CN110116798A - A kind of unmanned thermomechanical components and unmanned plane - Google Patents
A kind of unmanned thermomechanical components and unmanned plane Download PDFInfo
- Publication number
- CN110116798A CN110116798A CN201910426335.2A CN201910426335A CN110116798A CN 110116798 A CN110116798 A CN 110116798A CN 201910426335 A CN201910426335 A CN 201910426335A CN 110116798 A CN110116798 A CN 110116798A
- Authority
- CN
- China
- Prior art keywords
- component
- assembly
- unmanned
- hole
- thermomechanical components
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
- B64C1/069—Joining arrangements therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Abstract
Present patent application proposes a kind of unmanned thermomechanical components, and the component plays waterproof action, for preventing the UAV Components in component from contacting with water；The component includes first assembly and the second component；The first assembly includes at least one opening, and second component is used to close the opening of first assembly to prevent water from pouring into component from opening；Present patent application expands the application range of common UAV Components, and common UAV Components can be made to have water-proof function.
Description
Technical field
The present invention relates to air vehicle technique fields.
Background technique
For existing common unmanned plane greatly most without water-proof function, even waterproof unmanned plane and design structure is complicated
It without versatility, and the heat dissipation of existing waterproof unmanned plane and is not all well solved, limits with the connectivity of air
Application scenarios and the region of unmanned plane are made.
The content of background technology part is only the technology that inventor is known, not the existing skill of natural representative this field
Art.
Summary of the invention
While to make common unmanned plane that there is water-proof function, the radiating efficiency and air communication of unmanned plane are improved
Property, propose the invention patent.
The invention proposes a kind of unmanned thermomechanical components, and the component plays waterproof action, for preventing the unmanned plane in component
Component is contacted with water；The component includes first assembly and the second component；The first assembly includes at least one opening, described
Second component is used to close the opening of first assembly to prevent water from pouring into component from opening.
It is provided at least one through-hole in the unmanned thermomechanical components, is passed through for the UAV Components in unmanned thermomechanical components logical
Hole connects external equipment.
The through-hole is set in first assembly that the perhaps through-hole is set on the second component or the through-hole is set
It is placed in the junction of first assembly and the second component.
The through-hole is set to first assembly and the junction of the second component includes that a part of through-hole is set to first group
On part, another part of through-hole is set on the second component, in the connection after opening of the second component closing first assembly
Place forms complete through-hole.
There is sealing ring in the junction of second component and first assembly, to prevent water from penetrating into component from the junction
It is interior.
Together with the first assembly and the second component are snapped connection by least one, to close opening for first assembly
Mouthful.
The buckle includes pillar and cutting ferrule；The cutting ferrule is by socket pillar to fix first assembly and the second component
It links together.
The cutting ferrule is set in first assembly, and the pillar is set on the second component.
The unmanned thermomechanical components further include rotatable parts, and the rotatable parts include Rotational Cylindrical and rotation slot, the rotation
Column is set on the second component, and the rotation slot is set in first assembly；Second component is by rotatable parts with the
To be rotated relative to first assembly in the state of the connection of one component.
It is provided with sealing ring around the through-hole, in external equipment when passing through through-hole to prevent external device and unmanned plane
The local leak of component touch.
The first assembly and/or the second component is at least a part of is transparent.
The shape of the first assembly and/or the shape of the second component are oval or round.
The unmanned thermomechanical components further include waterproof and breathable component；
The waterproof and breathable component is set in unmanned thermomechanical components, can prevent leak and gas is allowed to pass through.
The waterproof and breathable component is waterproof ventilated membrane.
The component that the unmanned thermomechanical components domestic demand will be contacted with air is connect with waterproof and breathable component.
The unmanned thermomechanical components further include thermal component；
The thermal component is set in unmanned thermomechanical components, and the heat that can generate unmanned plane component internal passes through heat dissipation
Component outflow.
Heat generating components in the unmanned thermomechanical components and thermal component are close or contact.
The thermal component is to be made of thermally conductive good material.
The invention discloses a kind of unmanned plane, the unmanned plane includes the unmanned thermomechanical components and unmanned plane main body；Institute
Stating unmanned plane main body includes unmanned aerial vehicle body main body and horn；The unmanned aerial vehicle body main body is installed in unmanned thermomechanical components, institute
Horn is stated to connect across through-hole with unmanned aerial vehicle body main body.
As it can be seen that can make common unmanned plane that there is water-proof function using technical solution of the present invention, solve waterproof unmanned plane
Heat dissipation and the problem of air communication, extends the application scenarios of unmanned plane so that common unmanned plane be also provided with it is amphibious
Flight function, even also can takeoff and landing in the rainy day.
Detailed description of the invention
Fig. 1 is the schematic diagram of the first unmanned thermomechanical components of the embodiment of the present invention；
Fig. 2 is the schematic diagram of second of unmanned thermomechanical components of the embodiment of the present invention；
Fig. 3 is the schematic diagram of the third unmanned thermomechanical components of the embodiment of the present invention；
Fig. 4 is second of schematic diagram of the third unmanned thermomechanical components of the embodiment of the present invention；
Fig. 5 is the third unmanned thermomechanical components and unmanned plane combination diagram of the embodiment of the present invention；
Fig. 6 is second of schematic diagram that the third unmanned thermomechanical components of the embodiment of the present invention are combined with unmanned plane；
Fig. 7 is the third schematic diagram of the third unmanned thermomechanical components of the embodiment of the present invention；
Fig. 8 is the 4th kind of schematic diagram of the third unmanned thermomechanical components of the embodiment of the present invention；
Fig. 9 is the schematic diagram in the unmanned thermomechanical components of the embodiment of the present invention comprising waterproof and breathable component；
Figure 10 is the schematic diagram in the unmanned thermomechanical components of the embodiment of the present invention comprising thermal component；
Figure 11 is a kind of schematic diagram of unmanned plane of the embodiment of the present invention；
100 unmanned 101 first assemblies of thermomechanical components；
102 second components；103 openings；
104 water proof rings；105 through-holes；
106 unmanned aerial vehicle body main bodys；107 external equipments；
108 pillars；109 cutting ferrules；
110 Rotational Cylindricals；111 rotation slots；
1111 structural slabs；112 waterproof and breathable components；
113 thermal components；114 unmanned plane horns；
Specific embodiment
Hereinafter, certain exemplary embodiments are simply just described.As one skilled in the art will recognize that
Like that, without departing from the spirit or scope of the present invention, described embodiment can be modified by various different modes.
Therefore, attached drawing and description are considered essentially illustrative rather than restrictive.
In the description of the present invention, it is to be understood that, term " center ", " longitudinal direction ", " transverse direction ", " length ", " width
Degree ", " thickness ", " go up ", " under ", " preceding ", " afterwards ", " left side ", " right side ", " heavily fortified point, and directly ", " level ", " top ", " bottom ", " is interior ", " outside ", "
Clockwise ", " counterclockwise " wait the orientation or positional relationship of instructions to be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for description the present invention and simplify description, rather than the device or component of indication or suggestion meaning must have a particular orientation,
It is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In the description of the present invention, " multiple "
It is meant that 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 ", " phase
Even ", " 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: can
To be mechanical connection, it is also possible to be electrically connected or can mutually communicate；It can be directly connected, it can also be by between intermediary
It connects connected, can be the connection inside two elements or the interaction relationship of two elements.For the ordinary skill of this field
For personnel, the specific meanings of the above terms in the present invention can be understood according to specific conditions.
In the present invention unless specifically defined or limited otherwise, fisrt feature second feature its " upper " or it " under "
It may include that the first and second features directly contact, also may include that the first and second features are not direct contacts but pass through it
Between other characterisation contact.Moreover, fisrt feature second feature " on ", " top " and " above " include first spy
Sign is right above second feature and oblique upper, or is merely representative of first feature horizontal height higher than second feature.Fisrt feature exists
Second feature " under ", " lower section " and " following " be directly below and diagonally below the second feature including fisrt feature, or be merely representative of
First feature horizontal height is less than second feature.
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 the component of specific examples and setting are described.Certainly, they are merely examples, and
And it is not intended to limit the present invention.In addition, the present invention can in different examples repeat reference numerals and/or reference letter,
This repetition is for purposes of simplicity and clarity, itself not indicate between discussed various embodiments and/or setting
Relationship.
Hereinafter, preferred embodiments of the present invention will be described with reference to the accompanying drawings, it should be understood that preferred reality described herein
Apply example only for the purpose of illustrating and explaining the present invention and is not intended to limit the present invention.
As shown in Figure 1, a kind of embodiment disclosed by the invention is a kind of unmanned thermomechanical components 100, the component plays waterproof and makees
With for preventing the UAV Components in component from contacting with water；The component includes first assembly 101 and the second component 102；Institute
Stating first assembly 101 includes at least one opening, and second component 102 is used to close the opening of first assembly 101 to prevent
Water pours into component from opening.
First assembly 101 has waterproof action, has at least one opening in first assembly 101, can by the opening
UAV Components are put into first assembly 101, to prevent water from pouring into first assembly 102 by opening, pass through the second component
102 by the closure of openings；The UAV Components can be a part of unmanned plane entirety or unmanned plane.
In one embodiment, only has an opening in the first assembly 101, the second component 102 is for closing first
Opening on component 101, as shown in Figure 1, by the other openings of closing alternatively, UAV Components can enter nothing by opening
In man-machine component 100,
For example, the first assembly 101 is made of elastic material, second component 102 is waterproof slide fastener；Further
, the first assembly 101 being made of elastic material is unmanned plane housing, and unmanned plane passes through the opening in first assembly 101
It fills in first assembly 101, using waterproof slide fastener by closure of openings, to play the role of protecting unmanned plane；Second component
102 can also be waterproof buckle or the second component 102 is other can to prevent water from pouring into from the opening of first assembly 101
Waterproof part.
On the basis of Fig. 1, further as shown in Fig. 2, having at least in the first assembly 101 being made of elastic material
One through-hole 105, external equipment pass through through-hole 105 and connect with the unmanned aerial vehicle body in first assembly 101, the first assembly
101 because the reason of elastic material, is fitted closely in the place contacted with external equipment to prevent water from passing through external equipment and the
The place of one component 101 contact is penetrated into, so that the UAV Components in first assembly 101 have water-proof function；
When the UAV Components in first assembly 101 are unmanned aerial vehicle body main bodys, the external equipment be can be
Unmanned plane horn, unmanned plane horn and unmanned aerial vehicle body main body form waterproof unmanned plane；The external equipment can also be other
The equipment that can be connect with the unmanned aerial vehicle body main body in first assembly 101, for example the external equipment is hand-held support, it is described
Hand-held support forms watertight handheld camera with the unmanned aerial vehicle body main body with holder camera.
As shown in Figure 3 and Figure 4, the embodiment of the invention discloses a kind of unmanned thermomechanical components 100, the component plays waterproof and makees
With for preventing the UAV Components in component from contacting with water；The component includes first assembly 101 and the second component 102；Institute
Stating first assembly 101 includes at least one opening 103, and second component 102 is used to close the opening 103 of first assembly 101
To prevent water from pouring into component from opening 103.
The UAV Components can be a part of unmanned plane entirety or unmanned plane.
At least one opening 103 in the first assembly 101, second component 102 can close first assembly 101
On opening 103 to form complete unmanned thermomechanical components 100, the junction of the second component 102 and first assembly 101 is provided with anti-
Hydrosphere 104, with prevent the second component 102 closing first assembly 101 opening 103 after water by junction infiltration, in some feelings
Under condition, the water proof ring 104 is elastic material；Fluted, the water proof ring is set at the opening 103 of the first assembly 101
104 are fixed at the opening 103 of first assembly 101 by groove, alternatively, being provided at the opening 103 of the first assembly 101
Protrusion, the water proof ring 104 are fixed in the protrusion at the opening 103 of first assembly 101 by the groove of itself；When first group
When part 101 and the second component 102 merge, by first assembly 101 and the second component 102 in junction to the crowded of water proof ring 104
It presses to fill up the gap of junction, so that waterproof action is played in junction；For example, unmanned plane passes through opening in first assembly 101
Mouth 103 is directly placed into unmanned thermomechanical components 100, forms a kind of waterproof unmanned plane.
