CN204726659U - The coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall - Google Patents
The coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall Download PDFInfo
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- CN204726659U CN204726659U CN201520311391.9U CN201520311391U CN204726659U CN 204726659 U CN204726659 U CN 204726659U CN 201520311391 U CN201520311391 U CN 201520311391U CN 204726659 U CN204726659 U CN 204726659U
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- coaxial
- collision
- rotor aerocraft
- spider
- slurry multi
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Abstract
The utility model relates to the coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall, comprises the spider that inside is provided with master control system and battery; Described spider is provided with the strut bar of at least four horizontal positioned and circle distribution, below is provided with the alighting gear of horizontal positioned; Both sides up and down in the middle part of described strut bar are separately installed with coaxial flying wing, and each described flying wing is connected with master control system respectively; The guard collar of arc is provided with between adjacent described strut bar; The utility model, by increasing guard collar in outer ring, makes coaxial two slurry multi-rotor aerocraft in flight course, run into obstacle and loss can be dropped to minimum, and guard collar is detachable, convenient transport.
Description
Technical field
The utility model relates to aircraft field, refers in particular to the coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall.
Background technology
Aircraft quietly rose in recent years, domestic now existing many enterprises carry out development & production to electronic multi-rotor aerocraft, run into obstacle in current multi-rotor aerocraft flight course to be easy to cause wing impaired, multi-rotor aerocraft is caused to fall, cause unnecessary loss, for this reason, we have developed the coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall, by increasing guard collar in coaxial two slurry multi-rotor aerocraft outer ring, making coaxial two slurry multi-rotor aerocraft in flight course, run into obstacle can drop to minimum by loss, and guard collar is detachable, convenient transport.
Utility model content
The utility model object provides a kind of anti-collision and anti-fall coaxial two slurry multi-rotor aerocraft to overcome the deficiencies in the prior art, by increasing guard collar in coaxial two slurry multi-rotor aerocraft outer ring, making coaxial two slurry multi-rotor aerocraft in flight course, run into obstacle can drop to minimum by loss, and guard collar is detachable, convenient transport.
For achieving the above object, the technical solution adopted in the utility model is: the coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall, comprises the spider that inside is provided with master control system and battery; Described spider is provided with the strut bar of at least four horizontal positioned and circle distribution, below is provided with the alighting gear of horizontal positioned; Both sides up and down in the middle part of described strut bar are separately installed with coaxial flying wing; Each described flying wing is connected with master control system respectively; The guard collar of arc is provided with between adjacent described strut bar.
Preferably, described strut bar comprises the carbon fiber pipe and pipe link linearly placed; Described carbon fiber pipe is fixedly connected with by screw thread with pipe link, and the both sides up and down of junction are separately installed with coaxial flying wing; Described in every root, the other end of carbon fiber pipe is fixed by screws on spider, is provided with reinforcing rod between the other end of pipe link described in every root and alighting gear.
Preferably, described reinforcing rod arranges sleeved one end correspondence and is set on pipe link, and the other end is respectively by being weldingly fixed on alighting gear.
Preferably, the top of described spider is provided with protective case.
Preferably, the two ends of described guard collar are fixedly connected with by screw with the junction of pipe link with reinforcing rod respectively.
Preferably, four supports circumferentially distributed are provided with between described spider and alighting gear; Described in every root, the upper end of support is fixedly connected with by screw with spider respectively, and lower end is fixedly connected by welding with alighting gear respectively.
Preferably, described support is curved.
Preferably, described alighting gear is circular.
Due to the utilization of technique scheme, the utility model compared with prior art has following advantages:
The coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall described in the utility model, by increasing guard collar in outer ring, makes coaxial two slurry multi-rotor aerocraft in flight course, run into obstacle and loss can be dropped to minimum, and guard collar is detachable, convenient transport.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, technical solutions of the utility model are described further:
Accompanying drawing 1 is the front view of the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall described in the utility model;
Accompanying drawing 2 is the birds-eye view of the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall described in the utility model;
Accompanying drawing 3 is the constructional drawing of the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall described in the utility model;
Wherein: 1, alighting gear; 2, reinforcing rod; 3, support; 4, carbon fiber pipe; 5, spider; 6, protective cover; 7, flying wing; 8, guard collar; 9, pipe link.
Detailed description of the invention
Below in conjunction with drawings and the specific embodiments, the utility model is described in further detail.
Accompanying drawing 1-3 is the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall described in the utility model, comprises spider 5; Described spider 5 is provided with four horizontal positioned and the strut bar of even circumferential distribution, inside is provided with master control system and battery, the top of described spider 5 is provided with protective case, and for the protection of master control system and battery, it is circular alighting gear 1 that below is provided with horizontal positioned; Described strut bar comprises the carbon fiber pipe 4 and pipe link 9 linearly placed; Described carbon fiber pipe 4 is fixedly connected with by screw thread with pipe link 9, and the both sides up and down of junction are separately installed with coaxial flying wing 7; Each described flying wing 7 is connected with master control system respectively; The other end of carbon fiber pipe 4 described in every root is fixed by screws on spider 5, is provided with reinforcing rod 2 between the other end of pipe link 9 described in every root and alighting gear 1; Described reinforcing rod 2 arranges sleeved one end correspondence and is set on pipe link 9, and the other end is respectively by being weldingly fixed on alighting gear; The guard collar 8 of arc is provided with between adjacent described pipe link 9; The two ends of described guard collar 8 are fixedly connected with by screw with the junction of reinforcing rod 2 with pipe link 9 respectively; Four even circumferential distributions are provided with and curved support 3 between described spider 5 and alighting gear 1; Described in every root, the upper end of support 3 is fixedly connected with by screw with spider 5 respectively, and lower end is fixedly connected by welding with alighting gear 1 respectively.
Due to the utilization of technique scheme, the utility model compared with prior art has following advantages:
The coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall described in the utility model, by increasing guard collar in outer ring, makes coaxial two slurry multi-rotor aerocraft in flight course, run into obstacle and loss can be dropped to minimum, and guard collar is detachable, convenient transport.
Below be only embody rule example of the present utility model, protection domain of the present utility model is not constituted any limitation.The technical scheme that all employing equivalents or equivalence are replaced and formed, all drops within the utility model rights protection scope
.
Claims (8)
1. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall, is characterized in that: comprise the spider that inside is provided with master control system and battery; Described spider is provided with the strut bar of at least four horizontal positioned and circle distribution, below is provided with the alighting gear of horizontal positioned; Both sides up and down in the middle part of described strut bar are separately installed with coaxial flying wing; Each described flying wing is connected with master control system respectively; The guard collar of arc is provided with between adjacent described strut bar.
2. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall according to claim 1, is characterized in that: described strut bar comprises the carbon fiber pipe and pipe link linearly placed; Described carbon fiber pipe is fixedly connected with by screw thread with pipe link, and the both sides up and down of junction are separately installed with coaxial flying wing; Described in every root, the other end of carbon fiber pipe is fixed by screws on spider, is provided with reinforcing rod between the other end of pipe link described in every root and alighting gear.
3. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall according to claim 2, is characterized in that: described reinforcing rod arranges sleeved one end correspondence and is set on pipe link, and the other end is respectively by being weldingly fixed on alighting gear.
4. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall according to claim 1, is characterized in that: the top of described spider is provided with protective case.
5. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall according to claim 1, is characterized in that: the two ends of described guard collar are fixedly connected with by screw with the junction of pipe link with reinforcing rod respectively.
6. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall according to claim 1, is characterized in that: be provided with four supports circumferentially distributed between described spider and alighting gear; Described in every root, the upper end of support is fixedly connected with by screw with spider respectively, and lower end is fixedly connected by welding with alighting gear respectively.
7. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall according to claim 6, is characterized in that: described support is curved.
8. the coaxial two slurry multi-rotor aerocraft of anti-collision and anti-fall according to claim 1, is characterized in that: described alighting gear is circular.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520311391.9U CN204726659U (en) | 2015-05-14 | 2015-05-14 | The coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520311391.9U CN204726659U (en) | 2015-05-14 | 2015-05-14 | The coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204726659U true CN204726659U (en) | 2015-10-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520311391.9U Expired - Fee Related CN204726659U (en) | 2015-05-14 | 2015-05-14 | The coaxial two slurry multi-rotor aerocraft of a kind of anti-collision and anti-fall |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204726659U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908932A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Crashproof shockproof coaxial double-propeller multi-rotor aircraft |
-
2015
- 2015-05-14 CN CN201520311391.9U patent/CN204726659U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908932A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Crashproof shockproof coaxial double-propeller multi-rotor aircraft |
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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: 20151028 Termination date: 20200514 |