CN207157483U - Unmanned vehicle and flight instruments - Google Patents

Abstract

The utility model provides a kind of unmanned vehicle and flight instruments, is related to flight instruments technical field.The unmanned vehicle includes upper lid, side plate, bottom and battery flat hatchcover, the section of upper lid is in inverse u shape, the top surface of upper lid is respectively formed slope from its middle part to both sides, and the intersection in sloped sides face is arc transition, battery flat hatchcover is fixed on lid, and side plate is two pieces, and is respectively and fixedly connected with the madial wall of upper lid both sides, bottom is fixed in the bottom of two blocks of side plates, and upper lid, bottom, two blocks of side plates and battery flat hatchcover surround the accommodating chamber of closing jointly；The flight instruments includes undercarriage and above-mentioned unmanned vehicle, undercarriage are fixedly arranged on side plate.The inverse u shape structure of upper lid, and the connected mode of upper lid and side plate can realize that rain-proof acts on；Upper lid, side plate, bottom and the installation of battery flat hatchcover, convenient disassembly, and during the manufacturing, can be each separately fabricated, so as to reduce the maintenance of unmanned vehicle and manufacturing cost.

Description

Unmanned vehicle and flight instruments

Technical field

It the utility model is related to flight instruments technical field, more particularly to a kind of unmanned vehicle and flight instruments.

Background technology

Unmanned vehicle is the not manned vehicle manipulated using radio robot and the presetting apparatus provided for oneself, Without driving cabin on aircraft, but the equipment such as automatic pilot, presetting apparatus are installed, on ground, naval vessels or machine tool is remotely controlled The personnel that stand are tracked to it by equipment such as radars, positioned, are remotely controlled, remote measurement and Digital Transmission.With society high speed development, The rapid advances of science and technology, unmanned vehicle have been widely used for the industries such as mapping, fire-fighting, electric power, guard.

Existing unmanned vehicle is mostly electric drive control, and during aircraft flight in the air, electronic equipment once makes moist Or water inlet, aircraft even fall operation irregularity, and great threat is caused to the safety of ground installation and personnel；People are Prevent rainwater from entering in aircraft, the fuselage manufacture of aircraft is formed in one, fuselage moulding process is complex, shaping Die manufacturing cost is high, and once some position of fuselage, impaired, it is necessary to change whole fuselage, maintenance cost is high.

That is, existing unmanned vehicle is that fuselage is arranged to integrated formed structure by rain-proof, and manufacture and maintenance cost are high.

Utility model content

The purpose of this utility model is to provide a kind of unmanned vehicle and flight instruments, to solve to exist in the prior art Unmanned vehicle fuselage is arranged to integrated formed structure for rain-proof, manufacture and the high technical problem of maintenance cost.

Unmanned vehicle provided by the utility model, including upper lid, side plate, bottom and battery flat hatchcover, the upper lid Section is in inverse u shape, and the top surface of the upper lid is respectively formed slope from its middle part to both sides, and slope described in both sides is intersecting Locate as arc transition；One end of the upper lid is blind end, and the other end is openend, and the battery flat hatchcover is detachable affixed In on the openend of the upper lid；The side plate is two pieces, and two blocks of side plates are detachable respectively is fixed in the upper lid On the madial wall of both sides, the bottom is fixed in the bottom of two blocks of side plates, the upper lid, the bottom, two pieces of sides Plate and the battery flat hatchcover surround the accommodating chamber of closing jointly；Horn is installed with the side plate, is articulated with the horn Rotor.

Further, the openend of the upper lid is provided with guiding gutter along its periphery, and the battery flat hatchcover is provided with clamping Bar, the clamping bar match with the guiding gutter.

Further, one end of the side plate and the madial wall of the upper lid are detachable affixed, and the end of the other end is certainly Its outer wall inward wall is provided with inclined-plane, and the inclined-plane is towards the inside of the upper lid.

Further, the madial wall of the upper lid both sides is completely or the lateral wall not exclusively with the side plate overlaps, described Linked together between the side wall of upper lid both sides and the side plate by threaded fastener.

Further, the bottom is provided with multiple passages.

Further, the top surface of the bottom and bottom surface are equipped with projection, the raised edge for surrounding the passage Set.

Further, the battery flat hatchcover is provided with the first buckle, and the side plate is provided with the second buckle, and described first Connector is connected between buckle and the second buckle.

Further, it is connected with tie-beam between two blocks of side plates.