Further, it is provided at least one through-hole 105 in the unmanned thermomechanical components 100, in unmanned thermomechanical components 100
UAV Components by through-hole 105 connect external equipment；The through-hole 105 is set in first assembly 101 or described logical
Hole is set on the second component 102 or the through-hole is set to the junction of first assembly 101 and the second component 102；It is external
Equipment passes through through-hole 105 and connect with the UAV Components in unmanned thermomechanical components 100, is provided with water proof ring around the through-hole 105
104, the local leak contacted around external equipment and through-hole can be prevented；Further, the water proof ring 104 is elastic material
Matter, 105 surrounding of the through-hole setting is fluted, and the water proof ring 104 is fixed on around through-hole 105 by groove, alternatively, described
Protrusion is provided with around through-hole 105, the water proof ring 104 is fixed in the protrusion around through-hole by the groove of itself.
When the through-hole 105 is set to the junction of first assembly 101 and the second component 102, the one of through-hole 105
Part is set in first assembly 101, and another part of through-hole is set on the second component, around two parts of through-hole 105 all
It is provided with water proof ring 104, is formed completely behind opening 103 of the second component 102 closing first assembly 101 in the junction
Through-hole 105；Water proof ring 104 around the through-hole is also classified into two parts, the waterproof around through-hole 105 in first assembly 101
Circle 104 is connect with the water proof ring 104 of 101 junction of first assembly, when the opening 103 of the second component 102 closing first assembly 101
Afterwards, 105 surrounding of through-hole forms complete water proof ring 104.
For example, as shown in Figure 5 and Figure 6, the UAV Components inside the unmanned thermomechanical components 100 are unmanned aerial vehicle body main bodys
106, unmanned aerial vehicle body main body 106 is packed into first assembly by the opening in first assembly, by described in the closing of the second component
Opening, the external equipment 107 passes through through-hole and connect with unmanned aerial vehicle body main body, when the external equipment 107 is unmanned plane machine
When arm, complete waterproof unmanned plane is formed；When the external equipment 107 is the dynamic equipment of other bands or mechanical knot
When structure, complete water proof type intelligent apparatus is formed.
As shown in fig. 7, together with the first assembly 101 and the second component 102 snapped connection by least one, with envelope
Close the opening of first assembly；The buckle includes pillar 108 and cutting ferrule 109；The cutting ferrule 109 by socket pillar 108 with incite somebody to action
First assembly 101 and the second component 102 are fixed together；The cutting ferrule 109 is set on the second component 102, described convex
Column 108 is set in first assembly 101；When the second component 102 is connect with first assembly 101, the cutting ferrule 109 stretches out
To be socketed on pillar 108, by pulling back cutting ferrule 109 so that first assembly 101 and the second component 102 are closely connected to one
It rises；By the effect of buckle, but also sealing is played the role of in the junction of first assembly 101 and the second component 102.
As shown in figure 8, the unmanned thermomechanical components further include rotatable parts, the rotatable parts include Rotational Cylindrical 110 and turn
Dynamic slot 111, the Rotational Cylindrical 110 are set on the second component 102, and the rotation slot 111 is set in first assembly 101；Institute
It states the second component 102 and passes through rotatable parts in the state of connecting with first assembly 101 to rotate relative to first assembly 101.
The rotation slot 111 by two pieces hold up Lai structural slab 1111 form, screw hole is provided on structural slab 1111, it is described
It is provided in Rotational Cylindrical 110 corresponding to the screw hole on structural slab, Rotational Cylindrical 110 is set among two structure plates 1111, is passed through
Bolt or screw connect rotation slot 111 and Rotational Cylindrical 110, to guarantee first assembly 101 and the second component 102 always
It links together, and be by rotatable parts can be relative to first under the connection status of first assembly 101 for the second component 102
Component 101 rotates.
The rotatable parts be clasped, when including buckle and when a rotatable parts in unmanned thermomechanical components
It waits, second component 102 can be rotated relative to first assembly 101 to open the opening of first assembly 101 or closing the
The opening of one component 101 needs rotatable parts and is clasped will be open when closing the opening of first assembly 101
It is completely enclosed；Further, the buckle can be multiple, and the cooperation of multiple buckles and rotatable parts is to close the opening.
Unmanned thermomechanical components as described above, the first assembly 101 and/or the second component 102 are at least a part of in saturating
Bright shape；Such as unmanned plane main body is packed into unmanned thermomechanical components, the part that the unmanned thermomechanical components correspond to the camera on unmanned plane is in
Transparence, so that camera being capable of image outside the unmanned thermomechanical components of normal photographing.
In the embodiment of the present invention, the shape of the shape of the first assembly 101 and/or the second component 102 can be any
A kind of shape that can be packed into UAV Components, such as the shape of the first assembly and/or the shape of the second component are in ellipse
Shape or circle.
As shown in figure 9, further include waterproof and breathable component 112 in the unmanned thermomechanical components 100, the waterproof and breathable component
112 are set in unmanned thermomechanical components 100, can prevent leak and gas is allowed to pass through；Needed in the unmanned thermomechanical components 100 with
The component of air contact is connect with waterproof and breathable component 112, and can prevent the infiltration of water；The waterproof and breathable component 112 can
Be set in first assembly or the second component on；In some embodiments, the waterproof and breathable component 112 is waterproof and breathable
Film.
For example, unmanned aerial vehicle body main body is packed into unmanned thermomechanical components 100, unmanned plane horn passes through through-hole and unmanned aerial vehicle body
Main body connects, and the barometer on unmanned plane can be contacted by waterproof and breathable component 112 with air to obtain data, both ensure that
The waterproofness of unmanned plane guarantees that all parts can work normally on unmanned plane again.
As shown in Figure 10, shown unmanned thermomechanical components 100 further include thermal component 113；The thermal component 113 is set to nothing
On man-machine component 100, the heat generated inside unmanned thermomechanical components 100 can be spread out of by thermal component 113；The radiating part
Part 113 can be set in first assembly or on the second component；Heat generating components and thermal component in the unmanned thermomechanical components
113 close or contacts；The thermal component 113 is to be made of thermally conductive good material.
For example, unmanned aerial vehicle body main body is packed into unmanned thermomechanical components 100, unmanned plane horn passes through through-hole and unmanned aerial vehicle body
Main body connection, forms a kind of waterproof unmanned plane, unmanned plane is conducted the heat that fuselage interior generates to hair by conduction-convection problem
Thermal part, and by the thermal component 113 in unmanned thermomechanical components by heat shed or unmanned plane on generate heat component it is straight
It connects close or contact with thermal component.
As shown in figure 11, the embodiment of the invention discloses a kind of unmanned plane, the unmanned plane includes unmanned plane main body and this
Unmanned thermomechanical components 100 described in inventive embodiments, the unmanned plane main body include unmanned aerial vehicle body main body 106 and horn；It is described
Unmanned aerial vehicle body main body is installed in unmanned thermomechanical components, and the horn 114 passes through through-hole and connect with unmanned aerial vehicle body main body 106.
Unmanned plane main body and unmanned thermomechanical components 100 collectively constitute a kind of waterproof unmanned plane, so that unmanned plane rises with the water surface
The function of flying and land；Further, increase waterproof and breathable component and/or thermal component in unmanned thermomechanical components 100, so that nothing
The man-machine all devices in inside can work normally, and it is bad to solve the problems, such as that waterproof unmanned plane radiates because of airtightness.
Description through the embodiment of the present invention is as it can be seen that common transformation of the unmanned plane Jing Guo technical solution of the embodiment of the present invention
It is provided with the function of waterproof, and it is bad bad with air communication to solve the problems, such as that waterproof unmanned plane radiates, and extends common
The usage scenario of unmanned plane.
Finally, it should be noted that the foregoing is only a preferred embodiment of the present invention, it is not intended to restrict the invention,
Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features.
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in of the invention
Within protection scope.
Claims (19)
1. a kind of unmanned thermomechanical components, which is characterized in that the component plays waterproof action, for preventing the UAV Components in component
It is contacted with water；The component includes first assembly and the second component；The first assembly includes at least one opening, and described second
Component is used to close the opening of first assembly to prevent water from pouring into component from opening.
2. component according to claim 1, which is characterized in that it is provided at least one through-hole in the unmanned thermomechanical components,
External equipment is connected by through-hole for the UAV Components in unmanned thermomechanical components.
3. component according to claim 2, which is characterized in that the through-hole is set in first assembly or described logical
Hole is set on the second component or the through-hole is set to the junction of first assembly and the second component.
4. component according to claim 3, which is characterized in that the through-hole is set to the company of first assembly and the second component
The place of connecing includes that a part of through-hole is set in first assembly, and another part of through-hole is set on the second component, when second group
Complete through-hole is formed in the junction after the opening of part closing first assembly.
5. component according to claim 1, which is characterized in that there is sealing in the junction of second component and first assembly
Circle, to prevent water from penetrating into component from the junction.
6. component according to claim 1, which is characterized in that the first assembly and the second component are blocked by least one
Button links together, to close the opening of first assembly.
7. component according to claim 6, which is characterized in that the buckle includes pillar and cutting ferrule；The cutting ferrule passes through
Pillar is socketed so that first assembly and the second component to be fixed together.
8. component according to claim 7, which is characterized in that the cutting ferrule is set in first assembly, and the pillar is set
It is placed on the second component.
9. component according to claim 1, which is characterized in that the unmanned thermomechanical components further include rotatable parts, and described turn
Dynamic component includes Rotational Cylindrical and rotation slot, and the Rotational Cylindrical is set on the second component, and the rotation slot is set to first assembly
On；Second component is by rotatable parts to rotate relative to first assembly in the state of connecting with first assembly.
10. component according to claim 2, which is characterized in that sealing ring is provided with around the through-hole, in external equipment
The local leak of external device Yu unmanned plane component touch is prevented when passing through through-hole.
11. component according to claim 1, which is characterized in that the first assembly and/or the second component at least one
Divide and is transparent.
12. component according to claim 1, which is characterized in that the shape of the shape of the first assembly and/or the second component
Shape is oval or round.
13. component according to claim 1, which is characterized in that the unmanned thermomechanical components further include waterproof and breathable component；
The waterproof and breathable component is set in unmanned thermomechanical components, can prevent leak and gas is allowed to pass through.
14. component according to claim 13, which is characterized in that the waterproof and breathable component is waterproof ventilated membrane.
15. component according to claim 13, which is characterized in that the portion that the unmanned thermomechanical components domestic demand will be contacted with air
Part is connect with waterproof and breathable component.
16. component according to claim 1, which is characterized in that the unmanned thermomechanical components further include thermal component；
The thermal component is set in unmanned thermomechanical components, and the heat that can generate unmanned plane component internal passes through thermal component
Outflow.
17. component according to claim 16, which is characterized in that heat generating components and radiating part in the unmanned thermomechanical components
Part is close or contacts.
18. component according to claim 16, which is characterized in that the thermal component is by thermally conductive good material structure
At.
19. a kind of unmanned plane, which is characterized in that the unmanned plane includes such as the described in any item unmanned units of claim 1-18
Part and unmanned plane main body；The unmanned plane main body includes unmanned aerial vehicle body main body and horn；The unmanned aerial vehicle body main body installation
In in unmanned thermomechanical components, the horn passes through through-hole and connect with unmanned aerial vehicle body main body.
Priority Applications (13)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910426335.2A CN110116798A (en) | 2019-05-20 | 2019-05-20 | A kind of unmanned thermomechanical components and unmanned plane |
| JPD2020-11288F JP1668469S (en) | 2019-04-01 | 2019-10-01 | |
| JPD2019-22128F JP1678428S (en) | 2019-04-01 | 2019-10-01 | |
| US29/707,762 USD900675S1 (en) | 2019-04-01 | 2019-10-01 | Intelligent device |
| JPD2020-11290F JP1667922S (en) | 2019-04-01 | 2019-10-01 | |
| JPD2020-11289F JP1694319S (en) | 2019-04-01 | 2019-10-01 | |
| PCT/CN2019/130770 WO2020233132A1 (en) | 2019-05-20 | 2019-12-31 | Unmanned aerial vehicle component, arm, counterweight float, and unmanned aerial vehicle |
| EP19929576.7A EP3971085A1 (en) | 2019-05-20 | 2019-12-31 | Unmanned aerial vehicle component, arm, counterweight float, and unmanned aerial vehicle |
| US17/612,227 US20220212790A1 (en) | 2019-05-20 | 2019-12-31 | Unmanned aerial vehicle component, arm, counterweight float, and unmanned aerial vehicle |
| US29/745,242 USD927353S1 (en) | 2019-04-01 | 2020-08-04 | Intelligent device |
| US29/745,246 USD934776S1 (en) | 2019-04-01 | 2020-08-04 | Intelligent device |
| US29/745,265 USD938861S1 (en) | 2019-04-01 | 2020-08-05 | Intelligent device |
| US29/745,267 USD926632S1 (en) | 2019-04-01 | 2020-08-05 | Intelligent device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910426335.2A CN110116798A (en) | 2019-05-20 | 2019-05-20 | A kind of unmanned thermomechanical components and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110116798A true CN110116798A (en) | 2019-08-13 |
Family
ID=67523004
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910426335.2A Pending CN110116798A (en) | 2019-04-01 | 2019-05-20 | A kind of unmanned thermomechanical components and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110116798A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020233132A1 (en) * | 2019-05-20 | 2020-11-26 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle component, arm, counterweight float, and unmanned aerial vehicle |
| CN112455648A (en) * | 2019-09-09 | 2021-03-09 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle |
| CN112572766A (en) * | 2020-12-17 | 2021-03-30 | 重庆工程职业技术学院 | Water vapor propeller of unmanned aerial vehicle on water and processing technology thereof |
| CN113401359A (en) * | 2021-05-28 | 2021-09-17 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle stop device and unmanned aerial vehicle hangar |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105775133A (en) * | 2016-03-03 | 2016-07-20 | 致导科技（北京）有限公司 | Waterproof unmanned aerial vehicle |
| CN105923142A (en) * | 2016-05-13 | 2016-09-07 | 深圳市斯威普科技有限公司 | Unmanned aerial vehicle waterproof structure |
| CN105966595A (en) * | 2016-05-13 | 2016-09-28 | 深圳市斯威普科技有限公司 | Waterproof structure of unmanned aerial vehicle |
| CN205854501U (en) * | 2016-07-22 | 2017-01-04 | 珠海银通农业科技有限公司 | A kind of available water rinses waterproof unmanned plane |
| CN206407123U (en) * | 2016-12-30 | 2017-08-15 | 东莞市光点电子科技有限公司 | A kind of water proof structure for aircraft |
| CN206528617U (en) * | 2017-02-28 | 2017-09-29 | 珠海瑞科科技研发有限公司 | A kind of plant protection unmanned plane radiating water-proof ventilation road structure |
| CN207354768U (en) * | 2017-08-16 | 2018-05-11 | 广州极飞科技有限公司 | Waterproof construction, electronic device and unmanned plane |
| CN208868291U (en) * | 2018-07-11 | 2019-05-17 | 深圳市道通智能航空技术有限公司 | Waterproof unmanned plane |
-
2019
- 2019-05-20 CN CN201910426335.2A patent/CN110116798A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105775133A (en) * | 2016-03-03 | 2016-07-20 | 致导科技（北京）有限公司 | Waterproof unmanned aerial vehicle |
| CN105923142A (en) * | 2016-05-13 | 2016-09-07 | 深圳市斯威普科技有限公司 | Unmanned aerial vehicle waterproof structure |
| CN105966595A (en) * | 2016-05-13 | 2016-09-28 | 深圳市斯威普科技有限公司 | Waterproof structure of unmanned aerial vehicle |
| CN205854501U (en) * | 2016-07-22 | 2017-01-04 | 珠海银通农业科技有限公司 | A kind of available water rinses waterproof unmanned plane |
| CN206407123U (en) * | 2016-12-30 | 2017-08-15 | 东莞市光点电子科技有限公司 | A kind of water proof structure for aircraft |
| CN206528617U (en) * | 2017-02-28 | 2017-09-29 | 珠海瑞科科技研发有限公司 | A kind of plant protection unmanned plane radiating water-proof ventilation road structure |
| CN207354768U (en) * | 2017-08-16 | 2018-05-11 | 广州极飞科技有限公司 | Waterproof construction, electronic device and unmanned plane |
| CN208868291U (en) * | 2018-07-11 | 2019-05-17 | 深圳市道通智能航空技术有限公司 | Waterproof unmanned plane |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020233132A1 (en) * | 2019-05-20 | 2020-11-26 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle component, arm, counterweight float, and unmanned aerial vehicle |
| CN112455648A (en) * | 2019-09-09 | 2021-03-09 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle |
| CN112572766A (en) * | 2020-12-17 | 2021-03-30 | 重庆工程职业技术学院 | Water vapor propeller of unmanned aerial vehicle on water and processing technology thereof |
| CN113401359A (en) * | 2021-05-28 | 2021-09-17 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle stop device and unmanned aerial vehicle hangar |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110116798A (en) | A kind of unmanned thermomechanical components and unmanned plane | |
| CN108810199A (en) | Display screen component, electronic equipment and display control method | |
| CN205430400U (en) | Camera seal structure , shooting device and shooting equipment | |
| US10324315B2 (en) | Electronic device | |
| CN109145721A (en) | Terminal | |
| WO2018152909A1 (en) | Cradle head device and unmanned aerial vehicle | |
| CN105785650B (en) | Backlight and its assemble method, display device | |
| US20220212790A1 (en) | Unmanned aerial vehicle component, arm, counterweight float, and unmanned aerial vehicle | |
| CN109073849A (en) | Lens module, clouds terrace system and unmanned vehicle | |
| CN101334953B (en) | Waterproof LED display module set | |
| US20190288480A1 (en) | Laser module and laser projection device | |
| CA2382773A1 (en) | A fairing arrangement for an aircraft | |
| CN107040707A (en) | A kind of electronic equipment, CCD camera assembly and its protection eyeglass | |
| CN106659028B (en) | Electronic equipment shell and electronic equipment | |
| CN206528630U (en) | Power is set with and unmanned vehicle | |
| KR101795320B1 (en) | Ominidirectional camera with water-proof and dust-proof function | |
| CN107539452B (en) | Unmanned aerial vehicle inner bag | |
| CN107465862A (en) | Composite decking, camera module and mobile terminal | |
| CN206711805U (en) | Keyboard case for industrial control equipment | |
| WO2020114525A1 (en) | Avionic structure of unmanned aerial vehicle and unmanned aerial vehicle | |
| CN205991445U (en) | Down straight aphototropism mode set and display device | |
| CN211580473U (en) | Electronic equipment | |
| CN206394887U (en) | Unmanned plane | |
| CN206686198U (en) | A kind of gateway shell | |
| CN208204587U (en) | A kind of lighting device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190813 |
|
| WD01 | Invention patent application deemed withdrawn after publication |