CN207433790U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN207433790U CN207433790U CN201721137499.6U CN201721137499U CN207433790U CN 207433790 U CN207433790 U CN 207433790U CN 201721137499 U CN201721137499 U CN 201721137499U CN 207433790 U CN207433790 U CN 207433790U
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- CN
- China
- Prior art keywords
- unmanned plane
- enclosure
- axis
- rotors
- sensor
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- 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.)
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Abstract
The utility model embodiment discloses a kind of unmanned plane.The utility model unmanned plane includes fuselage and four axis stretched out from the fuselage center; in four axis rotor is respectively arranged on each axis; four rotors are symmetrical arranged two-by-two; four rotors are on same mounting plane, and the unmanned plane further includes to protect the enclosure formula shell of the unmanned plane.The utility model unmanned plane structure novel is simple; unmanned plane is additionally provided with to protect the enclosure formula shell of the unmanned plane simultaneously; high-speed rotating unmanned plane rotor can be effectively protected, avoids damaging, is on the other hand also reduced to the people that may be collided or the injury of object.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of unmanned plane.
Background technology
Unmanned plane (Unmanned Aerial Vehicle, UAV) be one kind should not driver's boarding any drive manually
Operation is sailed, the aircraft river of thru-flight process can be automatically performed under the monitoring of electronic equipment completely, its appearance makes respectively
A country enters a brand-new epoch to the research of aircraft.Unmanned plane is with its survival ability is relatively strong, flexibility is high, motor-driven
The advantages that property good, very easy to use and zero injures and deaths risk of personnel, can play extremely important effect in modern war, together
When in civilian and commercial kitchen area unmanned plane also have boundless application prospect.
Unmanned plane can be divided into the species such as fixed-wing formula, rotary wind type and flapping wings type unmanned plane by flight characteristic, wherein miniature
Rotor wing unmanned aerial vehicle have the characteristics that small volume, it is simple in structure, control it is more flexible, can VTOL, freely hover, moreover it is possible to
Various natural environments are enough adapted to, possess the advantages that autonomous flight and throwing power, answering for mankind's entrance can be not suitable at some
Operation is carried out in miscellaneous and hazardous environment, in recent years in scientific research institution, government organs, broadcast medium, individual application and military field
Suffer from more and more important application.
At present, unmanned plane is relatively simple for structure, and the structure design of unmanned plane is when unmanned plane collides to unmanned plane
Protection is weak, after unmanned plane collides, crushing blow is easily caused to unmanned plane, while high-speed rotating blade is also easy
The people or object collided is damaged.
Utility model content
The utility model embodiment provides a kind of unmanned plane, to solve easily to damage after existing unmanned plane protection weakness is collided
Bad the problem of.
The utility model provides a kind of unmanned plane, and the unmanned plane includes fuselage and stretched out from its center
Four axis are respectively arranged with a rotor in four axis on each axis, and four rotors are symmetrical arranged two-by-two, at four rotors
In on same mounting plane, the unmanned plane further includes to protect the enclosure formula shell of the unmanned plane.
Further, four rotors are surrounded protection by the enclosure formula shell respectively.
Further, the enclosure formula shell includes four enclosure portions, and four enclosure portions are respectively by described four
Rotor surrounds protection, and four enclosure portions structure is identical, the hollow placement rotor of each enclosure portion inner circular.
Further, four enclosure portions are symmetrical arranged two-by-two.
Further, two corners are formed outside each enclosure portion, the corner is in " ︵ " type.
Further, it is built-in with to perceive six axis gyroscopes of the unmanned plane during flying posture in the unmanned plane.
Further, it is built-in with to estimate the barometer of the unmanned plane hovering height in the unmanned plane.
Further, sensor is built-in in the unmanned plane, the sensor is used in flight course described in sensing
Barrier near unmanned plane.
Further, the sensor includes range sensor, image sensor or/and GPS sensor.
Further, the sensor is arranged in surrounding, and sets four axis in the one side back to rotor.
Unmanned plane includes fuselage and four axis that are stretched out from fuselage center in the utility model embodiment, each in four axis
A rotor is respectively arranged on axis, four rotors are symmetrical arranged two-by-two, and four rotors are on same mounting plane, and structure is new
It is clever simple, while unmanned plane is additionally provided with to protect the enclosure formula shell of the unmanned plane, can effectively protect and rotate at a high speed
Unmanned plane rotor, avoid damaging, on the other hand also reduce to may collision people or object injury.
Description of the drawings
Fig. 1 is one embodiment schematic diagram of unmanned plane in the utility model embodiment；
Fig. 2 is another embodiment schematic diagram of unmanned plane in the utility model embodiment；
Fig. 3 is another embodiment schematic diagram of unmanned plane in the utility model embodiment.
Specific embodiment
It is real below in conjunction with the utility model in order to which those skilled in the art is made to more fully understand the utility model
The attached drawing in example is applied, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that described
Embodiment is only the embodiment of the utility model part, instead of all the embodiments.Based on the reality in the utility model
Apply example, those of ordinary skill in the art's all other embodiments obtained without making creative work all should
When the scope for belonging to the utility model protection.
As shown in Figure 1, Figure 2, Figure 3 shows, the utility model provides a kind of unmanned plane, the unmanned plane include fuselage 10 and from
Four axis 20 that its center stretches out are respectively arranged with a rotor 30, four rotors in four axis 20 on each axis
30 are symmetrical arranged two-by-two, and four rotors 30 are on same mounting plane, and the unmanned plane further includes to protect described
The enclosure formula shell 40 of unmanned plane.
Further, four rotors 30 are surrounded protection by the enclosure formula shell 40 respectively.
Further, the enclosure formula shell 40 includes four enclosure portions 41, and four enclosure portions 41 are respectively by institute
It states four rotors 40 and surrounds protection, four enclosure portions, 41 structure is identical, and each 41 inner circular of enclosure portion is hollow to place rotation
The wing.
Further, four enclosure portions 41 are symmetrical arranged two-by-two.
Further, 41 outside of each enclosure portion forms two corners, and the corner is in " ︵ " type.
Further, it is built-in with to perceive six axis gyroscopes of the unmanned plane during flying posture in the unmanned plane.
Further, it is built-in with to estimate the barometer of the unmanned plane hovering height in the unmanned plane.
Further, sensor is built-in in the unmanned plane, the sensor is used in flight course described in sensing
Barrier near unmanned plane.
Further, the sensor includes range sensor, image sensor or/and GPS sensor.
Further, the sensor includes infrared sensor.
Further, the sensor is arranged in surrounding, and sets four axis in the one side back to rotor, to avoid existing
Unmanned plane sensor is typically mounted on horn or on fuselage, and noise, air-flow that the rotation of propeller generates can usually disturb
The ultrasonic wave or electromagnetic wave sent, thereby increases and it is possible to the situation in the visual field of visual sensor can be hindered.
Further, the unmanned plane, which further includes, is arranged at being used to support on ground or object of the fuselage bottom
Two support legs 50, described two 50 structures of support leg are identical, it is preferred that the support leg 50 is in arch-shaped, this sample practicality
New unmanned plane can be not only parked on smooth ground, but also according to the arch-shaped structure, can be parked in object or the area of out-of-flatness
On domain (such as sharp objects or region).
Unmanned plane includes fuselage and four axis that are stretched out from fuselage center in the utility model embodiment, each in four axis
A rotor is respectively arranged on axis, four rotors are symmetrical arranged two-by-two, and four rotors are on same mounting plane, and structure is new
It is clever simple, while unmanned plane is additionally provided with to protect the enclosure formula shell of the unmanned plane, can effectively protect and rotate at a high speed
Unmanned plane rotor, avoid damaging, on the other hand also reduce to may collision people or object injury.
It is apparent to those skilled in the art that for convenience and simplicity of description, in the above-described embodiments,
It all emphasizes particularly on different fields to the description of each embodiment, there is no the part being described in detail in some embodiment, may refer to other embodiment
Associated description.
The above, above example are only to illustrate the technical solution of the utility model, rather than its limitations；Although ginseng
The utility model is described in detail according to previous embodiment, it will be understood by those of ordinary skill in the art that：It is still
It can modify to the technical solution recorded in foregoing embodiments or which part technical characteristic is equally replaced
It changes；And these modifications or replacement, the essence of appropriate technical solution is not made to depart from various embodiments of the utility model technical solution
Spirit and scope.
Claims (10)
1. a kind of unmanned plane, which is characterized in that the unmanned plane includes fuselage and four axis stretched out from the fuselage center,
A rotor is respectively arranged on each axis in four axis, four rotors are symmetrical arranged two-by-two, and four rotors are in same
On one mounting plane, the unmanned plane further includes to protect the enclosure formula shell of the unmanned plane.
2. unmanned plane according to claim 1, which is characterized in that the enclosure formula shell respectively encloses four rotors
Firmly protect.
3. unmanned plane according to claim 2, which is characterized in that the enclosure formula shell includes four enclosure portions, institute
It states four enclosure portions and four rotors is surrounded into protection respectively, four enclosure portions structure is identical, inside each enclosure portion
Circular hollow places rotor.
4. unmanned plane according to claim 3, which is characterized in that four enclosure portions are symmetrical arranged two-by-two.
5. unmanned plane according to claim 4, which is characterized in that form two corners, institute outside each enclosure portion
Corner is stated in " ︵ " type.
6. unmanned plane according to claim 1, which is characterized in that be built-in with to perceive in the unmanned plane it is described nobody
Six axis gyroscopes of machine flight attitude.
7. unmanned plane according to claim 1, which is characterized in that be built-in with to estimate in the unmanned plane it is described nobody
The barometer of machine hovering height.
8. unmanned plane according to claim 1, which is characterized in that sensor, the sensing are built-in in the unmanned plane
Device is used to sense the barrier near the unmanned plane in flight course.
9. unmanned plane according to claim 8, which is characterized in that the sensor includes range sensor, image sensing
Device or/and GPS sensor.
10. unmanned plane according to claim 9, which is characterized in that the sensor is arranged in surrounding, and sets four axis
In the one side back to rotor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721137499.6U CN207433790U (en) | 2017-09-06 | 2017-09-06 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721137499.6U CN207433790U (en) | 2017-09-06 | 2017-09-06 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207433790U true CN207433790U (en) | 2018-06-01 |
Family
ID=62302227
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721137499.6U Expired - Fee Related CN207433790U (en) | 2017-09-06 | 2017-09-06 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207433790U (en) |
-
2017
- 2017-09-06 CN CN201721137499.6U patent/CN207433790U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180601 Termination date: 20210906 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |