CN204197286U - Double-deck detachable unmanned plane - Google Patents
Double-deck detachable unmanned plane Download PDFInfo
- Publication number
- CN204197286U CN204197286U CN201420649616.7U CN201420649616U CN204197286U CN 204197286 U CN204197286 U CN 204197286U CN 201420649616 U CN201420649616 U CN 201420649616U CN 204197286 U CN204197286 U CN 204197286U
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- CN
- China
- Prior art keywords
- control box
- bracket
- master control
- unmanned plane
- extension set
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- Withdrawn - After Issue
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Abstract
The utility model discloses a kind of double-deck detachable unmanned plane, comprise extension set and lower extension set, described upper extension set comprises upper bracket, upper master control box and screw wing, described upper bracket is triangular supports, three described screw wings are arranged on three angles of described upper bracket, described upper master control box is fixedly connected with described upper bracket by three upper connecting rods, described lower extension set comprises lower bracket and lower master control box, described lower bracket is triangular supports, three angles of described lower bracket are provided with described screw wing, described lower master control box is fixedly connected with described lower bracket by three lower connecting rods, the lower surface of described upper master control box is connected by the upper surface of connecting device with described upper master control box.Upper extension set is connected with lower extension set by connecting device by the double-deck detachable unmanned plane of the utility model, makes it when needs use multiple unmanned plane, upper extension set and lower extension set can be separated, two extension sets are worked alone, easy to operate.
Description
Technical field
The utility model relates to unmanned plane, particularly relates to a kind of double-deck detachable unmanned plane.
Background technology
The field condition of timely acquisition disaster, burst accident, rides vital effect in whole disaster relief work, and in the face of precipitate disaster and accident, traditional technological means is difficult to obtain on-the-spot situation in time.By carrying relevant equipment, unmanned plane can from completing special task in the air, unmanned plane has the advantages such as cost is low, flexibility ratio is high, strong adaptability, in various burst accident, there is stronger application potential, traditional unmanned plane is standalone unmanned plane, if when subregion needs more unmanned plane, then need multiple unmanned plane to finish the work.
Utility model content
The purpose of this utility model is just to provide a kind of double-deck detachable unmanned plane to solve the problem.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind of double-deck detachable unmanned plane, comprise extension set and lower extension set, described upper extension set comprises upper bracket, upper master control box and screw wing, described upper bracket is triangular supports, three described screw wings are arranged on three angles of described upper bracket, described upper master control box is fixedly connected with described upper bracket by three upper connecting rods, described lower extension set comprises lower bracket and lower master control box, described lower bracket is triangular supports, three angles of described lower bracket are provided with described screw wing, described lower master control box is fixedly connected with described lower bracket by three lower connecting rods, the lower surface of described upper master control box is connected by the upper surface of connecting device with described upper master control box.
Particularly, described upper bracket and described lower bracket are equilateral triangle, and the length of side of described upper bracket is equal with the length of side of described lower bracket.
Particularly, the angle between described upper bracket and described lower bracket is 60 °.
Particularly, described connecting device comprises screw rod, coupling link, miniature motor and Stroke Control ring, the bottom of described upper master control box is provided with groove, described connecting device is arranged in described groove, described coupling link is fixedly connected with the upper surface of described lower master control box, described screw rod is arranged in described groove, and through described coupling link and described Stroke Control ring, the inner side of described Stroke Control ring is provided with and the negative thread coordinated outside described screw rod, and the arranged outside of described Stroke Control ring has the gear teeth coordinated with the torque output shaft of described miniature motor.
Further, the number of described connecting device is three, and described screw rod and described coupling link are provided with signal transmitting apparatus.
Particularly, described unmanned plane also comprises both direction rotor, and two described direction rotors are fixedly connected with the lower surface of described lower master control box with the upper surface of described upper master control box respectively by pipe link.
The beneficial effects of the utility model are:
Upper extension set is connected with lower extension set by connecting device by the double-deck detachable unmanned plane of the utility model, makes it when needs use multiple unmanned plane, upper extension set and lower extension set can be separated, two extension sets are worked alone, easy to operate.
Accompanying drawing explanation
Fig. 1 is the birds-eye view of the detachable unmanned plane of bilayer described in the utility model;
Fig. 2 is the lateral plan of the detachable unmanned plane of bilayer described in the utility model;
Fig. 3 is the structural representation of connecting device described in the utility model.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail:
As Fig. 1, shown in Fig. 2 and Fig. 3, the double-deck detachable unmanned plane of the utility model, comprise extension set, lower extension set and both direction rotor 7, upper extension set comprises upper bracket 1, upper master control box 4 and screw wing 3, upper bracket 1 is triangular supports, three screw wings 3 are arranged on three angles of upper bracket 1, upper master control box 4 is fixedly connected with upper bracket 1 by three upper connecting rods 5, lower extension set comprises lower bracket 2 and lower master control box 6, lower bracket 2 is triangular supports, three angles of lower bracket 2 are provided with screw wing 3, lower master control box 6 is fixedly connected with lower bracket 2 by three lower connecting rods, the lower surface of upper master control box 4 is connected by the upper surface of connecting device with upper master control box 4, upper bracket 1 and lower bracket 2 are equilateral triangle, and the length of side of upper bracket 1 is equal with the length of side of lower bracket 2, angle between upper bracket 1 and lower bracket 2 is 60 °, connecting device comprises screw rod 10, coupling link 9, miniature motor 12 and Stroke Control ring 11, the bottom of upper master control box 4 is provided with groove, connecting device is arranged in groove, coupling link 9 is fixedly connected with the upper surface of lower master control box 6, screw rod 10 is arranged in groove, and through coupling link 9 and Stroke Control ring 11, the inner side of Stroke Control ring 11 is provided with and the negative thread coordinated outside screw rod 10, the arranged outside of Stroke Control ring 11 has the gear teeth coordinated with the torque output shaft of miniature motor 12, the number of connecting device is three, and screw rod 10 and coupling link 9 are provided with signal transmitting apparatus, both direction rotor 7 is fixedly connected with the lower surface of lower master control box 6 with the upper surface of upper master control box 4 respectively by pipe link.
The principle of work of the double-deck detachable unmanned plane of the utility model is as follows:
When needs use single unmanned plane, coupling link 9 on the lower master control box 6 of lower extension set is inserted in the groove of upper master control box 4 of upper extension set, then control satellite motor to rotarily drive Stroke Control ring 11 and rotate, thus make screw rod 10 insert in coupling link 9, lower extension set is fixedly connected with upper extension set, simultaneously because screw rod 10 be connected change in be provided with signal transmitting apparatus, when it can be made to be in coupled condition, upper extension set and upper extension set receive common control signal, can proper motion; When needs use two unmanned planes, control miniature motor 12 rotation and screw rod 10 is regained, thus extension set and lower extension set are departed from, synchronous signal transmitting device is separated, then two extension sets can be made independently to control, the object that complete independently is corresponding.Because connecting device makes employing Electronic control, then the utility model can be made to be separated in state of flight, the situation needing suddenly multiple unmanned plane in some emergency case can be tackled.
The technical solution of the utility model is not limited to the restriction of above-mentioned specific embodiment, and every technology distortion made according to the technical solution of the utility model, all falls within protection domain of the present utility model.
Claims (6)
1. the detachable unmanned plane of bilayer, it is characterized in that: comprise extension set and lower extension set, described upper extension set comprises upper bracket, upper master control box and screw wing, described upper bracket is triangular supports, three described screw wings are arranged on three angles of described upper bracket, described upper master control box is fixedly connected with described upper bracket by three upper connecting rods, described lower extension set comprises lower bracket and lower master control box, described lower bracket is triangular supports, three angles of described lower bracket are provided with described screw wing, described lower master control box is fixedly connected with described lower bracket by three lower connecting rods, the lower surface of described upper master control box is connected by the upper surface of connecting device with described upper master control box.
2. the detachable unmanned plane of bilayer according to claim 1, is characterized in that: described upper bracket and described lower bracket are equilateral triangle, and the length of side of described upper bracket is equal with the length of side of described lower bracket.
3. the detachable unmanned plane of bilayer according to claim 1, is characterized in that: the angle between described upper bracket and described lower bracket is 60 °.
4. the detachable unmanned plane of bilayer according to claim 1, it is characterized in that: described connecting device comprises screw rod, coupling link, miniature motor and Stroke Control ring, the bottom of described upper master control box is provided with groove, described connecting device is arranged in described groove, described coupling link is fixedly connected with the upper surface of described lower master control box, described screw rod is arranged in described groove, and through described coupling link and described Stroke Control ring, the inner side of described Stroke Control ring is provided with and the negative thread coordinated outside described screw rod, the arranged outside of described Stroke Control ring has the gear teeth coordinated with the torque output shaft of described miniature motor.
5. the detachable unmanned plane of bilayer according to claim 4, is characterized in that: the number of described connecting device is three, and described screw rod and described coupling link are provided with signal transmitting apparatus.
6. the detachable unmanned plane of bilayer according to claim 1, is characterized in that: also comprise both direction rotor, and two described direction rotors are fixedly connected with the lower surface of described lower master control box with the upper surface of described upper master control box respectively by pipe link.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420649616.7U CN204197286U (en) | 2014-11-03 | 2014-11-03 | Double-deck detachable unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420649616.7U CN204197286U (en) | 2014-11-03 | 2014-11-03 | Double-deck detachable unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204197286U true CN204197286U (en) | 2015-03-11 |
Family
ID=52655273
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420649616.7U Withdrawn - After Issue CN204197286U (en) | 2014-11-03 | 2014-11-03 | Double-deck detachable unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204197286U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104386248A (en) * | 2014-11-03 | 2015-03-04 | 成都好飞机器人科技有限公司 | Double-layer separation type unmanned aerial vehicle |
| CN105438458A (en) * | 2015-12-04 | 2016-03-30 | 上海交通大学 | Double-layer and eight-rotor-wing aircraft |
| CN106155075A (en) * | 2016-08-22 | 2016-11-23 | 上海交通大学 | A kind of detachable unmanned aerial vehicle control system |
| CN106275402A (en) * | 2016-08-30 | 2017-01-04 | 上海交通大学 | Detachable four oar double-vane unmanned planes |
| CN106394865A (en) * | 2016-08-30 | 2017-02-15 | 上海交通大学 | Separable type double multi-rotor unmanned aircrafts |
| CN107600384A (en) * | 2017-08-30 | 2018-01-19 | 泸州深远世宁无人机科技有限公司 | A kind of rack construction for unmanned plane |
-
2014
- 2014-11-03 CN CN201420649616.7U patent/CN204197286U/en not_active Withdrawn - After Issue
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104386248A (en) * | 2014-11-03 | 2015-03-04 | 成都好飞机器人科技有限公司 | Double-layer separation type unmanned aerial vehicle |
| CN105438458A (en) * | 2015-12-04 | 2016-03-30 | 上海交通大学 | Double-layer and eight-rotor-wing aircraft |
| CN106155075A (en) * | 2016-08-22 | 2016-11-23 | 上海交通大学 | A kind of detachable unmanned aerial vehicle control system |
| CN106155075B (en) * | 2016-08-22 | 2020-07-14 | 上海交通大学 | Separable unmanned aerial vehicle control system |
| CN106275402A (en) * | 2016-08-30 | 2017-01-04 | 上海交通大学 | Detachable four oar double-vane unmanned planes |
| CN106394865A (en) * | 2016-08-30 | 2017-02-15 | 上海交通大学 | Separable type double multi-rotor unmanned aircrafts |
| CN106394865B (en) * | 2016-08-30 | 2019-05-24 | 上海交通大学 | Detachable double multi-rotor unmanned aerial vehicles |
| CN106275402B (en) * | 2016-08-30 | 2019-10-08 | 上海交通大学 | Detachable four paddles double-vane unmanned plane |
| CN107600384A (en) * | 2017-08-30 | 2018-01-19 | 泸州深远世宁无人机科技有限公司 | A kind of rack construction for unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20150311 Effective date of abandoning: 20161019 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |