CN211711042U - Aircraft of airship and many rotor unmanned aerial vehicle combinations - Google Patents
Aircraft of airship and many rotor unmanned aerial vehicle combinations Download PDFInfo
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- CN211711042U CN211711042U CN202020005426.7U CN202020005426U CN211711042U CN 211711042 U CN211711042 U CN 211711042U CN 202020005426 U CN202020005426 U CN 202020005426U CN 211711042 U CN211711042 U CN 211711042U
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- airship
- aerial vehicle
- unmanned aerial
- rotor
- rotor unmanned
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- 238000000429 assembly Methods 0.000 claims description 6
- 239000001307 helium Substances 0.000 description 3
- 229910052734 helium Inorganic materials 0.000 description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 3
- 239000002775 capsule Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
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Abstract
The utility model discloses an aircraft of airship and many rotor unmanned aerial vehicle combination, include: airship envelope, gasbag baffle, group battery, coupling assembling and many rotor unmanned aerial vehicle, the gasbag baffle sets up make in the airship envelope forms upper chamber and cavity down, the group battery sets up cavity down, many rotor unmanned aerial vehicle pass through coupling assembling connects the airship envelope cavity one end down, the group battery with many rotor unmanned aerial vehicle wire are connected. The utility model provides an aircraft of airship and many rotor unmanned aerial vehicle combination, the lift that provides through airship boat bag has increased many rotor unmanned aerial vehicle's the weight of taking off by a wide margin, makes many rotor unmanned aerial vehicle can carry the large capacity group battery, overcomes the relatively poor and poor problem of many rotor unmanned aerial vehicle continuation of current airship mobility.
Description
Technical Field
The utility model belongs to the technical field of aerostatics technique and specifically relates to an aircraft of airship and many rotor unmanned aerial vehicle combinations.
Background
An airship belongs to one type of aerostat, and is also an aircraft that uses lighter-than-air gas to provide lift. The lift obtained by the airship mainly comes from lighter-than-air gas filled inside the airship, such as hydrogen, helium and the like. Modern airships generally use helium, which is safer, to provide lift, and in addition, an engine mounted on the airship provides part of the lift. The airship has poor maneuverability, is easily influenced by wind power, has strong cruising ability and can float and fly for a long time. The multi-rotor unmanned aerial vehicle is an unmanned aerial vehicle controlled by radio remote control equipment and a self-contained program control device, and is widely applied to the fields of aerial photography, agriculture, plant protection, self-shooting, express transportation, disaster rescue and the like. Because many rotor unmanned aerial vehicle volumes are limited, in order to guarantee weight, the volume, nimble characteristic, the event can not carry the large capacity battery, the main problem that faces of many rotor unmanned aerial vehicle of leading to the fact present stage is that duration is short, can not fly for a long time, under the general condition, many rotor unmanned aerial vehicle longest operating time is about half an hour, if need carry out the work that the time of execution has the requirement or to the long work of working distance, just need fall into many times of flight operation and accomplish, a large amount of not high time has been consumed like this, working strength has been increased, cause many rotor unmanned aerial vehicle work efficiency, therefore, the problem of solving many rotor unmanned aerial vehicle duration becomes the problem that needs to be solved in order to present many rotor unmanned aerial vehicle control field. Therefore, how to organically combine the advantages of an airship and a multi-rotor unmanned aerial vehicle is a technical problem to be solved in the field.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aircraft of airship and many rotor unmanned aerial vehicle combination overcomes the relatively poor and many rotor unmanned aerial vehicle of current airship mobility problem poor of endurance.
In order to achieve the above object, the utility model provides an aircraft of airship and many rotor unmanned aerial vehicle combinations, include: airship envelope, gasbag baffle, group battery, coupling assembling and many rotor unmanned aerial vehicle, the gasbag baffle sets up make in the airship envelope forms upper chamber and cavity down, the group battery sets up cavity down, many rotor unmanned aerial vehicle pass through coupling assembling connects the airship envelope cavity one end down, the group battery with many rotor unmanned aerial vehicle wire are connected.
Optionally, the airship envelope comprises: gasbag and skeleton, support the gasbag the skeleton sets up the gasbag inner wall, the skeleton includes first ring and the second ring that the vertical cross set up, first ring with coupling assembling sets up perpendicularly.
Optionally, four driving assemblies are uniformly arranged along an outer circle of the airship envelope, and the driving assemblies are connected with the first circular ring.
Optionally, the driving assembly includes: first motor, first rotor and linking bridge, first motor passes through linking bridge connects first ring, first rotor is connected first motor.
Optionally, the gasbag is close to many rotor unmanned aerial vehicle one end is provided with the end cover, coupling assembling passes through the end cover connects the airship capsule, coupling assembling includes: connecting pipe, nut and radome fairing, the connecting pipe upper end with end cover fixed connection, the connecting pipe lower extreme with many rotor unmanned aerial vehicle threaded connection is used for locking the connecting pipe with many rotor unmanned aerial vehicle the nut sets up the connecting pipe lower extreme, the radome fairing is worn to establish the connecting pipe lower extreme and is detained on the nut.
Optionally, the power cord of group battery passes through the connecting pipe is connected many rotor unmanned aerial vehicle.
Optionally, the multi-rotor drone comprises: the upper bracket, the lower bracket, the flight control unit, the rotor support, the second motor and the second rotor, the flight control unit sets up the upper bracket with between the lower bracket, the rotor support is followed the circumference of upper bracket sets up, the second motor sets up the cantilever distal end of rotor support, the second rotor sets up on the second motor.
Optionally, a pan-tilt support for connecting a camera is further disposed on the lower support.
The utility model provides an aircraft of airship and many rotor unmanned aerial vehicle combinations, include: airship envelope, gasbag baffle, group battery, coupling assembling and many rotor unmanned aerial vehicle, the gasbag baffle sets up make in the airship envelope forms upper chamber and cavity down, the group battery sets up cavity down, many rotor unmanned aerial vehicle pass through coupling assembling connects the airship envelope cavity one end down, the group battery with many rotor unmanned aerial vehicle wire are connected. The utility model provides an aircraft of airship and many rotor unmanned aerial vehicle combination, the lift that provides through airship boat bag has increased many rotor unmanned aerial vehicle's the weight of taking off by a wide margin, makes many rotor unmanned aerial vehicle can carry the large capacity group battery, overcomes the relatively poor and poor problem of many rotor unmanned aerial vehicle continuation of current airship mobility.
Drawings
Fig. 1 is a schematic front view of an aircraft combining an airship and a multi-rotor drone according to an embodiment of the present invention;
fig. 2 is a schematic view of an airship and a multi-rotor drone according to an embodiment of the present invention;
FIG. 3 is a schematic top view of the combined airship and multi-rotor drone aircraft of FIG. 1;
fig. 4 is a schematic top view of another airship and multi-rotor drone combined aircraft according to an embodiment of the present invention;
fig. 5 is a schematic view of a multi-rotor drone provided by an embodiment of the present invention looking down.
Wherein: 1-airship envelope, 101-airbag, 102-skeleton, 103-upper chamber, 104-lower chamber, 2-driving assembly, 201-first motor, 202-first rotor, 203-connecting bracket, 3-airbag partition, 4-battery pack, 401-power line, 5-end cover, 6-connecting assembly, 601-connecting pipe, 602-nut, 603-fairing, 7-multi-rotor unmanned plane, 701-lower bracket, 702-upper bracket, 703-flight control unit, 704-rotor bracket, 705-second motor, 706-second rotor, 707-tripod head bracket.
Detailed Description
The following description of the embodiments of the present invention will be described in more detail with reference to the drawings. Advantages and features of the present invention will become apparent from the following description and claims. It should be noted that the drawings are in simplified form and are not to precise scale, and are provided for convenience and clarity in order to facilitate the description of the embodiments of the present invention.
The utility model provides an aircraft of airship and many rotor unmanned aerial vehicle combination, figure 1 is the utility model discloses an embodiment provides an aircraft owner of airship and many rotor unmanned aerial vehicle combination looks the schematic diagram, and figure 2 is the utility model discloses an embodiment provides an airship and many rotor unmanned aerial vehicle connect the schematic diagram, it is shown to see figure 1 and figure 2, the aircraft of airship and many rotor unmanned aerial vehicle combination includes: airship bag 1, gasbag baffle 3, group battery 4, coupling assembling 6 and many rotor unmanned aerial vehicle 7, gasbag baffle 3 sets up make in the airship bag 1 cavity 103 and lower cavity 104 are formed to airship bag 1, it fills the helium to go up cavity 103, group battery 4 sets up cavity 104 down, many rotor unmanned aerial vehicle 7 passes through coupling assembling 6 connects airship bag 1 cavity 104 one end down, group battery 4 with many rotor unmanned aerial vehicle 7 wire connection.
Present many rotor unmanned aerial vehicle is because the volume is limited, in order to guarantee weight, the volume, nimble characteristic, the event can not carry the large capacity battery, cause the main problem that faces of many rotor unmanned aerial vehicle of present stage to be duration short, can not fly for a long time, under the general condition, many rotor unmanned aerial vehicle longest operating time is about half an hour, if need carry out the time and have the work of requirement or to the long work of working distance, just need fall into the operation of flying many times and accomplish, a large amount of time has been consumed like this, the working strength has been increased, cause many rotor unmanned aerial vehicle work efficiency not high. The airship has poor maneuverability, is easily influenced by wind power, has strong cruising ability and can float and fly for a long time. The utility model provides an aircraft of airship and many rotor unmanned aerial vehicle combination, the lift that provides through airship boat bag has increased many rotor unmanned aerial vehicle's the weight of taking off by a wide margin, makes many rotor unmanned aerial vehicle can carry the large capacity group battery, overcomes the relatively poor and poor problem of many rotor unmanned aerial vehicle continuation of current airship mobility.
Fig. 3 is a schematic top view of the combined airship and multi-rotor drone aircraft of fig. 1, the airship envelope 1 comprising, as shown in fig. 1-3: gasbag 101 and skeleton 102 support gasbag 101 skeleton 102 sets up gasbag 101 inner wall, skeleton 102 includes the first ring and the second ring of perpendicular crossing arrangement, first ring with coupling assembling sets up perpendicularly, gasbag 101 is the casing of ellipsoid. Four driving components 2 are uniformly arranged along an outer circle of the airship capsule 1, and the driving components 2 are fixedly connected with the first circular ring. The drive assembly 2 comprises: first motor 201, first rotor 202 and linking bridge 203, first motor 201 passes through linking bridge 203 connects the first ring, first rotor 202 connects the first motor. First rotor 202 can arrange with many rotor unmanned aerial vehicle's the same vertical direction of rotor, adopts many rotor unmanned aerial vehicle flight and turns to principle control. Fig. 4 is a schematic top view of another airship and multi-rotor drone combined aircraft according to an embodiment of the present invention, referring to fig. 4, the driving assemblies 2 may also be arranged in a horizontal direction, and the propulsion directions of the opposing sets of driving assemblies 2 are perpendicular to each other, so as to push the airship envelope 1 to move in a plane.
Referring to fig. 1-3, the air bag 101 is provided with an end cap 5 near one end of the multi-rotor drone 7, the connecting assembly 6 is connected to the airship envelope 1 through the end cap 5, and the connecting assembly 6 includes: connecting pipe 601, nut 602 and radome fairing 603, connecting pipe 601 upper end with 5 fixed connection of end cover, connecting pipe 601 lower extreme with many rotor unmanned aerial vehicle 7 threaded connection for locking connecting pipe 601 with many rotor unmanned aerial vehicle 7 nut 602 sets up connecting pipe 601 lower extreme, radome fairing 603 is the hemisphere casing, radome fairing 603 wears to establish connecting pipe 601 lower extreme and knot are in on the nut 602. The power cord 401 of the battery pack 4 is connected to the multi-rotor unmanned aerial vehicle 7 through the connection pipe 601.
Fig. 5 is a schematic top view of a multi-rotor drone, as provided by an embodiment of the present invention, and as shown in fig. 1 to 5, the multi-rotor drone 7 includes: the aircraft comprises an upper bracket 701, a lower bracket 702, a flight control unit 703, a rotor bracket 704, a second motor 705 and a second rotor 706, wherein the flight control unit 702 is arranged between the upper bracket 701 and the lower bracket 702, and the middle part of the upper bracket 701 is in threaded connection with a connecting pipe 601. The rotor support 704 is disposed along the circumferential direction of the upper support 701, the second motor 705 is disposed at the boom distal end of the rotor support 704, and the second rotor 706 is disposed on the second motor 705. Each rotor support 704 is provided with a second rotor 706, and the multi-rotor drone 7 is provided with 4 rotor supports 704. As a person skilled in the art, it is easily understood that the multi-rotor drone 7 can provide power to control the takeoff and landing of the whole aircraft, and the details are not repeated in this embodiment. The lower support 702 is also provided with a holder support for connecting a camera, and the lower support can carry the camera or other photographic instruments for aerial photography. The lower support 702 can also carry various functional modules, such as a suspended storage box for express transportation, a fire extinguishing agent for fire extinguishing and the like.
To sum up, the embodiment of the utility model provides an in the aircraft of a combination of dirigible and many rotor unmanned aerial vehicle, the aircraft of dirigible and many rotor unmanned aerial vehicle combination includes: airship bag 1, gasbag baffle 3, group battery 4, coupling assembling 6 and many rotor unmanned aerial vehicle 7, gasbag baffle 3 sets up make in airship bag 1 forms upper chamber 103 and lower chamber 104, group battery 4 sets up lower chamber 104, many rotor unmanned aerial vehicle 7 passes through coupling assembling 6 connects airship bag 1 cavity 104 one end down, group battery 4 with many rotor unmanned aerial vehicle 7 wire is connected. The utility model provides an aircraft of airship and many rotor unmanned aerial vehicle combination, the lift that provides through airship boat bag has increased many rotor unmanned aerial vehicle's the weight of taking off by a wide margin, makes many rotor unmanned aerial vehicle can carry the large capacity group battery, overcomes the relatively poor and poor problem of many rotor unmanned aerial vehicle continuation of current airship mobility.
The above description is only for the preferred embodiment of the present invention, and does not limit the present invention. Any technical personnel who belongs to the technical field, in the scope that does not deviate from the technical scheme of the utility model, to the technical scheme and the technical content that the utility model discloses expose do the change such as the equivalent replacement of any form or modification, all belong to the content that does not break away from the technical scheme of the utility model, still belong to within the scope of protection of the utility model.
Claims (8)
1. An aircraft of airship and many rotor unmanned aerial vehicle combination, its characterized in that includes: airship envelope, gasbag baffle, group battery, coupling assembling and many rotor unmanned aerial vehicle, the gasbag baffle sets up make in the airship envelope forms upper chamber and cavity down, the group battery sets up cavity down, many rotor unmanned aerial vehicle pass through coupling assembling connects the airship envelope cavity one end down, the group battery with many rotor unmanned aerial vehicle wire are connected.
2. The airship and multi-rotor drone combined aircraft according to claim 1, characterised in that the airship envelope comprises: gasbag and skeleton, support the gasbag the skeleton sets up the gasbag inner wall, the skeleton includes first ring and the second ring that the vertical cross set up, first ring with coupling assembling sets up perpendicularly.
3. The airship and multi-rotor drone combined aircraft according to claim 2, characterised in that four driving assemblies are evenly arranged along an outer circle of the airship envelope, said driving assemblies being connected to the first circular ring.
4. The airship and multi-rotor drone combined aircraft according to claim 3, wherein the drive assembly comprises: first motor, first rotor and linking bridge, first motor passes through linking bridge connects first ring, first rotor is connected first motor.
5. The airship and multi-rotor drone combined aircraft according to claim 2, wherein the envelope is provided with an end cap near one end of the multi-rotor drone, the connection assembly connecting the airship envelope through the end cap, the connection assembly comprising: connecting pipe, nut and radome fairing, the connecting pipe upper end with end cover fixed connection, the connecting pipe lower extreme with many rotor unmanned aerial vehicle threaded connection is used for locking the connecting pipe with many rotor unmanned aerial vehicle the nut sets up the connecting pipe lower extreme, the radome fairing is worn to establish the connecting pipe lower extreme and is detained on the nut.
6. The airship and multi-rotor drone combined aircraft according to claim 5, wherein the power cord of the battery pack connects the multi-rotor drone through the connecting tube.
7. The airship and multi-rotor drone combined aircraft according to claim 2, characterised in that the multi-rotor drone comprises: the upper bracket, the lower bracket, the flight control unit, the rotor support, the second motor and the second rotor, the flight control unit sets up the upper bracket with between the lower bracket, the rotor support is followed the circumference of upper bracket sets up, the second motor sets up the cantilever distal end of rotor support, the second rotor sets up on the second motor.
8. The airship and multi-rotor drone combined aircraft according to claim 7, wherein the lower cradle is further provided with a pan-tilt cradle for connecting a camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020005426.7U CN211711042U (en) | 2020-01-03 | 2020-01-03 | Aircraft of airship and many rotor unmanned aerial vehicle combinations |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020005426.7U CN211711042U (en) | 2020-01-03 | 2020-01-03 | Aircraft of airship and many rotor unmanned aerial vehicle combinations |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211711042U true CN211711042U (en) | 2020-10-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020005426.7U Expired - Fee Related CN211711042U (en) | 2020-01-03 | 2020-01-03 | Aircraft of airship and many rotor unmanned aerial vehicle combinations |
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| Country | Link |
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| CN (1) | CN211711042U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114261502A (en) * | 2021-12-28 | 2022-04-01 | 同济大学 | Novel rotor airship mechanism |
| WO2022257586A1 (en) * | 2021-06-08 | 2022-12-15 | 刘焕章 | Flying boat |
-
2020
- 2020-01-03 CN CN202020005426.7U patent/CN211711042U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022257586A1 (en) * | 2021-06-08 | 2022-12-15 | 刘焕章 | Flying boat |
| CN114261502A (en) * | 2021-12-28 | 2022-04-01 | 同济大学 | Novel rotor airship mechanism |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201020 |
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| CF01 | Termination of patent right due to non-payment of annual fee |