Further, the inwall of the side plate is installed with contiguous block, and the tie-beam is detachable to be fixed in the connection On block.

The utility model unmanned vehicle has the beneficial effect that：

Unmanned vehicle provided by the utility model, including close accommodating chamber for being combined and installed together to be formed Lid, side plate, bottom and battery flat hatchcover, wherein, upper lid is positioned at the top of unmanned vehicle, and the blind end of upper lid is located at nobody The head of aircraft, two blocks of side plates are located at the side of unmanned vehicle, and battery flat hatchcover is located at the afterbody of unmanned vehicle, bottom Electronic component in the bottom of unmanned vehicle, unmanned vehicle is arranged in the accommodating chamber；Also include being used to drive nothing The rotor that people's aircraft rises or falls, the horn for supporting fixed rotor.

The upper lid back-off of unmanned vehicle is set, and two side plates are detachable to be fixed on the madial wall of lid inverse u shape, That is, the inside covered in two side plate insertions, the detachable bottom for being fixedly arranged on two side plates of bottom, the top surface and side wall of upper lid exist Two side plates of protection and bottom can be covered on vertical direction；Run into the air when unmanned vehicle flies under the drive of rotor During rainy weather, rainwater is dropped onto on the top surface of lid, and the top surface of upper lid is the low arc in the high both sides in middle part, in Action of Gravity Field Under, rainwater can be flowed down along the slope of upper lid both sides, and fuselage is flowed downward out then along side plate；When rainwater tilt drop to the wind When, the side wall of upper lid both sides can also play barrier effect to rainwater, and two blocks of side plates overlap with two inner sidewall parts of upper lid, The generation for even avoiding rainwater from pouring into accommodating chamber inner case from side plate and upper lid madial wall junction is further reduced, specifically , the side wall of upper lid can stop is less than pouring into for 30 degree of rainwater with vertical direction.The inverse u shape structure of upper lid, and upper lid It can be realized with the connected mode of side plate and play a part of rain-proof and protection to the electronic component of unmanned vehicle.

In addition, the fuselage of unmanned vehicle is assembled by single upper lid, side plate, bottom and battery flat hatchcover and is formed closing Accommodating chamber, when the electronic component in accommodating chamber needs to repair or changed, peace that can be according to the electronic component in accommodating chamber Holding position, correspondingly the body parts of the position are disassembled, after the completion of electronic component reparation or replacing, by the fuselage Part is reinstalled, so as to reduce the cost for safeguarding unmanned vehicle；In addition, when manufacturing, on each body parts Lid, side plate, bottom and battery flat hatchcover can be manufactured individually, and technique is simple, manufacturing cost is low.

Another purpose of the present utility model is to provide a kind of flight instruments, including undercarriage and above-mentioned unmanned flight Device, the undercarriage is detachable to be fixedly arranged on the side plate, and the flight instruments has all technologies of above-mentioned unmanned vehicle Effect.

The utility model flight instruments has the beneficial effect that：

Flight instruments provided by the utility model, including what is played a supporting role to it when being landed for unmanned vehicle are risen Fall frame and above-mentioned unmanned vehicle, the undercarriage is detachable to be fixedly arranged on the side plate of unmanned vehicle, unmanned vehicle flight When, undercarriage can play a part of maintaining balance, and when unmanned vehicle lands, undercarriage plays support to unmanned vehicle and made With directly being landed with reducing unmanned vehicle, collide the hair of situation of being caused damage to fuselage, horn or rotor with ground It is raw.Upper lid, side plate, bottom and battery flat hatchcover collectively constitute electronics of the closing accommodating chamber to unmanned vehicle in the flight instruments Element plays a part of rain-proof and protection, can be according to the electronics when the electronic component in accommodating chamber needs to repair or changed Installation site of the element in accommodating chamber, correspondingly disassembles the body parts of the position, electronic component reparation or After the completion of replacing, the body parts are reinstalled, so as to reduce the cost for safeguarding unmanned vehicle；In addition, production During manufacture, lid, side plate, bottom and battery flat hatchcover can be manufactured individually on each body parts, and technique is simple, manufacturing cost It is low.

Brief description of the drawings

, below will be right in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art The required accompanying drawing used is briefly described in embodiment or description of the prior art, it should be apparent that, describe below In accompanying drawing be some embodiments of the present utility model, for those of ordinary skill in the art, do not paying creativeness On the premise of work, other accompanying drawings can also be obtained according to these accompanying drawings.

Fig. 1 is the three dimensional structure diagram for the flight instruments that the utility model embodiment provides；

Fig. 2 is that upper lid, side plate, bottom and battery flat hatchcover are common in the unmanned vehicle that the utility model embodiment provides Form the three dimensional structure diagram of fuselage；

Fig. 3 is the vertical view knot that unmanned vehicle latus inframedium, the tie-beam that the utility model embodiment provides connect with horn Structure schematic diagram；

Fig. 4 is above to cover the cross-sectional view being connected with side plate in the unmanned vehicle that the utility model embodiment provides；

Fig. 5 is above to cover the sectional structure being connected with battery flat hatchcover in the unmanned vehicle that the utility model embodiment provides Schematic diagram.

Icon：Covered on 1-；2- side plates；3- bottoms；4- battery flat hatchcovers；5- horns；6- tie-beams；7- rises and falls Frame；11- slopes；12- blind ends；13- openends；14- guiding gutters；21- inclined-planes；The buckles of 22- second；23- connections Block；31- passages；32- is raised；41- clamping bars；The buckles of 42- first；43- connectors.

Embodiment

The technical solution of the utility model is clearly and completely described below in conjunction with accompanying drawing, it is clear that described Embodiment is the utility model part of the embodiment, rather than whole embodiments.Based on the embodiment in the utility model, sheet The every other embodiment that field those of ordinary skill is obtained under the premise of creative work is not made, belongs to this practicality Novel protected scope.

, it is necessary to explanation in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular Directly ", the orientation of the instruction such as " level ", " interior ", " outer " or position relationship are based on orientation shown in the drawings or position relationship, are only Described for the ease of description the utility model and simplifying, rather than instruction or imply signified device or element must have it is specific Orientation, with specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.

, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly Connection；Can be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected by intermediary, It can be the connection of two element internals.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition Concrete meaning of the language in the utility model.

The present embodiment provides a kind of unmanned vehicle, as depicted in figs. 1 and 2, including upper lid 1, side plate 2, bottom 3 and battery Cabin hatchcover 4, the section of upper lid 1 is in inverse u shape, and the top surface of upper lid 1 is respectively formed slope 11, and two skew backs from its middle part to both sides Domatic 11 intersection is arc transition；One end of upper lid 1 is blind end 12, and the other end is openend 13, and battery flat hatchcover 4 can Detachable is fixed on the openend 13 of lid 1；Side plate 2 is two pieces, and two blocks of side plates 2 are detachable respectively is fixed in lid 1 On the madial wall of both sides, bottom 3 is fixed in the bottom of two blocks of side plates 2, upper lid 1,3, two blocks of side plates 2 of bottom and battery flat hatchcover 4 The accommodating chamber of closing is surrounded jointly；Horn 5 is installed with side plate 2, rotor is articulated with horn 5.

The unmanned vehicle that the present embodiment provides, including for being combined and installed together with the upper lid of formation closing accommodating chamber 1st, side plate 2, bottom 3 and battery flat hatchcover 4, wherein, upper lid 1 is located at the top of unmanned vehicle, and the blind end of upper lid 1 12 In the head of unmanned vehicle, two blocks of side plates 2 are located at the side of unmanned vehicle, and battery flat hatchcover 4 is located at unmanned vehicle Afterbody, bottom 3 are located at the bottom of unmanned vehicle, and the electronic component in unmanned vehicle is arranged in the accommodating chamber；Also include For rotor, the horn 5 for supporting fixed rotor for driving unmanned vehicle to rise or fall.

The back-off of upper lid 1 of unmanned vehicle is set, the detachable madial wall for being fixed in the inverse u shape of lid 1 of two side plates 2 On, i.e. the inside of two upper lids 1 of the insertion of side plate 2, the detachable bottom for being fixedly arranged on two side plates 2 of bottom 3, the top surface of upper lid 1 Two side plates 2 of protection and bottom 3 can be covered with side wall in the vertical direction；When unmanned vehicle flies under the drive of rotor When running into rainy weather in the air, rainwater is dropped onto on the top surface of lid 1, and the top surface of upper lid 1 is the low arc in the high both sides in middle part, Under gravity, rainwater can be flowed down along the slope 11 of the upper both sides of lid 1, and fuselage is flowed downward out then along side plate 2；Work as rain Water to the wind tilt drop when, the side walls of the upper both sides of lid 1 can also play barrier effect, two blocks of side plates 2 and the two of upper lid 1 to rainwater Individual inner sidewall part overlaps, and further reduces even avoiding rainwater from being poured into from side plate 2 and the upper madial wall junction of lid 1 in accommodating chamber The occurrence of portion, specifically, the side wall of upper lid 1 can stop is less than pouring into for 30 degree of rainwater with vertical direction.Upper lid 1 falls U-typed structure, and upper lid 1 and side plate 2 connected mode can realize the electronic component of unmanned vehicle is played rain-proof and The effect of protection.

In addition, the fuselage of unmanned vehicle is assembled by individually upper lid 1, side plate 2, bottom 3 and battery flat hatchcover 4 forms envelope The accommodating chamber closed, can be according to the electronic component in accommodating chamber when the electronic component in accommodating chamber needs to repair or changed Installation site, correspondingly the body parts of the position are disassembled, electronic component reparation or change after the completion of, by this Body parts are reinstalled, so as to reduce the cost for safeguarding unmanned vehicle；In addition, when manufacturing, each main body section Lid 1, side plate 2, bottom 3 and battery flat hatchcover 4 can be manufactured individually on part, and technique is simple, manufacturing cost is low.

In the present embodiment, as shown in figure 5, guiding gutter 14, battery flat can be provided with along its periphery in the openend 13 of upper lid 1 Hatchcover 4 is provided with clamping bar 41, and clamping bar 41 matches with guiding gutter 14.The upper openend 13 of lid 1 is set along the periphery of its inverse u shape There is a guiding gutter 14, the matching of clamping bar 41 on battery flat hatchcover 4 is caught in the guiding gutter 14, lid 1 and battery flat hatchcover 4 in completions Between connection positioning (for degree of being connected firmly, upper lid 1 and battery flat hatchcover 4 can also be carried out by other connection member Connection), when unmanned vehicle runs into rainy weather in the air, rainwater falls from top to bottom falls into guiding gutter 14 and card on lid 1 In gap after the cooperation of narrow bars 41, the shape of guiding gutter 14 corresponding to the upper cross sectional shape of lid 1 is also inverse u shape, and rainwater, which enters, leads Flowed down in chute 14 and along guiding gutter 14, subsequently pass through side plate 2 and flow out fuselage；Guiding gutter 14 and clamping bar 41 are arranged on reality On the basis of now above being connected between lid 1 and battery flat hatchcover 4, additionally it is possible to rainwater diversion is gone out into fuselage, reduces and even avoids rainwater The occurrence of penetrating into fuselage interior from upper lid 1 and the junction of battery flat hatchcover 4, improve the water-resistant performance of unmanned vehicle.

Specifically, battery is arranged on the inside of battery flat hatchcover 4, it is necessary to when changing battery, only need to be by the card of battery flat hatchcover 4 Narrow bars 41 are extracted out of upper lid 1 guiding gutter 14, and battery flat hatchcover 4 is disassembled；After the completion of battery altering, by battery Cabin hatchcover 4 is reinstalled on lid 1, convenient disassembly.

In the present embodiment, as shown in figure 4, one end of side plate 2 and the madial wall of upper lid 1 are detachable affixed, the other end End is provided with inclined-plane 21 from its outer wall inward wall, and inclined-plane 21 is towards the inside of upper lid 1.Rain in the upper top surface of lid 1 or guiding gutter 14 Water is flowed downwardly on side plate 2 by Action of Gravity Field, and rainwater flows straight down on side plate 2, when reaching the bottom of side plate 2, due to The setting on the inwall inclined-plane 21 of side plate 2, the inclined-plane 21 form wedge angle with the outer wall of side plate 2 in bottom, and the rainwater of the bottom of side plate 2 reaches point It can not be flowed at angle along the inclined-plane 21 to the inwall of side plate 2, and disengaging fuselage is directly dripped from sharp corner, the setting on the inclined-plane 21 The rainwater up to the bottom of side plate 2 can be effectively reduced to inwardly to flow along end, penetrate into fuselage to the electronics member inside accommodating chamber Part causes the generation of damaged condition.

Specifically, in the present embodiment, as shown in figure 4, the madial wall of the both sides of upper lid 1 can completely or not exclusively with side plate 2 Lateral wall overlap, linked together between the side wall and side plate 2 of the upper both sides of lid 1 by threaded fastener.Covered in the insertion of side plate 2 Inside 1, the inner sidewall part of upper lid 1 or overlapped completely with side plate 2, then by threaded fastener by the side of side plate 2 and upper lid 1 Wall is fixed together, and side wall of the rainwater on the upper top surface of lid 1 along upper lid 1 flows down, and rainwater reaches the bottom of the upper side wall of lid 1 When, bottom end face of the rainwater along the upper side wall of lid 1 inwardly flow to side plate 2, is flowed down then along side plate 2, until outflow fuselage； The madial wall of upper lid 1 has intersection with side plate 2, i.e. after upper lid 1 is connected with side plate 2, the gap between upper lid 1 and side plate 2 For the gap between the upper inwall side of lid 1 and side plate 2, the gap is vertical direction, and the rainwater of the side wall bottom of lid 1 can not edge in arrival Fuselage interior is penetrated into the gap, and damaged condition is caused to its internal electronic element so as to further reduce rainwater infiltration fuselage interior Generation.

In the present embodiment, as shown in Fig. 2 multiple passages 31 can be provided with bottom 3.Unmanned vehicle flies in the air During row, unmanned vehicle external fuselage air velocity is more than fuselage interior air velocity, therefore the air pressure of fuselage interior is more than machine Body external pressure, the presence of this draught head promote the air of fuselage interior to flow to external fuselage by passage 31, and air is such Flowing, heat caused by fuselage interior electronic component can be carried and distributed in external fuselage, complete fuselage interior electronic component Radiating.Specifically, battery is arranged on inside battery flat hatchcover 4, unmanned vehicle is being pacified in the rain using 32000 milliamperes of battery Full flight 35 minutes, after safe falling, for temperature below 50 degrees Celsius, the safe handling for having reached electrical equipment will in fuselage Ask.

In the present embodiment, as shown in Fig. 2 projection 32 can also be equipped with the top surface of bottom 3 and bottom surface, projection 32 surrounds The edge of passage 31 is set.The projection 32 of the bottom surface of bottom 3 can stop that the rainwater on bottom 3 enters air-vent, the top surface of bottom 3 The length of passage 31 can be lengthened with the projection 32 of bottom surface, further increases rainwater and fuselage interior is entered by passage 31 Difficulty, fuselage interior is entered by passage 31 so as to reduce rainwater, the hair of damaged condition is caused to fuselage interior electronic component It is raw.

In the present embodiment, as shown in Fig. 2 the first buckle 42 can be provided with battery flat hatchcover 4, side plate 2 is provided with the Two buckles 22, connector 43 is connected between the first buckle 42 and the second buckle 22.When installing battery flat hatchcover 4, first by battery Clamping bar 41 on cabin hatchcover 4 is caught in the guiding gutter 14 of lid 1, completes the preliminary connection between battery flat hatchcover 4 and upper lid 1 The second buckle 22 on the first buckle 42 and side plate 2 on battery flat hatchcover 4, is then connected by positioning by connector 43 Together, being connected for battery flat hatchcover 4 and side plate 2 is completed, so as to improve company of the battery flat hatchcover 4 on unmanned vehicle Connect firmness.Specifically, connector 43 can select rigid cord, elastic threads (rubber band) or other first card that can be connected The part of the buckle 22 of button 42 and second can be with.

In the present embodiment, as shown in figure 3, tie-beam 6 can be connected between two blocks of side plates 2.The setting of tie-beam 6, On the one hand, the relative position between two blocks of side plates 2 can be defined, improves the accurate shape in position of side plate 2；On the other hand, Tie-beam 6 is played a supporting role in fuselage interior, is reduced the stress of side plate 2 and is deformed upon, and causes the generation of fuselage damaged condition.

In the present embodiment, as shown in figure 3, contiguous block 23 can be installed with the inwall of side plate 2, tie-beam 6 is detachable It is fixed on contiguous block 23.Tie-beam 6 and the vertical connection of side plate 2, the setting of contiguous block 23 can be in order to tie-beam 6 and side plate 2 Connection, reduce the difficulty for being directly connected the end of tie-beam 6 with side plate 2；When the replacing of tie-beam 6 is reinstalled, do not influence The intensity of side plate 2.Similar, contiguous block 23 can also be provided with the outer wall of side plate 2, horn 5 is fixed on by contiguous block 23 On side plate 2.

The present embodiment also provides a kind of flight instruments, as shown in figure 1, including undercarriage 7 and above-mentioned unmanned vehicle, rises and falls Frame 7 is detachable to be fixedly arranged on side plate 2.

The flight instruments that the present embodiment provides, including what is played a supporting role to it when being landed for unmanned vehicle are risen and fallen Frame 7 and above-mentioned unmanned vehicle, on the detachable side plate 2 for being fixedly arranged on unmanned vehicle of the undercarriage 7, unmanned vehicle flight When, undercarriage 7 can play a part of maintaining balance, and when unmanned vehicle lands, undercarriage 7 plays support to unmanned vehicle Effect, is directly landed with reducing unmanned vehicle, is collided the situation that caused damage to fuselage, horn 5 or rotor with ground Occur.Upper lid 1, side plate 2, bottom 3 and battery flat hatchcover 4 collectively constitute closing accommodating chamber to unmanned vehicle in the flight instruments Electronic component play a part of rain-proof and protection, when in accommodating chamber electronic component need repair or change when, can basis Installation site of the electronic component in accommodating chamber, correspondingly disassembles the body parts of the position, electronic component After the completion of repairing or changing, the body parts are reinstalled, so as to reduce the cost for safeguarding unmanned vehicle；This Outside, during the manufacturing, lid 1, side plate 2, bottom 3 and battery flat hatchcover 4 can be manufactured individually on each body parts, technique letter List, manufacturing cost are low.

Finally it should be noted that：Above example is only to illustrate the technical solution of the utility model, rather than its limitations； Although the utility model is described in detail with reference to the foregoing embodiments, it will be understood by those within the art that： It can still modify to the technical scheme described in previous embodiment, either to which part or all technical characteristic Carry out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from the utility model embodiment The scope of technical scheme.

Claims (10)

1. a kind of unmanned vehicle, it is characterised in that including upper lid (1), side plate (2), bottom (3) and battery flat hatchcover (4), institute The section for stating lid (1) is in inverse u shape, and the top surface of the upper lid (1) is respectively formed slope (11), and two from its middle part to both sides The intersection of slope described in side (11) is arc transition；One end of the upper lid (1) is blind end (12), and the other end is opening Hold (13), the battery flat hatchcover (4) is detachable to be fixed on the openend (13) of the upper lid (1)；The side plate (2) is Two pieces, and two pieces of side plates (2) respectively it is detachable be fixed in it is described it is upper lid (1) both sides madial wall on, the bottom (3) It is fixed in the bottom of two pieces of side plates (2), upper lid (1), the bottom (3), two pieces of side plates (2) and the battery Cabin hatchcover (4) surrounds the accommodating chamber of closing jointly；

Horn (5) is installed with the side plate (2), rotor is articulated with the horn (5).

2. unmanned vehicle according to claim 1, it is characterised in that the openend (13) of the upper lid (1) is along outside it It is provided with guiding gutter (14) week, the battery flat hatchcover (4) is provided with clamping bar (41), the clamping bar (41) and the guiding gutter (14) match.

3. unmanned vehicle according to claim 2, it is characterised in that one end of the side plate (2) and the upper lid (1) Madial wall it is detachable affixed, the end of the other end is provided with inclined-plane (21) from its outer wall inward wall, inclined-plane (21) direction The inside of the upper lid (1).

4. according to the unmanned vehicle any one of claim 1-3, it is characterised in that it is described it is upper lid (1) both sides it is interior Side wall is completely or the lateral wall not exclusively with the side plate (2) overlaps, the side wall and the side plate (2) of described upper lid (1) both sides Between linked together by threaded fastener.

5. according to the unmanned vehicle any one of claim 1-3, it is characterised in that the bottom (3) is provided with more Individual passage (31).

6. unmanned vehicle according to claim 5, it is characterised in that the top surface of the bottom (3) and bottom surface are equipped with Raised (32), the projection (32) are set around the edge of the passage (31).

7. according to the unmanned vehicle any one of claim 1-3, it is characterised in that on the battery flat hatchcover (4) Provided with the first buckle (42), the side plate (2) is provided with the second buckle (22), first buckle (42) and the second buckle (22) Between be connected with connector (43).

8. according to the unmanned vehicle any one of claim 1-3, it is characterised in that between two pieces of side plates (2) It is connected with tie-beam (6).

9. unmanned vehicle according to claim 8, it is characterised in that the inwall of the side plate (2) is installed with contiguous block (23), the tie-beam (6) is detachable is fixed on the contiguous block (23).

10. a kind of flight instruments, it is characterised in that including nobody any one of undercarriage (7) and claim 1-9 Aircraft, the undercarriage (7) is detachable to be fixedly arranged on the side plate (2).