CN205574251U - Organism is four rotor unmanned aerial vehicle of streamlined - Google Patents
Organism is four rotor unmanned aerial vehicle of streamlined Download PDFInfo
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- CN205574251U CN205574251U CN201620237218.3U CN201620237218U CN205574251U CN 205574251 U CN205574251 U CN 205574251U CN 201620237218 U CN201620237218 U CN 201620237218U CN 205574251 U CN205574251 U CN 205574251U
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- unmanned aerial
- fuselage
- wing unmanned
- rotor wing
- aerial vehicles
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Abstract
The utility model discloses an organism is four rotor unmanned aerial vehicle of streamlined, four rotor unmanned aerial vehicle include: screw (1), motor (2), motor mounting (3), horn (4), fuselage (5), undercarriage (6), fixed box (7), GPS status indicator lamp (8) and engine room cover (9) of GPS. The utility model discloses a four rotor unmanned aerial vehicle organisms adopt streamlined design, can effectively reduce the air to unmanned aerial vehicle's flight resistance, reinforcing unmanned aerial vehicle's flight stability.
Description
Technical field
This utility model relates to unmanned plane field, and being specifically related to a kind of body is fairshaped four rotations
Wing unmanned plane
Background technology
UAV is called for short " unmanned plane ", is to utilize radio robot and the journey provided for oneself
Sequence controls the most manned aircraft that device is handled.Being provided with automatic pilot on machine, programme-control fills
The equipment such as put.The most most four rotor wing unmanned aerial vehicle body shell designs are simple and crude, very
To without housing so that the wind loading rating of unmanned plane is poor, and in flight course, air is to unmanned plane
Flight resistance big, reduce the flight stability of unmanned plane, when shortening the continuation of the journey of unmanned plane
Between.
Utility model content
(1) to solve the technical problem that
The technical problems to be solved in the utility model is: provide one can effectively reduce air resistance
Power, the body strengthening flight stability is fairshaped four rotor wing unmanned aerial vehicles.
(2) technical scheme
For solving above-mentioned technical problem, it is fairshaped four that this utility model provides a kind of body
Rotor wing unmanned aerial vehicle, described four rotor wing unmanned aerial vehicles include: propeller, motor, motor fixture,
Horn, fuselage, undercarriage, GPS fixed bin, GPS status indicator lamp and cabin cover.
Wherein, described four rotor wing unmanned aerial vehicles also include: be arranged at two LED of fuselage head
Blinker.
Wherein, described fuselage is smooth streamlined, and further, the head of described fuselage is oblate
Shape.
Wherein, described fuselage and described undercarriage all use composite by Mold Making
Become.
Wherein, described GPS status indicator lamp is arranged at the afterbody of fuselage.
Wherein, described horn and horizontal direction are the upper counterangle of 6 °.
Wherein, described undercarriage is connected with the side of fuselage bottom.
(3) beneficial effect
Compared with prior art, the beneficial effects of the utility model are: of the present utility model four
Rotor wing unmanned aerial vehicle fuselage uses airflow design, can effectively reduce air and hinder the flight of unmanned plane
Power, strengthens the flight stability of unmanned plane.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model；
Fig. 2 is top view of the present utility model；
Fig. 3 is front view of the present utility model；
Fig. 4 is side view of the present utility model.
Reference numerals list
1, propeller 2, motor
3, motor fixture 4, horn
5, fuselage 6, undercarriage
7, GPS fixed bin 8, GPS status indicator lamp
9, cabin cover 10, LED blinker
Detailed description of the invention
A kind of body that the utility model proposes is fairshaped four rotor wing unmanned aerial vehicles, in conjunction with accompanying drawing
Describe in detail as follows with embodiment.
As illustrated in fig. 1 and 2, four rotor wing unmanned aerial vehicles of the present embodiment include: propeller 1, electricity
Machine 2, motor fixture 3, horn 4, fuselage 5, undercarriage 6, GPS fixed bin 7, GPS
Status indicator lamp 8 and cabin cover 9.Fuselage 5 is in smooth streamlined, and the head of fuselage 5
In oblateness.
Fuselage 5 and undercarriage 6 all use composite to be formed by Mold Making, lightweight,
Intensity is good, and air resistance coefficient is little.The junction of horn 4 and fuselage 5 is smooth excessively, is completely embedded,
GPS status indicator lamp 8 is arranged at the afterbody of fuselage 5, is used for indicating GPS in flight course
Signal is the most normal.
As shown in Figures 3 and 4, four rotor wing unmanned aerial vehicles of the present embodiment also include: be arranged at fuselage
Two LED blinkers 10 of 5 heads, time in unmanned plane during flying away from driver,
Head and the tail of unmanned plane is distinguished for driver.Horn 4 and horizontal direction be 6 ° upper instead
Angle, is conducive to increasing the stability of unmanned plane, strengthens the ability of anti-side wind.Undercarriage 6 and machine
Side bottom body 5 connects, it is possible to increase the carry space of unmanned plane.
This utility model, by using airflow design, effectively reduces air and flies unmanned plane
Row resistance, enhances the flight stability of unmanned plane.
Embodiment of above is merely to illustrate this utility model, and not to limit of the present utility model
System, about the those of ordinary skill of technical field, without departing from spirit of the present utility model and model
In the case of enclosing, it is also possible to make a variety of changes and modification, the technical scheme of the most all equivalents
Falling within category of the present utility model, scope of patent protection of the present utility model should be by claim
Limit.
Claims (7)
1. a body is fairshaped four rotor wing unmanned aerial vehicles, it is characterised in that described four rotations
Wing unmanned plane includes: propeller (1), motor (2), motor fixture (3), horn (4),
Fuselage (5), undercarriage (6), GPS fixed bin (7), GPS status indicator lamp (8) and
Cabin cover (9).
2. body as claimed in claim 1 is fairshaped four rotor wing unmanned aerial vehicles, its feature
Being, described four rotor wing unmanned aerial vehicles also include: be arranged at two LED of fuselage (5) head
Blinker (10).
3. body as claimed in claim 1 is fairshaped four rotor wing unmanned aerial vehicles, its feature
Being, described fuselage (5) is in smooth streamlined；
Further, the head of described fuselage (5) is oblateness.
4. body as claimed in claim 1 is fairshaped four rotor wing unmanned aerial vehicles, its feature
Being, described fuselage (5) and described undercarriage (6) all use composite by mould system
Form.
5. body as claimed in claim 1 is fairshaped four rotor wing unmanned aerial vehicles, its feature
Being, described GPS status indicator lamp (8) is arranged at the afterbody of fuselage (5).
6. body as claimed in claim 1 is fairshaped four rotor wing unmanned aerial vehicles, its feature
Being, described horn (4) and horizontal direction are the upper counterangle of 6 °.
7. body as claimed in claim 1 is fairshaped four rotor wing unmanned aerial vehicles, its feature
Being, described undercarriage (6) is connected with the side of fuselage (5) bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620237218.3U CN205574251U (en) | 2016-03-24 | 2016-03-24 | Organism is four rotor unmanned aerial vehicle of streamlined |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620237218.3U CN205574251U (en) | 2016-03-24 | 2016-03-24 | Organism is four rotor unmanned aerial vehicle of streamlined |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205574251U true CN205574251U (en) | 2016-09-14 |
Family
ID=56866308
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620237218.3U Active CN205574251U (en) | 2016-03-24 | 2016-03-24 | Organism is four rotor unmanned aerial vehicle of streamlined |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205574251U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108238243A (en) * | 2016-12-27 | 2018-07-03 | 中国科学院遥感与数字地球研究所 | 5kg load-carryings length six rotor wing unmanned aerial vehicles of continuation of the journey |
| CN109353513A (en) * | 2018-11-20 | 2019-02-19 | 飞智控（天津）科技有限公司 | Monoblock type logistics unmanned plane |
| CN113184185A (en) * | 2021-06-17 | 2021-07-30 | 华航高科(北京)技术有限公司青岛分公司 | Streamlined coaxial many rotor unmanned aerial vehicle of adaptable adverse circumstances |
-
2016
- 2016-03-24 CN CN201620237218.3U patent/CN205574251U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108238243A (en) * | 2016-12-27 | 2018-07-03 | 中国科学院遥感与数字地球研究所 | 5kg load-carryings length six rotor wing unmanned aerial vehicles of continuation of the journey |
| CN109353513A (en) * | 2018-11-20 | 2019-02-19 | 飞智控（天津）科技有限公司 | Monoblock type logistics unmanned plane |
| CN113184185A (en) * | 2021-06-17 | 2021-07-30 | 华航高科(北京)技术有限公司青岛分公司 | Streamlined coaxial many rotor unmanned aerial vehicle of adaptable adverse circumstances |
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|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |