CN205440859U - A six rotor craft frames for disaster relief supplies are put in - Google Patents
A six rotor craft frames for disaster relief supplies are put in Download PDFInfo
- Publication number
- CN205440859U CN205440859U CN201521058137.9U CN201521058137U CN205440859U CN 205440859 U CN205440859 U CN 205440859U CN 201521058137 U CN201521058137 U CN 201521058137U CN 205440859 U CN205440859 U CN 205440859U
- Authority
- CN
- China
- Prior art keywords
- disaster relief
- lower installation
- installation board
- mounting plate
- relief supplies
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model provides a six rotor craft frames for disaster relief supplies are put in, the frame includes fuselage and six cantilevers, the fuselage includes mounting panel, lower mounting panel and is used for connecting the spliced pole of going up mounting panel and lower mounting panel, goes up and forms accommodation space between mounting panel and the lower mounting panel, goes up the first connecting seat that the mounting panel edge was equipped with six circumference evenly distributed, and lower mounting panel edge is equipped with six circumference evenly distributed's second connecting seat, and the setting is just presented down with second connecting seat one -to -one to first connecting seat, first mount pad forms the installation station rather than the second mount pad that corresponds, and cantilever one end is installed on the installation station, the other end of cantilever is equipped with the motor, and the output shaft and the screw of motor are connected. The utility model discloses the carrying capacity is big, can realize the input of goods and materials, and is reliable and stable. (U /)
Description
Technical field
This utility model aircraft, a kind of six rotorcraft thrown in for disaster relief supplies.
Background technology
The design of existing unmanned plane during flying device is generally used for taking photo by plane, therefore the limited mass of its energy payload.Such as a kind of unmanned plane that China Patent Publication No. is 204642144, including fuselage.Described fuselage is provided with containing cavity, air inlet and air outlet, described air inlet and described air outlet and connects with containing cavity；Described air outlet and/or described air inlet can be opened and be closed, and wherein, described air inlet is for sucking the air-flow of the propeller generation of described unmanned plane, and described air-flow can flow out from described air outlet via after described containing cavity.This kind of unmanned plane only has four motors to drive, and carrying capacity is very limited amount of.The development of unmanned plane during flying device is more and more faster, the field of its application is more and more wider, input such as disaster area goods and materials, for China, annual the most all because of earthquake, typhoon, the generation of geological disaster of mud-rock flow, and certain areas can be made to become disaster area, towards disaster area road often disaster occurs when by broken soon, thus can have a strong impact on the transport of relief materials and equipment, so how design a impact by surface state and seem particularly necessary for the aircraft transporting disaster relief supplies.
Summary of the invention
Technical problem to be solved in the utility model is to provide a kind of six rotorcraft frame thrown in for disaster relief supplies, and carrying capacity is big, can realize the input of goods and materials, reliable and stable.
For solving above-mentioned technical problem, the technical solution of the utility model is: a kind of six rotorcraft frame thrown in for disaster relief supplies, described frame includes fuselage and six cantilevers, described fuselage includes upper mounting plate, lower installation board and for connecting the connection post of upper mounting plate and lower installation board, formed between upper mounting plate and lower installation board and accommodate space, described upper mounting plate edge is provided with a connecting seat of six even circumferential distributions, described lower installation board edge is provided with the second connection seat of six even circumferential distributions, a connecting seat and second connects seat one_to_one corresponding and in setting up and down；The second mounting seat formation installation station that first mounting seat is corresponding, described cantilever one end is arranged on described installation station；The other end of described cantilever is provided with motor, and the output shaft of described motor is connected with propeller.Use the frame of six axle construction, make aircraft aloft keep more stable navigation, even if one of them motor breaks down all without the most out of control；The main body mechanism being made up of upper mounting plate and lower installation board, simple in construction, overall weight is light, can reduce aircraft overall weight；Cantilever is separable with fuselage, and the convenient cantilever to damaging repairs or replaces.The actual relief goods launch process of aircraft is as follows: operator is wirelessly transmitted to aircraft the geographical coordinate of goods and materials to be thrown in by computer upper computer software, then sends startup order；After aircraft receives startup order, self-navigation is to the geographical coordinate set by operator；After reaching target location, target location is accurately positioned by operator by the photographic head entrained by aircraft, finally target is thrown in disaster relief supplies.
As improvement, one end that described cantilever is connected with fuselage is gradually reduced to one end width being used for installing motor.
As improvement, described cantilever includes girder and is positioned at the curb girder of girder both sides, is connected by reinforcement between described girder and curb girder.The cantilevered weights of this structure is light, and structural strength is high.
As improvement, described cantilever is provided with mounting platform for the one end installing motor, and described mounting platform is provided with installing hole.
As improvement, described cantilever is connected fixing by screw with upper mounting plate and lower installation board.
As improvement, described upper mounting plate and lower installation board are equipped with hollow hole, alleviate the weight of fuselage, and hollow out cabling can be passed through.
As improvement, described upper mounting plate and lower installation board are regular hexagon.
As improvement, bottom described lower installation board, it is provided with landing gear.
This utility model is compared with prior art had the benefit that
This utility model uses the frame of six axle construction, makes aircraft aloft keep more stable navigation, even if one of them motor breaks down all without the most out of control；The main body mechanism being made up of upper mounting plate and lower installation board, simple in construction, overall weight is light, can reduce aircraft overall weight；Cantilever is separable with fuselage, and the convenient cantilever to damaging repairs or replaces.
Accompanying drawing explanation
Fig. 1 is aircraft frame structure schematic diagram.
Fig. 2 is flying vehicles control circuit block diagram.
Detailed description of the invention
Below in conjunction with Figure of description, the utility model is described in further detail.
A kind of six rotorcraft thrown in for disaster relief supplies, including frame and control circuit.As it is shown in figure 1, described frame includes fuselage and six cantilevers 4, described fuselage includes upper mounting plate 1, lower installation board 2 and for connecting the connection post 3 of upper mounting plate 1 and lower installation board 2；Formed between upper mounting plate 1 and lower installation board 2 and accommodate space 7；Described upper mounting plate 1 and lower installation board 2 are in regular hexagon, it is equipped with hollow hole 12 on described upper mounting plate 1 and lower installation board 2, described upper mounting plate 1 edge is provided with a connecting seat 13 of six even circumferential distributions, described lower installation board 2 edge is provided with the second connection seat 23 of six even circumferential distributions, and a connecting seat 13 is connected seat 23 one_to_one corresponding and in setting up and down with second；The second mounting seat formation installation station that first mounting seat is corresponding.One end that described cantilever 4 is connected with fuselage is gradually reduced to one end width being used for installing motor；Described cantilever 4 includes girder 42 and is positioned at the curb girder 41 of girder 42 both sides, is connected by reinforcement 43 between described girder 42 and curb girder 41；Described cantilever 4 one end is arranged on described installation station and is connected with the screw 11 of upper mounting plate 1 and lower installation board 2 by screw fixing；Described cantilever 4 is provided with mounting platform 44 for the one end installing motor, and described mounting platform 44 is provided with installing hole, mounting platform 44 is fixed with motor 5.Described motor 5 is DC brushless motor 5, and the output shaft of motor 5 upward and is connected with propeller 6.Be provided with landing gear 8 bottom described lower installation board 2, for aircraft stable drop to ground.As in figure 2 it is shown, described control circuit includes single-chip microcomputer, self-navigation module, GPS locating module, interface control circuit, photographic head, night vision light compensating lamp and WIFI transceiver module, described single-chip microcomputer is connected with controlling equipment by WIFI transceiver module.Can arrange two single-chip microcomputer forming control system cores, it is provided that enough storage areas, to meet the realization that complex software controls, two machine communication makes information transmission more accurate, reduces channel transmission time；Interface control circuit includes serial ports, ISP DLL, is connected with computer by serial ports asynchronous communication, facilitates transmission and the control of its information, its software operation portion can be facilitated to modify by ISP DLL.
This utility model uses 6 brshless DC motors 5 to form six rotorcraft as power set, is come by the rotating speed of 6 motors 5 of regulation；Use the frame of six axle construction, make aircraft aloft keep more stable navigation, even if one of them motor 5 breaks down all without the most out of control；The main body mechanism being made up of upper mounting plate 1 and lower installation board 2, simple in construction, overall weight is light, can reduce aircraft overall weight；Cantilever 4 is separable with fuselage, and the convenient cantilever 4 to damaging repairs or replaces；Increase GPS module, precise positioning, the tracking of flight locations can be carried out, increase self-navigation module, make aircraft carry out taking off, automatically navigating by water and land along both tramp-liners.The actual relief goods launch process of aircraft is as follows: operator is wirelessly transmitted to aircraft the geographical coordinate of goods and materials to be thrown in by computer upper computer software, then sends startup order；After aircraft receives startup order, self-navigation is to the geographical coordinate set by operator；After reaching target location, target location is accurately positioned by operator by the photographic head entrained by aircraft, finally target is thrown in disaster relief supplies.
Claims (8)
1.A kind of six rotorcraft frame thrown in for disaster relief supplies, it is characterized in that: described frame includes fuselage and six cantilevers, described fuselage includes upper mounting plate, lower installation board and for connecting the connection post of upper mounting plate and lower installation board, formed between upper mounting plate and lower installation board and accommodate space, described upper mounting plate edge is provided with a connecting seat of six even circumferential distributions, described lower installation board edge is provided with the second connection seat of six even circumferential distributions, and a connecting seat and second connects seat one_to_one corresponding and in setting up and down；The second mounting seat formation installation station that first mounting seat is corresponding, described cantilever one end is arranged on described installation station；The other end of described cantilever is provided with motor, and the output shaft of described motor is connected with propeller.
2.A kind of six rotorcraft frame thrown in for disaster relief supplies according to claim 1, it is characterised in that: one end that described cantilever is connected with fuselage is gradually reduced to one end width being used for installing motor.
3.A kind of six rotorcraft frame thrown in for disaster relief supplies according to claim 1, it is characterised in that: described cantilever includes girder and is positioned at the curb girder of girder both sides, is connected by reinforcement between described girder and curb girder.
4.A kind of six rotorcraft frame thrown in for disaster relief supplies according to claim 1, it is characterised in that: described cantilever is provided with mounting platform for the one end installing motor, and described mounting platform is provided with installing hole.
5.A kind of six rotorcraft frame thrown in for disaster relief supplies according to claim 1, it is characterised in that: described cantilever is connected fixing by screw with upper mounting plate and lower installation board.
6.A kind of six rotorcraft frame thrown in for disaster relief supplies according to claim 1, it is characterised in that: it is equipped with hollow hole on described upper mounting plate and lower installation board.
7.A kind of six rotorcraft frame thrown in for disaster relief supplies according to claim 1, it is characterised in that: described upper mounting plate and lower installation board are regular hexagon.
8.A kind of six rotorcraft frame thrown in for disaster relief supplies according to claim 1, it is characterised in that: it is provided with landing gear bottom described lower installation board.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521058137.9U CN205440859U (en) | 2015-12-18 | 2015-12-18 | A six rotor craft frames for disaster relief supplies are put in |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521058137.9U CN205440859U (en) | 2015-12-18 | 2015-12-18 | A six rotor craft frames for disaster relief supplies are put in |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205440859U true CN205440859U (en) | 2016-08-10 |
Family
ID=57181295
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521058137.9U Expired - Fee Related CN205440859U (en) | 2015-12-18 | 2015-12-18 | A six rotor craft frames for disaster relief supplies are put in |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205440859U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741825A (en) * | 2016-11-21 | 2017-05-31 | 西安三翼航空科技有限公司 | A kind of six rotor unmanned aircrafts |
| CN114408171A (en) * | 2022-01-28 | 2022-04-29 | 北京理工大学 | Polymorphic multi-cabin liftable automatic material feeding quad-rotor unmanned aerial vehicle and working method |
-
2015
- 2015-12-18 CN CN201521058137.9U patent/CN205440859U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741825A (en) * | 2016-11-21 | 2017-05-31 | 西安三翼航空科技有限公司 | A kind of six rotor unmanned aircrafts |
| CN114408171A (en) * | 2022-01-28 | 2022-04-29 | 北京理工大学 | Polymorphic multi-cabin liftable automatic material feeding quad-rotor unmanned aerial vehicle and working method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160810 Termination date: 20161218 |