CN209454990U - A kind of fixed-wing unmanned plane - Google Patents
A kind of fixed-wing unmanned plane Download PDFInfo
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- CN209454990U CN209454990U CN201821332351.2U CN201821332351U CN209454990U CN 209454990 U CN209454990 U CN 209454990U CN 201821332351 U CN201821332351 U CN 201821332351U CN 209454990 U CN209454990 U CN 209454990U
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Abstract
The utility model discloses a kind of fixed-wing unmanned planes, which includes: fuselage, which includes air-flow flow device；At least one first propeller module, the first propeller module are set to the air-flow flow device and connect with the fuselage；At least one second propeller module, the second propeller module are connect with the fuselage；The first propeller module and the second propeller module can change the fuselage state.The utility model directly realizes rising and falling for unmanned plane vertical direction by the first and second propeller modules, without on runway run-up the vertical rise and fall of unmanned plane, the convenient operation to unmanned plane can be realized；The utility model also directly realizes the state of flight of other unmanned planes such as the forward retrogressing, steering, overturning of unmanned plane by the first and second propeller modules, does not need rudder face control, and manipulation is flexible.
Description
Technical field
The utility model relates to unmanned aerial vehicle design technical fields, and in particular to a kind of fixed-wing unmanned plane.
Background technique
Fixed-wing unmanned plane, which refers to, generates the thrust advanced or pulling force by power device, is generated and is risen by the fixation wing of fuselage
Power, a kind of unmanned plane to fly in the sky.
Existing fixed-wing unmanned plane is usually the power dress of thrust before and after the setting said on wing or fuselage generates
It sets (such as propeller etc.), this kind of fixed-wing unmanned plane has the following problems:
1, can not vertical rise and fall, need on runway run-up to promote lift；
2, the change of the various postures such as steering, the overturning for needing to realize unmanned plane by the rudder face on control fuselage, behaviour
It bothers；
3, structure is complicated, and assembling is inconvenient, and assembly, maintenance cost are high.
Utility model content
In order to solve existing fixed-wing unmanned plane can not vertical rise and fall, it is troublesome in poeration the problems such as, the utility model provides
A kind of fixed-wing unmanned plane, comprising:
Fuselage, the fuselage include air-flow flow device；
At least one first propeller module, the first propeller module be set to the air-flow flow device and with the fuselage
Connection；
At least one second propeller module, the second propeller module are connect with the fuselage；
The first propeller module and the second propeller module can change the fuselage state.
Preferably, the first propeller module can generate air flow power, the air flow power can pass through the air-flow stream
Dynamic device changes the fuselage state.
Preferably, the air-flow flow device includes airflow channel, which is set on the fuselage, described first
Propeller module is set to the airflow channel and connect with the fuselage.
Preferably, the first propeller module is detachably connected with the fuselage.
Preferably, the second propeller module is detachably connected with the fuselage.
Preferably, further including having control circuit plate module, the control circuit plate module is mounted on the fuselage, and institute
State the first propeller module, the second propeller module is electrically connected with the control circuit plate module.
Preferably, the control circuit plate module is detachably connected with the fuselage.
Preferably, between the first propeller module and the fuselage, the second propeller module and the fuselage
Between, connected using tool-free Quick-dismantle component between the control circuit plate module and the fuselage.
Preferably, the tool-free Quick-dismantle component includes dongle configuration and inserting slot construction, described in the dongle configuration injects
It realizes and is detachably connected in inserting slot construction, wherein
By the first tool-free Quick-dismantle component connection between the first propeller module and the fuselage, described first exempts from
Tool Quick-dismantle component includes the first dongle configuration and the first inserting slot construction, and first dongle configuration is mounted on first spiral
In paddle module, first inserting slot construction is mounted on the fuselage or first dongle configuration is mounted on the fuselage
On, first inserting slot construction is mounted in the first propeller module；
By the second tool-free Quick-dismantle component connection between the second propeller module and the fuselage, described second exempts from
Tool Quick-dismantle component includes the second dongle configuration and the second inserting slot construction, and second dongle configuration is mounted on second spiral
In paddle module, second inserting slot construction is mounted on the fuselage or second dongle configuration is mounted on the fuselage
On, second inserting slot construction is mounted in the second propeller module；
By the tool-free Quick-dismantle component connection of third between the control circuit plate module and the fuselage, the third is exempted from
Tool Quick-dismantle component includes third dongle configuration and third inserting slot construction, and the third dongle configuration is mounted on the control circuit
In plate module, the third inserting slot construction is mounted on the fuselage or the third dongle configuration is mounted on the fuselage
On, the third inserting slot construction is mounted in the control circuit plate module.
Preferably, the first propeller module, the second propeller module and the control circuit plate module can be from
The fuselage separates and is combined into an aircraft.
Preferably, the fuselage includes fuselage main body and the wing that the fuselage main body left and right sides is arranged in, and described in two
Wing is made into integration with the fuselage.
Preferably, the two first propeller modules are provided on the fuselage, two described first propeller modules or so
Side-by-side horizontal is arranged on the fuselage.
Preferably, the two second propeller modules are provided on the fuselage, the two second propeller module difference
It is in tilted layout on two wings.
Preferably, second propeller arrangement is arranged in the rear airfoil end.
Preferably, the first propeller module, the second propeller module include duct, are arranged in the culvert
Motor cabinet among road, the motor and propeller being mounted on the motor cabinet.
Preferably, further include having battery module, the battery module be mounted on above the control circuit plate module or under
Side.
The utility model due to using the technology described above, is allowed to compared with prior art, have the following advantages that and accumulate
Pole effect:
1, fixed-wing unmanned plane provided by the utility model directly passes through the first propeller module, the second propeller module
Cooperation realizes that unmanned plane vertical direction rises and falls, without on runway run-up can be realized the vertical rise and fall of unmanned plane, convenient pair
The operation of unmanned plane；The utility model is also directly realized the forward retrogressing of unmanned plane by the second propeller module, turns to, turns over
The state of flight for turning other unmanned planes of grade, is omitted the design of traditional rudder face, does not need rudder face control, and manipulation is flexible；
2, fixed-wing unmanned plane provided by the utility model, the first propeller module, the cooperation of the second propeller module, control
It is all made of dismountable connection type between circuit board module and fuselage, realizes modular assembly, the first propeller module and the
Use can be alternateed between two propeller modules；Meanwhile this connection type assists connecting without structures such as screws, dismounts
When without auxiliary tool, dismount more convenient.
Detailed description of the invention
In conjunction with attached drawing, by hereafter state detailed description, can be more clearly understood that the above-mentioned and other spy of the utility model
It seeks peace advantage, in which:
Fig. 1 is the structural schematic diagram of fixed-wing unmanned plane provided by the utility model；
Fig. 2 is the front view of fixed-wing unmanned plane provided by the utility model；
Fig. 3 is the top view of fixed-wing unmanned plane provided by the utility model；
Fig. 4 is the side view of fixed-wing unmanned plane provided by the utility model.
Symbol description:
1- fuselage main body, 101- supporting fuselage seat, 2- wing, 3- control circuit plate module, 4,5- the first propeller module,
6, the second propeller of 7- module, 401,501- motor cabinet.
Specific embodiment
Referring to the attached drawing for showing the utility model embodiment, the utility model is described in more detail.However, this reality
It can be realized in many different forms with novel, and should not be construed as being limited by the embodiment herein proposed.On the contrary, proposing
These embodiments be in order to reach sufficiently and complete disclosure, and make those skilled in the art understands completely this it is practical newly
The range of type.In these attached drawings, for clarity, the size and relative size in layer and region may be exaggerated.
Embodiment 1
The utility model provides a kind of fixed-wing unmanned plane, including fuselage, at least one first spiral shell is provided on fuselage
Paddle module and at least one second propeller module are revolved, the first propeller module, the second propeller module are mounted on the fuselage
On；Fuselage also includes air-flow flow device, and the first propeller module is set to air-flow flow device and connect with fuselage；First spiral shell
Rotation paddle module and the second propeller module can change the fuselage state.
Fixed-wing unmanned plane provided by the utility model, directly by the first propeller module and the second propeller module come
Realize rising and falling for unmanned plane vertical direction；Specifically, air-flow flow device is arranged on fuselage, and the first propeller module is set
In the air-flow flow device, the first propeller module can generate air flow power, which flows up and down, so that fuselage is not necessarily to
The function of vertical rise and fall, the convenient operation to unmanned plane can be completed in run-up on runway；The utility model can also be by
One propeller module, the second propeller module are controlled, other nothings such as the forward retrogressing of Lai Shixian unmanned plane, steering, overturning
The design of traditional rudder face is omitted in man-machine state of flight, does not need rudder face control, and manipulation is flexible.
In the present embodiment, air-flow flow device includes airflow channel, which is set on fuselage, the first propeller
Module is set to airflow channel and connect with the fuselage.Certainly, in other embodiments, when fuselage is lesser, on fuselage
There is no enough space setting airflow channels, the first propeller module can also be set up directly on fuselage head side at this time, as long as
Guarantee that the first propeller module can generate the air-flow flowed up and down, herein with no restrictions.
Referring to Fig.1-4, in the present embodiment, fuselage includes fuselage main body 1 and the wing that 1 two sides of fuselage main body are arranged in
2, further wing 2 is made into integration to constitute the fuselage of fixed-wing unmanned plane with fuselage main body 1, certainly, in other implementations
Wing can not also be made into integration with fuselage main body in example, and the two fits together.Wherein, the specific constructive form of fuselage can adopt
With the structure type in Fig. 1, can also be adjusted as the case may be, herein with no restrictions.
In the present embodiment, which includes that there are two the first propeller modules, respectively the first propeller
Module 4 and the first propeller module 5, the first propeller module 4 and the first propeller module 5 or so are arranged side by side in fuselage main body
On 1；Certainly, the setting number of the first propeller module can be adjusted according to situation in other embodiments, such as can
It is only provided with a first propeller module, there are three the first propeller modules in another example settable, herein with no restriction.
Further, the first propeller module 4, the first propeller module 5 are horizontally set on fuselage roof；Certainly, may be used
In fuselage bottom, in other embodiments, the first propeller module 4, the first propeller module 5 can also with respect to the horizontal plane incline
Oblique certain angle, as long as the air-flow that can guarantee that the first propeller module 4, the first propeller module 5 generate can make unmanned plane
It flies up upwards, herein with no restrictions.
Further, the first propeller module 4, the first propeller module 5 include duct, are arranged among duct
Motor cabinet, the motor being mounted on motor cabinet, the propeller being mounted on motor.Certainly, the first spiral in other embodiments
Paddle module 4, the specific constructive form of the first propeller module 5 can also be adjusted as the case may be, herein with no restrictions.When
So, in other embodiments the first propeller module 4, the specific constructive form of the first propeller module 5 be not limited to it is above
It is described, it can also be adjusted as the case may be, such as the setting etc. of duct can be omitted.
Further, the bottom of 4 upper mounting seat of the first propeller module has extended downwardly extension 401, the first propeller
The bottom of 5 upper mounting seat of module has extended downwardly extension 501, the machine of extension 401, extension 501 and 1 bottom of fuselage main body
Body support base 101 together constitutes the undercarriage of fixed-wing unmanned plane, as shown in Figure 2.
In the present embodiment, which includes that there are two the second propeller modules, respectively the second propeller
Module 6 and the second propeller module 7；Second propeller module 6 and the second propeller module 7 are separately positioned on two wings 2；When
So, in other embodiments, the second propeller module may also be arranged among wing or lower section, number can also be as the case may be
It is adjusted, such as a second propeller module being arranged among back body can also be only included, in another example may include
There are three second propeller module of back body etc. is disposed side by side on, herein with no restrictions.
Further, the second propeller module 6, the second propeller module 7 are in tilted layout on the rear end of wing 1, this reality
It applies example to be obliquely installed the second propeller module 6, the second propeller module 7, so that fixed-wing unmanned plane is when taking off
The inclined thrust that two propeller modules 6, the second propeller module 7 generate, the inclined thrust and two first propeller modules
The vertical thrust generated, collective effect ensure that the stability of unmanned plane takeoff heading.
Certainly, the second propeller module 6, the second propeller module 7 can also be vertically installed at wing 1 in other embodiments
On, as long as guaranteeing that the second propeller module 6, the second propeller module 7 can generate the air-flow pushed in the front-back direction, this
Place is with no restrictions.
Further, the second propeller module 6, the second propeller module 7 include duct, are arranged among duct
Motor cabinet, the motor being mounted on motor cabinet, the propeller being mounted on motor.Certainly, the second spiral in other embodiments
Paddle module 6, the specific constructive form of the second propeller module 7 can also be adjusted as the case may be, herein with no restrictions.
In the present embodiment, which further includes having control circuit plate module 3, control circuit plate module 3 with
Two first propeller modules, the electrical connection of two second propeller modules, for controlling each first propeller module, each second spiral shell respectively
It revolves the revolving speed of paddle module, turn to；For example, control circuit plate module 3 passes through control the first propeller module 4, the first propeller mould
The revolving speed of block 5 realizes fixed-wing unmanned plane nose-high lifting and decline, in another example control circuit plate module 3 passes through control the
Two propeller modules 6, the second propeller module 7 revolving speed realize the forward retrogressing of fixed-wing unmanned plane, in another example control electricity
Road plate module 3 passes through control the second propeller module 6, the rotational speed difference of the second propeller module 7, Lai Shixian fixed-wing unmanned plane
Turning etc., herein with no restrictions.
Further, 6 axis gyroscopes are provided in control circuit plate module 3, for controlling the first propeller module 4, the
One propeller module 5, the second propeller module 6, the second propeller module 7, consequently facilitating realizing the automatic control of UAV Attitude
System.
In the present embodiment, the first propeller module 4, the first propeller module 5, the second propeller module 6, the second spiral
Paddle module 7, control circuit plate module 3 are detachably arranged on fuselage.By the first propeller module 4, in the present embodiment
One propeller module 5, the second propeller module 6, the second propeller module 7 are directly detachably mounted on fuselage, structure
Simply, modular assembly is realized, easy to assembly, assembly, maintenance cost are low.
Further, the first propeller module 4, the first propeller module 5, the second propeller module 6, the second propeller mould
It can be used between block 7, control circuit plate module 3 and fuselage and exempt from the realization of tool-free Quick-dismantle component and be detachably connected, thus further
Facilitate the assembly of fixed-wing unmanned plane.
Specifically, tool-free Quick-dismantle component includes dongle configuration and inserting slot construction, dongle configuration injects real in inserting slot construction
Now it is detachably connected；
Wherein, by the first tool-free Quick-dismantle component connection between the first propeller module and fuselage, first is tool-free fast
Tearing component open includes the first dongle configuration and the first inserting slot construction, and the first dongle configuration is mounted in the first propeller module 4,5, the
One inserting slot construction is mounted on fuselage；Alternatively, the first dongle configuration is mounted on fuselage, the first inserting slot construction is mounted on the first spiral shell
It revolves 4,5 in paddle module；
Wherein, by the second tool-free Quick-dismantle component connection between the second propeller module and fuselage, second is tool-free fast
Tearing component open includes the second dongle configuration and the second inserting slot construction, and the second dongle configuration is mounted in the second propeller module 6,7, the
Two inserting slot constructions are mounted on fuselage；Alternatively, the second dongle configuration is mounted on fuselage, the second inserting slot construction is mounted on the second spiral shell
It revolves in paddle module 6,7；
Wherein, by the tool-free Quick-dismantle component connection of third between control circuit plate module and fuselage, third is tool-free fast
Tearing component open includes third dongle configuration and third inserting slot construction, and third dongle configuration is mounted in control circuit plate module 3, third
Inserting slot construction is mounted on fuselage；Or third dongle configuration is mounted on fuselage, third inserting slot construction is mounted on control circuit
In plate module 3.
Certainly, the first propeller module 4, the first propeller module 5, the second propeller module 6, in other embodiments
Detachable connection method between two propeller modules 7, control circuit plate module 3 and fuselage is not limited to the above, can
It is adjusted as the case may be.
Those skilled in the art should be understood that the utility model can be realized with many other concrete forms without de-
Spirit or scope from itself.Although the case study on implementation of the utility model has been described, it should be understood that the utility model should not limit
Be made as these embodiments, those skilled in the art can as defined by the following claims the spirit of the utility model and
Within the scope of make change and modification.
Claims (16)
1. a kind of fixed-wing unmanned plane characterized by comprising
Fuselage, the fuselage include air-flow flow device；
At least one first propeller module, the first propeller module are set to the air-flow flow device and connect with the fuselage
It connects；
At least one second propeller module, the second propeller module are connect with the fuselage；
The first propeller module and the second propeller module can change the fuselage state.
2. fixed-wing unmanned plane according to claim 1, which is characterized in that the first propeller module can generate air-flow
Power, the air flow power can change the fuselage state by the air-flow flow device.
3. fixed-wing unmanned plane according to claim 1 or 2, which is characterized in that the air-flow flow device includes air-flow
Channel, the airflow channel be set to the fuselage on, the first propeller module be set to the airflow channel and with the fuselage
Connection.
4. fixed-wing unmanned plane according to claim 1, which is characterized in that the first propeller module and the fuselage
It is detachably connected.
5. fixed-wing unmanned plane according to claim 1, which is characterized in that the second propeller module and the fuselage
It is detachably connected.
6. fixed-wing unmanned plane according to claim 1, which is characterized in that it further include having control circuit plate module, it is described
Control circuit plate module is mounted on the fuselage, and the first propeller module, the second propeller module and the control
Circuit board module electrical connection.
7. fixed-wing unmanned plane according to claim 6, which is characterized in that the control circuit plate module and the fuselage
It is detachably connected.
8. fixed-wing unmanned plane according to claim 6 or 7, which is characterized in that the first propeller module with it is described
It is adopted between fuselage, between the second propeller module and the fuselage, between the control circuit plate module and the fuselage
It is connected with tool-free Quick-dismantle component.
9. fixed-wing unmanned plane according to claim 8, which is characterized in that the tool-free Quick-dismantle component includes plug-in unit knot
Structure and inserting slot construction, the dongle configuration inject realization in the inserting slot construction and are detachably connected, wherein
By the first tool-free Quick-dismantle component connection between the first propeller module and the fuselage, described first is tool-free
Quick-dismantle component includes the first dongle configuration and the first inserting slot construction, and first dongle configuration is mounted on the first propeller mould
On block, first inserting slot construction is mounted on the fuselage or first dongle configuration is mounted on the fuselage, institute
The first inserting slot construction is stated to be mounted in the first propeller module；
By the second tool-free Quick-dismantle component connection between the second propeller module and the fuselage, described second is tool-free
Quick-dismantle component includes the second dongle configuration and the second inserting slot construction, and second dongle configuration is mounted on the second propeller mould
On block, second inserting slot construction is mounted on the fuselage or second dongle configuration is mounted on the fuselage, institute
The second inserting slot construction is stated to be mounted in the second propeller module；
By the tool-free Quick-dismantle component connection of third between the control circuit plate module and the fuselage, the third is tool-free
Quick-dismantle component includes third dongle configuration and third inserting slot construction, and the third dongle configuration is mounted on the control circuit template die
On block, the third inserting slot construction is mounted on the fuselage or the third dongle configuration is mounted on the fuselage, institute
Third inserting slot construction is stated to be mounted in the control circuit plate module.
10. fixed-wing unmanned plane according to claim 6, which is characterized in that the first propeller module, described second
Propeller module and the control circuit plate module can separate from the fuselage and be combined into an aircraft.
11. fixed-wing unmanned plane described according to claim 1 or 2 or 5, which is characterized in that the fuselage includes fuselage main body
With the wing that the fuselage main body left and right sides is arranged in, and two wings are made into integration with the fuselage.
12. fixed-wing unmanned plane according to claim 11, which is characterized in that be provided with two described first on the fuselage
Propeller module, two described first propeller modules or so side-by-side horizontal are arranged on the fuselage.
13. fixed-wing unmanned plane according to claim 11, which is characterized in that be provided with two described second on the fuselage
Propeller module, the two second propeller modules are in tilted layout respectively on two wings.
14. fixed-wing unmanned plane according to claim 13, which is characterized in that second propeller arrangement is arranged in institute
State rear airfoil end.
15. fixed-wing unmanned plane according to claim 1, which is characterized in that the first propeller module, described second
Propeller module include duct, the motor cabinet being arranged among the duct, the motor being mounted on the motor cabinet and
Propeller.
16. fixed-wing unmanned plane according to claim 6, which is characterized in that it further include having battery module, the battery mould
Block is mounted on above or below the control circuit plate module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821332351.2U CN209454990U (en) | 2018-08-17 | 2018-08-17 | A kind of fixed-wing unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821332351.2U CN209454990U (en) | 2018-08-17 | 2018-08-17 | A kind of fixed-wing unmanned plane |
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| CN209454990U true CN209454990U (en) | 2019-10-01 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110834727A (en) * | 2018-08-17 | 2020-02-25 | 昆山合朗电子有限公司 | Fixed-wing unmanned aerial vehicle and control method |
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2018
- 2018-08-17 CN CN201821332351.2U patent/CN209454990U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110834727A (en) * | 2018-08-17 | 2020-02-25 | 昆山合朗电子有限公司 | Fixed-wing unmanned aerial vehicle and control method |
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| CP01 | Change in the name or title of a patent holder |
Address after: Room No. 388, Zhengwei East Road, Jinxi Town, Kunshan City, Suzhou City, Jiangsu Province, 215324 Patentee after: Kunshan Helang Aviation Technology Co.,Ltd. Address before: Room No. 388, Zhengwei East Road, Jinxi Town, Kunshan City, Suzhou City, Jiangsu Province, 215324 Patentee before: KUNSHAN HELANG ELECTRONICS Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder |