CN109641645A - The fuselage and unmanned plane of unmanned plane - Google Patents
The fuselage and unmanned plane of unmanned plane Download PDFInfo
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- CN109641645A CN109641645A CN201780053436.9A CN201780053436A CN109641645A CN 109641645 A CN109641645 A CN 109641645A CN 201780053436 A CN201780053436 A CN 201780053436A CN 109641645 A CN109641645 A CN 109641645A
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- fuselage
- unmanned plane
- groove
- upper casing
- casing
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 18
- 238000007789 sealing Methods 0.000 claims description 37
- 238000009423 ventilation Methods 0.000 claims description 31
- 238000005192 partition Methods 0.000 claims description 14
- 239000000428 dust Substances 0.000 claims description 13
- 239000003292 glue Substances 0.000 claims description 11
- 241000237983 Trochidae Species 0.000 claims description 9
- 238000004026 adhesive bonding Methods 0.000 claims description 8
- 230000003993 interaction Effects 0.000 claims description 6
- 230000002093 peripheral effect Effects 0.000 claims description 6
- 230000000903 blocking effect Effects 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 3
- 230000001681 protective effect Effects 0.000 abstract description 5
- 239000012535 impurity Substances 0.000 description 8
- 238000010586 diagram Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000001914 filtration Methods 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/70—Constructional aspects of the UAV body
- B64U20/75—Constructional aspects of the UAV body the body formed by joined shells or by a shell overlaying a chassis
Abstract
A kind of unmanned plane (100) and fuselage (10), fuselage (10) includes upper casing (11) and lower casing (12), upper casing (11) includes the upper casing groove (112) for being provided with upper casing (11) periphery, lower casing (12) can cooperate with upper casing (11), lower casing (12) includes convex block (122) of the setting in lower casing (12) periphery, when lower casing (12) and upper casing (11) cooperate, convex block (122) can extend into upper casing groove (112) to cooperate with upper casing groove (112).Unmanned plane (100) includes fuselage (10) and multiple horns (30), multiple horns (30) are fixedly connected with fuselage (10), and radially it is arranged outwardly from fuselage (10), when lower casing (12) and upper casing (11) cooperate, convex block (122) can extend into upper casing groove (112) to cooperate with upper casing groove (122).In actual use, it can prevent fit clearance of the water droplet between lower casing (12) and upper casing (11) from entering fuselage (10), enhance the protective performance of fuselage (10).
Description
The present invention relates to air vehicle technique fields, more specifically, are related to the fuselage and unmanned plane of a kind of unmanned plane.
The fuselage of unmanned plane includes upper cover and lower cover, since the gap cooperated between upper cover and lower cover is larger, when unmanned plane is by fly close to water surface or in rainy day flight, water is easy from the gap into fuselage interior, and cause the line short etc. of fuselage interior, cause unmanned plane can not work normally.
Summary of the invention
Embodiment of the present invention aims to solve at least one of the technical problems existing in the prior art.For this purpose, embodiment of the present invention needs to provide a kind of fuselage of unmanned plane.
In a first aspect, the fuselage that the present invention provides a kind of unmanned plane includes upper casing and lower casing.
The upper casing includes the upper casing groove for being provided with the upper casing periphery.When the lower casing can include the convex block that the lower casing periphery is arranged in, the lower casing and the top shells fit with the top shells fit, the lower casing, the convex block can extend into the upper casing groove to cooperate with the upper casing groove.
Second aspect, the present invention provide a kind of unmanned plane, comprising: the fuselage of unmanned plane；And multiple horns, it is fixedly connected with the fuselage, and be radially arranged outwardly from the fuselage；The fuselage includes: upper casing, and the upper casing includes the upper casing groove for being provided with the upper casing periphery；And the lower casing with the top shells fit, when the lower casing includes the convex block that the lower casing periphery is arranged in, the lower casing and the top shells fit, the convex block can extend into the upper casing groove to cooperate with the upper casing groove.
In above-mentioned fuselage and unmanned plane, when lower casing is with top shells fit, convex block can extend into upper casing groove to cooperate with upper casing groove, so that water droplet, which is not easy the fit clearance between lower casing and upper casing, enters fuselage, the protective performance of fuselage is preferable.
The additional aspect and advantage of embodiment of the present invention will be set forth in part in the description, and partially will become apparent from the description below, or the practice of embodiment is recognized through the invention.
