated up one is the mechanical rocking arm by being fixed on back Open or rotate down closing, allow head hatch door 6 opening's edge and airframe structure opening's edge pairing (the concordant hinge type of attached drawing 1, attached drawing 2 With 3 half cover hinge type of attached drawing).One is being closed from the mechanical rocking arm for being fixed on fuselage side wall to side opening or into cabin, allow The head hatch door 6 of the opening's edge of head hatch door 6 and the opening's edge pairing of airframe structure, this side opening can be under head hatch door 6 Portion increases pulley mechanism that is retractable and being supported on ground, to increase the support force to head hatch door 6.One is along fixation Telescopic two or more lead arm 8 and 6 lower part of head hatch door under fuselage floor or on side wall are retractable simultaneously It is supported on the pulley mechanism on ground, by being opened along ground moving (4 mobile model of attached drawing).

Tail hatch door is designed in the tail end of airframe structure, the cabin that fuselage cargo hold is passed in and out from fuselage axial rearward end is provided for cargo Door, equally, contour dimension and the fuselage compartment door physical dimension of hatch door coincide, and inner dimensions are kissed substantially with fuselage inner wall size It closes, so that big build cargo passes in and out fuselage cargo hold by the rear end of fuselage axial direction, especially adapts to the docking of ground installation, realize Automated handling cargo.Tail hatch door opens and closes mode it can be selected that one is simple gate structure, and it is upward to rotate down opening Rotation is closed, and tail hatch door outside wall surface may be supported on ground (about 5 hinge type of attached drawing, dotted line expression close stance in figure after opening Set and the auxiliary hatch door 29 at top), therefore the wear-resisting composite wood of material selection hard pressure resistance of the external surface grounded part of tail hatch door Material, and the curve shape of this partial outer face meets part surface when opening and can support ground, when closing, is conducive to pneumatic drag reduction, The internal face of tail hatch door sustainable goods movement when opening passes in and out fuselage cargo hold.The internal face of tail hatch door can be installed just In the smooth surface structure of the low cost of mobile cargo, or the semi-buried transmission mechanism mechanically or electrically moved of design.One is two-door Structure, respectively to fuselage side rotating opening (7 bilateral hinge type of attached drawing) or reversed closing, in addition cargo disengaging fuselage cargo hold carries The springboard of fuselage cargo hold is passed in and out for cargo.

In the sidewall design fuselage side wall hatch door of airframe structure, the cabin that fuselage cargo hold is passed in and out from fuselage side wall is provided for cargo Door, size are rationally determined according to fuselage force transferring structure and cross sectional dimensions, or are wanted according to loading cargo size Ask customization.Univalve door, bivalve door, hanging ladder door and upward-acting door 3 (attached drawing 7) may be selected and by these hatch doors layout in fuselage unilateral side Or the structure type of both sides.

It can be according to the requirement custom design head hatch door 6 or tail hatch door of handling goods on fuselage cargo component Or the topology layout of fuselage side wall hatch door.The unlocking and locking of head hatch door 6 or tail hatch door, using mechanical lock or electronic lock Servo mechanism, which is realized, to be opened and closed, wherein the unlocking and blocking order of electronic lock can be manual by wireless remote control or Field Force Command signal is generated by compressing switch.The light that design facilitates the low cost auxiliary of goods movement mobile on the floor of airframe structure Sliding 18 structure of surface, such as the smooth material of hard stainless steel and surface, and bedding is removably anti-skidding on smooth surface 18 Mat structure (attached drawing 8), it is solid with the lock of a plurality of reinforced belt in cushion both sides if strength braid over braid substrate and surface are bonded anti-slip material It is scheduled on the groove structure of fuselage floor side or is tethered in structure, cushion is avoided to slide.It is set on floor panel structure along fuselage axis Count the transmission mechanism (attached drawing 8) that semi-buried installation covers independent mechanically or electrically dynamic complementary goods movement more.In fuselage cargo hold Respective design fixes cargo location and is tethered at mechanism 15 or structure in portion's structure, such as mooring ring linkage, or is tethered at 14 knot of hole slot Structure and lighting apparatus 21.

Insulation construction is designed in the airframe structure inner wall of fuselage cargo compartment, insulation construction is made of thermal insulation material, such as The space wadding of the low conduction of lightweight and its cotton pad or light porous foam heat insulating material.And refrigeration can be configured in cargo hold or is added The special equipment of temperature, constitutes the refrigeration of enhancing or the heat preservation cargo hold of heating.Bulk goods can be installed in cargo hold, or installed several A refrigeration container, aquatic products container, customization container, and it is subject to fixed position using the retention mechanism built in fuselage cargo hold.And in machine Ventilation and discharge-channel (attached drawing 8) are designed on floor 28 or bulkhead in body cargo hold, discharge includes draining blowdown.

Shipping unmanned plane, such as selection home-built aircraft fortune 7, fortune 8, fortune 9, fortune 12 are reequiped by preceding method for service aircraft Aircraft, and the other outsourcing aircrafts of selection.The original machine body structure of service aircraft is carried out plus reequips design and constitutes required hatch door Airframe structure, the structure or mechanism that Design assistant moves on cargo deck design the fastening structure and mechanism of fixed cargo, Design installation ventilation and lighting apparatus, and increase insulation construction in fuselage cargo hold inner wall.

Inside the wing structure of airframe structure, or in the outside or inside of fuselage back, and in floor panel structure bottom Structure in, integrally-built or absolute construction fuel tank (attached drawing 8) is installed in design.

Please refer to Fig. 8,10 and 11, the shipping unmanned aerial vehicle body structure of embodiment of the utility model a kind of can be according to Such design, the airframe structure include fuselage body 1 and head 2, and hanging ladder door is provided on the right side of 1 surface bottom portion of fuselage body 26, the shaft that passes on left on 1 surface of fuselage body is connected with upward-acting door 3, and the right side of 1 bottom of fuselage body is lived by hinge It is dynamic be connected with it is double open tail-gate plate 4, double sides for opening tail-gate plate 4 are provided with loading ramp 5, and the top in 2 left side of head is by turning Axis is connected with head hatch door 6, the left side of head 2 and the lower section of head hatch door 6 is provided with fuselage cargo deck 7, machine Guid arm 8 is provided between body ontology 1 and head 2, the both sides of 1 bottom of fuselage body have been fixedly connected with holder 9, holder 9 Bottom is connected with idler wheel 10 by shaft, and the top of fuselage body 1 is provided with wing 11, and the both sides of 11 inner cavity of wing are all provided with It is equipped with wing fuel volume 12, the inner cavity of fuselage body 1 is provided with insulating layer 13, and the inner cavity of fuselage body 1, which is provided with, is tethered at hole slot 14, it has been fixedly connected at the top and bottom of 1 inner cavity both sides of fuselage body and has been tethered at mechanism 15, the inner cavity of fuselage body 1 is provided with The both sides of floor panel structure 16,16 bottom of floor panel structure have been fixedly connected with fixed block 25, bottom and the fuselage body 1 of fixed block 25 Inner cavity be fixedly connected, the inner cavity of floor panel structure 16 is provided with floor fuel tank 17, and the top of floor panel structure 16 is fixedly connected with Smooth surface 18, the top of smooth surface 18, which is provided with, can load and unload non-slip mat 24, can load and unload non-slip mat 24 by anti-skid wearable material It makes and surface may be provided with anti-skid chequer, the inner cavity of fuselage body 1 and be both provided with positioned at the both sides of 18 bottom of smooth surface The both sides of discharge-channel 19,1 inner cavity of fuselage body are both provided with cooling device 20, and fuselage body is all provided at the top of 1 inner cavity both sides It is equipped with lighting apparatus 21, the top of fuselage body 1 is communicated with ventilation equipment 22, and organic back of the body fuel tank is arranged in 1 top of fuselage body 23, the space that the top of machine back of the body fuel tank 23 is fixedly connected and is collectively formed with the bottom of wing 11 can also constitute machine back of the body fuel A part for case 23 can cool down the cargo of 1 inner cavity of fuselage body by cooling device 20, by insulating layer 13 to machine The cargo of 1 inner cavity of body ontology carries out cooling heat preservation, is carried out to 1 inner cavity of fuselage body by ventilation equipment 22 during transport Ventilation, can also illuminate the inner cavity of fuselage body 1 by lighting apparatus 21, by being tethered at mechanism 15 and being tethered at hole slot 14 Be used cooperatively, the cargo of 1 inner cavity of fuselage body can be fixed, prevent cargo occur arbitrary sliding the phenomenon that, pass through The setting of guid arm 8 increases the accommodation space of fuselage, convenient for being carried to more cargos, therefore has automated handling Cargo passes in and out the advantages of fuselage cargo hold, provides heat preservation shipping environment for short-distance cold fresh goods object, efficiency is improved for shipping unmanned plane, The source of goods is extended, value is promoted, is convenient for using.

It freights to the inner cavity of fuselage body 1 in use, putting down fuselage cargo deck 7 by opening head hatch door 6, when Cargo needs to be moved by opening cooling device 20 when refrigeration, cargo of the cooling device 20 to 1 inner cavity of fuselage body It is cooled down, the cargo of 1 inner cavity of fuselage body is sealed by insulating layer 13, to increase the cooling effect of cargo, 1 inner cavity of fuselage body is aerated by ventilation equipment 22 during transport, by lighting apparatus 21 to fuselage body 1 Inner cavity is illuminated, and can open tail-gate plate 4 by opening pair when needing to unload cargo declines loading ramp 5 to goods Object is unloaded.

The shipping unmanned aerial vehicle body structure, by fuselage body 1, head 2, upward-acting door 3, it is double open tail-gate plate 4, handling goods jump Plate 5, head hatch door 6, fuselage cargo deck 7, guid arm 8, holder 9, idler wheel 10, wing 11, wing fuel volume 12, insulating layer 13, it is tethered at hole slot 14, is tethered at mechanism 15, floor panel structure 16, floor fuel tank 17, smooth surface 18, discharge-channel 19, cooling dress The cooperation for setting 20, lighting apparatus 21, ventilation equipment 22 and machine back of the body fuel tank 23 solves existing unmanned plane transportation cost height, The low problem of insulating efficiency.

The application case 1 of the utility model, the cargo handling of shipping unmanned plane, as shown in Figure 9：

Unmanned planes are transported in the double deliveries of one frame high mounted wing, head hatch door and tail hatch door are designed simultaneously on airframe structure, to adopt Tail hatch door shipment is taken, what head hatch door was stocked up synchronizes operation of removing stage makeup and costume.Shipping unmanned plane drives into cargo handling place, side automatically It is unloading warehouse district 31, receives the storage for unloading cargo, offside is loading warehouse district 31, and storage is ready for sending the cargo of shipment. The mobile handling facilities of ground configuration, the cargo that fuselage cargo compartment ships, by artificial kickoff mechanism deck store door, the cargo unloaded passes through It crosses transfer station and is sent into warehouse district 31, the cargo being ready for shipment is sent to head hatch door mouth by another frame transfer station from warehouse district 31, Artificial push-in fuselage cargo hold.

32 height of ground transfer station and the height of fuselage floor of the mobile handling facilities of ground configuration can be adjusted, so as to Adapt to the airplane floor height of different type of machines.The especially opening of tail hatch door, tail-gate plate 30 or springboard can be overlapped on biography On the docking step for sending platform special, so that cargo smoothly pushes to transfer station.

The application case 2 of the utility model, the cold chain transportation of shipping unmanned plane

After the airframe structure of shipping unmanned plane uses insulation construction, it can be used for transporting cold fresh goods object.Load and unload cold fresh goods object Link builds unmanned plane cold chain system in handling operation area, mating ground safeguard system is provided for the application of shipping unmanned plane, Include mainly：

Sunshade greenhouse is refrigerated, including cargo handling operation area, covers the items of equipment of handling goods, and refrigeration greenhouse area Spray cold air-water-atomization cooling equipment；

Freezer stores refrigerated goods；

Air-conditioning station, fuselage cargo hold or cargo to shipping unmanned plane provide ground air conditioner, and subregion provides heat-insulated gas curtain；

Handling operation vehicle, including handling engineering truck, the ancillary equipment of mobile cargo, especially with electric energy vehicle, electric energy Transmission equipment；

Airborne cargo handling pattern, is included as chartered plane, spelling machine, and in bulk or packaging provides mobile quick despatch equipment；

Cold chain freight transport information management system, acquisition or the shipping unmanned plane and cold chain that provide the collecting and distributing hinge of cargo to terminal are made The every terms of information network and dispatch command and its operating system in industry area.

Although the preferred embodiments of the utility model are described in above-mentioned combination attached drawing, above-mentioned specific implementation mode It is only schematical, and be not it is restrictive, those skilled in the art under the objective enlightenment of the utility model, The accommodation made in the rights protection scope for not departing from the utility model, it is within the protection scope of the present utility model.

Claims (3)

1. a kind of shipping unmanned aerial vehicle body structure, including fuselage body (1) and head (2), it is characterised in that：The fuselage body (1) shaft that passes on left on surface is connected with upward-acting door (3), and the right side of fuselage body (1) bottom is lived by hinge It is dynamic be connected with it is double open tail-gate plate (4), double sides for opening tail-gate plate (4) are provided with loading ramp (5), the head (2) The top in left side is connected with head hatch door (6) by shaft, the left side of the head (2) and positioned at head hatch door (6) Lower section is provided with fuselage cargo deck (7), and guid arm (8), the machine are provided between the fuselage body (1) and head (2) The both sides of body ontology (1) bottom have been fixedly connected with holder (9), and the bottom of the holder (9) is connected with rolling by shaft It takes turns (10), is provided with wing (11) at the top of the fuselage body (1), the both sides of wing (11) inner cavity are both provided with wing The inner cavity of fuel tank (12), the fuselage body (1) is provided with insulating layer (13), and the inner cavity of the fuselage body (1) is provided with It is tethered at hole slot (14), has been fixedly connected at the top and bottom of fuselage body (1) the inner cavity both sides and has been tethered at mechanism (15), it is described The inner cavity of fuselage body (1) is provided with floor panel structure (16), and the inner cavity of the floor panel structure (16) is provided with floor fuel tank (17), it is fixedly connected with smooth surface (18) at the top of the floor panel structure (16), the inner cavity of the fuselage body (1) and is located at The both sides of smooth surface (18) bottom are both provided with discharge-channel (19), and the both sides of fuselage body (1) inner cavity are both provided with Cooling device (20) is both provided with lighting apparatus (21), the fuselage body at the top of fuselage body (1) the inner cavity both sides (1) it is communicated with ventilation equipment (22) at the top of, organic back of the body fuel tank (23) is set at the top of the fuselage body (1) and along course cloth A certain range before and after wing (11) is set, the machine back of the body fuel tank (23) also utilizes the bottom of fuselage body (1) and wing (11) Portion is fixedly connected with the space of composition.

2. shipping unmanned aerial vehicle body structure according to claim 1, it is characterised in that：The top of the smooth surface (18) Non-slip mat (24) can be loaded and unloaded by being provided with, and the surface for loading and unloading non-slip mat (24) may be provided with anti-skid chequer.

3. shipping unmanned aerial vehicle body structure according to claim 1, it is characterised in that：Floor panel structure (16) bottom Both sides have been fixedly connected with fixed block (25), and the bottom of the fixed block (25) is fixedly connected with the inner cavity of fuselage body (1)；Institute It states and is provided with hanging ladder door (26) on the right side of fuselage body (1) surface bottom portion.