CN204895847U - Integral type rotor craft - Google Patents
Integral type rotor craft Download PDFInfo
- Publication number
- CN204895847U CN204895847U CN201520386666.5U CN201520386666U CN204895847U CN 204895847 U CN204895847 U CN 204895847U CN 201520386666 U CN201520386666 U CN 201520386666U CN 204895847 U CN204895847 U CN 204895847U
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- cabin
- arm
- supporter
- support arm
- arm supporter
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Abstract
The utility model provides an integral type rotor craft, including base, main part fuselage and a plurality of rotor support arm, pedestal mounting in main part fuselage bottom, be equipped with on every rotor support arm at least one motor and by motor drive's screw, what a plurality of rotor support arm were symmetrical installs around the main part fuselage, the main part fuselage is by cabin arm supporter, last cabin cover and top cap triplex, the pedestal mounting is in cabin arm supporter bottom, cabin arm supporter center downside form one be used for holding article hold a chamber or a medical kit that is used for connecing greatly agricultural medicament, arm supporter peripheral integrated into one piece in cabin has the spiral arm link of a plurality of rotor support arm of being convenient for installation, go up the cabin cover buckle closure in cabin arm supporter upside make cabin arm supporter center the chamber holds or the medical kit constitutes a sealed cavity, it offers one and is convenient for place and get in the chamber by article or to the hatch of medical kit filling medicament from holding to go up cabin cover top center, the sealed whole hatch of going up the cabin cover of top cap buckle closure.
Description
[technical field]
The utility model relates to unmanned aviation flight technology, particularly relates to integral type rotor craft.
[background technology]
Along with the development of society, the progress of science and technology, land used is sprayed insecticide on a large scale, the work such as fertilising progressively come by unmanned vehicle in farmland.Existing agricultural unmanned vehicle complex structure, bulky, heavier-weight, seriously constrain it and apply on a large scale.
To spray medicine system and fuselage, spray medicine system is agricultural carry-on important component, and be mainly used in splendid attire and spray liquid, but existing spray medicine system architecture is complicated, assemble loaded down with trivial details, Heavy Weight, productive costs is high; Fuselage is also agricultural carry-on vitals, but existing fuselage not only weight and volume is large, structural strength is poor, easily damage, and processing and manufacturing difficulty.Meanwhile, the medicine-chest of existing agricultural unmanned vehicle is generally placed on alighting gear, and the liquid in medicine-chest reduces gradually along with sprinkling, causes the unbalance of aircraft on the one hand, and connection structure is complicated on the other hand, is not easy to the assembling of body.
[utility model content]
The utility model provides that a kind of structure is simple, Assembly &Disassembly is convenient, the integral type rotor craft of stable and reliable operation.
In order to realize foregoing invention object, the technical solution adopted in the utility model is:
Integral type rotor craft, comprise base, main machine body and multiple flight support arm, floor installation, bottom main machine body, each flight support arm is equipped with at least one motor and by described motor-driven screw propeller, multiple flight support arm symmetry be installed on around main machine body; Described main machine body is made up of cabin arm supporter, upper hatchcover and top cover three part, described floor installation is bottom the arm supporter of cabin, form one on the downside of arm supporter center, described cabin for the container cavity or of containing objects for the medicine-chest of access agricultural chemicals, cabin arm supporter is peripheral one-body moldedly has multiple spiral arm coupling end be convenient to flight support arm and installed; Described upper-deck cabin cover buckle is placed on the upside of the arm supporter of cabin and makes the container cavity at arm supporter center, cabin or medicine-chest form a sealed cavity; Described upper-deck cabin caping end center offers one and is convenient to from container cavity, place and fetch article or the hatch to medicine-chest filling medicament, the hatch of the whole upper hatchcover of described top cover buckle closure sealing.
Preferably, the rearward end of described flight support arm is removably connected in the main machine body of aircraft, and flight support arm rearward end center shaft is to extending an inserted link, and corresponding cabin arm supporter is provided with the jack matched with inserted link.
Preferably, the buckle structure be convenient to both and be connected is provided with between described upper hatchcover with cabin arm supporter.
Preferably, described base is that an employing elastomeric material is made and has the cushion rubber of hollow structure.
Preferably, form one around the hatch of described upper hatchcover and be convenient to the caulking groove that top cover buckle closure connects.
The beneficial effects of the utility model are:
The main machine body that the utility model provides is made up of cabin arm supporter, upper hatchcover and top cover three part, on the downside of arm supporter center, cabin, form one for the container cavity or of containing objects for the medicine-chest of access agricultural chemicals, upper-deck cabin cover buckle is placed on the upside of the arm supporter of cabin and makes the container cavity at arm supporter center, cabin or medicine-chest form a sealed cavity; Described upper-deck cabin caping end center offers one and is convenient to from container cavity, place and fetch article or the hatch to medicine-chest filling medicament; Make complete engine set installation or dismantle very convenient, free-handly get final product complete operation, do not need to adopt specialist tools to install or remove, simple to operate, time saving and energy saving.Container cavity or medicine-chest are arranged at the center of cabin arm supporter, make whole aircraft profile one smooth, effectively can adapt to the flight environment of vehicle of high vibration, container cavity or medicine-chest are arranged at the center of cabin arm supporter simultaneously, the center of gravity of aircraft can also be made more stable, run more reliable and more stable.
[accompanying drawing explanation]
Fig. 1 is the connection structure schematic diagram of the utility model main body.
Fig. 2 is that the master of the utility model base and main machine body looks blast structure for amplifying schematic diagram;
Fig. 3 is the exploded perspective structure for amplifying schematic diagram of the utility model base and main machine body.
[detailed description of the invention]
Integral type rotor craft, as shown in Figure 1 to Figure 3, comprise base 1, main machine body 2 and multiple flight support arm 3, base 1 is installed on bottom main machine body 2, the screw propeller 5 each flight support arm 3 being equipped with a motor 4 and being driven by described motor 4, multiple flight support arm 3 symmetry be installed on main machine body 2 around, base 1 is that an employing elastomeric material is made and has the cushion rubber of hollow structure.
Continue as shown in Figure 1 to Figure 3, main machine body 2 is made up of cabin arm supporter 20, upper hatchcover 21 and top cover 22 3 part, base 1 is installed on bottom cabin arm supporter 20, on the downside of arm supporter 20 center, cabin, formation one is for the medicine-chest 6 of access agricultural chemicals, and arm supporter 20 periphery in cabin is one-body molded multiple spiral arm coupling end 7 be convenient to flight support arm 3 and installed; Upper hatchcover 21 buckle closure makes the medicine-chest 6 at arm supporter center, cabin form a sealed cavity on the upside of cabin arm supporter 20, is provided with the buckle structure be convenient to both and be connected between upper hatchcover 21 with cabin arm supporter 20; Offer a hatch 210 being convenient to medicine-chest filling medicament at center, upper hatchcover 21 top, the hatch 210 of the whole upper hatchcover 21 of top cover 22 buckle closure sealing, hatch 210 surrounding of upper hatchcover 21 forms one and is convenient to the caulking groove 211 that top cover 22 buckle closure connects.
Continue as shown in Figure 1 to Figure 3, the rearward end of flight support arm 3 is removably connected in the main machine body 2 of aircraft, flight support arm 3 rearward end center shaft is to extending an inserted link 30, and the cabin arm supporter 20 of corresponding main machine body 2 is provided with the jack 200 matched with inserted link 30.
Be formed centrally one in the cabin arm supporter 20 of the utility model main machine body 2 for the container cavity or of containing objects for the medicine-chest of access agricultural chemicals, be convenient to effectively carry load-bearing material; Upper hatchcover 21 buckle closure makes the container cavity at arm supporter 20 center, cabin or medicine-chest form a sealed cavity on the upside of cabin arm supporter 20; Offer one to be convenient to from container cavity, place and fetch article or the hatch 210 to medicine-chest filling medicament at center, upper hatchcover 21 top; Make complete engine set installation or dismantle very convenient, free-handly get final product complete operation, simple to operate, time saving and energy saving.Container cavity or medicine-chest are arranged at the center of cabin arm supporter 20, make whole aircraft profile one smooth, effectively can adapt to the flight environment of vehicle of high vibration, container cavity or medicine-chest are arranged at the center of cabin arm supporter simultaneously, the center of gravity of aircraft can also be made more stable, run more reliable and more stable.
The above embodiment is just preferred embodiment of the present utility model, not limits practical range of the present utility model with this, the equivalence change that all shapes according to the utility model, structure and principle are done, and all should be covered by protection domain of the present utility model.
Claims (5)
1. integral type rotor craft, comprise base, main machine body and multiple flight support arm, floor installation, bottom main machine body, each flight support arm is equipped with at least one motor and by described motor-driven screw propeller, multiple flight support arm symmetry be installed on around main machine body; It is characterized in that:
Described main machine body is made up of cabin arm supporter, upper hatchcover and top cover three part, described floor installation is bottom the arm supporter of cabin, form one on the downside of arm supporter center, described cabin for the container cavity or of containing objects for the medicine-chest of access agricultural chemicals, cabin arm supporter is peripheral one-body moldedly has multiple spiral arm coupling end be convenient to flight support arm and installed;
Described upper-deck cabin cover buckle is placed on the upside of the arm supporter of cabin and makes the container cavity at arm supporter center, cabin or medicine-chest form a sealed cavity;
Described upper-deck cabin caping end center offers one and is convenient to from container cavity, place and fetch article or the hatch to medicine-chest filling medicament, the hatch of the whole upper hatchcover of described top cover buckle closure sealing.
2. integral type rotor craft according to claim 1, it is characterized in that, the rearward end of described flight support arm is removably connected in the main machine body of aircraft, flight support arm rearward end center shaft is to extending an inserted link, and corresponding cabin arm supporter is provided with the jack matched with inserted link.
3. integral type rotor craft according to claim 1, is characterized in that, is provided with the buckle structure be convenient to both and be connected between described upper hatchcover with cabin arm supporter.
4. integral type rotor craft according to claim 1, is characterized in that, described base is that an employing elastomeric material is made and has the cushion rubber of hollow structure.
5. integral type rotor craft according to claim 1, is characterized in that, forms the caulking groove that is convenient to the connection of top cover buckle closure around the hatch of described upper hatchcover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520386666.5U CN204895847U (en) | 2015-06-04 | 2015-06-04 | Integral type rotor craft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520386666.5U CN204895847U (en) | 2015-06-04 | 2015-06-04 | Integral type rotor craft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204895847U true CN204895847U (en) | 2015-12-23 |
Family
ID=54918045
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520386666.5U Expired - Fee Related CN204895847U (en) | 2015-06-04 | 2015-06-04 | Integral type rotor craft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204895847U (en) |
Cited By (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106986010A (en) * | 2017-04-10 | 2017-07-28 | 西华酷农无人机产业园运营有限公司 | A kind of plant protection unmanned plane |
| WO2018152912A1 (en) * | 2017-02-24 | 2018-08-30 | 深圳市大疆创新科技有限公司 | Power kit and unmanned aerial vehicle |
| CN109229396A (en) * | 2018-08-29 | 2019-01-18 | 易瓦特科技股份公司 | Aircraft with novel power source |
| CN109319132A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The changeable aircraft of oily electricity |
| CN109319150A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Aircraft with closed type fuselage |
| CN109319155A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned vehicle with novel power source |
| CN109319148A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane |
| CN109319147A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with novel power source |
| CN109319145A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with closed type fuselage |
| CN109319142A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned vehicle with closed type fuselage |
| CN109319153A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with novel power source |
| CN109319131A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil |
| CN109319151A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with closed type fuselage |
| CN109319137A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | It can carry out the aircraft that oily cutting is changed |
| CN109319134A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with novel power source |
| CN109319136A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | It can carry out the aircraft that oily cutting is changed |
| CN109319154A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Flight equipment with novel power source |
| CN109319130A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil |
| CN109319149A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Flight equipment with closed type fuselage |
| CN109319133A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | It can carry out the unmanned vehicle that oily cutting is changed |
| CN109319152A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with novel power source |
| CN109319135A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed flight equipment of oil |
| CN109319144A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Aircraft with closed type fuselage |
| CN109319143A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with closed type fuselage |
| CN109319146A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Novel flight equipment |
| CN109319141A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Oily cutting with closed type fuselage changes aircraft |
| CN109335002A (en) * | 2018-08-29 | 2019-02-15 | 易瓦特科技股份公司 | Oily cutting with novel power source changes aircraft |
| CN109533349A (en) * | 2018-08-29 | 2019-03-29 | 易瓦特科技股份公司 | Aircraft with novel power source |
-
2015
- 2015-06-04 CN CN201520386666.5U patent/CN204895847U/en not_active Expired - Fee Related
Cited By (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018152912A1 (en) * | 2017-02-24 | 2018-08-30 | 深圳市大疆创新科技有限公司 | Power kit and unmanned aerial vehicle |
| CN106986010A (en) * | 2017-04-10 | 2017-07-28 | 西华酷农无人机产业园运营有限公司 | A kind of plant protection unmanned plane |
| CN109319134A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with novel power source |
| CN109319150A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Aircraft with closed type fuselage |
| CN109319136A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | It can carry out the aircraft that oily cutting is changed |
| CN109319154A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Flight equipment with novel power source |
| CN109319148A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane |
| CN109319147A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with novel power source |
| CN109319145A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with closed type fuselage |
| CN109319142A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned vehicle with closed type fuselage |
| CN109319153A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with novel power source |
| CN109319131A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil |
| CN109319151A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil with closed type fuselage |
| CN109319137A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | It can carry out the aircraft that oily cutting is changed |
| CN109533349A (en) * | 2018-08-29 | 2019-03-29 | 易瓦特科技股份公司 | Aircraft with novel power source |
| CN109319132A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The changeable aircraft of oily electricity |
| CN109319155A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned vehicle with novel power source |
| CN109319130A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed unmanned plane of oil |
| CN109319149A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Flight equipment with closed type fuselage |
| CN109319133A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | It can carry out the unmanned vehicle that oily cutting is changed |
| CN109319152A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with novel power source |
| CN109319135A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | The electric mixed flight equipment of oil |
| CN109319144A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Aircraft with closed type fuselage |
| CN109319143A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Unmanned plane with closed type fuselage |
| CN109319146A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Novel flight equipment |
| CN109319141A (en) * | 2018-08-29 | 2019-02-12 | 易瓦特科技股份公司 | Oily cutting with closed type fuselage changes aircraft |
| CN109335002A (en) * | 2018-08-29 | 2019-02-15 | 易瓦特科技股份公司 | Oily cutting with novel power source changes aircraft |
| CN109229396A (en) * | 2018-08-29 | 2019-01-18 | 易瓦特科技股份公司 | Aircraft with novel power source |
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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 |
Granted publication date: 20151223 Termination date: 20190604 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |