CN209126980U - Fly control module installation structure, fly control component and unmanned plane - Google Patents
Fly control module installation structure, fly control component and unmanned plane Download PDFInfo
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- CN209126980U CN209126980U CN201821641733.3U CN201821641733U CN209126980U CN 209126980 U CN209126980 U CN 209126980U CN 201821641733 U CN201821641733 U CN 201821641733U CN 209126980 U CN209126980 U CN 209126980U
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Abstract
The utility model provides one kind and flies control module installation structure, flies control component and unmanned plane.Wherein, fly control module installation structure to include and fly to control the substrate that is connected of module and set on the mounting plate of unmanned plane, substrate is connected by location structure with mounting plate, and location structure includes the first positioning region on substrate and the second positioning region on mounting plate and with the cooperation of the first positioning region.Winged control module installation structure provided by the utility model can be omitted the time that largely winged control module is demarcated and calibrated, and improve the efficiency of mass production.
Description
[technical field]
The utility model relates to air vehicle technique field, more particularly to it is a kind of fly control module installation structure, fly control component and
Unmanned plane.
[background technique]
Unmanned plane is the complication system for covering the multidisciplinary field such as flight control, vision algorithm, cradle head control, each function
The modularization and standardization of system are conducive to the research and development and manufacturing process that accelerate unmanned plane, facilitate the use and dimension in later period
Shield.
Flight control modules (hereinafter collectively referred to as flying control module) are subsystem important in UAV system, major function
It is the measurement status informations such as unmanned plane during flying posture, and the flight of real-time control unmanned plane.In order to guarantee the accuracy of measurement, nothing
It is man-machine installation fly control module after, it is necessary to first carry out fly control module calibration and calibration.
The commercial control module mounting arrangement that flies existing at present only has gluing and is screwed two kinds.Adhesive type mount scheme
Reliability is low, and although screw-fixing type mount scheme improves reliability, but still cannot be guaranteed to produce assembling process in enormous quantities
In fly control module positioning accuracy.That is, flying the installation site of control module in mass production, in different unmanned planes can not protect
End of certificate is exactly the same.Therefore, it for each unmanned plane in producing in enormous quantities, is required to devote a tremendous amount of time to winged control module
It is demarcated and is calibrated, this undoubtedly reduces assembly efficiency.And during flying the use and maintenance of control module in the later period, Wu Fashi
Existing " primary calibration calibration, repeatedly handling maintenance ".
[utility model content]
In order to solve the above-mentioned technical problem, the utility model embodiment provide it is a kind of realize fly control module accurately and fast,
The winged control module installation structure of convenient installation flies control component and unmanned plane.
In order to solve the above technical problems, the utility model embodiment the following technical schemes are provided:
One kind flying control module installation structure, for flying the connection between control module and unmanned plane, the winged control module installation
Structure includes with the winged substrate that is connected of control module and set on the mounting plate of the unmanned plane, and the substrate passes through location structure
It is connected with the mounting plate, the location structure includes the first positioning region on the substrate and is set on the mounting plate
And the second positioning region with first positioning region cooperation.
In an embodiment of the utility model, pass through face contact between first positioning region and second positioning region
Or line contact, the winged control module is limited around the straight line rotation perpendicular to the mounting plate.
In an embodiment of the utility model, first positioning region and second positioning region are limited by face contact
For the winged control module around the straight line rotation perpendicular to the mounting plate, first positioning region has the first bearing surface, and described the
Two positioning regions have the second bearing surface, first bearing surface abutted with second bearing surface with limit the winged control module around
Perpendicular to the straight line rotation of the mounting plate.
In an embodiment of the utility model, first positioning region is the first keyway, and second positioning region includes
Flat key.
In an embodiment of the utility model, first keyway and the flat key clearance fit.
In an embodiment of the utility model, first keyway is in U-shape.
In an embodiment of the utility model, second positioning region further includes the second keyway, and the flat key is set to institute
It states in the second keyway.
In an embodiment of the utility model, the flat key and second keyway are transition fit.
In an embodiment of the utility model, contacted between first positioning region and second positioning region by line
Limit it is described it is winged control module around perpendicular to the mounting plate straight line rotation, first positioning region be location hole, described second
Positioning region is positioning pin.
In an embodiment of the utility model, the location hole and the positioning pin clearance fit.
In an embodiment of the utility model, the short side that the mounting plate has long side and is connected with the long side, institute
It states the second positioning region to be located at the mounting plate center and be parallel on the straight line of the long side, first positioning region was located at
It the substrate center and is parallel on the straight line of the long side.
In an embodiment of the utility model, the location structure further includes the first positioning on the substrate
Hole, be set to the mounting plate on and second location hole corresponding with the first positioning hole position and pass through it is described first positioning
The positioning pin in hole and the second location hole.
In an embodiment of the utility model, the positioning pin and the first positioning hole and the positioning pin with
It is interference fit between the second location hole.
In an embodiment of the utility model, the excessively described base of line of the first positioning hole and first positioning region
Plate center and the long side for being parallel to the mounting plate, the excessively described installation of line of the second location hole and second positioning region
Plate center and the long side for being parallel to the mounting plate.
In an embodiment of the utility model, the positioning pin is taper bolt.
In an embodiment of the utility model, the taper of the taper bolt is 1: 50.
In an embodiment of the utility model, the location structure further includes the at the position of four angles of the substrate
One mounting hole is set on the mounting plate and the second mounting hole corresponding with first position of mounting hole and passes through described the
The fastening bolt of one mounting hole and second mounting hole；
It is connected by the fastening bolt with the mounting plate at four angles position of the substrate, so that the base
Plate towards the surface of the mounting plate, with the mounting plate towards the substrate and the surface that is connected with the substrate is closely pasted
It closes.
It is between the fastening bolt and first mounting hole and described tight in an embodiment of the utility model
It is clearance fit between fixing bolt and second mounting hole.
In an embodiment of the utility model, the substrate includes base main body and is convexly equipped in the substrate master respectively
Installation position at four angles position of body, first mounting hole penetrate through the installation position.
In an embodiment of the utility model, the installation position is rounded.
In an embodiment of the utility model, the installation position is towards the surface of the mounting plate for through over mechanical processing
To make it have the surface of certain flatness.
In an embodiment of the utility model, the mounting plate includes that mounting plate main body and two parallel intervals are arranged in institute
The boss in mounting plate main body is stated, the extending direction of the boss is parallel to the short side of the mounting plate, second positioning region
On the boss.
In an embodiment of the utility model, the boss is the boss of strip.
In an embodiment of the utility model, the boss towards the surface of the substrate be through over mechanical processing so that
Its surface with certain flatness.
To solve its technical problem, the utility model additionally provides a kind of winged control component, and the winged control component includes flying control
Module and winged control module installation structure as described above.
To solve its technical problem, the utility model additionally provides a kind of unmanned plane, including fuselage, is connected with the fuselage
Horn and power device set on the horn, further include winged control component as described above.
The utility model proposes winged control module installation structure, solve and fly the quick of control module and be accurately positioned and installation
Problem simplifies the process of unmanned plane batch Assembling Production, improves the efficiency of mass production.And the utility model proposes
Fly control component, it can be achieved that " primary calibration calibration, repeatedly handling maintenance ".That is, this is practical new even across multiple disassembly and installation
The winged control component of type still can guarantee that positioning accuracy is constant, therefore can omit the calibration after dismounting each time and calibration steps, letter
The process of later period handling maintenance is changed.Meanwhile the utility model realizes winged control by plane restriction, coaxial constraint and point constraint
Module it is accurate fixed and positioned, realize to it is winged control the full freedom degree of module holonomic constriants and degree of precision positioning.Have
It is simple to operate, the advantages such as machining cost is low.
[Detailed description of the invention]
One or more embodiments are illustrated by the picture in corresponding attached drawing, these exemplary theorys
The bright restriction not constituted to embodiment, the element in attached drawing with same reference numbers label are expressed as similar element, remove
Non- to have special statement, composition does not limit the figure in attached drawing.
Fig. 1 is a kind of structural schematic diagram of a winged control component wherein embodiment of the utility model；
Fig. 2 is the structural schematic diagram of a substrate wherein embodiment in winged control component shown in FIG. 1；
Fig. 3 is the structural schematic diagram of a mounting plate wherein embodiment in winged control component shown in FIG. 1；
Fig. 4 is the structural schematic diagram of flat key in winged control component shown in FIG. 1；And
Fig. 5 is the structural schematic diagram of taper bolt in winged control component shown in FIG. 1.
[specific embodiment]
For the ease of understanding the utility model, in the following with reference to the drawings and specific embodiments, the utility model is carried out more detailed
Thin explanation.It should be noted that it can be directly in another element when element is expressed " being fixed on " another element
Upper or placed in the middle there may be one or more therebetween elements.When an element is expressed " connection " another element, it can
To be directly to another element or elements placed in the middle there may be one or more therebetween.This specification is used
Term " on ", "lower", "inner", "outside", the instructions such as " bottom " orientation or positional relationship be orientation based on the figure or
Positional relationship is merely for convenience of describing the present invention and simplifying the description, rather than the device or member of indication or suggestion meaning
Part must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
In addition, term " first ", " second " " third " etc. are used for description purposes only, it is not understood to indicate or imply relatively important
Property.
Unless otherwise defined, technical and scientific term all used in this specification and the skill for belonging to the utility model
The normally understood meaning of the technical staff in art field is identical.Art used in the description of the utility model in this specification
Language, which is only for the purpose of describing specific embodiments, is not intended to limitation the utility model.Term used in this specification
"and/or" includes any and all combinations of one or more related listed items.
In addition, as long as technical characteristic involved in the utility model difference embodiment disclosed below is each other not
Constituting conflict can be combined with each other.
Fig. 1 is a kind of structural schematic diagram of winged control component 10 of the utility model.It includes flying control module 20 that this, which flies control component 10,
With for by it is described it is winged control module 20 installation to unmanned plane winged control module installation structure.Unmanned plane include fuselage, with fuselage phase
The horn connected and the power device set on horn.Horn may be a fixed connection with fuselage, be also possible to detachable or with can phase
The mode folded for fuselage connects.The propeller that power device generally includes motor and is connected with the motor shaft of motor.Motor
Drive propeller rotation to provide the lift of unmanned plane during flying.In other embodiments, unmanned plane be also possible to fixed-wing nobody
Machine.The winged control module installation structure includes with the winged substrate 30 that is connected of control module 20 and set on the fuselage of the unmanned plane
Interior mounting plate 40.It is worth noting that, without limitation to the position the utility model of mounting plate 40 on fuselage.The substrate
30 are connected by location structure with the mounting plate 40.In high volume production process, can in the fuselage of each unmanned plane
The position for installing the mounting plate 40 is reserved, and the position of any two unmanned plane upper mounting plates 40 is identical.Pass through institute
Location structure is stated, being connected with position of the winged control module 20 of the substrate 30 on mounting plate 40 can be determined.Therefore,
For any two unmanned planes in high volume production process, it is also identical for flying the position of control module 20.Therefore,
It can be omitted largely to the time of winged control module calibration and calibration, improve the efficiency of mass production.It is worth noting that, peace
Loading board 40 can be an individual component, be also possible to process in the fuselage of unmanned plane part.
As shown in Fig. 2, the substrate 30 includes base main body 31 and the peace at the position of 31 4 angles of the base main body
Fill position 34.In an embodiment of the utility model, the installation position 34 is protruded and rounded from the base main body 31.At it
In his possible embodiment, installation position 34 is also possible to other shapes.
The location structure includes being set to first positioning region of the base main body 31 towards the surface of the mounting plate 40.
In the present embodiment, winged control module 20 and first positioning region two tables that be located at the base main body 31 opposite
On face.In an embodiment of the utility model, first positioning region is the first keyway 32, and first keyway 32 is in U-shape,
First keyway 32 penetrates through a side of the base main body 31.
In other possible embodiments, the location structure can also include first positioning hole 33 and perforation four respectively
First mounting hole 35 of the installation position 34.In other possible embodiments, it is convenient to omit installation position 34, and directly in substrate
First mounting hole 35 is opened up at four angles position of main body 31.
As shown in figure 3, the mounting plate 40 includes mounting plate main body 41 and is arranged in convex in the mounting plate main body 41
Platform.The boss includes first boss 421 and the second boss 422 with 421 parallel interval of first boss setting.The peace
The short side 412 that loading board main body 41 has long side 411 and is connected with the long side 411, i.e., in the present embodiment, the mounting plate master
Whole body 41 is in rectangle.In other possible embodiments, the mounting plate main body 41 can also be other shapes.It is practical at this
In a novel embodiment, the first boss 421 is identical as the shape of the second boss 422, be in bar shaped, described first
Boss 421 and the extending direction of the second boss 422 are parallel with the short side 412.In other embodiments, described first
Boss 421 also can be omitted with the second boss 422.
The location structure further includes set on the second positioning region of the first boss 421.One in the utility model is real
It applies in example, second positioning region includes the second keyway 43 in the first boss 421 and is set to second keyway
Flat key 50 (as shown in Figure 4) in 43.In an embodiment of the utility model, second keyway 43 and the flat key 50 it
Between be transition fit.In other possible embodiments, second positioning region can also only include flat key 50, i.e., will be described flat
Key 50 is directly molded in the first boss 421.
In other possible embodiments, the location structure can also include set on the second of the second boss 422
Location hole 44 and the second mounting hole 45 for being respectively arranged on the first boss 421 and the second boss 422.Described first is convex
It is set on platform 421 there are two the second mounting hole 45, two second mounting holes 45 penetrate through the first boss 421 and the installation
Plate main body 41.Two the second mounting holes 45 also are provided in the second boss 422, two second mounting holes 45 penetrate through described
Second boss 422 and the mounting plate main body 41.Pacify respectively with four described first the position of four second mounting holes 45
The position for filling hole 35 is corresponding.
In an embodiment of the utility model, second positioning region be located at the center of the mounting plate main body 41 and
It is parallel on the straight line of the long side 411, and the excessively described installation of line L of second positioning region and the second location hole 44
The center of plate main body 41 and it is parallel to the long side 411.Correspondingly, first positioning region also was located at 30 center of substrate
And it is parallel on the straight line of the long side 411, the excessively described substrate of line of first positioning region and the first positioning hole 33
30 center and it is parallel to the long side 411.
As shown in figure 5, the location structure may also include across the first positioning hole 33 and the second location hole 44
Positioning pin and fastening bolt 70 across first mounting hole 35 and second mounting hole 45.In the utility model
It is interference fit in one embodiment, between positioning pin and first positioning hole 33 and between positioning pin and second location hole 44.
Assembly precision can be improved using interference fit, frequently assemble and disassemble the occasion for flying control module suitable for not needing.It should be understood that fixed
It can also be matched using transition fit or gap between position pin and first positioning hole 33 and between positioning pin and second location hole 44
It closes, although relatively slightly lower using transition fit or clearance fit precision, is more applicable for needing frequently assembling and disassembling winged control module
Occasion.In an embodiment of the utility model, positioning pin is taper bolt 60, and the taper bolt 60 has 1: 50 taper.
The taper that taper bolt 60 has, so that taper bolt 60 itself has good mechanical self-latching performance, and positioning is more accurate, is filling
It is more more convenient than straight pin to tear aspect open.In an embodiment of the utility model, the fastening bolt 70 and first installation
It is clearance fit between hole 35 and between the fastening bolt 70 and second mounting hole 45, so that the substrate 30
Towards the mounting plate 40 surface, with the mounting plate 40 towards the substrate 30 and the surface that is connected with the substrate 30 it is tight
Closely connected conjunction.
During installation, first keyway 32 is directed at the flat key 50 in second keyway 43, i.e., installed from top to bottom,
The positioning of substrate 30 Yu mounting plate 40 can be realized.It installs very simple and convenient.It can also be along the direction straight line L in Fig. 3, by
The opening of one keyway 32 is directed at flat key 50, sliding substrate 30, until flat key 50 is fully inserted into first keyway 32.From upper past
When lower installation, it can be finely adjusted along the Y direction in Fig. 1, the positioning of substrate 30 Yu mounting plate 40 can be basically completed.So
The taper bolt 60 is tapped down into the first positioning hole 33 and the second location hole 44 afterwards, finally by four fastening bolts
70 are respectively charged into the first mounting hole 35 and the second mounting hole 45 and fasten, and can further complete the full freedom for flying control module 20
Degree constraint and installation.Whole installation process is not necessarily to special accurate operation, can guarantee higher positioning while convenient and efficient
Precision is very suitable for producing in enormous quantities.
In the embodiments of the present invention, in the assembled condition, first keyway 32 is gap with the flat key 50
Cooperation.When the winged control module 20 is relative to Z axis minor rotation of the mounting plate 40 in Fig. 1, first keyway 32 and institute
The rotation in winged control module 20 direction about the z axis can be limited by stating flat key 50 and cooperating.And due to the first keyway 32 with it is described
Flat key 50 is clearance fit, therefore the single side of only flat key 50 is abutted with the single cell wall of the first keyway 32, thus effectively
Prevent the generation of Planar Mechanisms phenomenon.For example, the first bearing surface 321 (cell wall of i.e. described first keyway 32) of the first keyway 32
It is abutted with the second bearing surface 501 (side of the i.e. described flat key 50) of flat key 50.
In the embodiments of the present invention, there are three effects for the tool of flat key 50.It is oriented to first is that can provide similar to sliding rail
Effect so that in assembling process, substrate 30 can rapid alignment mounting plate 40, complete positioning.Second is that flat key 50 and circular cone
Pin 60 forms asymmetric arrangement, and reversed installation can be effectively prevented.Finally, by reasonable tolerance fit design (flat key 50 with
Clearance fit between first keyway 32), it effectively prevent the generation of Planar Mechanisms phenomenon.
First positioning hole 33 and the may be implemented in the cooperation of taper bolt 60 and first positioning hole 33 and second location hole 44
The coaxial constraint of two location holes 44 can limit winged to limit position of the winged control module 20 relative to unmanned aerial vehicle body
Control module 20 in Fig. 1 in X direction with the movement in Y-direction.Meanwhile the taper that taper bolt 60 has, so that taper bolt 60 has
Standby good mechanical self-latching performance, registration are assembled and disassembled also more convenient.
In addition, realizing plane and mounting plate 40 of the substrate 30 towards the mounting plate 40 by four fastening bolts 70
Towards fitting closely between the substrate 30 and the plane that is connected with the substrate 30, so that limitation flies control module 20 around X-axis
Rotation, around the rotation of Y-axis and moving along Z axis.In an embodiment of the utility model, in order to guarantee two planes it
Between fit closely, can also to substrate 30 towards the mounting plate 40 plane and mounting plate 40 towards the substrate 30
And the plane being connected with the substrate 30 is machined, and certain flatness is made it have.In order to reduce processing capacity, at this
In embodiment, it is only necessary to be machined to four installation positions 34, first boss 411 and the second boss 412 on substrate 30
?.Therefore, the presence of installation position 34, first boss 411 and second boss 412 reduces machining amount.In addition, should also
Guarantee flatness of the installation position 34 towards the surface of mounting plate 40, the putting down towards the surface of the substrate 30 with two boss as far as possible
Face degree is equal.It is understood that first boss 411 and second boss can also be omitted in other possible embodiments
412, the region being directly connected on mounting plate 40 with substrate 30 is machined, while to substrate 30 towards mounting plate 40
Whole surface is machined, to guarantee fitting closely between two planes.The flatness of two planes can be according to winged
The specific installation accuracy of module is controlled to determine, in this regard, the utility model is without limitation.
The utility model proposes winged control module installation structure, solve and fly the quick of control module and be accurately positioned and installation
Problem simplifies the process of unmanned plane batch Assembling Production, improves the efficiency of mass production.And the utility model proposes
Fly control component, it can be achieved that " primary calibration calibration, repeatedly handling maintenance ".That is, this is practical new even across multiple disassembly and installation
The winged control component of type still can guarantee that position location is constant, keeps certain positioning accuracy, therefore can omit every when later maintenance
Calibration and calibration steps after primary dismounting, simplify the process of later period handling maintenance.Meanwhile the utility model passes through plane about
Beam, coaxial constraint and point constraint fly the accurate fixed and positioned of control module to realize, realize to the winged control full freedom degree of module
Holonomic constriants and the positioning of degree of precision.With simple to operate, the advantages such as machining cost is low.
Utility model finally, it should be noted that above embodiments are only to illustrate the technical solution of the utility model, rather than
It is limited；It can also be under the thinking of the utility model, between the technical characteristic in above embodiments or different embodiment
Be combined, step can be realized with random order, and there are the different aspect of the utility model as described above it is many its
It changes, for simplicity, they are not provided in details；Although having been carried out in detail to the utility model with reference to the foregoing embodiments
Explanation, those skilled in the art should understand that: it still can be to technical solution documented by foregoing embodiments
It modifies or equivalent replacement of some of the technical features；And these are modified or replaceed, and do not make relevant art
The essence of scheme departs from the scope of the technical solutions of the embodiments of the present invention.
Claims (26)
1. one kind flies control module installation structure, for flying the connection between control module and unmanned plane, which is characterized in that the winged control
Module installation structure includes with the winged substrate that is connected of control module and set on the mounting plate of the unmanned plane, and the substrate passes through
Location structure is connected with the mounting plate, and the location structure includes the first positioning region on the substrate and is set to described
The second positioning region on mounting plate and with first positioning region cooperation.
2. winged control module installation structure according to claim 1, which is characterized in that first positioning region and described second
It is contacted between positioning region by face contact or line, limits the winged control module around the straight line rotation perpendicular to the mounting plate.
3. winged control module installation structure according to claim 2, which is characterized in that first positioning region and described second
Positioning region limits the winged control module around the straight line rotation perpendicular to the mounting plate, the first positioning region tool by face contact
There is the first bearing surface, second positioning region has the second bearing surface, and first bearing surface is abutted with second bearing surface
To limit the winged control module around the straight line rotation perpendicular to the mounting plate.
4. winged control module installation structure according to any one of claim 1-3, which is characterized in that first positioning region
For the first keyway, second positioning region includes flat key.
5. winged control module installation structure according to claim 4, which is characterized in that between first keyway and the flat key
Gap cooperation.
6. winged control module installation structure according to claim 4, which is characterized in that first keyway is in U-shape.
7. winged control module installation structure according to claim 4, which is characterized in that second positioning region further includes second
Keyway, the flat key are set in second keyway.
8. winged control module installation structure according to claim 7, which is characterized in that the flat key is with second keyway
Transition fit.
9. winged control module installation structure according to claim 1 or 2, which is characterized in that first positioning region with it is described
It is rotated by the line contact limitation winged control module around the straight line perpendicular to the mounting plate between second positioning region, described first
Positioning region is location hole, and second positioning region is positioning pin.
10. winged control module installation structure according to claim 9, which is characterized in that the location hole and the positioning pin
Clearance fit.
11. winged control module installation structure according to claim 1, which is characterized in that the mounting plate have long side and with
The connected short side of the long side, second positioning region was located at the mounting plate center and was parallel to the straight line of the long side
On, first positioning region was located at the substrate center and was parallel on the straight line of the long side.
12. winged control module installation structure according to claim 1, which is characterized in that the location structure further includes being set to
First positioning hole on the substrate is set on the mounting plate and second location hole corresponding with the first positioning hole position
And the positioning pin across the first positioning hole and the second location hole.
13. winged control module installation structure according to claim 12, which is characterized in that the positioning pin is fixed with described first
It is interference fit between position hole and the positioning pin and the second location hole.
14. winged control module installation structure according to claim 12, which is characterized in that the first positioning hole and described the
The excessively described substrate center of the line of one positioning region and the long side for being parallel to the mounting plate, the second location hole and described second
The excessively described mounting plate center of the line of positioning region and the long side for being parallel to the mounting plate.
15. winged control module installation structure described in any one of 2-14 according to claim 1, which is characterized in that the positioning pin
For taper bolt.
16. winged control module installation structure according to claim 15, which is characterized in that the taper of the taper bolt is 1:
50。
17. winged control module installation structure according to claim 1, which is characterized in that the location structure further includes being set to
First mounting hole at four angles of substrate position place, on the mounting plate and corresponding with first position of mounting hole the
Two mounting holes and fastening bolt across first mounting hole and second mounting hole；
It is connected by the fastening bolt with the mounting plate at four angles position of the substrate, so that the substrate court
To the surface of the mounting plate, with the mounting plate towards the substrate and the surface that is connected with the substrate fits closely.
18. winged control module installation structure according to claim 17, which is characterized in that the fastening bolt and described first
It is clearance fit between mounting hole and between the fastening bolt and second mounting hole.
19. winged control module installation structure described in 7 or 18 according to claim 1, which is characterized in that the substrate includes substrate master
Body and the installation position being convexly equipped at four angles position of the base main body respectively, first mounting hole penetrate through the peace
Fill position.
20. winged control module installation structure according to claim 19, which is characterized in that the installation position is rounded.
21. winged control module installation structure according to claim 19, which is characterized in that the installation position is towards the installation
The surface of plate is through over mechanical processing so that its surface with certain flatness.
22. winged control module installation structure according to claim 1, which is characterized in that the mounting plate includes mounting plate master
The boss in the mounting plate main body is arranged in body and two parallel intervals, and the extending direction of the boss is parallel to the mounting plate
Short side, second positioning region is located on the boss.
23. winged control module installation structure according to claim 22, which is characterized in that the boss is the convex of strip
Platform.
24. the winged control module installation structure according to claim 22 or 23, which is characterized in that the boss is towards the base
The surface of plate is through over mechanical processing so that its surface with certain flatness.
25. the winged control component of one kind, which is characterized in that the winged control component includes any in winged control module and such as claim 1-24
Winged control module installation structure described in.
It is special including fuselage, the horn being connected with the fuselage and power device set on the horn 26. a kind of unmanned plane
Sign is, further includes winged control component as claimed in claim 25.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821641733.3U CN209126980U (en) | 2018-10-10 | 2018-10-10 | Fly control module installation structure, fly control component and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821641733.3U CN209126980U (en) | 2018-10-10 | 2018-10-10 | Fly control module installation structure, fly control component and unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN209126980U true CN209126980U (en) | 2019-07-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821641733.3U Active CN209126980U (en) | 2018-10-10 | 2018-10-10 | Fly control module installation structure, fly control component and unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108974372A (en) * | 2018-10-10 | 2018-12-11 | 深圳市道通智能航空技术有限公司 | Fly control module installation structure, fly control component and unmanned plane |
-
2018
- 2018-10-10 CN CN201821641733.3U patent/CN209126980U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108974372A (en) * | 2018-10-10 | 2018-12-11 | 深圳市道通智能航空技术有限公司 | Fly control module installation structure, fly control component and unmanned plane |
| WO2020073798A1 (en) * | 2018-10-10 | 2020-04-16 | 深圳市道通智能航空技术有限公司 | Mounting structure for flight control module, flight control assembly and unmanned aerial vehicle |
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Address after: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Patentee after: Shenzhen daotong intelligent Aviation Technology Co.,Ltd. Address before: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Patentee before: AUTEL ROBOTICS Co.,Ltd. |
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