The above-mentioned and/or additional aspect and advantage of embodiment of the present invention will be apparent and are readily appreciated that in the description from combination following accompanying drawings to embodiment, in which:
Fig. 1 is the schematic top plan view of the fuselage of the unmanned plane of embodiment according to the present invention；
Fig. 2 is schematic cross-section of the fuselage in Fig. 1 along II-II line；
Fig. 3 is the enlarged diagram of III part of Fig. 2 middle fuselage；
Fig. 4 is the elevational schematic view of the upper casing of embodiment according to the present invention；
Fig. 5 is schematic cross-section of the upper casing in Fig. 4 along V-V line；
Fig. 6 is the enlarged diagram of VI part of upper casing in Fig. 5；
Fig. 7 is the schematic top plan view of the lower casing of embodiment according to the present invention；
Fig. 8 is schematic cross-section of the lower casing in Fig. 7 along VIII-VIII line；
Fig. 9 is the enlarged diagram of Ⅸ part of lower casing in Fig. 8；
Figure 10 is schematic cross-section of the fuselage in Fig. 1 along Ⅹ-Ⅹ line；
Figure 11 is the enlarged diagram of Ⅺ part of Figure 10 middle fuselage；
Figure 12 is the enlarged diagram of Ⅻ part of Fig. 1 middle fuselage；
Figure 13 is the floor map of the guard assembly of embodiment according to the present invention；
Figure 14 is schematic cross-section of the guard assembly in Figure 13 along XIV-XIV；
Figure 15 is the schematic top plan view of the unmanned plane of embodiment according to the present invention.
Main element and symbol description:
Unmanned plane 100, fuselage 10, upper casing 11, upper casing groove 112, upper mounting surface 114, lower casing 12, convex block 122, lower mounting surface 124, fuselage sealing element 13, mounting portion 14, interface slot 142, guide groove 144, tail shell 15, ontology 152, upper plate 1522, lower plate 1524, side plate 1525, upper groove 1526, lower groove 1528, tail shell sealing element 154, upper seal 1542, lower seal 1544, accommodating space 16, ventilation opening 17, air inlet 172, air outlet 174, guard assembly 18, partition 182, mainboard 1822, shielding plate 1824, ventilation hole 1826, filter screen 184, through-hole 1842, shell 186, strip-shaped hole 1862, external interface 20, data interaction Interface 22, expansion signal interface 24, expansion of power supply interface 26, horn 30.
Embodiments of the present invention are described below in detail, the example of the embodiment is shown in the accompanying drawings, and in which the same or similar labels are throughly indicated same or similar element or elements with the same or similar functions.It is exemplary below with reference to the embodiment of attached drawing description, for explaining only the invention, and is not considered as limiting the invention.
In the description of the present invention, it is to be understood that, term " first ", " second " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance or implicitly indicate the quantity of indicated technical characteristic." first " is defined as a result, the feature of " second " can explicitly or implicitly include one or more feature.In the description of the present invention, the meaning of " plurality " is two or more, unless otherwise specifically defined.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can be mechanical connection, be also possible to be electrically connected or can be in communication with each other；It can be directly connected, the connection inside two elements or the interaction relationship of two elements can also be can be indirectly connected through an intermediary.For the ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific conditions.
Following disclosure provides many different embodiments or example is used to realize different structure of the invention.In order to simplify disclosure of the invention, hereinafter to the component of specific examples and being set for describing.Certainly, they are merely examples, and is not intended to limit the present invention.In addition, the present invention repeat reference numerals and/or reference letter, this repetition can be for purposes of simplicity and clarity, itself not indicate the relationship between discussed various embodiments and/or setting in different examples.In addition, the present invention provides various specific techniques and material example, but those of ordinary skill in the art may be aware that other techniques application and/or other materials use.
Fig. 1-Fig. 3 and Figure 15 is please referred to, the fuselage 10 of the unmanned plane 100 of embodiment of the present invention includes upper casing 11 and lower casing 12.Fuselage 10 can be used as the installation carrier of the functional units such as the horn 30 of unmanned plane 100, flight control system, processor; when upper casing 11 and lower casing 12 cooperate; a relatively closed space is formed in fuselage 10 to protect the functional unit being mounted in fuselage 10; such as defencive function component not by the erosion of rainwater, not by the pollution of dust impurity, therefore require fuselage 10 with preferable leakproofness with the protective performances such as waterproof and dustproof, anti-pollution, anti-impurity.
Fig. 4-Fig. 6 is please referred to, in embodiments of the present invention, upper casing 11 refers to the top half of fuselage 10 when unmanned plane 100 is just put.Upper casing 11 includes upper casing groove 112.Specifically, upper casing 11 includes upper mounting surface 114, and upper mounting surface 114 is located at the periphery of upper casing 11, and upper casing groove 112 is provided on mounting surface 114.
Fig. 7-Fig. 9 is please referred to, lower casing 12 refers to the lower half portion of fuselage 10 when unmanned plane 100 is just put.Lower casing 12 includes convex block 122.Specifically, lower casing 12 includes lower mounting surface 124, and lower mounting surface 124 is located at the periphery of lower casing 12, and convex block 122 is upwardly extended from lower mounting surface 124.
Upper casing groove 112 can be along the depth direction of upper casing groove 112 it is vertical be also possible to it is inclined, accordingly, convex block 122 can be in the short transverse of convex block 122 it is vertical be also possible to it is inclined.Certainly, if convex block 122 is along short transverse be it is inclined, upper casing groove 112 should also tilt in the same direction with convex block 122 along short transverse along depth direction.
Along the depth direction of upper casing groove 112, the size of upper casing groove 112 can be it is identical be also possible to it is different, accordingly, in the short transverse of convex block 122, the size of convex block 122 can be it is identical be also possible to it is different.Such as the size of upper casing groove 112 can successively decrease along the direction of notch to the slot bottom of upper casing groove 112 and the size of convex block 122 can successively decrease along from lower mounting surface 124 to the direction far from lower mounting surface 124.
Upper casing groove 112 can extend one week in the periphery of upper casing 11, and accordingly, convex block 122 extends one week along the periphery of lower casing 12.Upper casing groove 112 can also be provided with the medium position of the periphery of upper casing 11, and accordingly, the medium position of the periphery of lower casing 12 and corresponding with the position of upper casing groove 112 is arranged in convex block 122.
When lower casing 12 and upper casing 11 cooperate, convex block 122 protrudes into upper casing groove 112 and cooperates with upper casing groove 112, the abutment of the periphery of the periphery and lower casing 12 of upper casing 11 is face contact, specifically, it can be that mounting surface 114 is in contact with lower mounting surface 124 and/or the top surface of convex block 122 is in contact with the slot bottom of upper casing groove 112.
In above-mentioned fuselage 10, when lower casing 12 and upper casing 11 cooperate, convex block 122 can extend into upper casing groove 112 to cooperate with upper casing groove 112, so that water droplet, which is not easy the fit clearance between lower casing 12 and upper casing 11, enters fuselage 10, the protective performance of fuselage 10 is preferable.Meanwhile convex block 122 and upper casing groove 112 cooperate but also fuselage 10 during installation, upper casing 11 and lower casing 12 are easy positioning.
Referring to Fig. 3, in some embodiments, fuselage 10 further includes fuselage sealing element 13.Fuselage is close
Sealing 13 is housed in upper casing groove 112, and when convex block 122 protrudes into upper casing groove 112 and cooperates with upper casing groove 112, convex block 122 offsets with fuselage sealing element 13.Specifically, fuselage sealing element 13 can be marine glue, fuselage sealing element 13 can inject upper casing groove 112 by way of gluing, since fuselage sealing element 13 has preferable elasticity, when so that convex block 122 and fuselage sealing element 13 offseting, gap between convex block 122 and fuselage sealing element 13 is smaller, further reduces the fit clearance between upper casing 11 and lower casing 12, improves the protective performance of fuselage 10.
It should be noted that convex block 122 offsets with fuselage sealing element 13, it can be the only top surface of convex block 122 and offset with fuselage sealing element 13, the side of the top surface and convex block 122 that are also possible to convex block 122 offsets with fuselage sealing element 13.When fuselage sealing element 13 being injected upper casing groove 112 by way of gluing, convex block 122 can be protruded into upper casing groove 112 again after fuselage sealing element 13 is fully cured and cooperated with upper casing groove 112.It is also possible to convex block 122 is protruded into upper casing groove 112 when fuselage sealing element 13 is not fully cured and cooperates with upper casing groove 112, fuselage sealing element 13 is more liquid at this time, due to the squeezing action of convex block 122, fuselage sealing element 13 can be full of the space between the side wall of convex block 122 and the inner wall of upper casing groove 112.
Figure 10-Figure 11 is please referred to, in some embodiments, fuselage 10 further includes mounting portion 14 and tail shell 15.The rear end of fuselage 10, that is, the rear end of 10 direction of advance of fuselage is arranged in mounting portion 14, and in embodiments of the present invention, the rear end of upper casing 11 is arranged in mounting portion 14.Mounting portion 14 is flexibly connected with tail shell 15, and specifically, tail shell 15 can be set on mounting portion 14, can also be extracted out from mounting portion 14 and be separated with mounting portion 14.
Mounting portion 14 includes interface slot 142 and guide groove 144.
Unmanned plane 100 includes external interface 20, and external interface 20 includes one or more of data interaction interface 22, expansion signal interface 24 and expansion of power supply interface 26 (as shown in Figure 2).Data interaction interface 22 is interacted for unmanned plane 100 with external memory.Expansion signal interface 24 is communicated to connect for the sensor of unmanned plane 100 and peripheral hardware.Sensor of the expansion of power supply interface 26 for unmanned plane 100 to peripheral hardware is powered.External interface 20 is arranged in interface slot 142, specifically, external interface 20 is arranged on the inner surface of interface slot 142, so that external interface 20 is in semi-enclosed space to allow external lug to protrude into interface slot 142 and connect with external interface 20, and when tail shell 15 is set on mounting portion 14, external interface 20 is then to prevent the impurity such as dust and/or water droplet from entering external interface 20 in the enclosure space that tail shell 15 and interface slot 142 are formed.
Incorporated by reference to Figure 12, guide groove 144 is corresponding with interface slot 142 and is located at the top of interface slot 142.The extending direction of guide groove 144 is identical as the extending direction of interface slot 142.
Tail shell 15 includes ontology 152 and tail shell sealing element 154.Tail shell sealing element 154 is fixed on the inner surface of ontology 152, when tail shell 15 is set on mounting portion 14, ontology 152 is set on mounting portion 14 and ontology 152 partially protrudes into interface slot 142 and blocks interface slot 142, tail shell sealing element 154 seals the junction of mounting portion 14 and tail shell 15 simultaneously, that is to say the junction of sealing mounting portion 14 and ontology 152.
Ontology 152 includes upper plate 1522, lower plate 1524 and the side plate 1525 for connecting upper plate 1522 and lower plate 1524.In embodiments of the present invention, when ontology 152 is set on mounting portion 14, upper plate 1522 protrudes into guide groove 144 and lower plate 1524 protrudes into interface slot 142, while side plate 1525 blocks interface slot 142.Upper groove 1526 is offered on the side wall of upper plate 1522, and lower groove 1528 is offered on the side wall of lower plate 1524.
Tail shell sealing element 154 includes upper seal 1542 and lower seal 1544.
1542 partial receipt of upper seal is in upper groove 1526, when upper plate 1522 protrudes into guide groove 144, upper seal 1542 and the side wall of guide groove 144 offset, since upper seal 1542 has preferable elasticity, when so that the side wall of upper seal 1542 and guide groove 144 offseting, gap between upper seal 1542 and the side wall of guide groove 144 is smaller, and the impurity such as dust and/or water droplet are not easy to pass through from gap between the two.Upper seal 1542 includes marine glue, and upper seal 1542 can be injected in upper groove 1526 by way of gluing.
1544 partial receipt of lower seal is in lower groove 1528, when lower plate 1524 protrudes into interface slot 142, lower seal 1544 and the side wall of interface slot 142 offset, since lower seal 1544 has preferable elasticity, when so that the side wall of lower seal 1544 and interface slot 142 offseting, gap between lower seal 1544 and the side wall of interface slot 142 is smaller, and the impurity such as dust and/or water droplet are not easy to pass through from gap between the two.Lower seal 1544 includes marine glue, and lower seal 1544 can be injected in lower groove 1528 by way of gluing.
Please refer to Figure 10, Figure 13 and Figure 14, in some embodiments, upper casing 11 and lower casing 12 cooperatively form accommodating space 16, the functional units such as flight control system, processor can be set in accommodating space 16, fuselage 10 offers the ventilation opening 17 being connected to accommodating space 16, ventilation opening 17 includes the air inlet 172 for being provided with 10 front end of fuselage and the air outlet 174 for being provided with 10 rear end of fuselage, and air can be from air inlet
172 enter accommodating space 16 and carry out heat exchange with the functional unit being arranged in accommodating space 16, such as take away the heat that functional unit work generates, and air flows out accommodating space 16 from air outlet 174 again.
In some embodiments, fuselage 10 further includes guard assembly 18, and guard assembly 18 is arranged at ventilation opening 17 and for blocking the sundries that dust and/or water droplet etc. are mixed in outside air.Guard assembly 18 includes partition 182, filter screen 184 and shell 186.
Partition 182 includes mainboard 1822 and multiple shielding plates 1824 for extending from mainboard 1822, and shielding plate 1824 and mainboard 1822, which can be integrated molding or shielding plate 1824 and mainboard 1822, can be seperated molding be detachably connected.Preferably, shielding plate 1824 and mainboard 1822 are detachably connected, in order to clean and replace partition 182.
Mainboard 1822 offers multiple ventilation holes 1826, and each shielding plate 1824 is substantially in " Z " font, and two adjacent shielding plates 1824 form the air-guiding aisle of a bending.1824 face ventilation hole 1826 of shielding plate setting, to block the dust and/or water droplet that front blows into ventilation hole 1826.After outside air enters guard assembly 18, since shielding plate 1824 is in " Z " font, the impurity such as dust and/or water droplet being mixed in outside air are liable to stick on shielding plate 1824, so that the impurity such as dust and/or water droplet be avoided to enter inside fuselage 10.
Filter screen 184 is set to the side of the separate accommodating space 16 of partition 182, and in one embodiment, mainboard 1822 is compared with shielding plate 1824 closer to filter screen 184.Filter screen 184 offers multiple through-holes 1842, and the full-size of through-hole 1842 is less than the minimum dimension of ventilation hole 1826.Specifically, the size of multiple through-holes 1842 can be identical, and the size of multiple ventilation holes 1826 can also be identical, at this point, the size of through-hole 1842 is less than the size of ventilation hole 1826.Or the size of multiple through-holes 1842 is not exactly the same, the size of multiple ventilation holes 1826 can also be not exactly the same, at this point, maximum 1842 corresponding size (full-size) of through-hole is less than the corresponding size of the smallest ventilation hole 1826 (the smallest size) in all ventilation holes 1826 in all through-holes 1842.Through-hole 1842 on filter screen 184 for filtering air in lesser sundries, the full-size of through-hole 1842 is less than the minimum dimension of the ventilation hole 1826 of partition 182, so that guard assembly 18 reduces windage after having filtered the lesser sundries in air as far as possible, increase the air capacity for entering accommodating space 16, improves the radiating efficiency to each functional unit in accommodating space 16.
Multiple strip-shaped holes 1862 are provided on shell 186, the minimum dimension of strip-shaped hole 1862 is greater than the full-size of through-hole 1842.Specifically, the size of multiple strip-shaped holes 1862 can be identical, Duo Getong
The size in hole 1842 can also be identical, at this point, the size of through-hole 1842 is less than the size of strip-shaped hole 1862.Or the size of multiple through-holes 1842 is not exactly the same, the size of multiple strip-shaped holes 1862 can also be not exactly the same, at this point, the corresponding size of the smallest strip-shaped hole 1862 (the smallest size) is greater than maximum 1842 corresponding size (full-size) of through-hole in all through-holes 1842 in all strip-shaped holes 1862.Shell 186 is arranged on guard assembly 18 farthest away from the position of accommodating space 16, and strip-shaped hole 1862 can protect the functional unit in filter screen 184 and accommodating space 16 with the biggish sundries in filtering external air.In embodiments of the present invention, shell 186 is bonded setting with filter screen 184, and shell 186 enhances the intensity of filter screen 184, and to prevent filter screen 184, deformation occurs.
When outside air enters accommodating space 16 across guard assembly 18, need successively by strip-shaped hole 1862, through-hole 1842, ventilation hole 1826 and air-guiding aisle.When outside air passes through strip-shaped hole 1862, strip-shaped hole 1862, which can filter, is mixed in relatively large sundries in outside air, such as paper, polybag etc..When air, which passes through strip-shaped hole 1862, enters through-hole 1842, through-hole 1842 can filter mixed relatively small in air sundries, such as paper scrap, leaf etc..Air, which passes through after through-hole 1842 enters ventilation hole 1826, enters air-guiding aisle, flow path of the air in air-guiding aisle is more tortuous and multiple-contact occurs for the easy side wall with shielding plate 1824, so that the impurity such as dust and/or water droplet relatively fine in air are liable to stick on shielding plate 1824 without entering accommodating space 16.
In embodiments of the present invention, the quantity of guard assembly 18 is two, and two guard assemblies 18 are separately positioned at air inlet 172 and air outlet 174.The structure of two guard assemblies 18 can be identical, can also be not exactly the same.For example, the middle position of the filter screen 184 for the guard assembly 18 being arranged at air inlet 172 is convex to the direction far from accommodating space 16, and the filter screen 184 that the guard assembly 18 at air outlet 174 is arranged in is tabular.
In some embodiments, the filter screen 184 in guard assembly 18 and/or shell 186 can be omitted.
In some embodiments, guard assembly 18 can be provided only at air inlet 172 or be provided only at air outlet 174.
Figure 15 is please referred to, the unmanned plane 100 of embodiment of the present invention includes fuselage 10 and multiple horns 30.Multiple horns 30 are fixedly connected with fuselage 10, and multiple horns 30 are radially arranged outwardly from fuselage 10.
When the lower casing 12 and upper casing 11 of above-mentioned unmanned plane 100 cooperate, convex block 122 can extend into upper casing
Groove 112 with upper casing groove 112 to cooperate, so that water droplet, which is not easy the fit clearance between lower casing 12 and upper casing 11, enters fuselage 10, the waterproof performance of fuselage 10 is preferable.
In the description of this specification, the description of reference term " embodiment ", " certain embodiments ", " exemplary embodiment ", " example ", " specific example " or " some examples " etc. means to be contained at least one embodiment or example of the invention in conjunction with the embodiment or example particular features, structures, materials, or characteristics described.In the present specification, schematic expression of the above terms are not necessarily referring to identical embodiment or example.Moreover, particular features, structures, materials, or characteristics described can be combined in any suitable manner in any one or more embodiments or example.
In addition, term " first ", " second " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance or implicitly indicate the quantity of indicated technical characteristic." first " is defined as a result, the feature of " second " can explicitly or implicitly include at least one of the features.In the description of the present invention, the meaning of " plurality " is at least two, such as two, three etc., unless otherwise specifically defined.
Although embodiments of the present invention have been shown and described above, it can be understood that, above embodiment is exemplary, it is not considered as limiting the invention, those skilled in the art can be changed above embodiment within the scope of the invention, modify, replacement and variant.
Claims (30)
- A kind of fuselage of unmanned plane, which is characterized in that the fuselage includes:Upper casing, the upper casing include the upper casing groove for being provided with the upper casing periphery；AndWith the lower casing of the top shells fit, when the lower casing includes the convex block that the lower casing periphery is arranged in, the lower casing and the top shells fit, the convex block can extend into the upper casing groove to cooperate with the upper casing groove.
- The fuselage of unmanned plane as described in claim 1, which is characterized in that the fuselage further includes the fuselage sealing element being housed in the upper casing groove, the convex block when cooperating with the upper casing groove convex block offset with the fuselage sealing element.
- The fuselage of unmanned plane as claimed in claim 2, which is characterized in that the fuselage sealing element includes marine glue, and the marine glue injects the upper casing groove by way of gluing.
- The fuselage of unmanned plane as described in claim 1, which is characterized in that the upper casing groove extends one week along the periphery of the upper casing, and the convex block extends one week along the periphery of the lower casing；OrThe upper casing groove is provided with the medium position of the periphery of the upper casing, and the convex block is set to the medium position of the periphery of the lower casing, and when the convex block and the upper casing groove cooperate, the abutment of the periphery of the periphery of the upper casing and the lower casing is face contact.
- The fuselage of unmanned plane as described in claim 1-4 any one, it is characterized in that, the fuselage includes the tail shell that the mounting portion of rear end is arranged in and is flexibly connected with the mounting portion, the tail shell includes the tail shell sealing element of ontology and the inner surface for being fixed on the ontology, the ontology can be set on the mounting portion, so that the tail shell sealing element seals the junction of the mounting portion Yu the tail shell.
- The fuselage of unmanned plane as described in claim 5, which is characterized in that the unmanned plane includes external interface, the mounting portion includes interface slot, the inner surface of the interface slot is arranged in the external interface, and the ontology can partially protrude into the interface slot and block the interface slotThe external interface includes following at least one: the data interaction interface for interacting with external memory, for the expansion signal interface with the communication connection of the sensor of peripheral hardware, the expansion of power supply interface powered for the sensor to peripheral hardware.
- The fuselage of unmanned plane as claimed in claim 6, it is characterized in that, the mounting portion includes guide groove, the guide groove is corresponding with the interface slot and is located at the top of the interface slot, the ontology includes the side plate of upper plate, lower plate and the connection upper plate and the lower plate, when the ontology protrudes into the interface slot, the upper plate protrudes into the guide groove and the lower plate protrudes into the interface slot.
- The fuselage of unmanned plane as claimed in claim 7, it is characterized in that, offering upper groove on the side wall of the upper plate, the tail shell sealing element includes upper seal of the partial receipt in the upper groove, when the upper plate protrudes into the guide groove, the upper seal and the side wall of the guide groove offset.
- The fuselage of unmanned plane as claimed in claim 8, which is characterized in that the upper seal includes marine glue, and the marine glue injects the upper groove by way of gluing.
- The fuselage of unmanned plane as claimed in claim 7, it is characterized in that, lower groove is offered on the side wall of the lower plate, the tail shell sealing element includes lower seal of the partial receipt in the lower groove, when the lower plate protrudes into the interface slot, the lower seal and the side wall of the interface slot offset.
- The fuselage of unmanned plane as described in claim 1-4 any one, it is characterized in that, the upper casing and the lower casing cooperatively form accommodating space, the fuselage offers the ventilation opening being connected to the accommodating space, the fuselage further includes guard assembly, the guard assembly is arranged in the ventilation opening, for blocking dust and/or water droplet.
- The fuselage of unmanned plane as claimed in claim 11, it is characterized in that, the guard assembly includes partition, the partition includes mainboard and multiple shielding plates for extending from the mainboard, the mainboard offers multiple ventilation holes, the setting of ventilation hole described in the shielding plate face, to block the dust and/or water droplet that front blows into the ventilation hole.
- The fuselage of unmanned plane as claimed in claim 12, it is characterized in that, the guard assembly further includes filter screen, side of the partition far from the accommodating space is arranged in the filter screen, the filter screen offers multiple through-holes, and the full-size of the through-hole is less than the minimum dimension of the ventilation hole of the partition.
- The fuselage of unmanned plane as claimed in claim 13, which is characterized in that the guard assembly further includes shell, and multiple strip-shaped holes are provided on the shell, and the minimum dimension of the strip-shaped hole is greater than the full-size of the through-hole of the filter screen.
- The fuselage of unmanned plane as claimed in claim 11, which is characterized in that the ventilation opening includes the air outlet for being provided with the air inlet of the front fuselage and being provided with the back body.
- A kind of unmanned plane characterized by comprisingThe fuselage of unmanned plane；AndMultiple horns are fixedly connected with the fuselage, and are radially arranged outwardly from the fuselage；The fuselage includes:Upper casing, the upper casing include the upper casing groove for being provided with the upper casing periphery；AndWith the lower casing of the top shells fit, when the lower casing includes the convex block that the lower casing periphery is arranged in, the lower casing and the top shells fit, the convex block can extend into the upper casing groove to cooperate with the upper casing groove.
- Unmanned plane as claimed in claim 16, which is characterized in that the fuselage further includes the fuselage sealing element being housed in the upper casing groove, the convex block when cooperating with the upper casing groove convex block offset with the fuselage sealing element.
- Unmanned plane as claimed in claim 17, which is characterized in that the fuselage sealing element includes marine glue, and the marine glue injects the upper casing groove by way of gluing.
- Unmanned plane as claimed in claim 16, which is characterized in that the upper casing groove is on described The periphery of shell extends one week, and the convex block extends one week along the periphery of the lower casing；OrThe upper casing groove is provided with the medium position of the periphery of the upper casing, and the convex block is set to the medium position of the periphery of the lower casing, and when the convex block and the upper casing groove cooperate, the abutment of the periphery of the periphery of the upper casing and the lower casing is face contact.
- Unmanned plane as described in claim 16-19 any one, it is characterized in that, the fuselage includes the tail shell that the mounting portion of rear end is arranged in and is flexibly connected with the mounting portion, the tail shell includes the tail shell sealing element of ontology and the inner surface for being fixed on the ontology, the ontology can be set on the mounting portion, so that the tail shell sealing element seals the junction of the mounting portion Yu the tail shell.
- Unmanned plane as described in claim 20, which is characterized in that the unmanned plane includes external interface, the mounting portion includes interface slot, the inner surface of the interface slot is arranged in the external interface, and the ontology can partially protrude into the interface slot and block the interface slotThe external interface includes following at least one: the data interaction interface for interacting with external memory, for the expansion signal interface with the communication connection of the sensor of peripheral hardware, the expansion of power supply interface powered for the sensor to peripheral hardware.
- Unmanned plane as claimed in claim 21, it is characterized in that, the mounting portion includes guide groove, the guide groove is corresponding with the interface slot and is located at the top of the interface slot, the ontology includes the side plate of upper plate, lower plate and the connection upper plate and the lower plate, when the ontology protrudes into the interface slot, the upper plate protrudes into the guide groove and the lower plate protrudes into the interface slot.
- Unmanned plane as claimed in claim 22, it is characterized in that, offering upper groove on the side wall of the upper plate, the tail shell sealing element includes upper seal of the partial receipt in the upper groove, when the upper plate protrudes into the guide groove, the upper seal and the side wall of the guide groove offset.
- Unmanned plane as claimed in claim 23, which is characterized in that the upper seal includes marine glue, and the marine glue injects the upper groove by way of gluing.
- Unmanned plane as claimed in claim 22, it is characterized in that, offering lower groove on the side wall of the lower plate, the tail shell sealing element includes lower seal of the partial receipt in the lower groove, when the lower plate protrudes into the interface slot, the lower seal and the side wall of the interface slot offset.
- Unmanned plane as described in claim 16-19 any one, it is characterized in that, the upper casing and the lower casing cooperatively form accommodating space, the fuselage offers the ventilation opening being connected to the accommodating space, the fuselage further includes guard assembly, the guard assembly is arranged in the ventilation opening, for blocking dust and/or water droplet.
- Unmanned plane as claimed in claim 26, it is characterized in that, the guard assembly includes partition, the partition includes mainboard and multiple shielding plates for extending from the mainboard, the mainboard offers multiple ventilation holes, the setting of ventilation hole described in the shielding plate face, to block the dust and/or water droplet that front blows into the ventilation hole.
- Unmanned plane as claimed in claim 27, it is characterized in that, the guard assembly further includes filter screen, side of the partition far from the accommodating space is arranged in the filter screen, the filter screen offers multiple through-holes, and the full-size of the through-hole is less than the minimum dimension of the ventilation hole of the partition.
- Unmanned plane as claimed in claim 28, which is characterized in that the guard assembly further includes shell, and multiple strip-shaped holes are provided on the shell, and the minimum dimension of the strip-shaped hole is greater than the full-size of the through-hole of the filter screen.
- Unmanned plane as claimed in claim 26, which is characterized in that the ventilation opening includes the air outlet for being provided with the air inlet of the front fuselage and being provided with the back body.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720175994.XU CN206528613U (en) | 2017-02-24 | 2017-02-24 | The fuselage and unmanned plane of unmanned plane |
| CN201720175994X | 2017-02-24 | ||
| PCT/CN2017/077744 WO2018152911A1 (en) | 2017-02-24 | 2017-03-22 | Fuselage of unmanned aerial vehicle and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109641645A true CN109641645A (en) | 2019-04-16 |
Family
ID=59919637
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720175994.XU Expired - Fee Related CN206528613U (en) | 2017-02-24 | 2017-02-24 | The fuselage and unmanned plane of unmanned plane |
| CN201780053436.9A Pending CN109641645A (en) | 2017-02-24 | 2017-03-22 | The fuselage and unmanned plane of unmanned plane |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720175994.XU Expired - Fee Related CN206528613U (en) | 2017-02-24 | 2017-02-24 | The fuselage and unmanned plane of unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN206528613U (en) |
| WO (1) | WO2018152911A1 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206528613U (en) * | 2017-02-24 | 2017-09-29 | 深圳市大疆创新科技有限公司 | The fuselage and unmanned plane of unmanned plane |
| CN109070988B (en) * | 2017-12-29 | 2022-01-14 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle's visor, fuselage subassembly and unmanned aerial vehicle of fuselage |
| CN109070987B (en) * | 2017-12-29 | 2022-07-15 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle's horn subassembly and unmanned aerial vehicle |
| CN111007207A (en) * | 2019-12-26 | 2020-04-14 | 重庆溢哲渝实业有限公司 | Simple installation and dirt-proof humidity sensor module |
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| IL199230A0 (en) * | 2009-06-08 | 2011-07-31 | Elta Systems Ltd | Air vehicle |
| CN205738053U (en) * | 2016-05-16 | 2016-11-30 | 哈瓦国际航空技术（深圳）有限公司 | A kind of unmanned plane structure |
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2017
- 2017-02-24 CN CN201720175994.XU patent/CN206528613U/en not_active Expired - Fee Related
- 2017-03-22 WO PCT/CN2017/077744 patent/WO2018152911A1/en active Application Filing
- 2017-03-22 CN CN201780053436.9A patent/CN109641645A/en active Pending
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| EP1397289B1 (en) * | 2001-06-05 | 2007-03-07 | Saab Ab | Device for bracing a shell in an aircraft fuselage |
| US8602357B2 (en) * | 2009-06-22 | 2013-12-10 | Airbus Operations Gmbh | Installation system for the connection of systems to a structure of an aircraft, a measurement system and a method |
| CN205524925U (en) * | 2016-01-26 | 2016-08-31 | 河北三丰航空科技发展有限公司 | It is alert with waterproof unmanned aerial vehicle of antifog smoke protection |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN206528613U (en) | 2017-09-29 |
| WO2018152911A1 (en) | 2018-08-30 |
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