CN206782066U - A kind of horn structure for being used to combine gyroplane - Google Patents
A kind of horn structure for being used to combine gyroplane Download PDFInfo
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- CN206782066U CN206782066U CN201720566383.8U CN201720566383U CN206782066U CN 206782066 U CN206782066 U CN 206782066U CN 201720566383 U CN201720566383 U CN 201720566383U CN 206782066 U CN206782066 U CN 206782066U
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- horn
- undercarriage
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Abstract
The utility model discloses a kind of horn structure for being used to combine gyroplane, it is related to unmanned vehicle field.The horn structure includes：Horn, rotor, rotor carry end and horn connector；One end of the horn sets horn connector, and the other end sets rotor to carry end；The rotor is fixed on the rotor and carried on end；The agent structure that the rotor carries end is column construction；Motor is set in the inner chamber of the column construction, and the motor is connected with the rotor.Structure described in the utility model realizes the more rotor single-blade horns of different task load and is total to the Rapid Combination of paddle structure up and down, it can need to realize unmanned plane from the rotor of three axle three is changed into the rotor of three axle six, the rotor of four axle four is changed into the rotor of four axle eight, the rotor of six axle six is changed into the rotor of six axle 12 according to mission payload, aircraft bearing capacity is improved, the production cost of gyroplane is reduced and improves the efficiency of unmanned plane outdoor study task.
Description
Technical field
Unmanned vehicle field is the utility model is related to, more particularly to a kind of horn structure for being used to combine gyroplane.
Background technology
Unmanned plane have flexible light, in light weight, small volume, rapid-assembling/disassembling, as needed can carry different task set
Standby, the features such as manufacturing cycle is short, largely used in military markets and commercial market.
But with the fast development of unmanned flight's technology, more and more higher is required to unmanned plane.Existing unmanned plane is single-blade machine
Arm and can not according to mission payload need to realize unmanned plane rotor change.
Utility model content
The purpose of this utility model is to provide a kind of horn structure for being used to combine gyroplane, so as to solve prior art
Present in foregoing problems.
To achieve these goals, the horn structure described in the utility model for being used to combine gyroplane, the horn structure
Including：Horn, rotor, rotor carry end and horn connector；One end of the horn sets horn connector, and the other end sets rotation
The wing carries end；The rotor is fixed on the rotor and carried on end；The agent structure that the rotor carries end is column construction；The cylindricality
Motor is set in the inner chamber of structure, and the motor is connected with the rotor.
Preferably, when the quantity of the rotor is 1, the upper bottom surface of the column construction sets rotor anchor tip, institute
Rotor is stated to be fixed on the rotor anchor tip；When the quantity of the rotor is 2, the upper and lower bottom surface of the column construction
On be respectively provided with rotor anchor tip, fix a rotor on each rotor anchor tip.
Preferably, when the quantity of the rotor is 1, the column construction is divided into motor waterproof from top to bottom
Lid, motor cabinet and lower bottom cover；The motor is set between the upper motor waterproof cover and the motor cabinet, and the motor is fixed on
On the motor cabinet；Electron speed regulator is set between the motor cabinet and the lower bottom cover.
Preferably, when the quantity of the rotor is 2, the column construction is divided into motor waterproof from top to bottom
Lid, motor cabinet and lower motor waterproof cover；The motor, the motor are set between the upper motor waterproof cover and the motor cabinet
It is fixed on the motor cabinet；Electron speed regulator is set between the motor cabinet and the lower motor waterproof cover.
Preferably, indicator lamp, the indicator lamp and the motor connection are set on the outer wall of the column construction.
Preferably, the horn structure also includes undercarriage, and by horizontal folding part, the undercarriage connects with the horn
Fitting is detachably connected.
It is highly preferred that the undercarriage includes undercarriage leg, undercarriage base and the undercarriage rubber base being sequentially arranged；
The fixed connector of the horizontal folding part is fixedly connected with the undercarriage leg and the horn connector respectively；The water
The flexible connection head of flat-folded overlapping piece and the horn connector pin connection.
The beneficial effects of the utility model are：
Structure described in the utility model realizes the more rotor single-blade horns of different task load and is total to the fast of paddle structure up and down
Speed combination, can need to realize that unmanned plane is changed into the rotor of three axle six, the rotor of four axle four from the rotor of three axle three according to mission payload
Be changed into the rotor of four axle eight, the rotor of six axle six is changed into the rotor of six axle 12, improve aircraft bearing capacity, reduce being produced into for gyroplane
Sheet and the efficiency for improving unmanned plane outdoor study task.
Brief description of the drawings
Fig. 1 is the horn structural representation for being used to combine gyroplane of no undercarriage；
Fig. 2 is the single-blade horn structural representation for being used to combine gyroplane of no undercarriage；
Fig. 3 is the double oar horn structural representations for being used to combine gyroplane of no undercarriage；
Fig. 4 is motor cabinet structural representation；
Fig. 5 is motor waterproof cover structural representation；
Fig. 6 is that the combination of double oar horn structure undercarriages in the deployed state for combining gyroplane for having undercarriage is shown
It is intended to；
Fig. 7 is that the fractionation of double oar horn structure undercarriages in the deployed state for combining gyroplane for having undercarriage is shown
It is intended to；
Fig. 8 is the signal of undercarriage in a folded configuration in the double oar horn structures for being used to combine gyroplane for have undercarriage
Figure；
Fig. 9 is the unmanned plane structural representation of the double oar horn structures of the rotor of three axle six；
Figure 10 is the unmanned plane structural representation of the rotor single-blade horn structure of six axle six.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, below in conjunction with accompanying drawing, to this reality
It is further elaborated with new.It should be appreciated that embodiment described herein is only explaining this practicality
It is new, it is not used to limit the utility model.
Embodiment
Reference picture 1, the horn structure for combining gyroplane is used for described in the present embodiment, and the horn structure includes：Horn 1,
Rotor 2, rotor carry end 3 and horn connector 4；One end of the horn 1 sets horn connector 4, and the other end sets rotor to carry
End 3；The rotor 2 is fixed on the rotor and carried on end 3；The agent structure that the rotor carries end 3 is column construction；The cylindricality
Setting motor 3-4, the motor 3-4 are connected with the rotor 2 in the inner chamber of structure.Horn structure described in the present embodiment is without rising and falling
Frame.
Explanation, which is explained in more detail, is：
(1) single-blade horn structure and double oar horn structures
1st, single-blade horn structure
Reference picture 2, the rotor quantity of single-blade horn structure is 1, and the upper bottom surface of the column construction sets rotor to fix
Joint, the rotor are fixed on the rotor anchor tip；The column construction is divided into motor waterproof from top to bottom
Cover 3-1, motor cabinet 3-2 and lower bottom cover 3-3；The motor is set between the upper motor waterproof cover 3-1 and the motor cabinet 3-2
3-4, the motor 3-4 are fixed on the motor cabinet 3-2；Electronics is set between the motor cabinet 3-2 and the lower bottom cover 3-3
Speed regulator 3-5.
2nd, double oar horn structures
Reference picture 3, the rotor quantity of double oar horn structures is 2, and rotation is respectively provided with the upper and lower bottom surface of the column construction
Wing anchor tip, each fix a rotor on the rotor anchor tip.The column construction is from top to bottom successively
It is divided into motor waterproof cover 3-1, motor cabinet 3-2 and lower motor waterproof cover 3-6；The upper motor waterproof cover 3-1 and the motor
The motor 3-4, the motor 3-4 is set to be fixed on the motor cabinet 3-2 between seat 3-2；The motor cabinet 3-2 with it is described
Electron speed regulator 3-5 is set between lower motor waterproof cover 3-6.
The structural representation of motor cabinet as shown in figure 4, setting dentalation on the outer wall of the motor cabinet, use by dentalation
In increase motor radiating area, facilitate motor radiating.The structural representation of upper and lower motor waterproof cover is as shown in Figure 5；For motor
With electron speed regulator waterproof.
(2) on the other structures on column construction
Indicator lamp is set on the outer wall of the column construction, and the indicator lamp is connected with the motor 3-4.
Embodiment 2
Reference picture 6, the present embodiment and the difference of embodiment 1 are：Horn structure has undercarriage 5 described in the present embodiment, leads to
Horizontal folding part 6 is crossed, the undercarriage is detachably connected with the horn connector.
Reference picture 7 and 8, the undercarriage 5 include undercarriage leg 5-1, the undercarriage base 5-2 being sequentially arranged and risen and fallen
Frame rubber base 5-3；The fixed connector of the horizontal folding part 6 is connected with the undercarriage leg 5-1 and the horn respectively
Part 4 is fixedly connected；The flexible connection head of the horizontal folding part 6 and the horn connector pin connection.Undercarriage is as needed
Rapid deployment and folding are realized by Quick-release pin.
By using above-mentioned technical proposal disclosed in the utility model, following beneficial effect has been obtained：
Structure described in the utility model realizes the more rotor single-blade horns of different task load and is total to the fast of paddle structure up and down
Speed combination, can need to realize that unmanned plane is changed into the rotor of three axle six, the rotor of four axle four from the rotor of three axle three according to mission payload
Be changed into the rotor of four axle eight, the rotor of six axle six is changed into the rotor of six axle 12, improve aircraft bearing capacity, reduce being produced into for gyroplane
Sheet and the efficiency for improving unmanned plane outdoor study task.
Described above is only preferred embodiment of the present utility model, it is noted that for the common skill of the art
For art personnel, on the premise of the utility model principle is not departed from, some improvements and modifications can also be made, these improve and
Retouching should also regard the scope of protection of the utility model.
Claims (7)
1. a kind of horn structure for being used to combine gyroplane, it is characterised in that the horn structure includes：Horn, rotor, rotor
Carry end and horn connector；
One end of the horn sets horn connector, and the other end sets rotor to carry end；The rotor is fixed on the rotor and carried
On end；The agent structure that the rotor carries end is column construction；Motor is set in the inner chamber of the column construction, the motor with
The rotor connection.
2. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that
When the quantity of the rotor is 1, the upper bottom surface of the column construction sets rotor anchor tip, and the rotor is fixed on
On the rotor anchor tip；
When the quantity of the rotor is 2, rotor anchor tip, Mei Gesuo are respectively provided with the upper and lower bottom surface of the column construction
State and a rotor is fixed on rotor anchor tip.
3. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the quantity of the rotor is 1
When individual, the column construction is divided into motor waterproof cover, motor cabinet and lower bottom cover from top to bottom；The upper motor waterproof cover
The motor is set between the motor cabinet, and the motor is fixed on the motor cabinet；The motor cabinet and the bottom
Electron speed regulator is set between lid.
4. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the quantity of the rotor is 2
When individual, the column construction is divided into motor waterproof cover, motor cabinet and lower motor waterproof cover from top to bottom；The upper motor
The motor is set between waterproof cover and the motor cabinet, and the motor is fixed on the motor cabinet；The motor cabinet and institute
State and electron speed regulator is set between lower motor waterproof cover.
5. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the outer wall of the column construction
Upper setting indicator lamp, the indicator lamp and the motor connection.
6. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the horn structure also includes
Undercarriage, by horizontal folding part, the undercarriage is detachably connected with the horn connector.
7. it is used for the horn structure for combining gyroplane according to claim 6, it is characterised in that the undercarriage is included sequentially
Undercarriage leg, undercarriage base and the undercarriage rubber base of setting；
The fixed connector of the horizontal folding part is fixedly connected with the undercarriage leg and the horn connector respectively；Institute
State the flexible connection head of horizontal folding part and the horn connector pin connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720566383.8U CN206782066U (en) | 2017-05-19 | 2017-05-19 | A kind of horn structure for being used to combine gyroplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720566383.8U CN206782066U (en) | 2017-05-19 | 2017-05-19 | A kind of horn structure for being used to combine gyroplane |
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| Publication Number | Publication Date |
|---|---|
| CN206782066U true CN206782066U (en) | 2017-12-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720566383.8U Active CN206782066U (en) | 2017-05-19 | 2017-05-19 | A kind of horn structure for being used to combine gyroplane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097943A (en) * | 2017-05-19 | 2017-08-29 | 北京帝测科技股份有限公司 | A kind of horn structure for being used to combine gyroplane |
| WO2020015257A1 (en) * | 2018-07-19 | 2020-01-23 | 深圳市道通智能航空技术有限公司 | Power device and unmanned aerial vehicle |
-
2017
- 2017-05-19 CN CN201720566383.8U patent/CN206782066U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097943A (en) * | 2017-05-19 | 2017-08-29 | 北京帝测科技股份有限公司 | A kind of horn structure for being used to combine gyroplane |
| WO2020015257A1 (en) * | 2018-07-19 | 2020-01-23 | 深圳市道通智能航空技术有限公司 | Power device and unmanned aerial vehicle |
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