CN207045722U - A kind of multipurpose captive unmanned plane - Google Patents
A kind of multipurpose captive unmanned plane Download PDFInfo
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- CN207045722U CN207045722U CN201720913345.5U CN201720913345U CN207045722U CN 207045722 U CN207045722 U CN 207045722U CN 201720913345 U CN201720913345 U CN 201720913345U CN 207045722 U CN207045722 U CN 207045722U
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Abstract
The utility model discloses a kind of multipurpose captive unmanned plane, four foldable horns for include casing, being connected on casing, it is fixedly installed on the skeleton of casing internal, it is installed on the electron speed regulator of bottom of shell, master controller, flying quality collector, parachute emergency set, power module and the signal transmission module being installed on skeleton, and the oar rotor of four axle eight being connected on four foldable horns；The motor of the oar rotor of four axle eight is connected with electron speed regulator, and electron speed regulator, flying quality collector, parachute emergency set, power module, signal transmission module are connected with master controller.The utility model horn is arranged to folding structure, convenient to carry out collapsed transportable, while is provided with parachute emergency set, is capable of the damage of the emergency landing in the case where unmanned plane breaks down, at utmost reduction unmanned plane.
Description
Technical field
It the utility model is related to and stay formula unmanned air vehicle technique field, specifically a kind of multipurpose captive unmanned plane.
Background technology
With the fast development of unmanned air vehicle technique, to the increasingly strong of the demand of unmanned plane, unmanned plane is in today's society
Role is more and more important.The development of battery technology is limited to, continuous working period is always one of unmanned air vehicle technique
Bottleneck, it is conventional to be often no more than a hour by the unmanned plane that battery is the energy, most long continuous working period.Many situations
Under, only the working time of dozens of minutes is far from being enough that therefore, captive unmanned plane arises at the historic moment, and is tethered at unmanned plane and leads to
The transmission of photoelectric comprehensive hawser is crossed electric energy and to carry out data transmission, allow unmanned plane not by electric energy limited and long lasting for work
Make.Existing captive unmanned plane is all integrated fixed structure, can not carry out collapsed transportable, cause the waste of transport space；
On the other hand when captive unmanned plane breaks down, safe falling can not be carried out, causes the damage of captive unmanned plane.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of multipurpose captive unmanned plane, and horn is arranged to roll over
Stack structure, it is convenient to carry out collapsed transportable, while parachute emergency set is provided with, it is easy to the safe falling of captive unmanned plane,
Avoid the damage of captive unmanned plane.
The technical solution of the utility model is：
A kind of multipurpose captive unmanned plane, four foldable horns for include casing, being connected on casing, fixation are set
The skeleton of casing internal is placed in, is installed on the electron speed regulator of bottom of shell, master controller, the flying quality being installed on skeleton
Collector, parachute emergency set, power module and signal transmission module, and four axles being connected on four foldable horns
Eight oar rotors；The motor of the described oar rotor of four axle eight is connected with electron speed regulator, described flying quality collector, drop
Fall umbrella emergency set, power module, signal transmission module, electron speed regulator to be connected with master controller；Set on described casing
Four horn connectors are equipped with, are set with the casing connector for being fixed with tubulose on four horn connectors, described four can
Fold on the inner end of horn suit and be fixed with the horn connector of tubulose, described casing connector and horn connector it
Between connected by axis of rotation, be set with removable connection ring outside described horn connector, may move connection ring relative to machine
Annular groove is provided with one annular end face of shell connector, the side wall of annular groove is connected with the wall contacts of casing connector.
Described casing connector and the outer end of horn connector are provided with the spacing harden structure of annular, horn connector
End, the inner end of foldable horn contacted with corresponding limiting plate it is spacing.
The bottom of described casing connector outer end is provided with the rotating shaft of integral plastotype, rotating shaft in it is horizontally disposed and perpendicular to
The casing connector of tubulose, the bottom of described horn connector outer end are fixed with rotating connector, and rotating connector is set in
Along axis of rotation in rotating shaft.
The side wall of described removable connection ring annular groove is provided with internal thread, and described casing connector is located at outer end
External screw thread is provided with outer wall, the side wall of described annular groove is connected with the outer wall thread of casing connector.
Described signal transmission module includes the wireless communication module and optical-electrical converter being connected respectively with master controller,
Described optical-electrical converter is gone out the optical signal transmission after conversion by optical fiber.
The GPS module being connected with master controller is additionally provided with described skeleton.The advantages of the utility model：
The utility model horn is rotatablely connected with casing using the casing connector and horn connector of rotation connection,
When needs fly in use, horn connector drives horn to turn to the position docked horizontal with casing connector and using removable
Dynamic connection ring is attached fixation, ensures to stay the normal flight of formula unmanned plane；Needed when staying formula unmanned plane to stop flight into luggage
Case transport when, removable connection ring can be separated with casing connector, horn connector rotate under gravity perpendicular to
Casing connector, realize the purpose of collapsed transportable；The utility model is provided with the parachute emergency set being connected with master controller,
When captive unmanned plane breaks down, main controller controls parachute emergency set is opened, while controls the oar rotor of four axle eight
Motor stop operating, realize the safe falling of captive unmanned plane, avoid the damage of captive unmanned plane.
Brief description of the drawings
Fig. 1 is top view of the present utility model.
Fig. 2 is upward view of the present utility model.
Fig. 3 is front view of the present utility model.
Fig. 4 is the structural representation of the utility model casing internal.
Fig. 5 is the structural representation under the utility model casing connector and horn connector horizontality.
Fig. 6 is the structural representation under the utility model casing connector and horn connector folded state.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
See Fig. 1-Fig. 4, a kind of multipurpose captive unmanned plane, include lower section and be hung with the casing 1 of workload 21, connect
Four foldable horns 2 being connected on casing 1, the skeleton 3 being fixedly installed on inside casing 1, the main control being installed on skeleton 3
Device 4, flying quality collector 5, parachute emergency set 6, power module 7, wireless communication module 8, optical-electrical converter 9 and GPS
Module 10, is installed on the electron speed regulator 11 of the bottom of casing 1, and the oar of four axle eight rotation being connected on four foldable horns 2
The wing 12；The motor of the oar rotor 12 of four axle eight is connected with electron speed regulator 11, the emergent dress of flying quality collector 5, parachute
6, power module 7, wireless communication module 8, optical-electrical converter 9, GPS module 10, electron speed regulator 11 is put with master controller 4 to connect
Connect；Wherein, optical-electrical converter 9 is gone out the optical signal transmission after conversion by optical fiber；
See Fig. 5 and Fig. 6, four horn connectors 13 are provided with casing 1（See Fig. 1）, on four horn connectors 13
Suit is fixed with the casing connector 14 of tubulose, and the horn for being fixed with tubulose is set with the inner end of four foldable horns 2
The outer end of connector 15, casing connector 14 and horn connector 15 is provided with the structure of limiting plate 16 of annular, horn connection
First 13 end, the inner end of foldable horn 2 contact spacing with corresponding limiting plate 15；The bottom of the outer end of casing connector 14
Portion is provided with the rotating shaft 17 of integral plastotype, and rotating shaft 17 is in horizontally disposed and perpendicular to the casing connector 14 of tubulose, horn connection
The bottom of the outer end of part 15 is fixed with rotating connector 18, and rotating connector 18 is set in rotating shaft 17 and rotated along rotating shaft 17；Horn
Removable connection ring 19 is set with outside connector 15, may move connection ring 19 relative on an annular end face of casing connector 14
Annular groove 110 is provided with, the side wall of annular groove 110 is provided with internal thread, and casing connector 14, which is located on the outer wall of outer end, to be set
There is external screw thread, the side wall of annular groove 110 is connected with the outer wall thread of casing connector 14.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
- A kind of 1. multipurpose captive unmanned plane, it is characterised in that：Four foldable machines for include casing, being connected on casing Arm, the skeleton of casing internal is fixedly installed on, is installed on the electron speed regulator of bottom of shell, the main control being installed on skeleton Device, flying quality collector, parachute emergency set, power module and signal transmission module, and be connected to four it is foldable The oar rotor of four axle eight on horn；The motor of the described oar rotor of four axle eight is connected with electron speed regulator, described flight Data acquisition unit, parachute emergency set, power module, signal transmission module, electron speed regulator are connected with master controller；Institute Four horn connectors are provided with the casing stated, the casing connector for being fixed with tubulose is set with four horn connectors, Suit is fixed with the horn connector of tubulose on the inner end of four described foldable horns, described casing connector and Connected between horn connector by axis of rotation, removable connection ring is set with outside described horn connector, the company of may move Ring is connect relative to being provided with annular groove on an annular end face of casing connector, the side wall of annular groove and the outer wall of casing connector Contact connection.
- A kind of 2. multipurpose captive unmanned plane according to claim 1, it is characterised in that：Described casing connector and The outer end of horn connector is provided with the spacing harden structure of annular, the end of horn connector, the inner end of foldable horn Contacted with corresponding limiting plate spacing.
- A kind of 3. multipurpose captive unmanned plane according to claim 1, it is characterised in that：Outside described casing connector The bottom at end is provided with the rotating shaft of integral plastotype, and rotating shaft is in horizontally disposed and perpendicular to the casing connector of tubulose, described machine The bottom of arm connector outer end is fixed with rotating connector, and rotating connector is set in rotating shaft along axis of rotation.
- A kind of 4. multipurpose captive unmanned plane according to claim 1, it is characterised in that：Described removable connection ring The side wall of annular groove is provided with internal thread, and described casing connector, which is located on the outer wall of outer end, is provided with external screw thread, described The side wall of annular groove is connected with the outer wall thread of casing connector.
- A kind of 5. multipurpose captive unmanned plane according to claim 1, it is characterised in that：Described signal transmission module Include the wireless communication module and optical-electrical converter being connected respectively with master controller, described optical-electrical converter will by optical fiber Optical signal transmission after conversion is gone out.
- A kind of 6. multipurpose captive unmanned plane according to claim 1, it is characterised in that：Also set up on described skeleton There is the GPS module being connected with master controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720913345.5U CN207045722U (en) | 2017-07-26 | 2017-07-26 | A kind of multipurpose captive unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720913345.5U CN207045722U (en) | 2017-07-26 | 2017-07-26 | A kind of multipurpose captive unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045722U true CN207045722U (en) | 2018-02-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720913345.5U Active CN207045722U (en) | 2017-07-26 | 2017-07-26 | A kind of multipurpose captive unmanned plane |
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| Country | Link |
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| CN (1) | CN207045722U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107352025A (en) * | 2017-07-26 | 2017-11-17 | 安徽云翼航空技术有限公司 | A kind of multipurpose captive unmanned plane |
-
2017
- 2017-07-26 CN CN201720913345.5U patent/CN207045722U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107352025A (en) * | 2017-07-26 | 2017-11-17 | 安徽云翼航空技术有限公司 | A kind of multipurpose captive unmanned plane |
| CN107352025B (en) * | 2017-07-26 | 2023-05-26 | 安徽云翼航空技术有限公司 | Multipurpose tethered unmanned aerial vehicle |
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