CN109625254A - Sports class unmanned plane - Google Patents
Sports class unmanned plane Download PDFInfo
- Publication number
- CN109625254A CN109625254A CN201811622316.9A CN201811622316A CN109625254A CN 109625254 A CN109625254 A CN 109625254A CN 201811622316 A CN201811622316 A CN 201811622316A CN 109625254 A CN109625254 A CN 109625254A
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- China
- Prior art keywords
- motor
- plate
- unmanned plane
- bottom plate
- sports class
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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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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of sports class unmanned planes, and bottom plate, electric-controlled plate, propeller and motor including rack, " X " type, the electric-controlled plate is installed in the rack, and rack is mounted on the upper surface in the middle part of bottom plate；The end of four arm bodies of the bottom plate is respectively mounted the motor, and the shaft of each motor is respectively mounted the propeller；Each motor is electrically connected with the electric-controlled plate；It further include the protection board that diameter is greater than diameter of motor；The lower end of each motor is respectively mounted the protection board, and each arm body is folded between corresponding motor and protection board.A possibility that present invention improves integrally-built intensity, increases flexibility, while improving the protection to motor, reduces image inclination.
Description
Technical field
The present invention relates to air vehicle technique fields, and in particular to a kind of sports class unmanned plane.
Background technique
The match most cases of sports class unmanned plane appear in teaching contest, also there is unmanned plane fan or social group
The match of body tissue.Sports class unmanned plane match and educational training in, can allow it is vast have intention study unmanned plane manipulation and
The winged hand of unmanned plane configuration and fans are more fully understood, and can be fully understanded welding, programming, aerodynamics, be driven
Mode, transmission of video etc. are sailed, so that this movement is widelyd popularize, it is very significant for imparting knowledge to students.
Sports class unmanned plane and our the daily machines of taking photo by plane seen are entirely different, and the machine of taking photo by plane is in order to shoot, so it is chased after
What is asked is stable, safety and shooting ability.But race class unmanned plane pursue be speed, reaction and flexibly.Primary structure: machine
Body external member, battery, rack, camera, propeller, flies control, electricity tune, figure biography, receiver, antenna at dynamical system.Common sports
Class unmanned plane is designed according to the principle of quadrotor.
Sports class unmanned plane there are problems that and disadvantage at present:
1. slimmer and more graceful, more tiny volume is needed because the sports unmanned function of class shuttles in obstacle with a varied topography, and
Current sports class unmanned plane wheelbase is larger, and flexibility is poor.
2. can reach 220km/ due to the F-Zero of sports class unmanned plane, and speed per hour is too fast, it is easy to lead to fuselage
Collision, fuselage total weight weighting will also result in power it is excessively high allow for battery also consume it is too fast, it is therefore desirable to fuselage material
Weight and intensity requirement are high, and current sports class unmanned aerial vehicle body material is slight not enough, weight is laid particular stress on, overall structure is not enough tied
It is real.
3. racing class unmanned plane when colliding, it is propeller and motor that most cases, which are impaired at first, and current
Sports class unmanned plane select thick protective case to protect motor, but protective case is heavier, will increase the weight of complete machine.
In addition, protective case also will affect the heat dissipation of motor, the probability of motor losses is increased.
4. general photographic device is mounted on the roof of unmanned plane, if imaging or taking pictures in flight course, because of nothing
It leans forward when man-machine flight and image is caused to tilt, there is a problem of that imaging is not upright.
Summary of the invention
For the defects in the prior art, the present invention provides a kind of sports class unmanned plane, to improve integrally-built intensity,
A possibility that increasing flexibility, while improving the protection to motor, reducing image inclination.
The present invention provides a kind of sports class unmanned planes, bottom plate, electric-controlled plate, propeller and horse including rack, " X " type
It reaches, the electric-controlled plate is installed in the rack, and rack is mounted on the upper surface in the middle part of bottom plate；Four arms of the bottom plate
The end of body is respectively mounted the motor, and the shaft of each motor is respectively mounted the propeller；Each horse
It is electrically connected up to equal with the electric-controlled plate；
It further include the protection board that diameter is greater than diameter of motor；The lower end of each motor is respectively mounted the protection
Plate, and each arm body is folded between corresponding motor and protection board.
Preferably, the rack includes top plate, side plate and tailgate；The two sides of the top plate are fixedly mounted by the side plate
It is reinforced between the upper surface of the bottom plate, two side plates by the tailgate and tailgate is located at the rear end of top plate, Jin Ertong
It crosses top plate, two side plates, tailgate and bottom plate and surrounds installation cavity；The electric-controlled plate is installed in installation cavity.
It preferably, further include the camera being electrically connected with the electric-controlled plate, the camera is installed in the installation cavity
And camera shooting front of the end towards bottom plate of camera.
Electric-controlled plate is the component for controlling whole equipment, and the component of signal transmission is carried out with other equipment, by electric-controlled plate
It is mounted in installation cavity, avoids making to damage electric-controlled plate in collision, improve the protection to electric-controlled plate.
It preferably, further include supporting element；Four supporting elements are installed between the top plate and bottom plate, are supported by four
Part tilts the front of top plate up in turn；Supporting element described in two of them be located in one of the lateral surface of side plate front and
Rear portion, other two supporting element are located at the front and rear of the lateral surface of another side plate.
Supporting element instead of the circular mounting aluminium column in existing unmanned plane, four supporting element middle bents and then make
The front of top plate up tilts, and inclined angle is identical as the angle of the front of the top plate in flight to lower swing, in turn
Keep top plate holding in flight course horizontal.In addition, supporting element strengthens integrally-built connection relationship, make complete machine structure more
It is solid.
Preferably, the direction at the camera shooting end of the camera and the front end of the top plate are towards identical.
Top plate keeps horizontal in flight course, to keep the image of the intake of camera upright, will not tilt, more favorably
Front environment is seen clearly in operator.
Preferably, the lower surface of the bottom plate is equipped with the non-slip mat for installing power supply.
This equipment can select the satisfactory power supply of voltage rating according to actual needs, such as 1300mAh-
2000mAh, electric discharge C are greater than the lithium battery of 90C.Power supply is fixed below bottom plate by non-slip mat, on the one hand installs power supply
It is stronger, it is not in the case where battery is detached from.Power supply design is mounted on the lower surface of bottom plate by still further aspect, makes originally to set
For standby center of gravity close to the geometric center of bottom plate, flare maneuver is more stable.
Preferably, the width in four arm body cross sections of the bottom plate is no more than 14mm.
It is designed using the narrow arm no more than 14mm, is conducive to reduce windage, flexibility when flight.
Being preferably located at diagonal the distance between two motors is 200-300mm.
Motor the distance between it is small, reduce the volume of this equipment, further make flight more slim and graceful, flexibly.
Preferably, the bottom plate and the material of rack include carbon fiber 3K cloth and epoxy resin；The material of the supporting element
It is aluminium alloy.
Preferably, the material of the protection board includes carbon fiber.
It selects carbon fiber and the material of epoxy resin and the material of aluminium alloy to be for reducing main screw lift, makes to fly
Row is flexible.These strengths of materials are big simultaneously, it is not easy to damage, further improve the compactedness of complete machine, crashworthiness is higher, no
It is easy to damage.
The beneficial effects of the present invention are embodied in:
Without wrapping up thick protective case, existing unmanned plane is compared, is subtracted in the outer surface of four motors in this equipment
Four protective cases are lacked, to reduce main screw lift, have made the more flexible property of fuselage.In addition, motor is directly exposed to air,
The speed of motor radiating is greatly promoted, it is excessively high and damage motor to avoid temperature.Meanwhile in order to avoid the horse in collision process
Direct collision occurs up to other objects, this equipment increases four protection boards, and the diameter of protection board is greater than the straight of motor
Diameter.Even if the only protection board that collides is knocked, and motor is intact.Therefore, the screening glass in this equipment both can be with
Play the role of protecting motor, mitigates main screw lift；The heat dissipation performance of motor can be improved again, improve the protection to motor.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art are briefly described.In all the appended drawings, similar element
Or part is generally identified by similar appended drawing reference.In attached drawing, each element or part might not be drawn according to actual ratio.
Fig. 1 is the structural schematic diagram of the present embodiment；
Fig. 2 is the bottom view of Fig. 1；
Fig. 3 is the rearview of Fig. 1；
Fig. 4 is the perspective view of Fig. 1；
Fig. 5 is the structural schematic diagram after Fig. 1 is split.
In attached drawing, rack 1, bottom plate 3, propeller 4, motor 5, top plate 6, side plate 7, tailgate 8, supporting element 9, is taken the photograph electric-controlled plate 2
As head 10, non-slip mat 11, protection board 12, arm body 13.
Specific embodiment
It is described in detail below in conjunction with embodiment of the attached drawing to technical solution of the present invention.Following embodiment is only used for
Clearly illustrate technical solution of the present invention, therefore be only used as example, and cannot be used as a limitation and limit protection model of the invention
It encloses.
It should be noted that unless otherwise indicated, technical term or scientific term used in this application should be this hair
The ordinary meaning that bright one of ordinary skill in the art are understood.
As shown in Figure 1, present embodiments provide a kind of sports class unmanned plane, the bottom plate 3, automatically controlled including rack 1, " X " type
Plate 2, propeller 4 and motor 5.The electric-controlled plate 2 is installed in the rack 1, and rack 1 is mounted on the upper of 3 middle part of bottom plate
Surface.Wherein the specific structure of rack 1 is as follows:
The rack 1 includes top plate 6, side plate 7 and tailgate 8；The two sides of the top plate 6 are fixedly mounted by the side plate 7
It is reinforced between the upper surface of the bottom plate 3, two side plates 7 by the tailgate 8 and tailgate 8 is located at the rear end of top plate 6, into
And installation cavity is surrounded by 6, two side plates 7 of top plate, tailgate 8 and bottom plate 3；The electric-controlled plate 2 is installed in installation cavity.Electric-controlled plate
2 be to control the component of whole equipment, and the component of signal transmission is carried out with other equipment, and electric-controlled plate 2 is mounted on installation cavity
In, it avoids making to damage electric-controlled plate 2 in collision, improves the protection to electric-controlled plate 2.
It as shown in Figure 4 and Figure 5, further include supporting element 9, the material of the supporting element 9 is equal in order to improve the intensity of rack 1
For aluminium alloy.Four supporting elements 9 are installed between the top plate 6 and bottom plate 3, make top plate 6 by four supporting elements 9
Front up tilts；Supporting element 9 described in two of them is located in one of the front and rear of the lateral surface of side plate 7, and in addition two
A supporting element 9 is located at the front and rear of the lateral surface of another side plate 7.Supporting element 9 instead of in existing unmanned plane
Circular mounting aluminium column, four 9 middle bents of supporting element tilt the front of top plate 6 up in turn, and inclined angle
It is identical as the angle of the front of the top plate 6 in flight to lower swing, and then keep the holding in flight course of top plate 6 horizontal.In addition,
Supporting element 9 strengthens integrally-built connection relationship, keeps complete machine structure more solid.
As depicted in figs. 1 and 2, the present embodiment further includes the camera 10 being electrically connected with the electric-controlled plate 2, the camera
10 are installed in the installation cavity and the camera shooting end of camera 10 is towards the front of bottom plate 3.And the camera 10 is taken the photograph
As direction and the front end of the top plate 6 at end are towards identical.Top plate 6 keeps horizontal in flight course, to make camera
The image of 10 intake is upright, will not tilt, and is more advantageous to operator and sees front environment clearly.
As shown in figure 3, this equipment can select the satisfactory power supply of voltage rating according to actual needs, such as
1300mAh-2000mAh, electric discharge C are greater than the lithium battery of 90C.The lower surface of the bottom plate 3 is equipped with for installing the anti-skidding of power supply
Pad 11.Power supply is fixed below bottom plate 3 by non-slip mat 11, is on the one hand more firmly mounted power supply, is not in battery
The case where disengaging.Power supply design is mounted on the lower surface of bottom plate 3 by still further aspect, makes the center of gravity of this equipment close to bottom plate 3
Geometric center, flare maneuver are more stable.
The end of four arm bodies 13 of bottom plate 3 described in the present embodiment is respectively mounted the motor 5, and each motor
5 shaft is respectively mounted the propeller 4；Each motor 5 is electrically connected with the electric-controlled plate 2.The bottom plate 3 four
The width in 13 cross section of arm body is no more than 14mm.It is designed using the narrow arm no more than 14mm, is conducive to reduce windage, when flight
Flexibility.It is 200-300mm positioned at diagonal the distance between two motors 5.Motor 5 the distance between it is small,
The volume of this equipment is reduced, further makes flight more slim and graceful, flexible.
This equipment further includes the protection board 12 that diameter is greater than 5 diameter of motor；The lower end of each motor 5 is respectively mounted one
The protection board 12, and each arm body 13 is folded between corresponding motor 5 and protection board 12.Due to four motors 5
Without wrapping up thick protective case, existing unmanned plane is compared, reduces four protective cases, to reduce complete machine in outer surface
Weight makes the more flexible property of fuselage.In addition, motor 5 is directly exposed to air, the speed for making motor 5 radiate is greatly promoted, and is kept away
It is excessively high and damage motor 5 temperature has been exempted from.Meanwhile in order to avoid direct collision occurs for the motor 5 in collision process and other objects,
This equipment increases four protection boards 12, and the diameter of protection board 12 is greater than the diameter of motor 5.Even if colliding only
Protection board 12 is knocked, and motor 5 is intact.Therefore, the screening glass in this equipment can both play the work of protection motor 5
With mitigation main screw lift；The heat dissipation performance of motor 5 can be improved again, improve the protection to motor 5.
The material of the present embodiment insole board 3 and rack 1 includes carbon fiber 3K cloth and epoxy resin, the material of the protection board 12
Material includes carbon fiber.Carbon fiber and the material of epoxy resin and the material of aluminium alloy is selected to be for reducing main screw lift,
Keep flight flexible.These strengths of materials are big simultaneously, it is not easy to damage, further improve the compactedness of complete machine, crashworthiness is more
Height is hardly damaged.
Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Pipe present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: its according to
So be possible to modify the technical solutions described in the foregoing embodiments, or to some or all of the technical features into
Row equivalent replacement；And these are modified or replaceed, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme should all cover within the scope of the claims and the description of the invention.
Claims (10)
1. a kind of sports class unmanned plane, bottom plate, electric-controlled plate, propeller and motor including rack, " X " type, the electric-controlled plate peace
Loaded in the rack, and rack is mounted on the upper surface in the middle part of bottom plate；The end of four arm bodies of the bottom plate is respectively mounted
One motor, and the shaft of each motor is respectively mounted the propeller；Each motor with it is described automatically controlled
Plate electrical connection；
It is characterized by also including the protection boards that diameter is greater than diameter of motor；The lower end of each motor is respectively mounted an institute
Protection board is stated, and each arm body is folded between corresponding motor and protection board.
2. sports class unmanned plane according to claim 1, it is characterised in that: the rack includes top plate, side plate and tailgate；
The two sides of the top plate are fixedly mounted on the upper surface of the bottom plate by the side plate, pass through the tailgate between two side plates
It reinforces and tailgate is located at the rear end of top plate, and then installation cavity is surrounded by top plate, two side plates, tailgate and bottom plate；The electricity
Control plate is installed in installation cavity.
3. sports class unmanned plane according to claim 2, it is characterised in that: further include being taken the photograph with what the electric-controlled plate was electrically connected
As head, the camera is installed in the installation cavity and camera shooting front of the end towards bottom plate of camera.
4. sports class unmanned plane according to claim 3, it is characterised in that: further include supporting element；The top plate and bottom plate
Between install four supporting elements, tilt the front of top plate up by four supporting elements；It is propped up described in two of them
Support member is located in one of the front and rear of the lateral surface of side plate, other two supporting element is located at the outside of another side plate
The front and rear in face.
5. sports class unmanned plane according to claim 4, it is characterised in that: the direction at the camera shooting end of the camera and institute
State the front end of top plate towards identical.
6. sports class unmanned plane according to claim 1, it is characterised in that: the lower surface of the bottom plate is equipped with for installing
The non-slip mat of power supply.
7. sports class unmanned plane according to claim 1, it is characterised in that: the width in four arm body cross sections of the bottom plate
No more than 14mm.
8. sports class unmanned plane according to claim 1, it is characterised in that: between two diagonal motors
Distance is 200-300mm.
9. sports class unmanned plane according to claim 4, it is characterised in that: the bottom plate and the material of rack include carbon fiber
Tie up 3K cloth and epoxy resin；The material of the supporting element is aluminium alloy.
10. sports class unmanned plane according to claim 1, it is characterised in that: the material of the protection board includes carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811622316.9A CN109625254A (en) | 2018-12-28 | 2018-12-28 | Sports class unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811622316.9A CN109625254A (en) | 2018-12-28 | 2018-12-28 | Sports class unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109625254A true CN109625254A (en) | 2019-04-16 |
Family
ID=66078866
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811622316.9A Pending CN109625254A (en) | 2018-12-28 | 2018-12-28 | Sports class unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109625254A (en) |
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